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Fundamentals of Solar PV system
Solar Energy Basics and solar
spectrum
Photovoltaic Cell:
Construction and working
principleSolar photovoltaic
technologies
Types of solar photovoltaic
systems
Designing of a solar
photovoltaic system
Advantages and disadvantages
of solar energy and systems
Applications of solar energy
Outline
What is Solar Energy?
 Originates with the thermonuclear fusion reactions occurring in
the sun.
 Represents the entire electromagnetic radiation (visible light,
infrared, ultraviolet, x-rays, and radio waves).
 This energy consists of radiant light and heat energy from the sun.
 Out of all energy emitted by sun only a small fraction of energy is
absorbed by the earth.
http://en.wikipedia.org/wiki/File:Breakdown_of_the_incoming_solar_ener
The surface receives about
47% of the total solar energy
that reaches the Earth. Only
this amount is usable.
Breakdown of incoming solar energy
Air Mass
 Amount of air mass through which light pass
 Atmosphere can cut solar energy reaching earth by 50%
and more
 Solar Thermal Energy
 Solar Heating
 Solar Water Heating
 Solar Space Heating
 Solar Space Cooling
 Solar Photovoltaic
 Solar Concentrators
Solar Energy Harvesting Using
Different Paths
Electricity Generation From Solar
Energy
Solar Energy can be used to generate electricity in 2 ways:
 Solar Thermal Energy:
Using solar thermal technologies for heating fluids which can be
used as a heat source or to run turbines to generate electricity.
 Solar Photovoltaic Energy:
Using solar energy for the direct generation of electricity
using photovoltaic phenomenon.
Technology Options for Solar Power
Parabolic Dish
Solar Power
Thermal
Low
Temperature
<100°C.
Solar Water
Heating
Solar Chimney
Solar Pond
Med Temp
<400°C
High Temp.
>400°C
Central Tower
PV
Technology
Mono
Crystalline
Silicon
Polycrystalline
Silicon
Amorphous
Silicon
Production
Process
Wafer
Thin Film
Energy Band Diagram of a Conductor,
Semiconductor and Insulator
conductor semiconductor insulator
Semiconductors are interested because their conductivity can be readily modulated (by impurity
doping or electrical potential), offering a pathway to control electronic circuits.
Semiconductors used for solar
cells
II III IV V VI
B C (6)
Al Si (14) P S
Zn Ga Ge (32) As Se
Cd In Sb Te
Semiconductors:
 Elementary – Si, Ge.
 Compound – GaAs, InP, CdTe.
 Ternary – AlGaAs, HgCdTe, CIS.
 Quaternary – CIGS, InGaAsP, InGaAIP.
Silicon
-
Si Si Si
Si
SiSi
Si
Si
Si
Shared electrons
 Silicon is group IV element – with 4 electrons in their valence shell.
 When silicon atoms are brought together, each atom forms covalent bond with
4 silicon atoms in a tetrahedron geometry.
Intrinsic Semiconductor
 At 0 ºK, each electron is in its lowest energy state so each covalent bond
position is filled. If a small electric field is applied to the material, no
electrons will move because they are bound to their individual atoms.
 At 0 ºK, silicon is an insulator.
 As temperature increases, the valence electrons gain thermal energy.
 If a valence electron gains enough energy (Eg), it may break its covalent bond
and move away from its original position. This electron is free to move within
the crystal.
 Conductor Eg <0.1eV, many electrons can be thermally excited at room
temperature.
 Semiconductor Eg ~1eV, a few electrons can be excited (e.g. 1/billion)
 Insulator, Eg >3-5eV, essentially no electron can be thermally excited at
room temperature.
Energy of a photon,
Extrinsic Semiconductor, n-type
Doping
Electron
-
Si Si Si
Si
SiSi
Si
Si
As
Extra
Valence band, Ev
Eg = 1.1 eV
Conducting band, Ec
Ed ~ 0.05 eV
 Doping silicon lattice with group V elements can creates extra electrons in the conduction
band — negative charge carriers (n-type), As- donor.
 Doping concentration #/cm3 (1016/cm3 ~ 1/million).
Valence band, Ev
Eg = 1.1 eV
Conducting band, Ec
Ea ~ 0.05 eV
Electron
-
Si Si Si
Si
SiSi
Si
Si
B
Hole
 Doping silicon with group III elements can creates empty holes in the valence band
positive charge carriers (p-type), B-(acceptor).
Extrinsic Semiconductor, p-type
doping
V
I
R O F
p n
p n
V>0 V<0
Reverse bias Forward bias
p-n Junction diode
 A p-n junction is a junction formed by combining p-type and n-type
semiconductors together in very close contact.
 In p-n junction, the current is only allowed to flow along one direction from
p-type to n-type materials.
i
p n
V<0 V>0
depletion layer
- +
 Get image from book
Efficiency – The Band Gap Problem
Photo+voltaic = convert
light to electricity
 A PV cell is a light illuminated pn-
junction diode which directly converts
solar energy into electricity via the
photovoltaic effect.
 A typical silicon PV cell is composed of a
thin wafer consisting of an ultra-thin
layer of phosphorus-doped (n-type)
silicon on top of a thicker layer of boron-
doped (p-type) silicon.
 When sunlight strikes the surface of a
PV cell, photons with energy above the
semiconductor bandgap impart enough
energy to create electron-hole pairs.
Photovoltaic Cell
Photovoltaic Cell: Operating Principle
 There are three basic steps for
generation of electricity using PV cells
which are following:
 First is absorption of solar
radiation,
 Second is generation of free
charge carriers and
 Third is transport and then
collection of charge carriers at PV
cell terminals.
Structure of a Solar Cell
1) Non absorbed photons
2) Lattice thermalization
3) Junction voltage drop
4) Contact voltage drop
5) Recombination
Standard PV cell Efficiency Losses
Blocking Diodes
 During sun shine, as long as the voltage produced by the panels is greater
than that of the battery, charging will take place.
 In the dark, the voltage of the battery would cause a current flow in
reverse direction through the panels, which can lead to the discharging of
battery.
 A blocking diode is used in series with the panels and battery in reverse
biasing to prevent reverse flow of the current.
 Normal p-n junction diodes can be used as blocking diodes.
 To select a blocking diode, following parameters should be kept in mind:
 The maximum current provided by the panels.
 The voltage ratings of the diode.
 The reverse breakdown voltage of the diode.
Hot- Spot and Bypass Diodes
 Hot Spot phenomenon happens when one or more
cells of the panel is shaded while the others are
illuminated.
 The shaded cells/panels starts behaving as a diode
polarized in reverse direction and generates reverse
power. The other cells generate a current that flows
through the shaded cell and the load.
 Any solar cell has its own critical power
dissipation Pc that must not be exceeded and
depends on its cooling and material structures, its
area, its maximum operating temperature and
ambient temperature.
 A shaded cell may be destroyed when its reverse
dissipation exceeds Pc. This is the hot spot.
 To eliminate the hot-spot phenomenon, a bypass
diode is connected parallel to the module or
group of cells in reverse polarity which provides
another path to the extra current.
Hot- Spot and Bypass Diodes
 When part of a PV module is shaded,
the shaded cells will not be able to
produce as much current as the
unshaded cells.
 Since all cells are connected in series,
the same amount of current must flow
through every cell.
 The unshaded cells will force the
shaded cells to pass more current
through it.
Bypass diode working phases
Bypass Diodes working
 The only way the shaded cells can operate at a current higher than their short
circuit current is to operate in a region of negative voltage i.e. to cause a net
voltage loss to the system.
 The voltage across the shaded or low current solar cell becomes greater than the
forward bias voltage of the other series cells which share the same bypass diode
plus the voltage of the bypass diode thus making the diode to work in forward
bias and hence allowing extra current to pass through it, preventing hot-spot.
 For an efficient operation, there are two conditions to fulfill:
 Bypass diode has to conduct when one cell is shadowed.
 The shadowed cell voltage Vs must stay under its breakdown voltage (Vc).
 Ideally, a bypass diode should have a forward voltage (VF) and a leakage current
(IR) as low as possible.
Bypass Diodes working
Bypass Diodes
 Two types of diodes are available as bypass diodes in solar
panels and arrays:
 p-n junction silicon diode
 Schottky barrier diode
 To select a bypass diode, following parameters should be
checked:
 The forward voltage and current ratings of the diode.
 The reverse breakdown voltage of the diode.
 The reverse leakage current.
 Junction Temperature Range
2 – 3 W
100 - 200 W
10 - 50 kW
Cell
Array
Module,Panel
Volt Ampere Watt Size
Cell 0.5V 5-6A 2-3W about 10cm
Module 20-30V 5-6A 100-200W about 1m
Array 200-300V 50A-200A 10-50kW about 30m
6x9=54 (cells) 100-300 (modules)
Hierarchy of PV
Solar cells are composed of various semiconducting materials
 Crystalline silicon
 Cadmium telluride
 Copper indium diselenide
 Gallium arsenide
 Indium phosphide
 Zinc sulphide
Materials for Solar cell
Cell Technologies
Crystalline
silicon
Mono-
crystalline
Pure and
efficient
15-19%
efficiency
Multi-
crystalline
12-15%
efficiency
Thin film
Non Silicon
based
CdTe
8.5%
efficiency
CIGS
9-11%
efficiency
Silicon
based
Amorphous
5-7%
efficiency
Technology Differences
Optical Properties
• Band gap (direct, indirect)
• Absorption Coefficient
• Absorption length
Electrical Properties
• Carrier Lifetime
• Mobility
• Diffusion length
Manufacturing
• Absorber material
• Cells
• Modules
Performance
• Efficiency
• Current, Voltage and FF
• Effect of temperature and
radiation
Optical Properties:
Band Gaps
Fixed band gap of c-Si material (mono, multi).
Tunable gaps of thin film compound semiconductors.
Optical Properties:
Material absorption lengths
Absorption Length in Microns
(for approx. 73% incoming light absorption)
Wavelength (nm) c-Si a-Si CIGS GaAs
400 nm (3.1eV) 0.15 0.05 0.05 0.09
600 nm (2eV) 1.8 0.14 0.06 0.18
800 nm (1.55eV) 9.3 Not absorbed 0.14 1.1
1000nm(1.24eV) 180.9 Not absorbed 0.25 Not absorbed
 Absorption length is much higher for Si because of lower absorption
coefficient.
 Longer wavelength photons require more materials to get absorbed.
Electrical Properties
Mobility
Ease with which carriers move in semiconductor.
Lifetime
Average time carriers spend in excited state.
Diffusion
Carrier movement due to concentration difference.
Diffusion Length
Average length travelled by carrier before recombining due to concentration difference.
Drift
Carrier movement due to electric field.
Drift length
Average length travelled by carrier before recombination under electric field.
Electrical Properties:
Drift and Diffusion lengths
High quality material
scenario
Low quality material
scenario
 Carrier are transported by diffusion
to the junction.
 Large diffusion length.
 Junction is very thin.
 Diffusion length are small.
 Drift length is about 10 times
greater than diffusion length.
 Intrinsic layer is thicker.
Three generations of solar cells
1. First Generation
 First generation cells consist of high quality and single junction devices.
 First Generation technologies involve high energy and labour inputs which prevent any
significant progress in reducing production costs.
2. Second Generation
 Second generation materials have been developed to address energy requirements and
production costs of solar cells.
 Alternative manufacturing techniques such as vapour deposition and electroplating are
advantageous as they reduce high temperature processing significantly.
 Produced from cheaper polycrystalline materials and glass
 High optical absorption coefficients
 Bandgap suited to solar spectrum
3. Third Generation
 Third generation technologies aim to enhance poor electrical performance of second
generation (thin-film technologies) while maintaining very low production costs.
 Current research is targeting conversion efficiencies of 30-60% while retaining low
cost materials and manufacturing techniques.
 They can exceed the theoretical solar conversion efficiency limit for a single energy
threshold material, 31% under 1 sun illumination and 40.8% under the maximal
artificial concentration of sunlight (46,200 suns).
