Abstract: A fuel pump uses an expanding spring to pressurize liquid fuel and cause it to flow through a pump outlet port. A cam and cam follower cause a piston to move in a direction opposite to the pumping stroke in order to transfer fluid from a first chamber to a second chamber within the body of the pump. During the spring actuated pumping stroke, liquid fuel is drawn from a fuel reservoir into the first chamber of the pump for later transfer to the second chamber during the return stroke caused by the cam mechanism. A flexible shaft connects the cam to mechanism to a source of motive power to allow the pump to be displaced from the source of motive power and away from certain potential sources of heat.

Abstract: An exhaust system for an internal combustion engine includes an air injection port in a designated region of an exhaust conduit having a converging-then-diverging nozzle providing increased exhaust gas flow velocity and decreased exhaust gas pressure. In another embodiment, an injection air conduit is connected between an alternator blower and the engine exhaust conduit to supply injection air to the latter.

Abstract: A connector combines a clamp member, an insert, and a conductor to provide a robust connection between a wire and an electrically conductive component. A set screw is used to provide a force in a clamping direction through the insert member and a segment of the conductor which is disposed in electrical communication and physical contact with an internal conductive portion of a wire.

Abstract: An encoder alternator for an internal combustion engine has a rotor with a plurality of circumferential magnetic rotor poles in a periodic pattern except for at least one magnetic irregularity. A sensor coil is wound around a stator pole and outputs a crankshaft position sensor signal when the magnet irregularity of the rotor passes the stator pole.

Abstract: A returnless fuel system module includes a fuel pump in a fuel pump cavity, a fuel pressure regulator in a fuel pressure regulator cavity, first and second transfer passages therebetween, and a heat exchanger integrally formed in the housing in thermally conductive relation with at least the bypass relief passage.

Abstract: A marine vessel is maneuvered by independently rotating first and second marine propulsion devices about their respective steering axes in response to commands received from a manually operable control device, such as a joystick. The marine propulsion devices are aligned with their thrust vectors intersecting at a point on a centerline of the marine vessel and, when no rotational movement is commanded, at the center of gravity of the marine vessel. Internal combustion engines are provided to drive the marine propulsion devices. The steering axes of the two marine propulsion devices are generally vertical and parallel to each other. The two steering axes extend through a bottom surface of the hull of the marine vessel.

Abstract: A gaseous fuel pressure regulator uses an inlet valve and an outlet valve to regulate an incoming pressure, from a gaseous fuel supply tank, and accurately control the pressure at the outlet of the regulator. The control of the outlet pressure is maintained by precise movement of the outlet valve which is controlled by an actuator. The actuator receiving pulse width modulated signals from a microprocessor in order to maintain the outlet valve in an opened, or gas flow permitting, position for a time period which is appropriate to maintain the desired pressure at the outlet port of the regulator. An inlet port maintains a pressure within a conduit, which is connected in fluid communication between the inlet port and the outlet port at an intermediate pressure which is used by the outlet valve to achieve the desired outlet pressure magnitude.

Abstract: A fuel pressure control system for a fuel injected engine measures the fuel pressure at an outlet of a fuel pump and controls the operating speed of the fuel pump as a function of the difference between a desired pressure and a measured pressure. Signals are provided to the fuel pump which are pulse width modulated signals that have a pulse width determined as a function of the desired pressure at the outlet of the pump and an actual measured pressure at the outlet of the pump. The desired pressure is determined as a function of air flow into the engine, a desired air/fuel ratio which, in turn, is a function of engine speed and the load on the engine, and a desired fuel rate which is determined as a function of the air/fuel ratio and the air flow into the engine. The desired fuel rate is then used to select a pressure at the outlet of the pump which will result in the desired fuel rate.

Abstract: A method for determining the proper fueling of an internal combustion engine when nitrous oxide is being injected into the air intake of the engine determines an equivalent air per cycle (APCequiv) by calculating the effect of both the air and the nitrous oxide on the oxygen content of the gas stream flowing into the cylinders of the engine. After calculating the equivalent air per cylinder magnitude, the fuel per cylinder (FPC) is calculated as a function of the stoichiometric air fuel ratio and an equivalence ratio that modifies the stoichiometric air/fuel ratio.