Abstract: The improved internal combustion engine of the cam drive axial piston type includes modification to the drive shaft, bearings and other internal elements to facilitate the flow of oil and lubricants to engine parts. The cooling system is modified to allow coolant flow directly to the engine block and head assembly simultaneously and to control flow through the engine and radiator to reduce hot spots. The valves and valve crown structure have been modified for ease of assembly and reliability of the roller valve lifter and valve interface. Use of alternate fuel supply systems which eliminate the need for a valve train are also accommodated. The drive shaft and engine have been modified to allow the mounting of a variety of aircraft propellers using a hub as well as mounting a flywheel for reduced start motor stress.

Abstract: The improved internal combustion engine of the cam drive axial piston type includes modification to the drive shaft, bearings and other internal elements to facilitate the flow of oil and lubricants to engine parts. The cooling system is modified to allow coolant flow directly to the engine block and head assembly simultaneously and to control flow through the engine and radiator to reduce hot spots. The valves and valve crown structure have been modified for ease of assembly and reliability of the roller valve lifter and valve interface. Use of alternate fuel supply systems which eliminate the need for a valve train are also accommodated. The drive shaft and engine have been modified to allow the mounting of a variety of aircraft propellers using a hub as well as mounting a flywheel for reduced start motor stress.

Abstract: The improved internal combustion engine of the cam drive axial piston type includes modification to the drive shaft, bearings and other internal elements to facilitate the flow of oil and lubricants to engine parts. The cooling system is modified to allow coolant flow directly to the engine block and head assembly simultaneously and to control flow through the engine and radiator to reduce hot spots. The valves and valve crown structure have been modified for ease of assembly and reliability of the roller valve lifter and valve interface. Use of alternate fuel supply systems which eliminate the need for a valve train are also accommodated. The drive shaft and engine have been modified to allow the mounting of a variety of aircraft propellers using a hub as well as mounting a flywheel for reduced start motor stress.

Abstract: The improved internal combustion engine of the cam drive axial piston type includes modification to the drive shaft, bearings and other internal elements to facilitate the flow of oil and lubricants to engine parts. The cooling system is modified to allow coolant flow directly to the engine block and head assembly and to control flow through the engine and radiator to reduce hot spots. The valves and valve crown structure have been modified for ease of assembly and reliability of the roller valve lifter and valve interface. Use of alternate fuel supply systems which eliminate the need for a valve train are also accommodated. The drive shaft and engine have been modified to allow the mounting of a variety of aircraft propellers using a hub as well as mounting a flywheel for reduced start motor stress.

Abstract: An internal combustion engine in which first and second elongate blocks of identical structure are axially aligned and held in longitudinally spaced relationship by a generally cylindrical connector. The first and second blocks cooperate to define a number of axially aligned cylinders, each of which has a double ended piston slidably mounted therein, and each of which piston supports a pair of cam engaging members. A drive shaft is rotatably supported in the first and second blocks, which drive shaft supports a force receiving cam that is engaged by the pairs of members on the pistons, with the cam situated within the confines of the connector.