 Approaches to achieving these high efficiencies including the use of multijunction
photovoltaic cells, concentration of the incident spectrum, the use of thermal
generation by UV light to enhance voltage or carrier collection, or the use of the
infrared spectrum for night-time operation.
Monocrystalline Silicon Modules
 Most efficient commercially
available module (14% - 17%)
 Most expensive to produce
 Circular (square-round) cell
creates wasted space on
module
Front Surface
(N-Type side)
• Aluminum Electrode
(Silver colored wire)
• To avoid shading,
electrode is very fine.
Anti reflection film
(Blue colored film)
• Back surface is P-type.
• All back surface is
aluminum electrode
with full reflection.
Poly Crystalline PV
Polycrystalline Silicon Modules
Polycrystalline Silicon Modules
 Less expensive to make than
single crystalline modules
 Cells slightly less efficient than
a single crystalline (10% - 12%)
 Square shape cells fit into
module efficiently using the
entire space
PV Module (Single crystal, Poly crystalline Silicon)
Single crystal Poly crystalline
120W
(25.7V, 4.7A)
1200mm
800mm800mm
1200mm
(3.93ft)
(2.62ft)
(3.93f)
(2.62ft)
128W
(26.5V ,4.8A)
Efficiency is higher Efficiency is lower
Same size
Amorphous Thin Film
 Most inexpensive technology to produce
 Metal grid replaced with transparent
oxides
 Efficiency = 6 – 8 %
 Can be deposited on flexible substrates
 Less susceptible to shading problems
 Better performance in low light conditions
that with crystalline modules
Solar Panel Manufacturing Technologies
Mono-Si Solar Panels
 Mono-Si is manufactured by Czochralski Process.
Si boule for the
production of
wafers.
Solar Panel Manufacturing Technologies
 Since they are cut from single crystal, they gives the module a uniform appearance.
Advantages
 Highest efficient module till now with efficiency between 13 to 21%.
 Commonly available in the market.
 Greater heat resistance.
 Acquire small area where ever placed.
Disadvantages
 More expensive to produce.
 High amount of Silicon.
 High embodied energy (total energy required to produce).
Poly-Si Solar Panels
 Polycrystalline (or multicrystalline) modules are composed of a number of different
crystals, fused together to make a single cell.
 Poly-Si solar panels have a non-uniform texture due to visible crystal grain present due
to manufacturing process.
Advantages
 Good efficiency between 14 to 16%.
 Cost effective manufacture.
 Commonly Available in the market.
Visible crystal grain in poly-Si
Solar Panel Manufacturing Technologies
Disadvantages
 Not as efficient as Mono-Si.
 Large amount of Si.
 High Embodied Energy.
Visible difference between Mono-Si and Poly-Si Panels
Mono-Si solar cells are of dark color and the corners of the cells
are usually missing whereas poly-Si panels are of dark or
light blue color. The difference between the structure is only
due to their manufacturing process.
Mono-Si Panel
Poly-Si Panel
Solar Panel Manufacturing
Technologies
Thin Film Solar Panels
 Made by depositing one or more thin layers (thin film) of
photovoltaic material on a substrate.
 Thin Film technology depend upon the type of material
used to dope the substrate.
 Cadmium telluride (CdTe), copper indium gallium
selenide (CIGS) and amorphous silicon (A-Si) are three
thin-film technologies often used as outdoor photovoltaic
solar power production.
Solar Panel Manufacturing Technologies
Amorphous-Si Panels
 Non-crystalline allotrope of Si with no definite
arrangement of atoms.
Advantages
 Partially shade tolerant
 More effective in hotter climate
 Uses less silicon - low embodied energy
 No aluminum frame - low embodied energy
Disadvantages
 Less efficient with efficiency between 6 to 9% .
 Less popular - harder to replace.
 Takes up more space for same output .
 New technology - less proven reliability.
Solar Panel Manufacturing Technologies
Thin Film Silicon Solar Cells
CdTe/CdS Solar Cell
 CdTe: Bandgap 1.5 eV; Absorption
coefficient 10 times that of Si
 CdS: Bandgap 2.5 eV; Acts as window layer
 Limitation: Poor contact quality with p-
CdTe (~ 0.1 Wcm2)
Cadmium Telluride Solar Cell
 Toxicity of Cd is an issue.
 Best lab efficiency = 16.5%.
 NREL has demonstrated an efficiency of 19.9% for the CIGS solar cell.
 Typically requires relatively high temperature processing (> 500C).
Copper-Indium-Gallium-Diselenide Cell
Comparison of Si on the basis of crystallinity
Comparison of Mono-Si, Poly-Si and Thin film Panels
Mono-Si Panels Poly-Si Panels Thin Film Panels
1. Most efficient with max.
efficiency of 21%.
1. Less efficient with efficiency of
16% (max.)
1. Least efficient with max.
efficiency of 12%.
2. Manufactured from single Si
crystal.
2. Manufactured by fusing
different crystals of Si.
2. Manufactured by depositing 1
or more layers of PV material on
substrate.
3. Performance best at standard
temperature.
3. Performance best at moderately
high temperature.
3. Performance best at high
temperatures.
4. Requires least area for a given
power.
4. Requires less area for a given
power.
4. Requires large area for a given
power.
5. Large amount of Si hence, high
embodied energy.
5. Large amount of Si hence, high
Embodied energy.
4. Low amount of Si used hence,
low embodied energy.
6. Performance degrades in low-
sunlight conditions.
6. Performance degrades in low-
sunlight conditions.
5. Performance less affected by
low-sunlight conditions.
7. Cost/watt: 1.589 USD 7. 1.418 USD 7. 0.67 USD
8. Largest Manufacturer: 8. Suntech (China) 8. First Solar (USA)
 Efficiency,  = (VocIscFF)/Pin
 Voc is proportional to Eg,
 Isc is proportional to # of absorbed
photons
 Decrease Eg, absorb more of the
spectrum
 But not without sacrificing output
voltage
hv > Eg
Semiconductor Material Efficiencies: The Impact of
Band Gap on Efficiency
 Direction of current inside PV cell
• Inside current of PV cell looks like
“Reverse direction.” Why?
P
N
Current appears
to be in the
reverse direction ?
?
• By Solar Energy, current is pumped up from
N-pole to P-pole.
• In generation, current appears reverse. It is
the same as for battery.
P
N
Looks like
reverse
Current-Voltage (I-V) Curve
 
0 exp 1S S
ph
C Sh
q V IR V IR
I I I
kT A R
    
     
    
max
,
mp mp OC SC
en PV
in PV PV
V IP V I FF
P A G A G
   
RL
+
-
Equivalent circuit of practical PV cell
•Voltage on normal operation point
0.5V (in case of Silicon PV)
•Current depend on
- Intensity of insolation
- Size of cell
(V)
(A)
Voltage(V)
Current(I)
P
N
A
Short Circuit
Open Circuit
P
N
V
about 0.5V (Silicon)
High insolation
Low insolation
Normal operation point
(Maximum Power point)
I x V = W
Open circuit voltage and short circuit current
(V)
(A)
Voltage(V)
Current(I)
0.49 V 0.62 V
4.95A
5.55A
Depend on
type of cell or
cell-material
( Si = 0.5V )
Depend on cell-size
Depend on
Solar insolation
 To obtain maximum power, current
control (or voltage control) is very
important.
P
N
A
V
(V)
(A)
Voltage(V)
Current(I)
I x V = W
P2
PMAX
P1
Vpmax
Ipmax
I/V curve
P- Max control
Power curve
(V)
(A)
Voltage(V)
Current(I)
12
10
8
6
4
2
0
0 0.1 0.2 0.3 0.4 0.5 0.6
P
N
A
)(05.0 R
PV characteristics
( I/V curve )
If the load has 0.05 ohm resistance,
cross point of resistance character and
PV-Character will be following point.
Then power is 10x0.5=5 W
)(05.0 R
05.0/VI 
R
V
I 
Ohm’s theory
Estimate obtained power by I / V curve
P
N
P
N
Mismatch
5A
1A
P
N
P
N
Bypass
Diode
5A
1A 4A
(V)
(A)
Current(I)
High intensity insolation
Low intensity insolation
I x V = W
5A
1A
 Current is affected largely by change
of insolation intensity.
 Partially shaded serial cell will
produce current mismatch.
I / V curve vs. Insolation intensity
Voltage(V)
Effects of Temperature
 As the PV cell temperature
increases above 25º C, the
module Vmp decreases by
approximately 0.5% per
degree C
 As insolation decreases
amperage decreases
while voltage remains
roughly constant
Effects of Shading/Low Insolation
Shading on Modules
 Depends on orientation of
internal module circuitry relative
to the orientation of the shading.
 Shading can half or even
completely eliminate the output
of a solar array
Series Connections
 Loads/sources wired in series
 VOLTAGES ARE ADDITIVE
 CURRENT IS EQUAL
Parallel Connections
Loads/sources wired in parallel:
 VOLTAGE REMAINS CONSTANT
 CURRENTS ARE ADDITIVE
 Roughly size of PV System
How much PV can we install in a given area?
1 kw PV need 10 m2 (108 feet2)
Please
remember
10m(33feet)
20m(66feet)
Room
Area = 200 m2
(2,178 feet2)
We can install about 20 kW PV
Solar Panel specifications
Mechanical Specifications
1. Solar Cell Type: Defines the type of module or cell used in the module.
e.g.- Mono-Si, Poly-Si or Thin Film.
Design Implication: This determines the class of conversion efficiency of the module.
2. Cell Dimension (in inches/mm.): Defines the size of cell used in the module.
e.g.- 125(l) × 125 mm(b) (5 inches).
Design Implication: This determines the output power of a single solar cell.
3. Module Dimension (in inches/mm.): Defines the size of the panel.
e.g.- 1580 (l)× 808 (b) × 35 (h) mm.
Design Implication: Determines the number of cells accommodated
in the module.
Across length: 1580/125 = 12.64 ~ 12 [least integer].
Across breadth: 808/125 = 6.4 ~ 6.
This means number of cell be 72 (6*12).
Solar Panel specifications
Mechanical Specifications
4. Module Weight (in kgs./lbs.): Defines the weight of the module.
e.g.- 15.5 kgs. (34.1 lbs.)
Design Implication: Determines the maximum number of panels which can be installed.
5. Glazing or front Glass: Defines the type and width of the front glass used.
e.g.- 3.2 mm (0.13 inches) tempered glass.
Design Implication: Width determines the strength of the covering. The type of glass
used depends upon thermal insulation requirements or strength requirement.
6. Frame: Defines the type of frame used in the module.
e.g.- Anodized aluminium alloy
Design Implication: Frame material is chosen so that it can
Withstand the environmental effects such as corrosion,
hard Impact etc.
Mechanical Specifications
7. Output Cables: Defines the type of cables and sometimes their dimensions provided at
output to connect with connector specifications.
e.g.- H+S RADOX® SMART cable 4.0 mm2 of length 1000 mm (39.4 inches) with RADOX®
SOLAR integrated twist locking connectors.
Design Implication: The rating of the cable is as per rating
of the PV module and of optimum length generally required
by the customers.
8. Junction Box: Defines the protection level of electrical
casing at the back of panel. Also includes the no. of bypass
diodes (if used).
e.g.- IP67 rated with 3 bypass diodes.
Solar Panel specifications
Electrical Specifications
1. Peak Power (W): Defines the maximum power of the panel.
e.g.- P: 195 Wp
2. Optimum operating Voltage: Defines the highest operating voltage of panel at the
maximum power at STC.
e.g.- Vmp: 36.6V
Design Implication: Determines the number of panels required in series.
3. Optimum operating current: Defines the highest operating current of panel at the
maximum power at STC.
e.g.- Imp: 5.33A
Design Implication: Determines the wire gauge.
Used to calculate the voltage drops across the modules or cells.
