FIELD: mechanical engineering; internal combustion engines. SUBSTANCE: compressor is arranged coaxially on rotor shaft in internal combustion engine consisting of housing, rotor, combustion chambers and ignition system. Channels are made in shaft body to supply fuel and let out exhaust gases. Channels made in rotor body are designed for compressed air blowing. These channels are arranged in parallel with longitudinal axis of rotor and are connected by smaller channels with mixing chambers made on inner cylindrical surface of engine. Combustion chambers with nozzle channels and ignition chambers are made on outer diameter of rotor. Fuel supply channels are made for delivering fuel into mixing chambers. EFFECT: increased power output of engine owing to complete filling up of combustion chamber with working mixture. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTICOMPRESSOR LIQUID-PROPELLANT ROCKET ENGINE | 1995 |
|
RU2120051C1 |
ROTARY JET ENGINE | 1994 |
|
RU2118687C1 |
ROTARY ENGINE | 1995 |
|
RU2094634C1 |
ROTARY ENGINE | 1995 |
|
RU2095589C1 |
TWO-STROKE MULTICYLINDER ROTARY-PISTON ENGINE | 1995 |
|
RU2101526C1 |
FUEL SYSTEM OF FOUR-STROKE INTERNAL COMBUSTION ENGINE | 1995 |
|
RU2105187C1 |
YUGI TURBO-ROTARY ENGINE | 2008 |
|
RU2372503C1 |
TURBOJET ENGINE | 1994 |
|
RU2122132C1 |
THREE-STAGE MULTIPLE-CIRCUIT COMPRESSOR | 1995 |
|
RU2097604C1 |
GAS-TURBINE ENGINE | 2004 |
|
RU2261998C1 |
Authors
Dates
1998-08-20—Published
1994-10-25—Filed