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Why is the pressure ratio higher in a centrifugal compressor than an axial compressor?

There is a substantial increase in radius across the rotating blade rows of a centrifugal compressor, which is its primary distinguishing feature from the axial-flow compressors to get higher-pressure ratio. Who says the compression ratio on a centrifugal is higher than that of a screw compressor? Unless I`m not properly understanding the question, these facts are true: a screw (axial) compressor is a positive displacement machine, meaning everything that goes into it will come out. There are no losses for re-expansion etc. A centrifugal compressor`s impeller is designed with a given amount of `lift` which is basically the difference between suction and discharge pressures or compression ratio. Exceeding the designed lift capability results in a surge where the gas momentarily goes backwards through the impeller until the excess lift condition is corrected.


What is the compressor retio?

The compressor ratio, or compression ratio, is the ratio of the maximum to minimum cylinder volume in an engine or compressor during the intake and compression cycles. It indicates how much the air-fuel mixture is compressed before combustion or compression occurs. A higher compression ratio generally leads to greater efficiency and power output, but it can also increase the risk of engine knock or detonation. The specific ratio can vary widely depending on the design and purpose of the engine or compressor.


What is compression ratio in air compressor?

The compression ratio is simply the ratio of the absolute stage discharge pressure to the absolute stage suction pressure.


The clearance ratio for a single stage compressor?

The clearance ratio for a single stage compressor is the ratio of the volume clearance at the end of the suction stroke to the volume displaced by the piston during the compression stroke. It is important to minimize clearance ratio to improve compressor efficiency. A lower clearance ratio indicates less trapped volume and better performance of the compressor.


What is compression ratio in jet engine?

The compression ratio in a jet engine is the ratio of the pressure of the air exiting the engine's compressor to the pressure of the air entering the compressor. It is a critical factor in determining engine efficiency and performance, as a higher compression ratio typically leads to improved thrust and fuel efficiency. It is calculated by dividing the absolute exit pressure by the absolute inlet pressure. For modern turbojet and turbofan engines, compression ratios typically range from 10:1 to 40:1.


Which compressor is used for supercharging of ic engines?

Centrifugal compressor


Why flywheel is used in reciprocating compressor not in centrifugal compressor?

Flywheel prevents fluctuation in the speed of the motor as a result of load fluctuation. It stores the energy and dissipates it to the compressor for prolonged period. So the load fluctuation which is high during compression stage and low during other stages during a cycle in reciprocating compressor gets nullified. On the other hand, centrifugal compressor continiously compresses the gas and does not have load fluctuations, hence flywheel is not required.


What will happen if suction temperature of centrifugal compressor increased?

There will be little change or effect if the suction temperature of centrifugal compression increases. This is because the gases included incur minimal changes. The required temperature for proper functionality is 43 degrees Celsius.


Which compressor is mostly used for supercharging of ic engines?

Centrifugal compressor


Which compressor is mostly used for the supercharging of IC engines?

Centrifugal compressor


What is balance line in centrifugal compressor?

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What is the balance drum used for a centrifugal compressor?

In a centrifugal compressor, the energy is transferred using a set of impeller blades and balancing drums. These balancing drums can be on the inlet or outlet side of the compressor and help to space out the energy in the compressor.