Solar Panel specifications
Electrical Specifications
4. Open Circuit Voltage: Defines the output voltage when no load is connected under STC.
e.g.- Voc : 45.4V
Design Implication: Determines the maximum possible voltage.
Determines the maximum number of modules in series.
5. Short Circuit Current: Defines the protection level of electrical casing at the back of
panel. Also includes the no. of bypass diodes (if used).
e.g.- Isc: 5.69A
Design Implication: Determines the current rating of fuse which is to be used for
protection.
Determines the conductor size.
Solar Panel specifications
Electrical Specifications
7. Module Efficiency: Defines the conversion efficiency given by a given module (which is
generally lesser than the single solar cell used in the module).
e.g.- 15.3%
Design Implication: This parameter helps in solving the problem of choosing a module.
8. Operating Temperature: Defines the range of temperature for which the module can
function.
e.g.- -40°C to 85°C
Design Implication: Determines the temperature range for the environment in which the
panel can be kept.
9. Max. Series Fuse Rating: Defines the max. current which can be handled by the module
without damage.
e.g.- 15 A
Design Implication: This defines the rating of fuse to be used with the module.
Solar Panel specifications
Electrical Specifications
10. Power Tolerance: Defines the range of power deviation from its stated power ratings due
to change in its operating condition. It is defined in %.
e.g.- 0/+5 %
Design Implication: This parameter determines the upper limit for power of a module.
11. Parameters defined under NOCT: These parameters are same as defined under STC
conditions with different values.
Difference between STC and NOCT:
STC (Standard Test Conditions):
Irradiance 1000 W/m2, Module temperature 25 °C, Air Mass=1.5
NOCT(Nominal Operating Cell Temperature):
Irradiance 800 W/m2, Ambient temperature 20 °C, Wind speed 1 m/s
Solar Panel specifications
Electrical Specifications
12. Temperature Coefficients: These coefficients are defined to show the possible rate of
change of values under varying module temperature and irradiance.
Design Implication: These parameters can be used to calculate the power, current and
voltage of the module.
Temperature Coefficient of Voc can also be used to determine the maximum panel voltage
at the lowest expected temperature.
Solar Panel specifications
Parameters at STC Sanyo (HIP-190DA3) Suntech (STP190S-24/Ad+) Trina (TSM-190DC01A)
Optimum Operating Voltage (Vmp) 55.3 V 36.5 V 36.8 V
Optimum Operating Current (Imp) 3.44 A 5.20 A 5.18 A
Open - Circuit Voltage (Voc) 68.1 V 45.2 V 45.1 V
Short - Circuit Current (Isc) 3.7 A 5.62 A 5.52 A
Maximum Power at STC (Pmax) 190 W 190 W 190 W
Module Efficiency 15.7% 14.9% 14.9%
Maximum Series Fuse Rating 15 A 15 A 10 A
Maximum System Voltage 600 VDC 1000 V DC 1000VDC
Power Tolerance +10/-0% 0/+5 % 0/+3
Temperature Coefficient of Pmax -0.34% / °C -0.48 %/°C - 0.45%/°C
Temperature Coefficient of Voc -0.191 V / °C -0.34 %/°C - 0.35%/°C
Temperature Coefficient of Isc 1.68 mA / °C 0.037 %/°C 0.05%/°C
Module Dimension 53.2 x 35.35 x 2.36 in.
(1351 x 898 x 60 mm)
62.2 × 31.8 × 1.4 inches
(1580 × 808 × 35mm)
62.24 x 31.85 x 1.57in.
(1581 x 809 x 40mm)
Warranty : 90% power output
80% power output
20 Years
20 Years
12 years
25 years
10 years
25 years
Cost: $570.00 $285.00 $459.00
Comparison between Suntech, Trina and Sanyo 190W
Monocrystalline modules
Parameters at STC Monocrystalline
(S.C. Origin)
Polycrystalline
(Moserbaer)
Thin Film (a-si)
(China Solar)
Optimum Operating Voltage (Vmp) 17.82V 17 V 18 V
Optimum Operating Current (Imp) 0.285A 0.29A 0.278 A
Open - Circuit Voltage (Voc) 21.396V 21V 26.7 V
Short - Circuit Current (Isc) 0.315A 0.35A 0.401 A
Maximum Power at STC (Pmax) 5W 5 W 5 W
Module Efficiency 16.2% 14% Not Available
Temperature Coefficient of Pmax -0.549% (°K) -0.43 (°K) -(0.19±0.03)%/°C
Temperature Coefficient of Voc -0.397% /°K -0.344 %/°K -(0.34±0.04)%/°C
Temperature Coefficient of Isc 0.06% /°K 0.11 %/ °K 0.08±0.02)%/°C
Maximum System Voltage 1000 VDC 600VDC 600 VDC
Module Dimension 350x176x34mm 359x197x26 mm 385 x322 x18 mm
Warranty: 90% power output
85% power output
10 years
25 years
10 years
15 years
10 years
15 years
Comparison between Mono-, Poly- and
Amorphous Si Solar Panels (5 W)
How to choose a solar panel?
Critical parameters to be considered for solar panel evaluation
1. Selecting the right technology : The selection of solar panel
technology generally depends on space available for installation
and the overall cost of the system.
2. Selecting the right manufacturer for better warranty.
3. Check operating specifications beyond STC ratings
4. Negative Tolerance can lead to a lower system performance
and reduced capacity.
5. Solar Panel efficiency under different conditions and over time.
 Stand-alone systems - those systems which use photovoltaics technology
only, and are not connected to a utility grid.
 Hybrid systems - those systems which use photovoltaics and some other
form of energy, such as diesel generation or wind.
 Grid-tied systems - those systems which are connected to a utility grid.
Types of Solar Photovoltaic System
Stand Alone PV System
Stand Alone PV System
Water pumping system
Hybrid PV System
Hybrid PV System
Ranching the Sun project in
Hawaii generates 175 kW of PV
power and 50 kW of wind power
from the five 10 kW wind
turbines
Grid-Tied PV System
Balance of System (BOS)
The BOS typically contains
 Structures for mounting the PV arrays or modules
 Power conditioning equipment that massages and
converts the do electricity to the proper form and
magnitude required by an alternating current (ac)
load.
 Sometimes also storage devices, such as batteries,
for storing PV generated electricity during cloudy
days and at night.
1. Collect some data viz. Latitude of the location, and solar
irradiance (one for every month).
2. Calculation of total solar energy.
3. Estimate the required electrical energy on a
monthly/weekly basis (in kwh):
Required Energy= Equipment Wattage X Usage Time.
4. Calculate the system size using the data from ‘worst
month’ which can be as follows:
a) The current requirement will decide the number of panels
required.
b) The days of autonomy decides the storage capacity of the
system i.e. the number of batteries required.
How to design a PV Off-grid system?
Designing a PV System
1. Determine the load (energy, not power)
The load is being supplied by the stored energy device, usually the battery,
and of the photovoltaic system as a battery charger.
2. Calculating the battery size, if one is needed
3. Calculate the number of photovoltaic modules required
4. Assessing the need for any back-up energy of flexibility for load growth
Determining Load
 The appliances and devices (TV's, computers, lights, water pumps etc.) that
consume electrical power are called loads.
 Important : examine power consumption and reduce power needs as much as
possible.
 Make a list of the appliances and/or loads to be run from solar electric
system.
 Find out how much power each item consumes while operating.
 Most appliances have a label on the back which lists the Wattage.
 Specification sheets, local appliance dealers, and the product
manufacturers are other sources of information.
Determining Loads II
 Calculate AC loads (and DC if necessary)
 List all AC loads, wattage and hours of use per week (Hrs/Wk).
 Multiply Watts by hrs/Wk to get Watt-hours per week (WH/Wk).
 Add all the watt hours per week to determine AC Watt Hours Per Week.
 Divide by 1000 to get kW-hrs/week
 Decide how much storage is provided by battery bank as per requirement (0 if
grid tied)
 expressed as "days of autonomy" because it is based on the number of
days the system should provide power without receiving an input charge
from the solar panels or the grid.
 Also consider usage pattern and critical nature of application.
 Alternatively, if a solar panel array is added as a supplement to a generator
based system, the battery bank can be slightly undersized since the generator
can be operated in needed for recharging.
Determining the Batteries
 Once the storage capacity has been determined, consider the following key
parameters:
 Amp hours, temperature multiplier, battery size and number
 To get Amp hours :
 daily Amp hours
 number of days of storage capacity ( typically 5 days no input )
 1 x 2 = A-hrs needed
 Note: For grid tied – inverter losses
Determining the Batteries
Determining Battery Size
 Determine the discharge limit for the batteries ( between 0.2 - 0.8 )
 Deep-cycle lead acid batteries should never be completely discharged,
an acceptable discharge average is 50% or a discharge limit of 0.5
 Divide A-hrs/week by discharge limit
 Determine A-hrs of battery and # of batteries needed - Round off to the next
highest number.
 This is the number of batteries wired in parallel needed.
 Divide system voltage ( typically 12, 24 or 48 ) by battery voltage.
 This is the number of batteries wired in series needed.
 Multiply the number of batteries in parallel by the number in series.
 This is the total number of batteries needed.
Total Number of Batteries Wired in Series
Determining the Number of PV Modules
 First find the Solar Irradiance at the location.
 Irradiance is the amount of solar power striking a given area and is a measure of the
intensity of the sunshine.
 PV engineers use units of Watts (or kiloWatts) per square meter (W/m2) for
irradiance.
 http://rredc.nrel.gov/solar/old_data/nsrdb/
Peak Sun Hours
 Peak sun hours is defined as the equivalent number of
hours per day, with solar irradiance equaling 1,000 W/m2,
that gives the same energy received from sunrise to
sundown.
 Peak sun hours only make sense because PV panel power
output is rated with a radiation level of 1,000W/m2.
 Many tables of solar data are often presented as an average
daily value of peak sun hours (kW-hrs/m2) for each month.
 Determine total A-hrs/day and increase by 20% for battery losses then
divide by “1 sun hours” to get total Amps needed for array
 Then divide your Amps by the Peak Amps produced by your solar module
 The peak amperage can be determined if the module's wattage is
dividedby the peak power point voltage
 Determine the number of modules in each series string needed to supply
necessary DC battery Voltage
 Then multiply the number (for A and for V) together to get the amount of
power you need
 P=IV [W]=[A]x[V]
Calculating Energy Output of a PV Array
Charge Controller
 Charge controllers are included in most PV systems to protect the batteries
from overcharge and/or excessive discharge.
 The minimum function of the controller is to disconnect the array when the
battery is fully charged and keep the battery fully charged without damage.
 The charging routine is not the same for all batteries: a charge controller
designed for lead-acid batteries should not be used to control NiCd
batteries.
 Size by determining total Amp max for the array.
Wiring
 Selecting the correct size and type of wire will enhance the
performance and reliability of the PV system.
 The size of the wire must be large enough to carry the maximum
current expected without undue voltage losses.
 All wire has a certain amount of resistance to the flow of current.
 This resistance causes a drop in the voltage from the source to the
load. Voltage drops cause inefficiencies, especially in low voltage
systems ( 12V or less ).
 See wire size charts here: www.solarexpert.com/Photowiring.html
Inverters
 For AC grid-tied systems you do not need a battery or
charge controller if the back up power is not needed–
just the inverter.
 The Inverter changes the DC current stored in the
batteries or directly from the PV into usable AC
current.
