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Test: Gas Turbine - 1 - Mechanical Engineering MCQ


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20 Questions MCQ Test - Test: Gas Turbine - 1

Test: Gas Turbine - 1 for Mechanical Engineering 2024 is part of Mechanical Engineering preparation. The Test: Gas Turbine - 1 questions and answers have been prepared according to the Mechanical Engineering exam syllabus.The Test: Gas Turbine - 1 MCQs are made for Mechanical Engineering 2024 Exam. Find important definitions, questions, notes, meanings, examples, exercises, MCQs and online tests for Test: Gas Turbine - 1 below.
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Test: Gas Turbine - 1 - Question 1

The compression ratio of a gas power plant cycle corresponding to maximum work output for the given temperature limits of Tmin and Tmax will be     

Test: Gas Turbine - 1 - Question 2

Isentropic compression of saturated vapour of all superheated vapour.

Detailed Solution for Test: Gas Turbine - 1 - Question 2

 

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Test: Gas Turbine - 1 - Question 3

. A gas turbine cycle with heat exchanger and reheating improves 

Test: Gas Turbine - 1 - Question 4

Which one of the following is correct?  

Test: Gas Turbine - 1 - Question 5

Consider the following statements:

1. The speed of rotation of the moving elements of gas turbines is muchhigher than those of steam turbines

2. Gas turbine plants are heavier and larger in size than steam turbineplants

3. Gas turbines require 'cooling water for its operations

4. Almost any kind of fuel can be used with gas turbines

Which of the statements given above are correct? 

Test: Gas Turbine - 1 - Question 6

Assertion (A): The thermal efficiency of a gas turbine plant is low as compared tothat of reciprocating IC engines.

Reason (R): In a gas turbine plant, the maximum pressure and temperature arelow when compared to those of reciprocating IC engines. 

Test: Gas Turbine - 1 - Question 7

Consider the following statements pertaining to gas turbines:

1. The degree of reaction of a reaction turbine is the ratio of energytransfer in fixed blade to the overall energy transfer across a stage.

2. The overall pressure drop in a turbine is the product of pressure dropper stage and number of stages.

3. Gas turbine cycle (Brayton cycle) is not as efficient as Rankine cycle forsteam.

Which of the above statements is/are correct? 

Test: Gas Turbine - 1 - Question 8

Assertion (A): The thermal efficiency of gas turbine plants is higher compared todiesel plants.

Reason (R): The mechanical efficiency of gas turbines is higher compared to dieselengines. 

Detailed Solution for Test: Gas Turbine - 1 - Question 8

A is false and R is true

Test: Gas Turbine - 1 - Question 9

Assertion (A): Gas turbines use very high air fuel ratio.                                                                  

Reason (R): The allowable maximum temperature at the turbine inlet is limited by available material considerations. 

Detailed Solution for Test: Gas Turbine - 1 - Question 9

Though A and R are true, but R is not correct reason for A.

Test: Gas Turbine - 1 - Question 10

Consider the following statements comparing I.C. engines and gasturbines:

1.     Gas turbines are simple, compact and light in weight.                                   

2.     Complete expansion of working substance is possible in I.C. engines and not in gas turbines.

3.     There is flexibility in the design of different components of gas turbines as different processes take place in different components.

4.     Even low grade fuels can be burnt in gas turbines.Of these statements 

Detailed Solution for Test: Gas Turbine - 1 - Question 10

Low grade fuel can't be burnt in gas turbine since it leads to poor life of turbine blades, etc.

Test: Gas Turbine - 1 - Question 11

The power coefficient (cp)variation of a wind mill with the speed ratio is correctly shown by

 

Test: Gas Turbine - 1 - Question 12

A Bell-Coleman air refrigeration cycle works as a reversed:      

Test: Gas Turbine - 1 - Question 13

Assertion (A): The thermal efficiency of Brayton cycle with regeneration decreases as the compressor ratio increases.                                                                                                                                              

Reason (R): As the   compression   ratio    of   compressor  increases, the   range    oftemperature in the regenerator decreases and the amount of heat recovered reduces. 

Detailed Solution for Test: Gas Turbine - 1 - Question 13

Test: Gas Turbine - 1 - Question 14

A gas turbine works on which one of the following cycles?     

Test: Gas Turbine - 1 - Question 15

Which one of the thermodynamic cycles shown in the following figures represents that of Brayton cycle? 

Test: Gas Turbine - 1 - Question 16

For a Brayton cycle, match the following using codes given below: 

Test: Gas Turbine - 1 - Question 17

Use of maximum pressure ratio, corresponding to maximum to minimum cycle temperature ratio in case of Joule cycle gives which one of the following?    

Test: Gas Turbine - 1 - Question 18

Consider the T-s diagram shown in thefollowing figure:Actual compression process in gasturbines is indicated by the process.

Detailed Solution for Test: Gas Turbine - 1 - Question 18

Curve 1-3 is actual compression process in gas turbine.

Test: Gas Turbine - 1 - Question 19

The given figure shows four plots A, B, C and D of thermal efficiency against pressure ratio:

The curve which represents that of a gas turbine plant using Brayton cycle (without regeneration) is the one labelled 

Test: Gas Turbine - 1 - Question 20

Consider the following statements in respect of gas turbines:

1. Supersonic flow leads to decrease in efficiency.

2. Supersonic flow leads to decrease in flow rate.Which of the statements given above is/are correct? 

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