ENGR217 Summer 2019 Q A3[VALID]
Answer ALL parts (a) - (c)
Formulas you may need
- Isentropic ideal gas: (on the formula sheet)
- SFEE per unit mass for each component: , (on the formula sheet)
- Brayton: , work ratio (on the formula sheet)
- (on the formula sheet)
- Isentropic efficiencies: , (learn this)
- (a)[14]2:2A gas turbine operating on the air standard Brayton cycle has a pressure ratio of 9, a compressor inlet temperature of 300 K and a turbine inlet temperature of 1400 K. Calculate the compressor and turbine outlet temperatures, the heat added, the work ratio (i.e. ) and the thermal efficiency. (For the air standard cycle take and )
- (b)[8]In practice the high temperatures during heating and in the turbine give a significant change to the specific heats and also the turbine and compressor are not perfectly efficient. Making the following assumptions:-
- during heating and in the turbine
- during expansion the ratio of specific heats becomes
- isentropic turbine efficiency is 0.85
- isentropic compressor efficiency is 0.80
- heat input increases to maintain the turbine inlet temperature of 1400 K
- air standard cycle parameters still apply to compression
- (c)[3]ThirdHow might re-generation be used to enhance efficiency.