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15.1 PRINCIPLE




   http://part66.blogspot.com/
ENERGY
• Energy : Capacity to do work (Joule)
• Potential Energy : Result from influence of
                     gravity on mass due to its
                     position
     PE = mass x gravity x height
• Kinetic Energy : Result from motion of mass
     KE = 1/2mv2
NEWTON LAW
• 1ST Law :
      A body will continue its state of rest or uniform motion
  unless external force changing it.

2nd Law :
       Rate of change of momentom of a body is proportional to
  the applied force.

3rd Law :
      In every action there will be equal and opposite reaction
BRAYTON CYCLE
• Brayton cycle :
  – The process of converting heat to do the work in
    jet engine.
  – Air is compress,heat and accelerate due to air
    molecule expand to produce the reaction force
RELATION
• Application to Jet engine :
    u = 0m/s
    mair= 260kg/s                               v=500m/s




        Acc = (V–U) ÷ t           Work = F x D
        Acc =(500 – 0) ÷ 1s       Work = Energy
        Acc = 500 m/s2            KE = ½(mv2)
                                  KE = ½(260)(500)2
                                  KE = 32.5MJ
        F = ma
        F =260 x 500              Power = Work/Time
        Thrust = 130kN            Pow = 32.5/1s
                                  Pow = 32.5Mwatt
TURBO JET
TURBOFAN
TURBOSHAFT
TURBOPROP

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EASA Part 66 Module 15.1 : Fundamental

  • 1. 15.1 PRINCIPLE http://part66.blogspot.com/
  • 2. ENERGY • Energy : Capacity to do work (Joule) • Potential Energy : Result from influence of gravity on mass due to its position PE = mass x gravity x height • Kinetic Energy : Result from motion of mass KE = 1/2mv2
  • 3. NEWTON LAW • 1ST Law : A body will continue its state of rest or uniform motion unless external force changing it. 2nd Law : Rate of change of momentom of a body is proportional to the applied force. 3rd Law : In every action there will be equal and opposite reaction
  • 4. BRAYTON CYCLE • Brayton cycle : – The process of converting heat to do the work in jet engine. – Air is compress,heat and accelerate due to air molecule expand to produce the reaction force
  • 5. RELATION • Application to Jet engine : u = 0m/s mair= 260kg/s v=500m/s Acc = (V–U) ÷ t Work = F x D Acc =(500 – 0) ÷ 1s Work = Energy Acc = 500 m/s2 KE = ½(mv2) KE = ½(260)(500)2 KE = 32.5MJ F = ma F =260 x 500 Power = Work/Time Thrust = 130kN Pow = 32.5/1s Pow = 32.5Mwatt