Measuring the total pressure of a centrifugal compressor

AI Thread Summary
The discussion focuses on redesigning a small centrifugal compressor to achieve a target pressure of 2 bar, up from the initial 1.01 bar. The user plans to increase motor speed with a gearbox and scale the model without altering the blade profile, while also measuring total pressure using an absolute pressure manometer. Suggestions include measuring the entire fan curve with an adjustable restriction and considering a diffuser to simplify static pressure measurement. Additionally, the importance of accounting for significant temperature increases at a compression ratio of 2.0 is highlighted. Accurate measurement and calculation methods are essential for validating performance improvements.
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Measuring the total pressure of centrifugal compressor by measuring the static temperature and the blade velocity
Hello everyone,

Nowadays I am planning to redesign my centrifugal compressor which I designed for a subsystem in my graduation project. It's a 3D printed and brushless motor driven centrifugal compressor and its about a hand size. However, due to its relatively small size and relatively low RPM ( about 15,000 RPM) it didn't provide enough pressure. In fact, I knew that it won't work because I designed it to reach 1.01 bar :) because I was limited by the material, motor and the budget. I just wanted to give it a try.
IMG_4528.jpg
IMG_4527.jpg
IMG_4523.jpg

Anyway, now I want to scale it in order to reach about a 2 bar. Without doing any changes on the blade profile or casing (maybe I do because there may be choking) I will increase the motor speed with a gearbox and also scale up the model to increase the tangential velocity of the blade tip.

This time, I want to measure the values in order to validate my calculations. Therefore, I need to know total pressure of the blowed air. I am going to buy an absolute pressure manometer for gases and place it to the end of the compressor. This will measure the static pressure of the air.

I will approximate the air velocity from the tangential velocity of the blade (because I will be able to measure motor speed with a tachometer).

But since the density in the dynamic pressure is coupled with the pressure and temperature. I am planning to calculate density from ideal gas law. Assuming the temperature increase is not significant, taking the room temperature and static pressure measured in the compressor the density and eventually total pressure can be calculated.

Calc.png


So my question is that is this process correct? Would I get reasonable values? Here, the total pressure will be a function of the static pressure measured and temperature (approximated).

Thank you in advance,
 
Engineering news on Phys.org
Measuring the output of a centrifugal compressor requires a little more sophistication. First, you need to measure the entire fan curve, not just one point. That requires an adjustable restriction on the downstream side. Good search terms to learn more are fan curve and measure fan curve. An example of a set of fan curves for a large industrial blower at various speeds:
Fan curve.jpg

I suggest adding a diffuser to the output so that you need only measure the static pressure. If you really want to measure both static and dynamic pressure, you need a pitot tube (search the term). A simplified sketch of a pitot tube is shown below:
Pitot tube.jpg

A diffuser is a tapered increase in duct diameter for the purpose of slowing down subsonic flow, thus increasing the pressure. An example is shown below:
Diffuser.jpg


If your compression ratio is 2.0, (1 bar to 2 bar), then the temperature increase will be significant.
 
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