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Building Services Engineering 5th Edition Handbook

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Ventilation and air conditioning 153<br />

Absolute pressure (bar)<br />

9.6<br />

3.6<br />

Liquid<br />

region<br />

3<br />

4<br />

Critical point 120°C, 45 bar<br />

Expansion<br />

Liquid–vapour<br />

mixture region<br />

Condensation<br />

Evaporation<br />

Specific enthalpy (kJ/kg)<br />

2<br />

Compression<br />

1<br />

Superheated<br />

vapour region<br />

5.17 Pressure–enthalpy diagram for a refrigerant showing the vapour-compression cycle.<br />

The pressure rise produced through the compressor is dissipated in friction through the fine<br />

orifice in the valve. Such a sudden pressure drop is almost an adiabatic thermodynamic process.<br />

This is represented by the vertical line 3–4 on the pressure–enthalpy diagram. Some heat loss<br />

from the valve body takes place so that 3–4 will be slightly curved. Condition 4 is at the lower<br />

pressure of the evaporation process, where the refrigerant temperature has dropped to 5 ◦ C.<br />

Some of the refrigerant liquid has flashed into vapour.<br />

The liquid and flash vapour mixture flows through the evaporator, where it is completely<br />

boiled into vapour and is then given a small degree of superheat (path 4–1). It then enters the<br />

compressor as dry low-pressure superheated vapour at 20 ◦ C. A suction temperature-sensing phial<br />

controls the refrigerant flow rate by means of a liquid-filled bellows on the thermostatic expansion<br />

valve. This matches refrigerant flow to the refrigerating effect required by the air-conditioning<br />

system and ensures that liquid droplets are not carried into the compressor, where they could<br />

cause damage.<br />

Large plant has refrigerant pressure controllers, which reduce compressor performance by<br />

unloading some cylinders. Lubricating oil contaminates the refrigerant leaving the compressor.<br />

This is separated gravitationally and returned to the crankcase.<br />

The pressure–enthalpy diagram depicts the reverse Carnot cycle. In the other direction, the<br />

cycle is for an internal combustion engine. The theoretical ideal coefficient of performance is<br />

given by,<br />

Ideal COP = T 1<br />

T 2 − T 1<br />

where T 1 is the evaporation absolute temperature (K) and T 2 is the condensation absolute<br />

temperature (K). With the temperatures previously used,<br />

Ideal COP =<br />

273 + 5<br />

(273 + 40) − (273 + 5)<br />

= 7.94<br />

Friction losses from fluid turbulence, heat transfers to the surroundings, and mechanical and<br />

electrical losses in the compressor all reduce this value to 2–4 in commercial equipment. The<br />

electricity consumption of fans and pumps adds to the running costs.

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