Net work output and heat supplied
Net work output and work done by turbine
Actual heat drop and isentropic heat drop
Net work output and isentropic heat drop
B. Net work output and work done by turbine
Reduced volume flow rate
Increased volume flow rate
Lower suction pressure
Lower delivery pressure
Provides greater flexibility
Provides lesser flexibility
In never used
Is used when gas is to be burnt
Radial flow compressors
Axial flow compressors
Pumps
All of these
Throttle control
Clearance control
Blow off control
Any one of the above
Less power requirement
Better mechanical balance
Less loss of air due to leakage past the cylinder
Lower volumetric efficiency
Compressor efficiency
Volumetric efficiency
Isothermal efficiency
Mechanical efficiency
The ratio of stroke volume to clearance volume
The ratio of the air actually delivered to the amount of piston displacement
Reciprocal of compression ratio
Index of compressor performance
Larger air handling ability per unit frontal area
Higher pressure ratio per stage
Aerofoil blades are used
Higher average velocities
In the diffuser only
In the impeller only
In the diffuser and impeller
In the inlet guide vanes only
0.2
0.3
0.4
0.5
75 %
85 %
90 %
99 %
Requires less space for installation
Has compressor and combustion chamber
Has less efficiency
All of these
In a two stage reciprocating air compressor with complete intercooling, maximum work is saved.
The minimum work required for a two stage reciprocating air compressor is double the work required for each stage.
The ratio of the volume of free air delivery per stroke to the swept volume of the piston is called volumetric efficiency.
None of the above
Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions
Volume of air delivered by the compressor
Volume of air sucked by the compressor during its suction stroke
None of the above
Decreases
Increases
Does not change
None of these
0.1 to 1.2 m³/s
0.15 to 5 m³/s
Above 5 m³/s
None of these
1 : 1
2 : 1
4 : 1
1 : 6
High nickel alloy
Stainless steel
Carbon steel
High alloy steel
Gas turbine uses low air-fuel ratio to economise on fuel
Gas turbine uses high air-fuel ratio to reduce outgoing temperature
Gas turbine uses low air-fuel ratio to develop the high thrust required
All of the above
It has high propulsive efficiency at high speeds
It can fly at supersonic speeds
It can fly at high elevations
It has high power for take off
To increase the output
To increase the efficiency
To save fuel
To reduce the exit temperature
Increases with increase in compression ratio
Decreases with increase in compression ratio
In not dependent upon compression ratio
May increase/decrease depending on compressor capacity
Centrifugal
Reciprocating
Axial
Screw
Increase
Decrease
Remain same
May increase or decrease depending on clearance volume
To cool the air during compression
To cool the air at delivery
To enable compression in two stages
To minimise the work of compression
Parallel
Perpendicular
Inclined
None of these
Does not change
Increases
Decreases
First decrease and then increase
Electric motor
Engine
Either (A) or (B)
None of these
Centrifugal pump
Reciprocating pump
Turbine
Sliding vane compressor
0.1 bar and 20°C
1 bar and 20°C
0.1 bar and 40°C
1 bar and 40°C