Submitted by samskiter t3_zsiyxn in askscience
So from my memory of thermodynamics, an ideal heat pump is the carnot cycle. This cycle uses an ideal gas on both the hot and cold sides of the pump. However in the real world we use the refridgeration cycle with an evaporator and a compressor.
I understand that the Carnot cycle is 'ideal' and therefore we can't get to Carnot efficiencies in real life.
But what real life factor means we can't try and use a gas both sides (with a turbine to replace the evaporator? Is it energy density? Cost? Complexity? Do space/military grade heat pumps with high performance requirements do something different?
Thanks!
Edit: just a quick edit to say thanks so much for all the responses so far, it's exactly the sort of detailed science and real world experience I wanted to understand and get a feeling for. I will try and respond to everyone shortly!
Edit2: bonus question and I think some commenters have already hinted at this: flip the question, what would it take / what would it look like to have an all-gas cycle and if money were no object could it outperform a phase change cycle? I'm assuming extremely high pressure nitrogen as the working fluid to achieve a good energy density... Enormous heat exchangers. Could it get closer to Carnot COPs?
[deleted] t1_j18a3mw wrote
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