# Why is there a compressor in an air cycle machine?

I'm a curious high school student. Why is there a compressor after the first heat exchanger in an air cycle machine? I've read that compressing the cold air is for the cause of efficiency because compressing hot air uses much more work than cold air, and the effect of this is that the compressed air temperature increases. But if so, why compress at all when the air itself is going to be cooled again in the second heat exchanger? Why not leave the compressor and place the turbine as it is from the ACM?

## 3 Answers

If I understand your question correctly, you don't really understand how the ACM works.

The idea of an ACM is to create 'cool' air. Especially on the ground (imagine landing on your tropical holiday destination), this means that the air must sometimes be made cooler than the outside (ambient) temperature. The second law of thermodynamics (and in this case, the law of common sense) states that you can't just cool your air against the warm ambient air, so you will need to do some special tricks.

In this case, the special trick is compression. You compress the air, which will make it quite hot (increase the temperature) (search for adiabatic compression on the internet). Then, this hot air can of course easily be cooled against ambient air, which happens in the second heat exchanger. In fact, the hotter the air after compression is, the more heat is exchanged in the second heat exchanger. This means the heat exchanger can be made smaller, which is especially useful since air-to-air heat exchangers are inefficient and thus relatively big.

Now, you expand your air again, which will cool it (decrease the temperature). However, since you already cooled it down in the second heat exchanger, it will now be cooler than when it originally encountered the compressor! This makes sense, since you removed energy from the air in the second heat exchanger. So, this way, you can cool the air down further than would have been possible by a heat exchanger (search for reverse Brayton cycle on the internet).

So, this system has two advantages:

1. It is possible to cool down air beyond ambient temperature, so it functions as 'airco' on the ground or at low altitude.
2. It is possible to cool hot compressed bleed air with a relatively small, light heat exchanger for pressurizing your cabin while not cooking your passengers medium-rare.
• Very nice answer Jun 18, 2020 at 5:57

Because there is an expansion stage, the energy of the compressed air can be used to run a second compressor. Doing this allows to cool the precompressed air before it is fed to the second compressor, thus improving overall efficiency.

For the same reason, some turbocharged engines use two turbocharging stages with an intercooler between the compressor stages. It keeps the volume of air low and allows for smaller, more efficient turbochargers.

You could also extract the air at a later stage of the engine compressor, cool it and expand it in a diffusor, but then the engine compressor has to do more work and the cooler needs to be bigger due to the higher temperature and lower density of the compressed air. But somehow you still need to shed the pressure energy in the air, and running it through a turbine is an ideal way to achieve this.

The ACM has a nozzle in the turbine which compression and rapid expansion of air through the conical holes of the nozzle, and inducer and exducer blades of the turbine wheel pulling and pushing air at high RPM's produces the cold air. Primary cools down bleed air from engine for perameter required, then temperature leaving compressor discharge into secondary heat exchanger cooling down air sufficiently for turbine inlet air temperature requirements and turbine discharge temperature. Example, testing HONEYWELL ACM for 757, and 767, from primary to compressor inlet is 197 to 207 deg. F. comp discharge temp is about 285 deg. entering secondary then exiting at 205 deg. F entering turbine inlet and outlet discharging at 25 deg. fer. or less. from turbine scroll. Also, the RPM is 46K to 51K. Some smaller ATR ACM's go over 100k.