Experiment 7: Gas Turbine ( Brayton Cycle Experiment)
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Transcript of Experiment 7: Gas Turbine ( Brayton Cycle Experiment)
PROF. ALVARADO 1
Experiment 7:Gas Turbine
(Brayton Cycle Experiment)
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Brayton Cycle
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A thermodynamic cycle that describes the workings of the gas turbine engine 1-2 Isentropic compression 2-3 Isobaric heat addition3-4 Isentropic expansion 4-1 Isobaric heat rejection
Gas Turbine Engine
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Parts Name
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Engine Sensor Locations
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Software Control Panel
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a) By pressing ”Log data to file”, you’ll be able to save data to excel file. But in the excel file, Pressure and Temperature at 3 and 4 are inversed.
b) Pressure shown here are gage pressure
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Data Analysis
1. Plot the following diagrams:• Compressor Inlet(P1)/Outlet Pressure (P2) vs. Time• Compressor Inlet(T1)/Outlet Temperature(T2) vs. Time• Turbine Inlet(P4)/Outlet Pressure(P3) vs. Time• Turbine Inlet(T4)/Outlet Temperature(T3) vs. Time• RPM vs. Time
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Data Analysis
2. Find T1-T4 and P1-P4 under peak RPM.
3. For the analysis point chosen in #2, find the Specific Enthalpy at each Cycle Point(Using air tables): h1, h2, h4, h3.
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Data Analysis
4.Determine specific work and specific heat transfer:
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Data Analysis5.Determine the efficiency
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(1-k)k
2
1
_ :
(%) 100
_ _ :
η=1-r (k 1.4, air)
r
cycle netT
in
p
Hp
L
Thermo efficiencywq
Brayton Cycle Efficiency
P PP P
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Data Analysis6. Determine the power of the system
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_3 _ 3abs ATM gageP P P
_ 3
3
absPRT
_32 gagePV
m AV
_cycle netW m w
20.00311A m
Gas Turbine Engine Video
ENTC-370 PROF. ALVARADO 12
• http://www.youtube.com/v/kw6nIo5LKqE?autoplay=1&rel=0