 To size increase the Watts expected to be used by
AC loads running simultaneously by 20%
Off-Grid Design Example
Step 1: Determine the DC Load
DC Device Device Watts Hours of
daily use
DC Watt-hrs per Day (Device
Watts x Hours of daily use)
Refrigerator 60 24 1440
Lighting fixtures 150 4 600
Device A 12 8 96
Total DC Watt-hrs/Day = 2,136
Total AC Watt-hrs/Day = 1,440
Divided by 0.85 (Inverter, losses)
Total DC Whrs/Day = 1,694
AC Device Device Watts Hours of
daily use
AC Watt-hrs per Day (Device
Watts x Hours of daily use)
Device B 6175 6 1050
Pump 80 0.5 40
Television 175 2 350
Total AC Watt-hrs/Day = 1440
Step 2: Determine the AC Load, Convert to DC
Step 3: Determine the Total System Load
Total DC Loads [A] 2,136
Total DC Loads [B] 1,694
Total System Load 3,830 Whrs/Day
Step 4: Determine Total DC Amp-hours/Day
Total System Load / System Nominal Voltage =
(3,830 Whrs/Day) / 12 Volts = 319 Amp-hrs/Day
Step 5: Determine Total Amp-hr/Day with Batteries
Total Amp-hrs/Day X 1.2(Losses and safety factor)
319 Amp-hrs/Day X 1.2 = 382.8 or 383 Amp-hrs/Day
Step 6: Determine Total PV Array Current
Total Daily Amp-hr requirement / Design Insolation*
=383 Amp-hrs / 5.0 peak solar hrs = 76.6 Amps
* Insolation Based on Optimum Tilt for Season
Step 7: Select PV Module Type
Choose BP Solar-Solarex MSX-60 module:
Max Power = 60 W (STP)
Max Current = 3.56 Amps
Max Voltage = 16.8 Volts
Nominal Output Voltage 12 Volts
Total PV Array Current / (Module Operating Current) X (Module Derate Factor)
= 76.6 Amps / (3.56 Amps/Module)(0.90) = 23.90 modules
= (Use 24 Modules)
Step 8: Determine Number of Modules in Parallel
Step 9: Determine Number of Modules in Series
System Nominal Voltage / Module Nominal Voltage
12 Volts / (12 Volts/module) = 1 Module
Step 10: Determine Total Number of Modules
Number of modules in parallel X Number of modules in Series
= 24 X 1 = 24 modules
Step 11: Determine Minimum Battery Capacity
[Total Daily Amp-hr/Day with Batteries (Step 5)
X Desired Reserve Time (Days)] / Percent of Usable Battery Capacity
=(383 Amp-hrs/Day X 3 Days) / 0.80 = 1,436 Amp-hrs
Step 12: Choose a Battery
Use an Interstate U2S – 100 Flooded Lead Acid Battery
Nominal Voltage = 6 Volts
Rated Capacity = 220 Amp-hrs
Step 13: Determine Number of Batteries in Parallel
Required Battery Capacity (Step 11) / Capacity of Selected Battery
=1,436 Amp-hrs / (220 Amp-hrs/Battery)
= 6.5 (Use 6 Batteries)
Step 14: Determine Number of Batteries in Series
Nominal System Voltage / Nominal Battery Voltage
= 12 Volts / (6 Volts/Battery) = 2 Batteries
Step 15: Determine Total Number of Batteries
Number of Batteries in Parallel X Number of Batteries in Series
=6 X 2 = 12 Batteries
Series: Voltage is additive
Parallel: Current is additive
+
-
+
- -
+
3 A
12 V
3 A
12 V 3 A
24 V
6 A
12 V
3 A
12 V
3 A
12 V
+ +
- -
+
-
Step 17: Complete Balance of System
a. Complete the design by specifying the:
Charge Controller
Inverter
Wire Sizes (Battery will have larger gage due to higher currents)
Fuses and Disconnects
Standby Generator, if needed
Battery Charger, if needed
Manual Transfer Switch, if needed.
b. Determine mounting method:
Roof mount
Ground mount with racks
Ground mount with pole.
c. Assure proper grounding for safety.
d. Obtain permits as required.
Step 16: Determine the need for a Standby
Generator to reduce other Components (number of Modules and
Batteries). Several iterations may be necessary to optimize costs.
Advantage
1.It is free, clean and non-polluting
2.It is a renewable and sustainable energy
3.Solar cells do not produce noise and they are totally silent.
4.Provide electricity to remote places
5.High power-to-weight ratio
6.They require very little maintenance
7.They are long lasting sources of energy which can be used almost anywhere
8.They have long life time
9.There are no fuel costs or fuel supply problems
Disadvantage
1.Soar power can be obtained in night time
2.Soar cells (or) solar panels are Less efficient and very expensive
3.Energy has not be stored in batteries
4.Reliability Depends On Location
5.Environmental Impact of PV Cell Production
6.Air pollution and whether can affect the production of electricity
7.They need large are of land to produce more efficient power supply.
8. Solar energy is a diffuse source.
USES OF SOLAR ENERGY
 Heaters Green houses
 Cars water pumps
 Lights Desalination
 Satellites Chilling
 Dryers Solar ponds
 Calculators Thermal
Commercial use
 On an office building , roof areas can be covered with solar panels .
 Remote buildings such as schools , communities can make use of solar
energy.
 In developing countries , this solar panels are very much useful.
 Even on the highways , for every five kilometres ,solar telephones are
used.
Solar Map of India
About 5,000 trillion kWh
per year energy is incident
over India’s land area
with most parts receiving
4-7 kWh per square
meter per day.
Thank You!!
Need Help?
Feel Free To Get In Touch
contact@sunrator.com
011-41605551

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Fundamentals of Solar PV System

  • 2. Solar Energy Basics and solar spectrum Photovoltaic Cell: Construction and working principleSolar photovoltaic technologies Types of solar photovoltaic systems Designing of a solar photovoltaic system Advantages and disadvantages of solar energy and systems Applications of solar energy Outline
  • 3. What is Solar Energy?  Originates with the thermonuclear fusion reactions occurring in the sun.  Represents the entire electromagnetic radiation (visible light, infrared, ultraviolet, x-rays, and radio waves).  This energy consists of radiant light and heat energy from the sun.  Out of all energy emitted by sun only a small fraction of energy is absorbed by the earth.
  • 4. http://en.wikipedia.org/wiki/File:Breakdown_of_the_incoming_solar_ener The surface receives about 47% of the total solar energy that reaches the Earth. Only this amount is usable. Breakdown of incoming solar energy
  • 5.
  • 6. Air Mass  Amount of air mass through which light pass  Atmosphere can cut solar energy reaching earth by 50% and more
  • 7.  Solar Thermal Energy  Solar Heating  Solar Water Heating  Solar Space Heating  Solar Space Cooling  Solar Photovoltaic  Solar Concentrators Solar Energy Harvesting Using Different Paths
  • 8. Electricity Generation From Solar Energy Solar Energy can be used to generate electricity in 2 ways:  Solar Thermal Energy: Using solar thermal technologies for heating fluids which can be used as a heat source or to run turbines to generate electricity.  Solar Photovoltaic Energy: Using solar energy for the direct generation of electricity using photovoltaic phenomenon.
  • 9. Technology Options for Solar Power Parabolic Dish Solar Power Thermal Low Temperature <100°C. Solar Water Heating Solar Chimney Solar Pond Med Temp <400°C High Temp. >400°C Central Tower PV Technology Mono Crystalline Silicon Polycrystalline Silicon Amorphous Silicon Production Process Wafer Thin Film
  • 10. Energy Band Diagram of a Conductor, Semiconductor and Insulator conductor semiconductor insulator Semiconductors are interested because their conductivity can be readily modulated (by impurity doping or electrical potential), offering a pathway to control electronic circuits.
  • 11. Semiconductors used for solar cells II III IV V VI B C (6) Al Si (14) P S Zn Ga Ge (32) As Se Cd In Sb Te Semiconductors:  Elementary – Si, Ge.  Compound – GaAs, InP, CdTe.  Ternary – AlGaAs, HgCdTe, CIS.  Quaternary – CIGS, InGaAsP, InGaAIP.
  • 12. Silicon - Si Si Si Si SiSi Si Si Si Shared electrons  Silicon is group IV element – with 4 electrons in their valence shell.  When silicon atoms are brought together, each atom forms covalent bond with 4 silicon atoms in a tetrahedron geometry.
  • 13. Intrinsic Semiconductor  At 0 ºK, each electron is in its lowest energy state so each covalent bond position is filled. If a small electric field is applied to the material, no electrons will move because they are bound to their individual atoms.  At 0 ºK, silicon is an insulator.  As temperature increases, the valence electrons gain thermal energy.  If a valence electron gains enough energy (Eg), it may break its covalent bond and move away from its original position. This electron is free to move within the crystal.  Conductor Eg <0.1eV, many electrons can be thermally excited at room temperature.  Semiconductor Eg ~1eV, a few electrons can be excited (e.g. 1/billion)  Insulator, Eg >3-5eV, essentially no electron can be thermally excited at room temperature. Energy of a photon,
  • 14. Extrinsic Semiconductor, n-type Doping Electron - Si Si Si Si SiSi Si Si As Extra Valence band, Ev Eg = 1.1 eV Conducting band, Ec Ed ~ 0.05 eV  Doping silicon lattice with group V elements can creates extra electrons in the conduction band — negative charge carriers (n-type), As- donor.  Doping concentration #/cm3 (1016/cm3 ~ 1/million).
  • 15. Valence band, Ev Eg = 1.1 eV Conducting band, Ec Ea ~ 0.05 eV Electron - Si Si Si Si SiSi Si Si B Hole  Doping silicon with group III elements can creates empty holes in the valence band positive charge carriers (p-type), B-(acceptor). Extrinsic Semiconductor, p-type doping
  • 16. V I R O F p n p n V>0 V<0 Reverse bias Forward bias p-n Junction diode  A p-n junction is a junction formed by combining p-type and n-type semiconductors together in very close contact.  In p-n junction, the current is only allowed to flow along one direction from p-type to n-type materials. i p n V<0 V>0 depletion layer - +
  • 17.  Get image from book Efficiency – The Band Gap Problem
  • 19.  A PV cell is a light illuminated pn- junction diode which directly converts solar energy into electricity via the photovoltaic effect.  A typical silicon PV cell is composed of a thin wafer consisting of an ultra-thin layer of phosphorus-doped (n-type) silicon on top of a thicker layer of boron- doped (p-type) silicon.  When sunlight strikes the surface of a PV cell, photons with energy above the semiconductor bandgap impart enough energy to create electron-hole pairs. Photovoltaic Cell
  • 20. Photovoltaic Cell: Operating Principle  There are three basic steps for generation of electricity using PV cells which are following:  First is absorption of solar radiation,  Second is generation of free charge carriers and  Third is transport and then collection of charge carriers at PV cell terminals.
  • 21. Structure of a Solar Cell
  • 22. 1) Non absorbed photons 2) Lattice thermalization 3) Junction voltage drop 4) Contact voltage drop 5) Recombination Standard PV cell Efficiency Losses
  • 23. Blocking Diodes  During sun shine, as long as the voltage produced by the panels is greater than that of the battery, charging will take place.  In the dark, the voltage of the battery would cause a current flow in reverse direction through the panels, which can lead to the discharging of battery.  A blocking diode is used in series with the panels and battery in reverse biasing to prevent reverse flow of the current.  Normal p-n junction diodes can be used as blocking diodes.  To select a blocking diode, following parameters should be kept in mind:  The maximum current provided by the panels.  The voltage ratings of the diode.  The reverse breakdown voltage of the diode.
  • 24. Hot- Spot and Bypass Diodes  Hot Spot phenomenon happens when one or more cells of the panel is shaded while the others are illuminated.  The shaded cells/panels starts behaving as a diode polarized in reverse direction and generates reverse power. The other cells generate a current that flows through the shaded cell and the load.
