Fuel supply system for a rotary piston engine

A rotary piston engine comprising a casing composed of a rotor housing having a trochoidal inner peripheral surface and side housings which close opposite ends of said rotor housing, a polygonal rotor adapted to rotate eccentrically in said casing with apex portions thereof sliding over said trochoidal surface thereby defining a plurality of combustion chambers between said trochoidal surface and individual flanks of said polygonal rotor, said casing having first and second intake ports which open in the inner wall of said casing, said second port being positioned so as to be advanced in the rotational direction of said rotor relative to said first port, first and second intake systems connected to said first and second ports, respectively, first and second fuel injection means for injecting fuel into said first and second intake systems, respectively, first and second means to detect intake air flow rate in said first and second intake systems and to dispatch first and second flow rate signals showing the intake air flow rate in said first and second intake systems, respectively, means to detect the rotation of said rotor and dispatch a timing signal showing the rotational timing of said rotor, a computer which operates depending upon said first and second flow rate signals and said timing signal to produce a first and second series of fuel injection signals for actuating said first and second fuel injection means in a manner that the duration and timing of the fuel injection in said first intake system are determined by said first flow rate signal and said timing signal, respectively, that the duration and timing of the fuel injection in said second intake system are determined by said second flow rate signal and said timing signal, respectively, and that said first fuel injection means is actuated for every sequential suction strokes performed by said plurality of combustion chambers while said second fuel injection means is actuated for only cyclically selected ones of said sequential suction strokes performed by said plurality of combustion chambers.