Workshop Manuals Factory service & repair Rover
01 General information02 Information03 Maintenance04 Engine 1.4 K805 Engine 1.606 Engine 1.6 D.O.H.C.07 Engine 2.0 T1608 Engine management system - PGM-Fi09 Modular engine management system - SPi10 Modular engine management system - MPi11 Fuel delivery system12 Cooling system13 Manifold and exhaust14 Clutch15 Manual gearbox 1.416 Manual gearbox 1.617 Automatic gearbox18 Drive shafts19 Steering20 Suspension21 Brakes22 Body23 Heating and ventilation24 Air conditioning25 Wipers and washers26 Electrical27 Instruments28 Supplementary restraint system (SRS)
Rover 200/400 Coupé, Cabriolet & Tourer Workshop Manual09 · Modular engine management system - SPi
09 · Engine

Modular engine management system - SPi (Fuel system): Description and operation

Make
Rover
Model
Coupé, Cabriolet & Tourer 200/400 Coupé, Cabriolet & Tourer Workshop Manual
Section
Description and operation › Fuel system
Modular engine management system - SPiFuel system

Distributor cap and rotor arm.

Exploded view of the distributor cap (9), rotor arm (23), retaining screw (24), and anti-flash shield (25).
The distributor cap (9), carrying a central carbon brush and four h.t. lead pick – ups, is located at the rear of the inlet camshaft and surrounds the rotor arm (23). The rotor arm is secured by a retaining screw (24) to a 'D' shaped stub shaft, which is press fitted into a vibration absorbing bush at the rear of the inlet camshaft, and is protected from contamination by an anti – flash shield (25) which incorporates an oil drain.

Fuel system

The M.E.M.S. Single Point injection system uses one injector (10) mounted in a throttle body, the solenoid operated injector directing its spray onto the back of the throttle disc. The amount of fuel delivered is determined by the length of time the injector is held open, this being governed by the E.C.U. in line with the inputs it receives. The fuel delivery system is of the pressure recirculation type, pressure being created by an electric pump (11) located inside the fuel tank and operated via the fuel pump relay (12), from which fuel is delivered via an under body line, to the fuel filter (13) where any impurities are removed. From the filter, fuel is pressurised around the injector housing against the pressure regulator (14), any excess pressure lifting the regulator and returning to the fuel tank. The air intake system includes a resonator to reduce intake noise and a stepper motor to control idle and fast idle speeds. An inlet manifold P.T.C. heater (15) controlled by the E.C.U. via a relay (16) and intake air temperature control system improve driveability during the warm – up period, and maintain intake air at the optimum temperature.
Throttle body assembly showing the stepper motor (26), cam (27), and throttle spindle stop (28).
At idle air/fuel delivery to the engine is further refined by the partial opening of the throttle disc to compensate for variations in temperature and engine load, this is achieved using a stepper motor (26) driven by the E.C.U. which rotates a cam (27) and push rod acting directly on the throttle spindle stop (28)

Calculation of air fuel ratio

The injector is a solenoid operated by the E.C.U. which earths the solenoid coil once for each cylinder cycle (twice per crankshaft revolution) during normal driving conditions. The amount of fuel injected is determined by how long the injector is held open (known as injector pulse width). To achieve the required air/fuel ratio the E.C.U. receives signals from the following inputs: Crankshaft sensor – engine speed. Manifold absolute pressure – engine load. Inlet air temperature sensor – inlet air temperature. Coolant temperature sensor – engine temperature. Throttle potentiometer – rate of throttle opening. Battery voltage – state of battery charge.

Cruise air/fuel ratio.

The cruise air/fuel ratio is calculated by the speed/density method. Speed is determined by the crankshaft sensor and density (engine load) by the manifold absolute pressure and inlet air temperature (17) sensors. The E.C.U. contains the cruise air/fuel ratio in the form of a 2 dimensional map providing the required air/fuel ratio for 10 different engine speeds and 8 different inlet manifold density conditions. The selection of air/fuel ratio is further refined by the E.C.U. using the coolant temperature sensor, throttle potentiometer (18), throttle pedal switch and battery voltage.

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