  • 25.  Any solar cell has its own critical power dissipation Pc that must not be exceeded and depends on its cooling and material structures, its area, its maximum operating temperature and ambient temperature.  A shaded cell may be destroyed when its reverse dissipation exceeds Pc. This is the hot spot.  To eliminate the hot-spot phenomenon, a bypass diode is connected parallel to the module or group of cells in reverse polarity which provides another path to the extra current. Hot- Spot and Bypass Diodes
  • 26.  When part of a PV module is shaded, the shaded cells will not be able to produce as much current as the unshaded cells.  Since all cells are connected in series, the same amount of current must flow through every cell.  The unshaded cells will force the shaded cells to pass more current through it. Bypass diode working phases Bypass Diodes working
  • 27.  The only way the shaded cells can operate at a current higher than their short circuit current is to operate in a region of negative voltage i.e. to cause a net voltage loss to the system.  The voltage across the shaded or low current solar cell becomes greater than the forward bias voltage of the other series cells which share the same bypass diode plus the voltage of the bypass diode thus making the diode to work in forward bias and hence allowing extra current to pass through it, preventing hot-spot.  For an efficient operation, there are two conditions to fulfill:  Bypass diode has to conduct when one cell is shadowed.  The shadowed cell voltage Vs must stay under its breakdown voltage (Vc).  Ideally, a bypass diode should have a forward voltage (VF) and a leakage current (IR) as low as possible. Bypass Diodes working
  • 28. Bypass Diodes  Two types of diodes are available as bypass diodes in solar panels and arrays:  p-n junction silicon diode  Schottky barrier diode  To select a bypass diode, following parameters should be checked:  The forward voltage and current ratings of the diode.  The reverse breakdown voltage of the diode.  The reverse leakage current.  Junction Temperature Range
  • 29. 2 – 3 W 100 - 200 W 10 - 50 kW Cell Array Module,Panel Volt Ampere Watt Size Cell 0.5V 5-6A 2-3W about 10cm Module 20-30V 5-6A 100-200W about 1m Array 200-300V 50A-200A 10-50kW about 30m 6x9=54 (cells) 100-300 (modules) Hierarchy of PV
  • 30. Solar cells are composed of various semiconducting materials  Crystalline silicon  Cadmium telluride  Copper indium diselenide  Gallium arsenide  Indium phosphide  Zinc sulphide Materials for Solar cell
  • 31. Cell Technologies Crystalline silicon Mono- crystalline Pure and efficient 15-19% efficiency Multi- crystalline 12-15% efficiency Thin film Non Silicon based CdTe 8.5% efficiency CIGS 9-11% efficiency Silicon based Amorphous 5-7% efficiency
  • 32. Technology Differences Optical Properties • Band gap (direct, indirect) • Absorption Coefficient • Absorption length Electrical Properties • Carrier Lifetime • Mobility • Diffusion length Manufacturing • Absorber material • Cells • Modules Performance • Efficiency • Current, Voltage and FF • Effect of temperature and radiation
  • 33. Optical Properties: Band Gaps Fixed band gap of c-Si material (mono, multi). Tunable gaps of thin film compound semiconductors.
  • 34. Optical Properties: Material absorption lengths Absorption Length in Microns (for approx. 73% incoming light absorption) Wavelength (nm) c-Si a-Si CIGS GaAs 400 nm (3.1eV) 0.15 0.05 0.05 0.09 600 nm (2eV) 1.8 0.14 0.06 0.18 800 nm (1.55eV) 9.3 Not absorbed 0.14 1.1 1000nm(1.24eV) 180.9 Not absorbed 0.25 Not absorbed  Absorption length is much higher for Si because of lower absorption coefficient.  Longer wavelength photons require more materials to get absorbed.
  • 35. Electrical Properties Mobility Ease with which carriers move in semiconductor. Lifetime Average time carriers spend in excited state. Diffusion Carrier movement due to concentration difference. Diffusion Length Average length travelled by carrier before recombining due to concentration difference. Drift Carrier movement due to electric field. Drift length Average length travelled by carrier before recombination under electric field.
  • 36. Electrical Properties: Drift and Diffusion lengths High quality material scenario Low quality material scenario  Carrier are transported by diffusion to the junction.  Large diffusion length.  Junction is very thin.  Diffusion length are small.  Drift length is about 10 times greater than diffusion length.  Intrinsic layer is thicker.
  • 37. Three generations of solar cells 1. First Generation  First generation cells consist of high quality and single junction devices.  First Generation technologies involve high energy and labour inputs which prevent any significant progress in reducing production costs. 2. Second Generation  Second generation materials have been developed to address energy requirements and production costs of solar cells.  Alternative manufacturing techniques such as vapour deposition and electroplating are advantageous as they reduce high temperature processing significantly.  Produced from cheaper polycrystalline materials and glass  High optical absorption coefficients  Bandgap suited to solar spectrum
  • 38. 3. Third Generation  Third generation technologies aim to enhance poor electrical performance of second generation (thin-film technologies) while maintaining very low production costs.  Current research is targeting conversion efficiencies of 30-60% while retaining low cost materials and manufacturing techniques.  They can exceed the theoretical solar conversion efficiency limit for a single energy threshold material, 31% under 1 sun illumination and 40.8% under the maximal artificial concentration of sunlight (46,200 suns).  Approaches to achieving these high efficiencies including the use of multijunction photovoltaic cells, concentration of the incident spectrum, the use of thermal generation by UV light to enhance voltage or carrier collection, or the use of the infrared spectrum for night-time operation.
  • 39. Monocrystalline Silicon Modules  Most efficient commercially available module (14% - 17%)  Most expensive to produce  Circular (square-round) cell creates wasted space on module
  • 40. Front Surface (N-Type side) • Aluminum Electrode (Silver colored wire) • To avoid shading, electrode is very fine. Anti reflection film (Blue colored film) • Back surface is P-type. • All back surface is aluminum electrode with full reflection. Poly Crystalline PV Polycrystalline Silicon Modules
  • 41. Polycrystalline Silicon Modules  Less expensive to make than single crystalline modules  Cells slightly less efficient than a single crystalline (10% - 12%)  Square shape cells fit into module efficiently using the entire space
  • 42. PV Module (Single crystal, Poly crystalline Silicon) Single crystal Poly crystalline 120W (25.7V, 4.7A) 1200mm 800mm800mm 1200mm (3.93ft) (2.62ft) (3.93f) (2.62ft) 128W (26.5V ,4.8A) Efficiency is higher Efficiency is lower Same size
  • 43. Amorphous Thin Film  Most inexpensive technology to produce  Metal grid replaced with transparent oxides  Efficiency = 6 – 8 %  Can be deposited on flexible substrates  Less susceptible to shading problems  Better performance in low light conditions that with crystalline modules
  • 44. Solar Panel Manufacturing Technologies Mono-Si Solar Panels  Mono-Si is manufactured by Czochralski Process.
  • 45. Si boule for the production of wafers. Solar Panel Manufacturing Technologies  Since they are cut from single crystal, they gives the module a uniform appearance. Advantages  Highest efficient module till now with efficiency between 13 to 21%.  Commonly available in the market.  Greater heat resistance.  Acquire small area where ever placed. Disadvantages  More expensive to produce.  High amount of Silicon.  High embodied energy (total energy required to produce).
  • 46. Poly-Si Solar Panels  Polycrystalline (or multicrystalline) modules are composed of a number of different crystals, fused together to make a single cell.  Poly-Si solar panels have a non-uniform texture due to visible crystal grain present due to manufacturing process. Advantages  Good efficiency between 14 to 16%.  Cost effective manufacture.  Commonly Available in the market. Visible crystal grain in poly-Si Solar Panel Manufacturing Technologies
  • 47. Disadvantages  Not as efficient as Mono-Si.  Large amount of Si.  High Embodied Energy. Visible difference between Mono-Si and Poly-Si Panels Mono-Si solar cells are of dark color and the corners of the cells are usually missing whereas poly-Si panels are of dark or light blue color. The difference between the structure is only due to their manufacturing process. Mono-Si Panel Poly-Si Panel Solar Panel Manufacturing Technologies
  • 48. Thin Film Solar Panels  Made by depositing one or more thin layers (thin film) of photovoltaic material on a substrate.  Thin Film technology depend upon the type of material used to dope the substrate.  Cadmium telluride (CdTe), copper indium gallium selenide (CIGS) and amorphous silicon (A-Si) are three thin-film technologies often used as outdoor photovoltaic solar power production. Solar Panel Manufacturing Technologies
  • 49. Amorphous-Si Panels  Non-crystalline allotrope of Si with no definite arrangement of atoms. Advantages  Partially shade tolerant  More effective in hotter climate  Uses less silicon - low embodied energy  No aluminum frame - low embodied energy Disadvantages  Less efficient with efficiency between 6 to 9% .  Less popular - harder to replace.  Takes up more space for same output .  New technology - less proven reliability. Solar Panel Manufacturing Technologies
  • 50. Thin Film Silicon Solar Cells
  • 51. CdTe/CdS Solar Cell  CdTe: Bandgap 1.5 eV; Absorption coefficient 10 times that of Si  CdS: Bandgap 2.5 eV; Acts as window layer  Limitation: Poor contact quality with p- CdTe (~ 0.1 Wcm2) Cadmium Telluride Solar Cell  Toxicity of Cd is an issue.  Best lab efficiency = 16.5%.
  • 52.  NREL has demonstrated an efficiency of 19.9% for the CIGS solar cell.  Typically requires relatively high temperature processing (> 500C). Copper-Indium-Gallium-Diselenide Cell
  • 53. Comparison of Si on the basis of crystallinity
  • 54. Comparison of Mono-Si, Poly-Si and Thin film Panels Mono-Si Panels Poly-Si Panels Thin Film Panels 1. Most efficient with max. efficiency of 21%. 1. Less efficient with efficiency of 16% (max.) 1. Least efficient with max. efficiency of 12%. 2. Manufactured from single Si crystal. 2. Manufactured by fusing different crystals of Si. 2. Manufactured by depositing 1 or more layers of PV material on substrate. 3. Performance best at standard temperature. 3. Performance best at moderately high temperature. 3. Performance best at high temperatures. 4. Requires least area for a given power. 4. Requires less area for a given power. 4. Requires large area for a given power. 5. Large amount of Si hence, high embodied energy. 5. Large amount of Si hence, high Embodied energy. 4. Low amount of Si used hence, low embodied energy. 6. Performance degrades in low- sunlight conditions. 6. Performance degrades in low- sunlight conditions. 5. Performance less affected by low-sunlight conditions. 7. Cost/watt: 1.589 USD 7. 1.418 USD 7. 0.67 USD 8. Largest Manufacturer: 8. Suntech (China) 8. First Solar (USA)
  • 55.  Efficiency,  = (VocIscFF)/Pin  Voc is proportional to Eg,  Isc is proportional to # of absorbed photons  Decrease Eg, absorb more of the spectrum  But not without sacrificing output voltage hv > Eg Semiconductor Material Efficiencies: The Impact of Band Gap on Efficiency
  • 56.  Direction of current inside PV cell • Inside current of PV cell looks like “Reverse direction.” Why? P N Current appears to be in the reverse direction ? ? • By Solar Energy, current is pumped up from N-pole to P-pole. • In generation, current appears reverse. It is the same as for battery. P N Looks like reverse
  • 57. Current-Voltage (I-V) Curve   0 exp 1S S ph C Sh q V IR V IR I I I kT A R                 max , mp mp OC SC en PV in PV PV V IP V I FF P A G A G     RL + - Equivalent circuit of practical PV cell
  • 58. •Voltage on normal operation point 0.5V (in case of Silicon PV) •Current depend on - Intensity of insolation - Size of cell (V) (A) Voltage(V) Current(I) P N A Short Circuit Open Circuit P N V about 0.5V (Silicon) High insolation Low insolation Normal operation point (Maximum Power point) I x V = W Open circuit voltage and short circuit current
  • 59. (V) (A) Voltage(V) Current(I) 0.49 V 0.62 V 4.95A 5.55A Depend on type of cell or cell-material ( Si = 0.5V ) Depend on cell-size Depend on Solar insolation
  • 60.  To obtain maximum power, current control (or voltage control) is very important. P N A V (V) (A) Voltage(V) Current(I) I x V = W P2 PMAX P1 Vpmax Ipmax I/V curve P- Max control Power curve
  • 61. (V) (A) Voltage(V) Current(I) 12 10 8 6 4 2 0 0 0.1 0.2 0.3 0.4 0.5 0.6 P N A )(05.0 R PV characteristics ( I/V curve ) If the load has 0.05 ohm resistance, cross point of resistance character and PV-Character will be following point. Then power is 10x0.5=5 W )(05.0 R 05.0/VI  R V I  Ohm’s theory Estimate obtained power by I / V curve
  • 62. P N P N Mismatch 5A 1A P N P N Bypass Diode 5A 1A 4A (V) (A) Current(I) High intensity insolation Low intensity insolation I x V = W 5A 1A  Current is affected largely by change of insolation intensity.  Partially shaded serial cell will produce current mismatch. I / V curve vs. Insolation intensity Voltage(V)
  • 63. Effects of Temperature  As the PV cell temperature increases above 25º C, the module Vmp decreases by approximately 0.5% per degree C
  • 64.  As insolation decreases amperage decreases while voltage remains roughly constant Effects of Shading/Low Insolation
  • 65. Shading on Modules  Depends on orientation of internal module circuitry relative to the orientation of the shading.  Shading can half or even completely eliminate the output of a solar array
  • 66. Series Connections  Loads/sources wired in series  VOLTAGES ARE ADDITIVE  CURRENT IS EQUAL
  • 67. Parallel Connections Loads/sources wired in parallel:  VOLTAGE REMAINS CONSTANT  CURRENTS ARE ADDITIVE
  • 68.  Roughly size of PV System How much PV can we install in a given area? 1 kw PV need 10 m2 (108 feet2) Please remember 10m(33feet) 20m(66feet) Room Area = 200 m2 (2,178 feet2) We can install about 20 kW PV
  • 69. Solar Panel specifications Mechanical Specifications 1. Solar Cell Type: Defines the type of module or cell used in the module. e.g.- Mono-Si, Poly-Si or Thin Film. Design Implication: This determines the class of conversion efficiency of the module. 2. Cell Dimension (in inches/mm.): Defines the size of cell used in the module. e.g.- 125(l) × 125 mm(b) (5 inches). Design Implication: This determines the output power of a single solar cell. 3. Module Dimension (in inches/mm.): Defines the size of the panel. e.g.- 1580 (l)× 808 (b) × 35 (h) mm. Design Implication: Determines the number of cells accommodated in the module. Across length: 1580/125 = 12.64 ~ 12 [least integer]. Across breadth: 808/125 = 6.4 ~ 6. This means number of cell be 72 (6*12).
