Abstract: This disclosure deals with a mechanism for adjusting the timing of initiation of injection by a fuel injector of an internal combustion engine. The mechanism includes a piston connected to be moved by a drive for the injector, and another piston which is connected to move the plunger of the injector. A timing fluid supply is provided for feeding a timing fluid into a timing chamber formed between the two pistons under selected operating conditions, the timing fluid forming a hydraulic link between the two pistons. The mechanism further includes pressure relief means for releasing a portion of the timing fluid after the termination of injection, the relief means comprising a pressure responsive mechanism.

Abstract: A diaphragm operated, air fuel control system for controlling the rate of fuel flow to an internal combustion engine in response to intake manifold pressure is disclosed wherein the transient response of the diaphragm operator is attenuated by a fuel filled control chamber. An attenuator assembly connected with the control chamber causes fuel to be supplied to the chamber at a rate which is greater than the rate at which fuel may be discharged from the control chamber. In one embodiment the chamber is formed on the side of the diaphragm operator which is opposite to the side to which intake manifold pressure is supplied. In another embodiment the control chamber is formed to receive one end of a plunger valve connected with the diaphragm operator.

Abstract: An interlock is disclosed for permitting only one of a plurality of interrelated valve elements to be operated at one time. A transverse channel is formed in each valve element for alignment with a channel formed in the valve housing when the valve elements are moved to their respective opened positions. When any one valve element is moved to its closed position, camming surfaces formed on the valve element are positioned and shaped to cause a train of end abutting links disposed within the valve and housing channels to be displaced in a manner to lock the remaining valves in their respective open positions. The valve channels and camming surfaces are formed by very simple and inexpensive linear cutting operations thereby allowing the disclosed device to be inexpensively manufactured.

Abstract: A cylinder liner is disclosed for an internal combustion engine including a cylindrical hollow body having a press fitted upper end and a stop located intermediate the liner ends for engaging an engine block liner stop to provide upper and lower seals for a coolant passage. The outside surfaces of the liner adjacent the press fitted upper end and the stop are formed to permit a settable plastic material to be used between the liner and engine block to assist in forming the coolant seal and to provide radial support to the liner to permit the lower 30 percent of the cylinder liner to be free of any direct contact with the engine block. This design also permits use of a smaller capacity cooling system and improves lubricating oil flow within the engine block.

Abstract: A turbomachine, operable as a compressor or a turbine, for a compressible fluid is provided which includes a wheel having a plurality of vanes extending from a generally axial flow section to a generally radial flow section. Adjacent vanes define fluid passageways having a generally axially oriented section and a generally radially oriented section. Located substantially within the generally radially oriented sections of a predetermined number of passageways is a reference station which has a configuration such that the mean tangential dimension of said passageway at said reference station is no more than about 60% of the circumference of the rotor at that mean radius divided by the number of vanes at that radius. Each reference station serves to effect substantial attachment of the flowing fluid to the surfaces defining said passageway, particularly at low mass flow, and, thus, broaden the usable flow range of the turbomachine.

Abstract: An optical alignment system for optically determining the translational and rotational orientation of portions of an object with respect to a system reference utilizing a reflective target (8) positioned on the object portion and adapted to receive an optical reference beam (6) transmitted to the target (8) from the reference position. The reflective target (8) includes a photoelectric sensor (22) for producing an electrical signal indicative of the lateral displacement of the reflective target (8) from the optical reference beam (6) and a reflective surface (mirror 24) for returning a portion (return beam 26) of the optical reference beam (6) to a photosensor (28) positioned adjacent the reference beam source (12) to provide information relative to the angular position of the reflective target (8). A method for operating the system is also disclosed.

Abstract: The disclosure illustrates an insulated composite piston comprising a crown of ceramic or other heat resistant material secured to an aluminum piston body by a bolt of temperature resistant alloy. A low conductivity interface between the crown and the body is provided by a series of stacked discs having low effective thermal conductivity. The relative thermal expansion of the parts is compensated for by bellville washers on the bolt. The above arrangement insulates the crown from the piston body thereby minimizing the temperature gradient across the crown so that its temperature can be maintained as high as necessary to increase efficiency and minimize noxious emissions.

