Rotary piston engines

• US 3,976,036 A
• Filed: 01/16/1975
• Issued: 08/24/1976
• Est. Priority Date: 01/25/1974
• Status: Expired due to Term

• Current Assignee: Toyo Kogyo Co Ltd (Mazda Motor Corporation)
• Original Assignee: Toyo Kogyo Co Ltd (Mazda Motor Corporation)
• Inventors: Hayashida, Motoyuki, Muroki, Takumi
• Primary Examiner(s): Croyle, Carlton R.
• Assistant Examiner(s): Koczo, Jr., Michael
• Application Number:
  US05/541,575
• Time in Patent Office: 586 Days
• Field of Search: 123/8.09, 123/8.11, 123/8.13, 123/32 C, 123/32 D
• US Class Current: 123/209
• CPC Class Codes: F02B 2053/005 Wankel engines
• CPC Class Codes: F02B 53/10 Fuel supply; Introducing fuel to combustion space
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A rotary piston type internal combustion engine comprising a casing which includes a rotor housing having cavity defined by a trochoidal inner peripheral wall having a major and a minor axes, and a pair of side housings sealingly secured to the opposite sides of the rotor housing, a substantially polygonal rotor disposed in said cavity for rotation with apices in sliding contact with the inner peripheral wall of the rotor housing to define working chambers of variable volume with the trochoidal inner peripheral wall of the casing, said casing having an air intake port and an exhaust port, a primary combustion chamber disposed outside the cavity in the casing, a communication passage connecting the primary combustion chamber with the cavity in the casing, a fuel injection nozzle provided in said primary combustion chamber, and an ignition plug provided in said primary combustion chamber, said primary combustion chamber having a volume which is 35 to 65 percent of the sum of volume of the primary combustion chamber and that of one of the working chambers in the most compressed position, said communication passage opening to the casing cavity at a position between 15° before and 30° after the minor axis of the rotor housing, said fuel nozzle being adapted to provide air-fuel mixture having air-fuel ratio of 10 to 16 in the primary combustion chamber and overall air-fuel ratio of 19 to 46 in the primary combustion chamber and the working chamber communicating therewith.

Claims

1. A rotary piston type internal combustion engine comprising a casing which includes a rotor housing having cavity defined by a trochoidal inner peripheral wall having a major and a minor axis, and a pair of side housings sealingly secured to the opposite sides of the rotor housing, a substantially polygonal rotor disposed in said cavity for rotation with apices in sliding contact with the inner peripheral wall of the rotor housing to define working chambers of variable volume with the trochoidal inner peripheral wall of the casing, said casing having air intake port means and exhaust port means, primary combustion chamber means disposed outside the cavity in the casing, communication passage means connecting the primary combustion chamber means with the cavity in the casing, means for supplying fuel to said primary combustion chamber means, and ignition means provided in said primary combustion chamber means, said primary combustion chamber means having a volume which is 35 to 65 percent of the sum of volume of the primary combustion chamber and that of one of the working chambers in the most compressed position, said communication passage opening to the casing cavity at a position between 15°

before and 30°

after the minor axis of the rotor housing, said fuel supply means being adapted to provide air-fuel mixture having air-fuel ratio of 10 to 16 in the primary combustion chamber and overall air-fuel ratio of 19 to 46 in the primary combustion chamber and the working chamber communicating therewith.

2. A rotary piston type engine in accordance with claim 1 in which said communication passage opens to the casing cavity at 5°

after the minor axis.

3. A rotary piston type engine in accordance with claim 1 in which said primary combustion chamber is of a substantially spherical configuration.

4. A rotary piston type engine in accordance with claim 3 in which said communication passage means is offset from the center of the sphere of the primary combustion chamber.

5. A rotary piston type engine in accordance with claim 1 in which said primary combustion chamber has a volume which is approximately 50 percent of the sum of volume of the primary combustion chamber and that of one of the working chambers in the most compressed position.