Workshop Manuals Factory service & repair Rover
01 Introduction02 General information03 Information04 Maintenance05 Engine - K1606 Engine - K16 with VVC07 Emission control08 Engine management system - MEMS09 Fuel delivery system10 Cooling system11 Manifold & exhaust systems12 Clutch13 Manual gearbox - R6514 Manual gearbox - PG115 Automatic gearbox - CVT16 Steering17 Front suspension18 Brakes19 Restraint systems20 Body21 Heating & ventilation22 Air conditioning23 Wipers & washers24 Electrical25 Instruments
Rover 200/400 Coupé, Cabriolet & Tourer Workshop Manual Supplement22 · Air conditioning
22 · Heating & A/C

Air conditioning system operation

Make
Rover
Model
Coupé, Cabriolet & Tourer 200/400 Coupé, Cabriolet & Tourer Workshop Manual Supplement
Section
Description and operation › Air conditioning system operation
Air conditioningAir conditioning system operation

AIR CONDITIONING SYSTEM OPERATION

The air conditioning system provides the means of supplying cooled and dehumidified, fresh or recirculated air to the interior of the ehicle. The cooling effect is obtained by blowing air through the matrix of an evaporator unit and when required, mixing that air with heated air by means of the heater distribution and blend unit, to provide the conditions required inside the vehicle. The volume of the conditioned air being supplied is controlled by a variable speed blower.

Sealed refrigerant

A sealed system, charged with Refrigerant R134a, together with a blower unit, blend unit and control system combine to achieve the cooled air condition.

The sealed system comprises of the following main components:

  1. Compressor
  2. Condenser
  3. Receiver/dryer
  4. Thermostatic expansion valve
  5. Evaporator

Refrigeration cycle

The compressor is driven by a belt from the crankshaft pulley. The compressor pressurises and circulates the refrigerant through the system. Mounted on the compressor, an electro-mechanical clutch maintains the correct temperature and pressure of the refrigerant by engaging or disengaging the compressor to support the systems requirements. Operation of the clutch is controlled by the engine control module (ECM), the trinary (triple) pressure switch and a thermostatic switch located on the exterior fins of the evaporator.

If the temperature at the evaporator falls low enough for ice to form on the fins, the thermostatic switch will open, breaking the circuit to the clutch and releasing the drive on the compressor. The ECM detects that the air conditioning system is not operating and switches off the condenser cooling fan. When the temperature at the evaporator rises sufficiently for the thermostatic switch to close, the air conditioning system will be restarted.

If the system pressure becomes excessive or drops sufficiently to cause damage to the compressor, a trinary pressure switch located in the high pressure line at the receiver dryer will break the electrical circuit to the compressor clutch, releasing drive from the compressor.

The two cooling fans are controlled by the ECM and dependent upon engine coolant temperature and air conditioning system pressure. With the air conditioning system switched off, only the inboard (radiator) cooling fan is operational with the ECM controlling the fan speed according to engine temperature. With the air conditioning system switched on, both the inboard and condenser cooling fans are connected in series by the ECM and operate at low speed. As the pressure of the air conditioning refrigerant rises above the threshold of the medium pressure setting on the trinary pressure switch, the cooling fans are connected in parallel and operate at high speed.

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