Knowee
Questions
Features
Study Tools

Which of the following factor (can be more than one factor) contribute to deviation of actual gas-turbine cycle from Brayton cycle? Question 7Select one or more:a.pressure drop in hat exchangerb.heat loss in turbinec.heat loss in compressord.friction in pipings

Question

Which of the following factor (can be more than one factor) contribute to deviation of actual gas-turbine cycle from Brayton cycle? Question 7Select one or more:a.pressure drop in hat exchangerb.heat loss in turbinec.heat loss in compressord.friction in pipings

🧐 Not the exact question you are looking for?Go ask a question

Solution

The factors that contribute to the deviation of the actual gas-turbine cycle from the Brayton cycle include:

a. Pressure drop in heat exchanger: In reality, the pressure drop in the heat exchanger is unavoidable due to the resistance to the flow of the working fluid. This pressure drop reduces the net work output and efficiency of the cycle, causing a deviation from the ideal Brayton cycle.

b. Heat loss in turbine: In an actual gas turbine, not all the heat supplied in the combustion chamber is converted into work. Some of it is lost to the surroundings due to the finite temperature difference, causing a deviation from the ideal cycle.

c. Heat loss in compressor: Similar to the turbine, heat loss also occurs in the compressor. The work input required by the compressor is more than what is predicted by the ideal Brayton cycle due to these losses.

d. Friction in pipings: Friction in the pipings causes a pressure drop, which reduces the net work output and efficiency of the cycle. This is another factor causing a deviation from the ideal Brayton cycle.

So, all of the factors listed (a, b, c, and d) contribute to the deviation of the actual gas-turbine cycle from the Brayton cycle.

This problem has been solved

Similar Questions

A Brayton Gas turbine cycle produces 14 MW with an inlet state of the compressor is T10C, P1 kPa, and a compression ratio of rP. The heat added in the combustion is 960 kJ/kg. Determine the mass flow rate of air in kg/s.Where,T1=190CP1= 115 kParP=15:1Specific heat at a constant pressure of air, CP= 1.004 kJ/kg kPolytropic Index, n for compressor, turbine and combustion chamber=1.4

In an ideal Brayton cycle, air is compressed from 84 kPa and 25C to 840 kPa. Under cold air standard conditions, the thermal efficiency of this cycle isQuestion 3Select one:a.48%b.52%c.10%d.60%e.74%

Consider a gas turbine that has a pressure ratio of 8 and operates on the Brayton cycle with regeneration between the temperature limits of 20 deg C and 900 deg C. If the specific heat ratio of the working fluid is 1.33, the highest thermal efficiency this gas turbine can have isQuestion 4Select one:a.42%b.49%c.58%d.63%e.69%

Consider an ideal Brayton cycle executed between the pressure limits of 1100 kPa and 100 kPa and temperature limits of 20 deg C and 1200 deg C with argon (k = 1.667, cp = 0.5203 kJ/kg.K) as the working fluid. The net work output of the cycle isQuestion 10Select one:a.136 kJ/kgb.96 kJ/kgc.227 kJ/kgd.439 kJ/kge.456 kJ/kg

In a regenerative Brayton cycle the maximum heat input that can be saved corresponds to the difference in enthalpy between the exhaust of the turbine and the inlet of the compressorQuestion 6Select one:a.TRUEb.FALSE

1/2

Upgrade your grade with Knowee

Get personalized homework help. Review tough concepts in more detail, or go deeper into your topic by exploring other relevant questions.