  • 70. Solar Panel specifications Mechanical Specifications 4. Module Weight (in kgs./lbs.): Defines the weight of the module. e.g.- 15.5 kgs. (34.1 lbs.) Design Implication: Determines the maximum number of panels which can be installed. 5. Glazing or front Glass: Defines the type and width of the front glass used. e.g.- 3.2 mm (0.13 inches) tempered glass. Design Implication: Width determines the strength of the covering. The type of glass used depends upon thermal insulation requirements or strength requirement. 6. Frame: Defines the type of frame used in the module. e.g.- Anodized aluminium alloy Design Implication: Frame material is chosen so that it can Withstand the environmental effects such as corrosion, hard Impact etc.
  • 71. Mechanical Specifications 7. Output Cables: Defines the type of cables and sometimes their dimensions provided at output to connect with connector specifications. e.g.- H+S RADOX® SMART cable 4.0 mm2 of length 1000 mm (39.4 inches) with RADOX® SOLAR integrated twist locking connectors. Design Implication: The rating of the cable is as per rating of the PV module and of optimum length generally required by the customers. 8. Junction Box: Defines the protection level of electrical casing at the back of panel. Also includes the no. of bypass diodes (if used). e.g.- IP67 rated with 3 bypass diodes. Solar Panel specifications
  • 72. Electrical Specifications 1. Peak Power (W): Defines the maximum power of the panel. e.g.- P: 195 Wp 2. Optimum operating Voltage: Defines the highest operating voltage of panel at the maximum power at STC. e.g.- Vmp: 36.6V Design Implication: Determines the number of panels required in series. 3. Optimum operating current: Defines the highest operating current of panel at the maximum power at STC. e.g.- Imp: 5.33A Design Implication: Determines the wire gauge. Used to calculate the voltage drops across the modules or cells. Solar Panel specifications
  • 73. Electrical Specifications 4. Open Circuit Voltage: Defines the output voltage when no load is connected under STC. e.g.- Voc : 45.4V Design Implication: Determines the maximum possible voltage. Determines the maximum number of modules in series. 5. Short Circuit Current: Defines the protection level of electrical casing at the back of panel. Also includes the no. of bypass diodes (if used). e.g.- Isc: 5.69A Design Implication: Determines the current rating of fuse which is to be used for protection. Determines the conductor size. Solar Panel specifications
  • 74. Electrical Specifications 7. Module Efficiency: Defines the conversion efficiency given by a given module (which is generally lesser than the single solar cell used in the module). e.g.- 15.3% Design Implication: This parameter helps in solving the problem of choosing a module. 8. Operating Temperature: Defines the range of temperature for which the module can function. e.g.- -40°C to 85°C Design Implication: Determines the temperature range for the environment in which the panel can be kept. 9. Max. Series Fuse Rating: Defines the max. current which can be handled by the module without damage. e.g.- 15 A Design Implication: This defines the rating of fuse to be used with the module. Solar Panel specifications
  • 75. Electrical Specifications 10. Power Tolerance: Defines the range of power deviation from its stated power ratings due to change in its operating condition. It is defined in %. e.g.- 0/+5 % Design Implication: This parameter determines the upper limit for power of a module. 11. Parameters defined under NOCT: These parameters are same as defined under STC conditions with different values. Difference between STC and NOCT: STC (Standard Test Conditions): Irradiance 1000 W/m2, Module temperature 25 °C, Air Mass=1.5 NOCT(Nominal Operating Cell Temperature): Irradiance 800 W/m2, Ambient temperature 20 °C, Wind speed 1 m/s Solar Panel specifications
  • 76. Electrical Specifications 12. Temperature Coefficients: These coefficients are defined to show the possible rate of change of values under varying module temperature and irradiance. Design Implication: These parameters can be used to calculate the power, current and voltage of the module. Temperature Coefficient of Voc can also be used to determine the maximum panel voltage at the lowest expected temperature. Solar Panel specifications
  • 77. Parameters at STC Sanyo (HIP-190DA3) Suntech (STP190S-24/Ad+) Trina (TSM-190DC01A) Optimum Operating Voltage (Vmp) 55.3 V 36.5 V 36.8 V Optimum Operating Current (Imp) 3.44 A 5.20 A 5.18 A Open - Circuit Voltage (Voc) 68.1 V 45.2 V 45.1 V Short - Circuit Current (Isc) 3.7 A 5.62 A 5.52 A Maximum Power at STC (Pmax) 190 W 190 W 190 W Module Efficiency 15.7% 14.9% 14.9% Maximum Series Fuse Rating 15 A 15 A 10 A Maximum System Voltage 600 VDC 1000 V DC 1000VDC Power Tolerance +10/-0% 0/+5 % 0/+3 Temperature Coefficient of Pmax -0.34% / °C -0.48 %/°C - 0.45%/°C Temperature Coefficient of Voc -0.191 V / °C -0.34 %/°C - 0.35%/°C Temperature Coefficient of Isc 1.68 mA / °C 0.037 %/°C 0.05%/°C Module Dimension 53.2 x 35.35 x 2.36 in. (1351 x 898 x 60 mm) 62.2 × 31.8 × 1.4 inches (1580 × 808 × 35mm) 62.24 x 31.85 x 1.57in. (1581 x 809 x 40mm) Warranty : 90% power output 80% power output 20 Years 20 Years 12 years 25 years 10 years 25 years Cost: $570.00 $285.00 $459.00 Comparison between Suntech, Trina and Sanyo 190W Monocrystalline modules
  • 78. Parameters at STC Monocrystalline (S.C. Origin) Polycrystalline (Moserbaer) Thin Film (a-si) (China Solar) Optimum Operating Voltage (Vmp) 17.82V 17 V 18 V Optimum Operating Current (Imp) 0.285A 0.29A 0.278 A Open - Circuit Voltage (Voc) 21.396V 21V 26.7 V Short - Circuit Current (Isc) 0.315A 0.35A 0.401 A Maximum Power at STC (Pmax) 5W 5 W 5 W Module Efficiency 16.2% 14% Not Available Temperature Coefficient of Pmax -0.549% (°K) -0.43 (°K) -(0.19±0.03)%/°C Temperature Coefficient of Voc -0.397% /°K -0.344 %/°K -(0.34±0.04)%/°C Temperature Coefficient of Isc 0.06% /°K 0.11 %/ °K 0.08±0.02)%/°C Maximum System Voltage 1000 VDC 600VDC 600 VDC Module Dimension 350x176x34mm 359x197x26 mm 385 x322 x18 mm Warranty: 90% power output 85% power output 10 years 25 years 10 years 15 years 10 years 15 years Comparison between Mono-, Poly- and Amorphous Si Solar Panels (5 W)
  • 79. How to choose a solar panel? Critical parameters to be considered for solar panel evaluation 1. Selecting the right technology : The selection of solar panel technology generally depends on space available for installation and the overall cost of the system. 2. Selecting the right manufacturer for better warranty. 3. Check operating specifications beyond STC ratings 4. Negative Tolerance can lead to a lower system performance and reduced capacity. 5. Solar Panel efficiency under different conditions and over time.
  • 80.  Stand-alone systems - those systems which use photovoltaics technology only, and are not connected to a utility grid.  Hybrid systems - those systems which use photovoltaics and some other form of energy, such as diesel generation or wind.  Grid-tied systems - those systems which are connected to a utility grid. Types of Solar Photovoltaic System
  • 81. Stand Alone PV System
  • 82. Stand Alone PV System Water pumping system
  • 84. Hybrid PV System Ranching the Sun project in Hawaii generates 175 kW of PV power and 50 kW of wind power from the five 10 kW wind turbines
  • 86. Balance of System (BOS) The BOS typically contains  Structures for mounting the PV arrays or modules  Power conditioning equipment that massages and converts the do electricity to the proper form and magnitude required by an alternating current (ac) load.  Sometimes also storage devices, such as batteries, for storing PV generated electricity during cloudy days and at night.
  • 87. 1. Collect some data viz. Latitude of the location, and solar irradiance (one for every month). 2. Calculation of total solar energy. 3. Estimate the required electrical energy on a monthly/weekly basis (in kwh): Required Energy= Equipment Wattage X Usage Time. 4. Calculate the system size using the data from ‘worst month’ which can be as follows: a) The current requirement will decide the number of panels required. b) The days of autonomy decides the storage capacity of the system i.e. the number of batteries required. How to design a PV Off-grid system?
  • 88. Designing a PV System 1. Determine the load (energy, not power) The load is being supplied by the stored energy device, usually the battery, and of the photovoltaic system as a battery charger. 2. Calculating the battery size, if one is needed 3. Calculate the number of photovoltaic modules required 4. Assessing the need for any back-up energy of flexibility for load growth
  • 89. Determining Load  The appliances and devices (TV's, computers, lights, water pumps etc.) that consume electrical power are called loads.  Important : examine power consumption and reduce power needs as much as possible.  Make a list of the appliances and/or loads to be run from solar electric system.  Find out how much power each item consumes while operating.  Most appliances have a label on the back which lists the Wattage.  Specification sheets, local appliance dealers, and the product manufacturers are other sources of information.
