Electronic control system

Claim 2

An electronic control system for controlling the operation of a fuel injection pump intended to supply fuel to a turbo supercharged compression ignition engine having an air inlet manifold, the system comprising a memory circuit in which can be stored test data relating to the variation of air inlet manifold pressure as a result of variation of at least one engine operating parameter, said engine operating parameter or parameters in use being supplied to said memory circuit to provide a derived air inlet manifold pressure signal.

Claim 3

A control system according to claim 1 including a delay circuit operable to delay the derived air inlet manifold pressure signal to compensate for the lag in the operation of the turbo supercharger of the engine.

Claim 4

An electronic control system for controlling the operation of a fuel injection pump which supplies fuel to a turbo supercharged compression ignition engine having an air inlet manifold, the pump including an electromagnetically controlled actuator for controlling fuel flow to the engine, the control system comprising first and second transducers responsive in use to two engine operating parameters, a memory circuit which receives the outputs of said transducers to provide a derived air inlet manifold pressure signal, said memory circuit containing test data relating to the variation of air inlet manifold pressure as a result of variation in said two engine operating parameters, a function generator which receives said derived air inlet manifold pressure signal and provides an output representing the maximum amount of fuel which can be supplied to the engine, a third transducer for providing a demand signal, circuit means for comparing the demand signal and the maximum fuel signal and for providing a demanded fuel signal and means receiving said demanded fuel signal and providing a control signal for said actuator.

Claim 5

An electronic control system for controlling the operation of a fuel injection pump which supplies fuel to a turbo supercharged compression ignition engine having an air inlet manifold, the pump including an electromagnetically controlled actuator for controlling fuel flow to the engine, the control system comprising first and second transducers responsive in use to two engine operating parameters, a memory circuit which receives the outputs of said transducers to provide a derived air inlet manifold pressure signal, said memory circuit containing test data relating to the variation of air inlet manifold pressure as a result of variation in said two engine operating parameters, a function generator which receives said derived air inlet manifold pressure signal and provides an output representing the maximum amount of fuel which can be supplied to the engine, a third transducer for providing a demand signal, circuit means for comparing the demand signal and the maximum fuel signal and for providing a demanded fuel signal and means receiving said demanded fuel signal and providing a control signal for said actuator.

Claim 6

A control system according to claim 3 including a delay circuit for delaying change in the maximum fuel signal to compensate for lag in the operation of the turbo supercharger.

Claim 7

A control system according to claim 4 in which said delay circuit is interposed between the memory circuit and the function generator.

Claim 8

A control system according to claim 3 in which said first transducer is responsive to the speed of the engine and said second transducer to the amount of fuel being supplied by the pump to the engine.

Claim 9

A control system according to claim 6 including a delay circuit for delaying the application of increasing demand signals to said circuit means, said delay circuit being inoperative when the demand signal is below a threshold value.

Claim 10

A control system according to claim 7 in which said threshold value is determined by a circuit responsive to the output signal of said first transducer.