Sleeve valve system for internal combustion engine having ellipt

Details Sleeve valve system for internal combustion engine having ellipt Sleeve valve system for internal combustion engine having ellipt

1991-10-18

1993-02-02

Okonsky, David A.

Internal-combustion engines

Multiple cylinder

Cylinders in-line

123 81C, 1231885, F02B 7520

Patent

active

051830140

ABSTRACT:
An improved internal combustion engine, particularly of the compression ignition, two cycle, aircraft type employing sleeve valves and a modular cylinder and removable cylinder head and retainer. The engine is turbocharged with the turbocharger separated into the compression turbine on one side of a V shaped cylinder array and the drive turbine on the opposite side. The exhaust is discharged through the center of the power output shaft making this engine particularly suited for pusher aircraft applications.

REFERENCES:
patent: 1129104 (1915-02-01), Knight
patent: 1953185 (1934-04-01), Meyer
patent: 2065600 (1936-12-01), Meyer
patent: 2134285 (1938-10-01), Kipfer
patent: 2230407 (1941-02-01), Kammer
patent: 2691970 (1954-10-01), Evans
patent: 3844109 (1974-10-01), Roos
patent: 4838214 (1989-06-01), Barrett
patent: 5054438 (1991-10-01), Takashima

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