Abstract: A composite engine block is disclosed including a main frame containing plural cylinder liner receiving cavities interleaved with plural cross walls extending generally perpendicularly between the outer side walls of the main frame and an oil pan adapter or ladder frame forming the lower section of the composite engine block between the main frame and the engine oil pan. Each main frame cross wall is combined with a pair of pillars extending between the upper head engaging surface of the main frame and a crankshaft bearing support located adjacent the lower surface of the engine block, wherein both the cross wall and pillars are shaped to strengthen and rigidify the composite engine block and to facilitate metal casting of the main frame.

Abstract: A turbomachine for a compressible fluid is provided which includes a compressor wheel having a plurality of vanes extending from a generally axial flow inlet to a generally radial flow outlet. Adjacent vanes define fluid passageways having a generally axially oriented section near the inlet and a generally radially oriented section near the outlet. Located substantially within the generally radially oriented sections of a predetermined number of passageways is a reference station which has a configuration such that the mean tangential dimension of said passageway at said reference station is no more than about 60% of the circumference of the rotor at that mean radius divided by the number of vanes at that radius. Each reference station serves to effect substantial attachment of the flowing fluid to the surfaces defining said passageway, particularly at low mass flow, and, thus, broaden the usable flow range of the compressor.

Abstract: A turbine assembly is provided for use on an internal combustion engine such as a diesel engine having conventional intake and exhaust manifolds. The assembly includes a hollow section which has an inlet communicating with the exhaust manifold, and an outlet communicating with an exhaust gas entry into a chamber in which a turbine wheel is mounted. Rotatably mounted within the hollow section is a rotor which is adjustable to various selected positions. When in a first selected position, the rotor permits substantially unrestricted exhaust gas flow through the assembly. When in a second selected position, a predetermined amount of exhaust gas is diverted from the turbine wheel chamber through a bypass passageway formed in the hollow section. The end of the bypass passageway terminates downstream of the turbine wheel chamber. When in a third selected position of adjustment, the rotor effects substantial blockage of the exhaust gas flow through the assembly.

Abstract: This disclosure deals with a fuel supply system for a compression ignition, internal combustion engine, which is simple in construction and inexpensive to manufacture. The system includes a plurality of fuel injectors, one injector for each combustion chamber of the engine, and a common fuel supply rail which is connected to all of the injectors. Means is provided to regulate the fuel pressure in the supply rail. The injectors are normally closed but they are sequentially actuated to inject fuel by operation of an injector control circuit. Each injector includes a pintle-type nozzle which normally is held closed by a force applying device, and the control circuit operates to remove the force applying device from each injector in turn. The nozzle of an actuated injector then opens by an amount that is a function of the pressure in the rail, and the quantity of fuel injected is related to the fuel pressure.

Abstract: An exhaust brake modulating control system is provided for an internal combustion engine having a turbo-charger and source of pressurized fluid. The system includes a double-acting piston-cylinder assembly having one cylinder end communicating with the engine exhaust manifold and an opposite end separated from the one end by a piston head. An adjustable control valve is provided having an outlet connected to the cylinder second end, and a plurality of inlets selectively connected to the outlet. One inlet communicates with the pressurized fluid source and a second inlet is vented to the atmosphere. Communicating with the exhaust manifold is an inlet of a hollow section in which a rotor is rotatably mounted. The hollow section has an outlet separated from the inlet by the rotor. The outlet communicates with the turbine wheel chamber of the turbo-charger. When the rotor assumes a first selected position, substantially unrestricted exhaust gas flow past the rotor occurs.

Abstract: A piston ring assembly for placement between a piston and a cylinder wall is provided. The assembly includes an annular expansion ring disposed around the piston, and an annular parted piston ring disposed around the expansion ring. A predetermined segment of the piston ring engages the expansion ring.

Abstract: This disclosure deals with apparatus for adjusting the timing of injection in an internal combustion engine wherein the fuel system includes unit injectors. The injector for each combustion chamber of the engine is actuated to inject fuel by a cam-follower-linkage mechanism that operates in time relation with the movement of the pistons of the engine. Each such mechanism includes a cam which is rotated in synchronism with the pistons of the engine, a pivotable cam follower which rides on the cam, and a linkage which connects the follower with an injector. The injector includes a plunger which seats on a cup or nozzle to terminate injection. To adjust the timing of injection, the pivot point of the follower and the angular point of engagement of the follower with the cam are moved. The relation of the cam, the follower and the linkage are arranged such that the movement of the linkage does not materially change the effective travel of the plunger as the timing is changed within a broad range.

