Cam sections for a "V"-type diesel engine

A unit cam section for use with a single cylinder and piston in a "V"-type fuel injected diesel engine wherein the unit cam section, having a longitudinal center axis, includes a plurality of cams for the single cylinder and piston wherein each of the cams has a base circle, the center of each base circle lying along the longitudinal center axis, and the plurality of cams include a fuel cam, interposed between an air cam and an exhaust cam, such that the fuel cam moves a fuel pump plunger mechanism for facilitating fuel flow to the cylinder, the air cam moves air valve means and the exhaust cam moves exhaust valve means, wherein each cam has an opening flank portion and a closing flank portion and a predetermined cam profile, the unit cam section being cooperative with an inverted fuel rocker mechanism and comprises:

• a base circle diameter of at least 3.75 inches for each cam;
• the fuel cam adapted to provide a fuel cam lift to fuel pump plunger lift ratio of at least 0.8:1.0;
• and
• a predetermined cam orientation between the fuel cam and the air cam and the fuel cam and the exhaust cam such that:
• a fuel cam to air cam angle is between 0.degree. and 7.degree. wherein the fuel cam to air cam angle is defined by an angle between a fuel cam reference line and an air cam line, the fuel cam reference line being defined by a first point, corresponding to a location of a center axis of a fuel cam roller which is at a position along the opening flank of the fuel cam where the fuel cam engages the inverted fuel rocker mechanism when the piston means is substantially at top dead center during a fuel injection portion of an engine cycle, and a second point corresponding to a center axis of the base circle of the fuel cam;
• the air cam line being defined by a first point corresponding to a location of a center axis of an air cam roller which is at a position along the opening flank of the air cam corresponding to a location on the opening flank of the air cam where the air cam causes the air valve means to start to open, and a second point corresponding to the center axis of the base circle of the air cam;
• and
• a fuel cam to exhaust cam angle is between 88.degree. and 98.degree. wherein the fuel cam to exhaust cam angle is defined by an angle between the fuel cam reference line and an exhaust cam line defined by a first point corresponding to a location of a center axis of an exhaust cam roller which is at a position along the opening flank of the exhaust cam corresponding to a location on the opening flank of the exhaust cam where the exhaust cam causes the exhaust valve means to start to open, and a second point corresponding to the center axis of the base circle of the exhaust cam.

An improved "V"-type direct fuel injection diesel engine having a first combustion cylinder on one side of the engine and a second combustion cylinder on another side of the engine wherein each cylinder has a corresponding piston means, the engine comprising:

• a first unit cam section associated with said first combustion cylinder;
• a second unit cam section associated with said second combustion cylinder;
• said first and second unit cam sections having at least an integrally formed air cam, fuel cam and exhaust cam and a base circle portion for each cam with a diameter of at least 3.75 inches;
• inverted fuel rocker means associated with each cylinder and cooperative with said fuel cams;
• fuel pump means associated with each cylinder and having a fuel plunger mechanism responsive to said inverted fuel rocker means;
• said fuel cams adapted to provide a fuel cam lift to fuel pump plunger lift ratio of at least 0.8:1.0;
• and
• said first unit cam section having a predetermined cam orientation between said fuel cam and said air cam and said fuel cam and said exhaust cam such that:
• a fuel cam to air cam angle is between 56.degree. and 63.degree. wherein the fuel cam to air cam angle is defined by an angle between a fuel cam reference line and an air cam line, said fuel cam reference line being defined by a first point, corresponding to a location of a center axis of a fuel cam roller which is at a position along an opening flank of said fuel cam where said fuel cam engages said inverted fuel rocker mechanism when the piston means is at substantially top dead center during a fuel injection portion of an engine cycle, and a second point corresponding to a center axis of the base circle of said fuel cam;
• said air cam line being defined by a first point corresponding to a location of a center axis of an air cam roller which is at a position along an opening flank of the air cam corresponding to a location on the opening flank of said air cam where said air cam causes air valve means to start to open, and a second point corresponding to the center axis of the base circle of said air cam;
• and
• a fuel cam to exhaust cam angle is between 143.degree. and 153.degree. wherein said fuel cam to exhaust cam angle is defined by an angle between said fuel cam reference line and an exhaust cam line defined by a first point corresponding to a location of a center axis of an exhaust cam roller which is at a position along an opening flank of said exhaust cam corresponding to a location on said opening flank of said exhaust cam where said exhaust cam causes exhaust valve means to start to open, and a second point corresponding to the center axis of the base circle of said exhaust cam;
• said second unit cam section having a predetermined cam orientation between said fuel cam and said air cam and said fuel cam and said exhaust cam such that:
• said fuel cam to air cam angle is between 0.degree. and 7.degree.;
• and said fuel cam to exhaust cam angle is between 88.degree. and 98.degree..