  • 90. Determining Loads II  Calculate AC loads (and DC if necessary)  List all AC loads, wattage and hours of use per week (Hrs/Wk).  Multiply Watts by hrs/Wk to get Watt-hours per week (WH/Wk).  Add all the watt hours per week to determine AC Watt Hours Per Week.  Divide by 1000 to get kW-hrs/week
  • 91.  Decide how much storage is provided by battery bank as per requirement (0 if grid tied)  expressed as "days of autonomy" because it is based on the number of days the system should provide power without receiving an input charge from the solar panels or the grid.  Also consider usage pattern and critical nature of application.  Alternatively, if a solar panel array is added as a supplement to a generator based system, the battery bank can be slightly undersized since the generator can be operated in needed for recharging. Determining the Batteries
  • 92.  Once the storage capacity has been determined, consider the following key parameters:  Amp hours, temperature multiplier, battery size and number  To get Amp hours :  daily Amp hours  number of days of storage capacity ( typically 5 days no input )  1 x 2 = A-hrs needed  Note: For grid tied – inverter losses Determining the Batteries
  • 93. Determining Battery Size  Determine the discharge limit for the batteries ( between 0.2 - 0.8 )  Deep-cycle lead acid batteries should never be completely discharged, an acceptable discharge average is 50% or a discharge limit of 0.5  Divide A-hrs/week by discharge limit  Determine A-hrs of battery and # of batteries needed - Round off to the next highest number.  This is the number of batteries wired in parallel needed.
  • 94.  Divide system voltage ( typically 12, 24 or 48 ) by battery voltage.  This is the number of batteries wired in series needed.  Multiply the number of batteries in parallel by the number in series.  This is the total number of batteries needed. Total Number of Batteries Wired in Series
  • 95. Determining the Number of PV Modules  First find the Solar Irradiance at the location.  Irradiance is the amount of solar power striking a given area and is a measure of the intensity of the sunshine.  PV engineers use units of Watts (or kiloWatts) per square meter (W/m2) for irradiance.  http://rredc.nrel.gov/solar/old_data/nsrdb/
  • 96. Peak Sun Hours  Peak sun hours is defined as the equivalent number of hours per day, with solar irradiance equaling 1,000 W/m2, that gives the same energy received from sunrise to sundown.  Peak sun hours only make sense because PV panel power output is rated with a radiation level of 1,000W/m2.  Many tables of solar data are often presented as an average daily value of peak sun hours (kW-hrs/m2) for each month.
  • 97.  Determine total A-hrs/day and increase by 20% for battery losses then divide by “1 sun hours” to get total Amps needed for array  Then divide your Amps by the Peak Amps produced by your solar module  The peak amperage can be determined if the module's wattage is dividedby the peak power point voltage  Determine the number of modules in each series string needed to supply necessary DC battery Voltage  Then multiply the number (for A and for V) together to get the amount of power you need  P=IV [W]=[A]x[V] Calculating Energy Output of a PV Array
  • 98. Charge Controller  Charge controllers are included in most PV systems to protect the batteries from overcharge and/or excessive discharge.  The minimum function of the controller is to disconnect the array when the battery is fully charged and keep the battery fully charged without damage.  The charging routine is not the same for all batteries: a charge controller designed for lead-acid batteries should not be used to control NiCd batteries.  Size by determining total Amp max for the array.
  • 99. Wiring  Selecting the correct size and type of wire will enhance the performance and reliability of the PV system.  The size of the wire must be large enough to carry the maximum current expected without undue voltage losses.  All wire has a certain amount of resistance to the flow of current.  This resistance causes a drop in the voltage from the source to the load. Voltage drops cause inefficiencies, especially in low voltage systems ( 12V or less ).  See wire size charts here: www.solarexpert.com/Photowiring.html
  • 100. Inverters  For AC grid-tied systems you do not need a battery or charge controller if the back up power is not needed– just the inverter.  The Inverter changes the DC current stored in the batteries or directly from the PV into usable AC current.  To size increase the Watts expected to be used by AC loads running simultaneously by 20%
  • 101. Off-Grid Design Example Step 1: Determine the DC Load DC Device Device Watts Hours of daily use DC Watt-hrs per Day (Device Watts x Hours of daily use) Refrigerator 60 24 1440 Lighting fixtures 150 4 600 Device A 12 8 96 Total DC Watt-hrs/Day = 2,136
  • 102. Total AC Watt-hrs/Day = 1,440 Divided by 0.85 (Inverter, losses) Total DC Whrs/Day = 1,694 AC Device Device Watts Hours of daily use AC Watt-hrs per Day (Device Watts x Hours of daily use) Device B 6175 6 1050 Pump 80 0.5 40 Television 175 2 350 Total AC Watt-hrs/Day = 1440 Step 2: Determine the AC Load, Convert to DC
  • 103. Step 3: Determine the Total System Load Total DC Loads [A] 2,136 Total DC Loads [B] 1,694 Total System Load 3,830 Whrs/Day Step 4: Determine Total DC Amp-hours/Day Total System Load / System Nominal Voltage = (3,830 Whrs/Day) / 12 Volts = 319 Amp-hrs/Day Step 5: Determine Total Amp-hr/Day with Batteries Total Amp-hrs/Day X 1.2(Losses and safety factor) 319 Amp-hrs/Day X 1.2 = 382.8 or 383 Amp-hrs/Day
  • 104. Step 6: Determine Total PV Array Current Total Daily Amp-hr requirement / Design Insolation* =383 Amp-hrs / 5.0 peak solar hrs = 76.6 Amps * Insolation Based on Optimum Tilt for Season Step 7: Select PV Module Type Choose BP Solar-Solarex MSX-60 module: Max Power = 60 W (STP) Max Current = 3.56 Amps Max Voltage = 16.8 Volts Nominal Output Voltage 12 Volts
  • 105. Total PV Array Current / (Module Operating Current) X (Module Derate Factor) = 76.6 Amps / (3.56 Amps/Module)(0.90) = 23.90 modules = (Use 24 Modules) Step 8: Determine Number of Modules in Parallel Step 9: Determine Number of Modules in Series System Nominal Voltage / Module Nominal Voltage 12 Volts / (12 Volts/module) = 1 Module Step 10: Determine Total Number of Modules Number of modules in parallel X Number of modules in Series = 24 X 1 = 24 modules
  • 106. Step 11: Determine Minimum Battery Capacity [Total Daily Amp-hr/Day with Batteries (Step 5) X Desired Reserve Time (Days)] / Percent of Usable Battery Capacity =(383 Amp-hrs/Day X 3 Days) / 0.80 = 1,436 Amp-hrs Step 12: Choose a Battery Use an Interstate U2S – 100 Flooded Lead Acid Battery Nominal Voltage = 6 Volts Rated Capacity = 220 Amp-hrs
  • 107. Step 13: Determine Number of Batteries in Parallel Required Battery Capacity (Step 11) / Capacity of Selected Battery =1,436 Amp-hrs / (220 Amp-hrs/Battery) = 6.5 (Use 6 Batteries) Step 14: Determine Number of Batteries in Series Nominal System Voltage / Nominal Battery Voltage = 12 Volts / (6 Volts/Battery) = 2 Batteries Step 15: Determine Total Number of Batteries Number of Batteries in Parallel X Number of Batteries in Series =6 X 2 = 12 Batteries
  • 108. Series: Voltage is additive Parallel: Current is additive + - + - - + 3 A 12 V 3 A 12 V 3 A 24 V 6 A 12 V 3 A 12 V 3 A 12 V + + - - + -
  • 109. Step 17: Complete Balance of System a. Complete the design by specifying the: Charge Controller Inverter Wire Sizes (Battery will have larger gage due to higher currents) Fuses and Disconnects Standby Generator, if needed Battery Charger, if needed Manual Transfer Switch, if needed. b. Determine mounting method: Roof mount Ground mount with racks Ground mount with pole. c. Assure proper grounding for safety. d. Obtain permits as required. Step 16: Determine the need for a Standby Generator to reduce other Components (number of Modules and Batteries). Several iterations may be necessary to optimize costs.
  • 110. Advantage 1.It is free, clean and non-polluting 2.It is a renewable and sustainable energy 3.Solar cells do not produce noise and they are totally silent. 4.Provide electricity to remote places 5.High power-to-weight ratio 6.They require very little maintenance 7.They are long lasting sources of energy which can be used almost anywhere 8.They have long life time 9.There are no fuel costs or fuel supply problems
  • 111. Disadvantage 1.Soar power can be obtained in night time 2.Soar cells (or) solar panels are Less efficient and very expensive 3.Energy has not be stored in batteries 4.Reliability Depends On Location 5.Environmental Impact of PV Cell Production 6.Air pollution and whether can affect the production of electricity 7.They need large are of land to produce more efficient power supply. 8. Solar energy is a diffuse source.
  • 112. USES OF SOLAR ENERGY  Heaters Green houses  Cars water pumps  Lights Desalination  Satellites Chilling  Dryers Solar ponds  Calculators Thermal Commercial use  On an office building , roof areas can be covered with solar panels .  Remote buildings such as schools , communities can make use of solar energy.  In developing countries , this solar panels are very much useful.  Even on the highways , for every five kilometres ,solar telephones are used.
  • 113. Solar Map of India About 5,000 trillion kWh per year energy is incident over India’s land area with most parts receiving 4-7 kWh per square meter per day.
  • 114. Thank You!! Need Help? Feel Free To Get In Touch contact@sunrator.com 011-41605551

Editor's Notes

  1. Solar Panels (Single-crystal and Polycrystalline Silicon)  On the left is a single-crystal silicon solar panel. Single-crystal is formed by melting high purity silicon, then sliced very thinly and processed into solar panel.  On the right is a polycrystalline silicon solar panel. To reduce the cost of solar panels, metal silicon pure enough to manufacture solar cell is poured into a mold and crystallized. Solar cell consists of many crystalline silicon.
  2. Crystal grain boundaries can trap electrons, which results in lower efficiency.
  3. I will introduce the principle to begin with. Solar cell, invented in the USA in 1954, is a kind of semiconductor to convert energy of light directly into electricity. Most semiconductor used for solar cell are silicon semiconductors and it is composed of P-type semiconductor and N-type semiconductor. Sunlight hitting the cell produces two types of electrons, negatively charged and positively charged electrons in the semiconductors. Negatively charged electrons gather around N-type semiconductor while positively charged electrons gather around P-type semiconductor. When youconnect loads such as a light bulb or motor, electric current occurs between two electrodes.
  4. Maximize power output by maximizing area under the curve.
  5. I will introduce the principle to begin with. Solar cell, invented in the USA in 1954, is a kind of semiconductor to convert energy of light directly into electricity. Most semiconductor used for solar cell are silicon semiconductors and it is composed of P-type semiconductor and N-type semiconductor. Sunlight hitting the cell produces two types of electrons, negatively charged and positively charged electrons in the semiconductors. Negatively charged electrons gather around N-type semiconductor while positively charged electrons gather around P-type semiconductor. When youconnect loads such as a light bulb or motor, electric current occurs between two electrodes.
  6. I will introduce the principle to begin with. Solar cell, invented in the USA in 1954, is a kind of semiconductor to convert energy of light directly into electricity. Most semiconductor used for solar cell are silicon semiconductors and it is composed of P-type semiconductor and N-type semiconductor. Sunlight hitting the cell produces two types of electrons, negatively charged and positively charged electrons in the semiconductors. Negatively charged electrons gather around N-type semiconductor while positively charged electrons gather around P-type semiconductor. When youconnect loads such as a light bulb or motor, electric current occurs between two electrodes.
