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Brayton cycle

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Brayton cycle Uses Auxiliary power generation Stand-alone power generation Naval propulsion Jet engine Gas Turbine Advantages High power:weight ratio Compact One ... – PowerPoint PPT presentation

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Title: Brayton cycle


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Brayton cycle
  • Uses
  • Auxiliary power generation
  • Stand-alone power generation
  • Naval propulsion
  • Jet engine

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Gas Turbine
  • Advantages
  • High powerweight ratio
  • Compact
  • One-direction motion vibration
  • Fewer moving parts
  • Better reliability
  • Variety of fuels
  • Low emissions
  • Disadvantages
  • Higher cost

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Brayton cycle
  • Working fluid air
  • Ideal gas
  • Specific heats steady or variable
  • High temperature reservoir
  • Open or closed model
  • Steady pressure heat exchange

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Cycle Analysis
  • Net work
  • Heat in
  • Thermal efficiency
  • Back work ratio

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Brayton cycle
  • 1?2 Isentropic compression
  • 2?3 steady pressure heat addition
  • 3?4 isentropic expansion
  • 4?1 steady pressure heat rejection

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Brayton cycle
  • Work in work out
  • Heat in heat out
  • Thermal efficiency
  • Pressure ratio
  • Back work ratio

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Brayton Cycle
  • Approaches
  • Variable specific heats Table h, pr
  • Steady specific heats ?h Cp ?T
  • P,v,T relationships T2 T1(P2/P1)(k-1)/k

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Compressor
  • Essential to compress large volumes of air for
    efficiency of cycle
  • Centrifugal
  • Axial more common rotor and stator blades

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Example
  • A simple Brayton cycle has a rp 12, a
    compressor inlet at 300K, and a turbine inlet at
    1000K. Determine the mass flow of air needed
    when the net power output is 70MW. Specific
    heats are constant.

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Example
  • An ideal air-standard Brayton cycle has air
    entering the compressor at 100kPa,300K, 5m3/s.
    The compressor ratio is 10 the turbine inlet is
    at 1400K.
  • Find power generated, bwr, and thermal efficiency.

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Brayton cycle
  • Irreversibilities isentropic efficiency
  • Gas turbine power plant operating at steady state
    receives air at 100kpa 300K. Air is compressed
    to 500kPa and reaches a maximum cycle temperature
    of 920K. The isentropic efficiencies of the
    compressor and turbine are both at 83.
  • Find the thermal efficiency and bwr of the cycle.

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Brayton cycle
  • Regenerator
  • Effectiveness

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Regeneration
  • Capital costs
  • Pressure losses

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Chapter 7 Exergy Analysis / F7-13To save, right click on the image and choose "Save As" from the pop-up menu.
              
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Brayton cycle
  • Ideal
  • ?th 45.6
  • With regenerator
  • ?th 57

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Brayton cycle
  • Ideal
  • ?th 45.6
  • With irreversibilities
  • ?th 24.9
  • With regenerator
  • ?th 56.8

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Assignment
  • Chapter 9 sections 9.5 through 9.10

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Brayton cycle
  • Isentropic compression power
  • Isothermal power
  • Intercooler

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Chapter 9 Gas Power Systems / F9-18To save, right click on the image and choose "Save As" from the pop-up menu.
              
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Brayton cycle
  • Reheat

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Chapter 9 Gas Power Systems / F9-16To save, right click on the image and choose "Save As" from the pop-up menu.
              
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