Abstract: A turbocharger assembly is provided for use with an internal combustion engine. The assembly includes a compressor chamber having a compressor wheel disposed therein and a turbine chamber having a turbine wheel disposed therein. The two wheels are affixed to a rotating shaft. A lubricated bearing assembly is disposed between the chambers and encompasses the shaft. A dynamic first seal encompasses the shaft and is disposed between the bearing assembly and the compressor chamber. A second seal encompasses the shaft and is disposed between the bearing assembly and the turbine chamber. Controlled first means is provided for braking rotation of the shaft. Second means is provided which, when the first means is in a shaft-braking mode, causes a predetermined gaseous pressure to be exerted on the first seal inhibiting migration of the lubricant from the bearing assembly to the compressor chamber.

Abstract: A test apparatus and method is disclosed for a fuel pump mounted on and driven by an engine, the speed of which is controlled by the pressure of fuel supplied thereto wherein the engine continues to be supplied with fuel from the fuel pump during the test. A fluid circuit is provided which is designed to supply fuel to the engine under controlled pressure to permit the engine speed to be controlled independently of the engine throttle position and to permit the flow rate of the fuel to be adjusted to a predetermined value at which the output pressure of the fuel pump may be measured for calibration purposes. The fluid circuitry and necessary measurement circuitry may be mounted within a small, portable housing to allow for field testing of a fuel pump.

Abstract: The disclosure illustrates a water to air aftercooler assembly in which an elongated coolant tube bundle is supported by plates spaced between heat exchange fins to form an aftercooler core. The support plates are secured to opposed walls forming a part of the aftercooler housing. This arrangement permits a simplified and economical aftercooler core. In addition it provides an improved support for the aftercooler core and structurally reinforces the aftercooler housing.

Abstract: An air fuel ratio control for an I.C. engine fuel supply system is disclosed including a diaphragm operator for a fuel flow modulating valve responsive to engine intake manifold pressure as sensed through an air line connecting the diaphragm operator with the intake manifold and a drain line for returning to the engine fuel tank all fuel which may leak into the diaphragm operator due to seal rupture. The disclosed system further including a specially designed flow restrictor in the air line to prevent engine fuel tank pressurization and reverse fuel flow into the engine's intake manifold should the diaphragm operator rupture. The flow restrictor includes a control orifice which is sufficiently large to allow proper control by the diaphragm operator but yet not so large as to allow fuel tank pressurization should the diaphram rupture. In one embodiment the flow restrictor includes a check valve designed to close only upon improper fuel flow from the air fuel control to the intake manifold.

Abstract: This disclosure relates to a turbocharged internal combustion engine. The exhaust manifold of the engine is divided into sections, and the engine exhaust from one of the sections is recirculated to the intake manifold. The engine cylinders that feed the EGR exhaust manifold section alternate in the engine firing order with the other cylinders, thereby providing a substantially uniform flow of exhaust gas to all of the cylinders. The turbine of the engine turbocharger is divided into two sections, one having a smaller flow area than the other. The turbine section having the smaller flow area is connected to receive the exhaust gasses from the exhaust manifold section that also supplies the EGR.

Abstract: A fuel injection system for a diesel engine. An injection rate control device, such as an auxiliary spring, is connected in line with the conventional injection train which operates the injector plunger in synchronism with the rotation of the camshaft. When an auxiliary spring is used as the injection rate control device, the auxiliary spring has a lower spring rate than that of the injection train so that the injector plunger is advanced at a different rate when it is under the control of the auxiliary spring. Means are included for rendering the auxiliary spring ineffective during a portion of the plunger advancement so that the rate of plunger advancement is controlled by the auxiliary spring during the initial part of the advancing stroke, and by the conventional part of the injection train during the balance of the advancing stroke. The auxiliary spring automatically varies ignition timing and injection rate as a function of engine speed and/or load.