Reciprocating compressor
Centrifugal compressor
Axial flow compressor
Turbo compressor
B. Centrifugal compressor
In one cylinder
In two cylinders
In a single cylinder on both sides of the piston
In two cylinders on both sides of the piston
Isothermal
Polytropic
Isentropic
Any one of these
Compression index
Compression ratio
Compressor efficiency
Mean effective pressure
Isothermal compression
Isentropic compression
Polytropic compression
None of these
Remove impurities from air
Reduce volume of air
Cause moisture and oil vapour to drop out
Cool the air
Increase first at fast rate and then slow
Increase first at slow rate and then fast
Decrease continuously
First increase, reach maximum and then decrease
Ideal compression
Adiabatic compression
Isentropic compression
Isothermal compression
Same as isothermal
Same as adiabatic
Better than isothermal and adiabatic
In between isothermal and adiabatic
Turbojet engine
Ramjet engine
Propellers
Rockets
To accommodate Valves in the cylinder head
To provide cushioning effect
To attain high volumetric efficiency
To provide cushioning effect and also to avoid mechanical bang of piston with cylinder head
Reduced volume flow rate
Increased volume flow rate
Lower suction pressure
Lower delivery pressure
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
The propulsive matter is ejected from within the propelled body
The propulsive matter is caused to flow around the propelled body
Its functioning does not depend upon presence of air
None of the above
7 : 1
15 : 1
30 : 1
50 : 1.
Equal to
Less than
More than
None of these
A propeller system
Gas turbine engine equipped with a propulsive nozzle and diffuse
Chemical rocket engine
Ramjet engine
Mechanical efficiency
Volumetric efficiency
Isothermal efficiency
Adiabatic efficiency
0.1 %
0.5 %
1.0 %
5 %
Increases the thermal efficiency
Increases the compressor work
Increases the turbine work
Decreases the thermal efficiency
Compression ratio
Work ratio
Pressure ratio
None of these
1 : 1.2
1 : 2
1 : 5
1 : 10
Large gas turbines employ axial flow compressors
Axial flow compressors are more stable than centrifugal type compressors but not as efficient
Axial flow compressors have high capacity and efficiency
Axial flow compressors have instability region of operation
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
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
Mass
Energy
Flow
Linear momentum
0.2
0.3
0.4
0.5
Vi = Vo
Vt > Vo
U < Vo
V = Uo
Large quantity of air at high pressure
Small quantity of air at high pressure
Small quantity of air at low pressure
Large quantity of air at low pressure
They can generate very high thrust
They have high propulsion efficiency
These engines can work on several fuels
They are not air breathing engines
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