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4

The work ratio of a gas turbine plant is defined as the ratio of

A. Net work output and heat supplied

B. Net work output and work done by turbine

C. Actual heat drop and isentropic heat drop

D. Net work output and isentropic heat drop

Correct Answer :

B. Net work output and work done by turbine


Related Questions

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4

A large clearance volume in a reciprocating compressor results in

A. Reduced volume flow rate

B. Increased volume flow rate

C. Lower suction pressure

D. Lower delivery pressure

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4

The closed cycle in gas turbines

A. Provides greater flexibility

B. Provides lesser flexibility

C. In never used

D. Is used when gas is to be burnt

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4

Euler's equation can be used for

A. Radial flow compressors

B. Axial flow compressors

C. Pumps

D. All of these

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4

An air compressor may be controlled by

A. Throttle control

B. Clearance control

C. Blow off control

D. Any one of the above

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4

Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

A. Less power requirement

B. Better mechanical balance

C. Less loss of air due to leakage past the cylinder

D. Lower volumetric efficiency

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4

The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

A. Compressor efficiency

B. Volumetric efficiency

C. Isothermal efficiency

D. Mechanical efficiency

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4

Volumetric efficiency is

A. The ratio of stroke volume to clearance volume

B. The ratio of the air actually delivered to the amount of piston displacement

C. Reciprocal of compression ratio

D. Index of compressor performance

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4

Axial flow compressor has the following advantage over centrifugal compressor

A. Larger air handling ability per unit frontal area

B. Higher pressure ratio per stage

C. Aerofoil blades are used

D. Higher average velocities

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4

The stagnation pressure rise in a centrifugal compressor takes place

A. In the diffuser only

B. In the impeller only

C. In the diffuser and impeller

D. In the inlet guide vanes only

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4

The degree of reaction is usually kept ________ for all types of axial flow compressors.

A. 0.2

B. 0.3

C. 0.4

D. 0.5

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4

The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

A. 75 %

B. 85 %

C. 90 %

D. 99 %

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4

Gas turbine as compared to steam turbine

A. Requires less space for installation

B. Has compressor and combustion chamber

C. Has less efficiency

D. All of these

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4

Which of the following statement is wrong?

A. In a two stage reciprocating air compressor with complete intercooling, maximum work is saved.

B. The minimum work required for a two stage reciprocating air compressor is double the work required for each stage.

C. The ratio of the volume of free air delivery per stroke to the swept volume of the piston is called volumetric efficiency.

D. None of the above

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4

The compressor capacity is defined as the

A. Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions

B. Volume of air delivered by the compressor

C. Volume of air sucked by the compressor during its suction stroke

D. None of the above

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4

The efficiency of roots blower ________ with the increase in pressure ratio.

A. Decreases

B. Increases

C. Does not change

D. None of these

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4

The volume of air delivered in a medium capacity air compressor per unit time is

A. 0.1 to 1.2 m³/s

B. 0.15 to 5 m³/s

C. Above 5 m³/s

D. None of these

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4

The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

A. 1 : 1

B. 2 : 1

C. 4 : 1

D. 1 : 6

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4

The blades of gas turbine are made of

A. High nickel alloy

B. Stainless steel

C. Carbon steel

D. High alloy steel

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4

Pick up the correct statement

A. Gas turbine uses low air-fuel ratio to economise on fuel

B. Gas turbine uses high air-fuel ratio to reduce outgoing temperature

C. Gas turbine uses low air-fuel ratio to develop the high thrust required

D. All of the above

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4

A turboprop is preferred to turbojet because

A. It has high propulsive efficiency at high speeds

B. It can fly at supersonic speeds

C. It can fly at high elevations

D. It has high power for take off

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4

High air-fuel ratio is used in gas turbines

A. To increase the output

B. To increase the efficiency

C. To save fuel

D. To reduce the exit temperature

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4

Volumetric efficiency of a compressor with clearance volume

A. Increases with increase in compression ratio

B. Decreases with increase in compression ratio

C. In not dependent upon compression ratio

D. May increase/decrease depending on compressor capacity

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4

For supplying intermittent small quantity of air at high pressure, following compressor is best suited

A. Centrifugal

B. Reciprocating

C. Axial

D. Screw

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4

The volumetric efficiency of compressor with increase in compression ratio will

A. Increase

B. Decrease

C. Remain same

D. May increase or decrease depending on clearance volume

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4

Inter-cooling in multistage compressors is done

A. To cool the air during compression

B. To cool the air at delivery

C. To enable compression in two stages

D. To minimise the work of compression

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4

In a centrifugal compressor, the flow of air is ________ to the axis of compressor.

A. Parallel

B. Perpendicular

C. Inclined

D. None of these

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4

With the decrease in compression ratio, the volumetric efficiency

A. Does not change

B. Increases

C. Decreases

D. First decrease and then increase

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4

A rotary compressor is driven by an

A. Electric motor

B. Engine

C. Either (A) or (B)

D. None of these

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4

Axial flow compressor resembles

A. Centrifugal pump

B. Reciprocating pump

C. Turbine

D. Sliding vane compressor

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4

Standard air is the air at ________ and relative humidity of 36 percent.

A. 0.1 bar and 20°C

B. 1 bar and 20°C

C. 0.1 bar and 40°C

D. 1 bar and 40°C