  7. Leave 6” space between roof and panel
  8. Insolation is a measure of solar radiation energy received on a given surface area in a given time.
  9. This is an example of a stand alone PV system. To pump water in India as shown here, you have the PV arrays which produce electricity, which travels through a disconnect switch and linear current booster to provide power to the water pump. This system is common in underdeveloped countries and agricultural applications. It is very simple to design and has no storage. Sources: http://www.sandia.gov/pv/docs/WPSize.html http://www.nrel.gov/data/pix/searchpix.cgi?getrec=9085241&display_type=verbose&search_reverse=1
  10. This is a block diagram of a hybrid PV system. The PV array produces electricity, which goes through the blocking diode and the fused disconnect to get to the maximum power tracker. If you need electricity immediately, it runs though the inverter and transformer and goes to your load. Otherwise, it is stored in a battery. Then if it became dark out, you can draw the energy from the battery. If it is dark for a very long time, you can draw the energy from the diesel generator. Source: http://www.sandia.gov/pv/docs/BOS.htm
  11. This example of a hybrid system is a ranch project in Hawaii where you have both wind and solar PV energy needed for the farm. There is 175 kW of PV power and 50 kW of wind power. Sources: http://www.nrel.gov/data/pix/Jpegs/13822.jpghttp://www.nrel.gov/data/pix/searchpix.cgi?getrec=491123&display_type=verbose&search_reverse=1
  12. Most of us are interested in grid-tied systems because most of us are connected on grid system houses, so if you don’t have a ranch or a cottage up in the country, you get your electricity from a grid. For this type of system it is very feasible to put a solar array on your roof. Here you have solar panel array on your roof, sun shines on it and produces a DC voltage (like a battery). Then it runs through the inverter and turns into AC Voltage (like the electricity that comes from a wall outlet). The inverter is usually monitored in some way. Usually you’ll have a panel inside your home. AC voltage goes straight to the main utility breaker panel. From there it can be used to power any electrical device in your home. In cases, lets say, at lunch time, if you’re at work, and the solar cell is doing really good because it’s a sunny day out, you’re going to be producing a lot of electricity, and then it can be fed back into grid and spin your utility meter backwards. You then only pay for the net amount of electricity you use. This is called net metering. You are only paying for the net amount of electricity you are consuming. Some solar users purposely make more electricity than they use so they can receive money back from the electric companies. Base definitions for grid tied solar photovoltaic systems: Solar Panels convert sunlight directly into electricity. The Inverter converts the solar electricity (DC) into household current (AC) that can be used to power loads in the house. The System Monitor is an easy-to-read digital meter that shows the homeowner the amount of electricity generated both cumulatively and daily. The Utility Meter tracks power usage and production, spinning forward when electricity is used from the grid, and spinning backwards, generating a credit, when the solar system creates more electricity than is used in the house. Sources: http://www.solarmarket.com/frontier.html
  13. The balance of system components (BOS) are comprised of the additional electrical equipment required for the system to operate properly and the structural support. The balance of systems usually contains structures for mounting the PV arrays or modules. In some the modules are located directly on the roof and we will see examples of this in a moment. There is significant savings doing this to avoid infrastructure such as concrete and metal poles used to support the structure of modules shown in the above photo. This is power conditioning equipment that massages and converts the electricity to the proper form and magnitude required by an alternating current (ac) load is also necessary. The electricity produced from solar cells is DC and then it goes through an inverter in order to make it AC. An inverter is shown in the second picture. The third picture is a battery stored system. When you are not on the grid, you need to store the energy in some way and you can store it in batteries for instances such as cloudy days or at night. Even if the array is connected to the grid, sometimes users want a battery backup for safety reasons. Sources: http://www.nrel.gov/data/pix/searchpix.cgi?getrec=1474463&display_type=verbose&search_reverse=1 http://www.nrel.gov/data/pix/searchpix.cgi?getrec=874836&display_type=verbose&search_reverse=1 http://www.nrel.gov/data/pix/searchpix.cgi?getrec=3336181&display_type=verbose&search_reverse=1
  14. So if you would like a PV system of your own, you can actually design it yourself. This can also be used for an exercise during class or do it for your own home. So the first thing you want to do is determine your load. This is the energy, not the power. You can think of this as supplied by the stored energy device, usually the battery, and of the photovoltaic system as a battery charger. The steps in this process are the following. You need to calculate your battery size, calculate the number of photovoltaic modules you’ll need, and then assess the need for any back-up energy of flexibility for load growth. A great place to get this information is Stand-Alone Photovoltaic Systems: A Handbook of Recommended Design Practices details the design of complete photovoltaic systems. Source: http://www.sandia.gov/pv/docs/Recommended%20Design%20Practices.htm
  15. Your first step in designing your PV system is determining your load. Any device that consumes electrical power are called loads. You want to examine your own power consumption. Its important to note, that you want to reduce your power needs as much as possible. That is because it will reduce the size of your PV system and reduce your initial costs. You will want to make a list of things you will run on your system and try to reduce it as much as possible. For example, change your lighting from incandescent to CFL. So after you’ve found every means to reduce energy use, figure out how much power each appliance or load uses and how much time you are using it for. Most appliances have the power it uses on the back label. Another means of finding how much power a device uses, you can look off specification sheets, local appliance dealers, and the product manufacturers are other sources of information. Sources: http://www.solarexpert.com/Pvload.html
  16. Then you need to calculate your AC and DC loads. Sometimes you have more complicated systems that are half AC and half DC. But here we are going to work with just the AC systems. So first you want to list your AC loads, like your hair dryer, refrigerator, computer. Then you would want to list the wattage and hours used per week. For example, say I use my 250 Watt computer for an hour a day every week day, that adds up to five hours a week. Then I would multiply 250 Watts by 5 hrs a week and I would get 1250 Watt-hours per week. Next I would divide by 1000 to get the kW-hrs/week. As you can see kW-hrs is how the electric companies measure your energy use and that is what you pay for on your bill. The other thing to note here is that, for a refrigerator, it is not running all the time so you should not calculate it running 24 hrs/ 7 days a week. For devices like this the manufacturers will have a good estimate of how much energy it uses per year. Sources: http://www.solarexpert.com/Pvload.html
  17. Now you need to determine the batteries needed for your system. Now if you are planning on doing a grid-type system, you can skip this step. But if you need battery back for places such as hospitals, or you are not tied to the grid, you need to first determine how long you want the electricity to be provided if there is no sunlight. This is usually expressed as “days of autonomy" because it is based on the number of days you expect your system to provide power without receiving an input charge from the solar panels or the grid. You also need to consider usage pattern and critical nature of your application. If its not very important to you to have electricity every single day, then its okay to use a small number for the days. If you are installing a system for a weekend home, you might want to consider a larger battery bank and a smaller PV array because your system will have all week to charge and store energy. Alternatively, if you are adding a solar panel array as a supplement to a generator based system, your battery bank can be slightly undersized since the generator can be operated in needed for recharging. Sources: http://www.solarexpert.com/Pvbattery.html
  18. Once you have determined your storage capacity, you are ready to consider the following key parameters. So after you know how many days you want to go just off the battery, you want to determine the number of daily amp hours. You do this by taking the number of days of storage capacity and multiply it by the daily amp hours and then you get the total amp-hours needed for your battery. Note if you are installing a grid-tied system you will need to take into account the efficiency of the inverter to convert battery loads into AC loads. Sources: http://www.solarexpert.com/Pvbattery.html Photovoltaics Design and Installation Manual --SEI
  19. Next you want to determine the discharge limit for the batteries. This is usually between 0.2 - 0.8. Normally for acid batteries you never want to discharge them completely. So an acceptable discharge is somewhere around 50 percent. So you divide the number of amp-hrs/week by discharge limit and multiply by “temperature multiplier” that we received from the last slide. If you end up with a fraction – round up to the next whole number of batteries to deliver the necessary current. Sources: http://www.solarexpert.com/Pvbattery.html
  20. Now to get the total number of batteries, you will be needing to think about the voltage. Remember, Power = Voltage x Current. You take your system voltage and divide by the battery voltage. For example you have a 48 volt system and you divide by 12 voltage battery, you get that you need 4 batteries. So now you need to wire 4 batteries in series and then you multiply the number of batteries in parallel by the number in series and this is the total number of batteries needed. Sources: http://www.solarexpert.com/Pvbattery.html
  21. After you have figured out your batteries or you have skipped the other steps because you are already attached to the grid, you can then determine the number of PV modules you will need. First you want to find the Solar Irradiance in your area. Irradiance is the amount of solar power striking a given area and is a measure of the intensity of the sunshine. PV engineers use units of Watts, or kiloWatts, per square meter (W/m2) for irradiance. And if you want your irradiance for any location in the US, go to this website: http://rredc.nrel.gov/solar/old_data/nsrdb/.
  22. Peak sun hours is defined as the equivalent number of hours per day, with solar irradiance equaling 1,000 W/m2. That gives the same energy received from sunrise to sunset. Peak sun hours only make sense because PV panel power output is rated with a radiation level of 1,000W/m2. In other words, six peak sun hours means that the energy received during total daylight hours equals the energy that would have been received had the sun shone for six hours with an irradiance of 1,000 W/m2. Many tables of solar data are often presented as an average daily value of peak sun hours (kwh/m2) for each month. In other words, six peak sun hours means that the energy received during total daylight hours equals the energy that would have been received had the sun shone for six hours with an irradiance of 1,000 W/m2. This is how you would determine your irradiance. Therefore, peak sun hours corresponds directly to average daily insolation given in kwh/m2. Sources: http://www.sandia.gov/pv/docs/FAQ.html#AnchorAfford
  23. Next you want to calculate energy output of a PV Array. You have already determined the total number of Amp-hrs per day and you will want to increase this by 20% for battery losses then divide by “1 sun hours”, from the map on an earlier slide, to get total Amps needed for array. Then divide your Amps by the Peak Amps produced by the solar module you have chosen to use. You will need to pick out a certain type of solar module and determine the peak amperage if you divide the module's wattage by the peak power point voltage. The power (P) equals the current (I) times the voltage (V). Dividing P by V gives you the current in Amps. Next, determine the number of modules in each series string needed to supply necessary DC battery Voltage. For example, if you need 12V and your peak power voltage is 4V you need 3 panels in series. Finally you can determine the total power for your PV system by multiplying the number of amps and the number of volts together. P=IV [W]=[A]x[V]. Sources: http://www.solarexpert.com/Pvmodule.html
  24. If your system has a battery, you’ll need a charge controller. Charge controllers are included in most PV systems to protect the batteries from overcharge and/or excessive discharge. The minimum function of the controller is to disconnect the array when the battery is fully charged and keep the battery fully charged without damage. The charging routine is not the same for all batteries: a charge controller designed for lead-acid batteries should not be used to control NiCd batteries. To determine the size of charge controller use the total Amp maximum for your array. The basic criteria for selecting a controller includes the operating voltage and the PV array current. Controllers are critical components in stand-alone PV systems because a controller failure can damage the batteries or load. The controller must be sized to handle the maximum current produced by the PV array. There are two types of controllers: series and shunt. Series controllers stop the flow of current by opening the circuit between the battery and the PV array. Shunt controllers divert the PV array current from the battery. Both types use solid state battery voltage measurement devices and shunt controllers are 100% solid state. Sources: http://www.solarexpert.com/PVchrginfo.html
  25. Wiring is also important. You want to select the correct size and type of wire to really make your PV system work properly. If your wiring is too small, you are going to lose a lot of your electricity to resistance losses. The size of the wire must be large enough to carry the maximum current expected without undue voltage losses. All wire has a certain amount of resistance to the flow of current. This resistance causes a drop in the voltage from the source to the load. Voltage drops cause inefficiencies, especially in low voltage systems. You can go to this website for sizing charts for wires based on the size of your PV array. The voltage (V) drop is given by the resistance (R), measured in Ohms in the wire times the current (I) flowing through the wire. V=IR is called Ohm’s Law – one of the most useful rules in electronics. Sources: http://www.solarexpert.com/Photowiring.html
  26. For AC grid-tied systems you do not need a battery or charge controller if you do not need back up power, just the inverter. The Inverter changes the DC current stored in the batteries or directly from the PV into usable AC current which is the most common type used by most household appliances and lighting. To size increase the Watts expected to be used by your AC loads running simultaneously by 20%. You most likely will not have all of your appliances running continuously at the same time but this will account for surges in the system. Sources: http://www.solarwarrior.com/gallery.htmlhttp://www.solarexpert.com/PVinverter.html
  27. India is endowed with vast solar energy potential.