13.5 Gas Refrigeration, Heat Pump Cycles & Cryogenics
Key Takeaways
- Vapour and gas refrigeration and heat pump cycles are named together in the Refrigeration and air-conditioning item of the CIL Mechanical Paper-II syllabus.
- The reversed Carnot cycle sets the maximum possible coefficient of performance, equal to the cold temperature divided by the temperature difference for a refrigerator.
- The COP of a heat pump always exceeds that of a refrigerator operating between the same temperatures by exactly one.
- The Bell-Coleman or reversed Brayton gas cycle has a much lower COP than vapour compression but is used in aircraft because the working fluid is free and the plant is light.
The Reversed Carnot Cycle: The Absolute Limit
Every refrigeration system is a heat engine run backwards: work is supplied to move heat from a cold reservoir at $T_L$ to a hot reservoir at $T_H$. The best possible performance is set by the reversed Carnot cycle.
Coefficient of performance is defined as the useful effect divided by the work input, and the definition of useful effect differs between the two applications:
Since $Q_H = Q_L + W$, the two are related by
This relation holds for any refrigeration system, not merely the Carnot one, and it is examined constantly. A heat pump is always "better" than a refrigerator by exactly one — not because it is a superior machine, but because the work input itself ends up as useful heat in the hot space.
Note also that COP is not an efficiency and routinely exceeds one. Quoting a COP as a percentage is a conceptual error.
Worked example
A refrigerator maintains $-10$ degrees Celsius while rejecting heat at 40 degrees Celsius. The maximum possible COP is
A heat pump between the same reservoirs would have $COP_{HP} = 6.26$. Note that temperatures must be absolute; using Celsius here would give a meaningless answer, which is the single commonest error in the topic.
The COP falls sharply as the temperature difference widens. Cooling to $-30$ degrees Celsius while rejecting at the same 40 gives $COP_R = 243/70 = 3.47$ — a third lower. This is why cold-storage design pays such attention to minimising the temperature lift.
Units of Refrigeration
One tonne of refrigeration is the rate of heat removal required to freeze one short ton of water at 0 degrees Celsius into ice at 0 degrees Celsius in 24 hours:
The Bell-Coleman (Reversed Brayton) Cycle
Where vapour compression uses a fluid that changes phase, the gas refrigeration cycle keeps the working fluid — normally air — in the gaseous phase throughout. It is the Brayton cycle run in reverse and comprises four processes:
| Process | Description |
|---|---|
| 1-2 | Isentropic compression in the compressor |
| 2-3 | Constant-pressure heat rejection in the cooler |
| 3-4 | Isentropic expansion in an expander |
| 4-1 | Constant-pressure heat absorption in the refrigerator |
The critical difference from vapour compression is that expansion occurs in an expander that recovers work, not through a throttle valve. Throttling a gas produces almost no cooling — as the Joule-Thomson analysis showed, an ideal gas does not cool on throttling at all — so an expansion machine is essential.
With $r_p$ the pressure ratio, the COP of the ideal cycle is
Equivalently, in terms of temperatures,
Comparison with vapour compression
| Feature | Vapour compression | Bell-Coleman gas cycle |
|---|---|---|
| Working fluid | Refrigerant, changes phase | Air, stays gaseous |
| Heat transfer | Latent heat; large per kg | Sensible heat only; small per kg |
| COP | Typically 3 to 5 | Typically 0.7 to 1.5 |
| Equipment mass per TR | Higher | Much lower |
| Expansion device | Throttle valve | Expander (work-recovering) |
The COP is poor because sensible heat capacity is far smaller than latent heat, so a large mass flow of air is needed for a given cooling duty. Yet the cycle survives in aircraft, where the working fluid is available free from the engine compressor, no refrigerant charge or leakage is possible, and the weight per tonne of refrigeration is far lower than any vapour-compression plant.
Aircraft Refrigeration Systems
Aircraft cabins need cooling even at altitude because ram air compression, avionics and solar gain generate substantial heat, while bleed air from the engine compressor arrives very hot. Standard configurations, in increasing sophistication:
| System | Description |
|---|---|
| Simple | Ram air compressed, cooled in a heat exchanger, expanded in a cooling turbine |
| Bootstrap | Adds a second compressor driven by the cooling turbine, with a secondary heat exchanger |
| Regenerative | Part of the cooled turbine discharge is used to pre-cool the air entering the turbine |
| Reduced ambient | Uses a separate expansion turbine to lower the cooling-medium temperature |
The bootstrap arrangement is the most common on commercial aircraft, because using the turbine output to drive a second compressor rather than wasting it improves the overall pressure ratio available for expansion.
Heat Pumps
A heat pump is thermodynamically identical to a refrigerator; only the useful effect differs. Where the ambient is the source and a building is the sink, the pump delivers $Q_H$ units of heat for every $W$ units of work, with $COP_{HP} = Q_H/W$ typically 3 to 4 in temperate conditions.
The engineering significance is that direct electric heating delivers one unit of heat per unit of electricity, while a heat pump delivers three or four. Heat pumps are therefore the most effective route to decarbonised space heating wherever the temperature lift is modest.
Performance falls as source temperature drops, because the lift $T_H - T_L$ widens. Ground-source heat pumps exploit the near-constant ground temperature below a few metres to keep the lift small year-round, at the cost of borehole or trench installation.
A reversible heat pump switches the roles of the two heat exchangers with a four-way valve, giving cooling in summer and heating in winter from one machine — the basis of the reverse-cycle air conditioner.
Cryogenics and Gas Liquefaction
Cryogenics concerns temperatures below about 123 K. Producing them requires a different approach, because no single cycle spans from ambient to a few kelvin.
| Gas | Normal boiling point |
|---|---|
| Ammonia | 240 K |
| Carbon dioxide (sublimes) | 195 K |
| Methane | 112 K |
| Oxygen | 90 K |
| Nitrogen | 77 K |
| Hydrogen | 20 K |
| Helium | 4.2 K |
The Linde-Hampson process
Gas is compressed, cooled to ambient, passed through a counter-current heat exchanger, then throttled. The throttling produces cooling only if the gas is below its inversion temperature, as established in the thermodynamic-relations section. The cooled gas returns through the heat exchanger, pre-cooling the incoming stream, so the system cascades down to progressively lower temperatures until liquefaction begins.
Air and nitrogen work directly because they sit well below their inversion temperatures at ambient. Hydrogen must be pre-cooled with liquid nitrogen and helium with liquid hydrogen before throttling produces any cooling at all.
The Claude process
An improvement in which part of the stream is diverted through an expansion engine rather than a throttle. Because the expander extracts work, the temperature drop is much greater than in throttling alone, and the process is thermodynamically far more efficient. Most industrial air-separation plants use this principle.
Industrial relevance
Cryogenic air separation produces the oxygen and nitrogen used in steelmaking and in inerting; liquefied natural gas transport depends on cryogenic containment; and in coal operations, nitrogen is used for inertisation of sealed-off districts to suppress spontaneous heating and mine fires — a direct link between this topic and mine safety practice.
For a refrigerator and a heat pump operating between the same two temperature reservoirs, the relationship between their coefficients of performance is:
In the Bell-Coleman gas refrigeration cycle, expansion is carried out in an expander rather than a throttle valve because:
A refrigerator maintains a cold space at minus 10 degrees Celsius while rejecting heat at 40 degrees Celsius. Its maximum possible COP is approximately:
Compared with a vapour compression system, a gas refrigeration cycle has a much lower COP mainly because: