FIELD: mechanical engineering; aircraft; air cushion vessels, various air blowers. SUBSTANCE: engine has air intake with center body serving as air pressure rise source, center return flow of gases, nozzle part, and fuel feed system with ignition system. Engine is designed for mounting in aircraft propeller blade and can be used also to set into motion propellers of aircraft, air cushion vessels and various air blowers. EFFECT: simplified design, low cost of manufacture, enhanced reliability and increased economy. 3 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
ROTARY ENGINE | 1995 |
|
RU2095589C1 |
JET ROTARY ENGINE AND ITS FEED SYSTEM | 1996 |
|
RU2115817C1 |
TRANSPORT TWO-SHAFT AND THREE-SHAFT GAS-TURBINE ENGINES (VARIANTS) | 1997 |
|
RU2126906C1 |
FEED SYSTEM FOR INTERNAL COMBUSTION ENGINE | 1995 |
|
RU2093689C1 |
RAMJET ENGINE | 2006 |
|
RU2330980C1 |
FUEL SYSTEM OF INTERNAL COMBUSTION ENGINE ADAPTED FOR OPERATION ON LIQUEFIED OIL GAS | 1995 |
|
RU2095610C1 |
JET ENGINE | 2006 |
|
RU2327891C1 |
FEEL SYSTEM OF INTERNAL COMBUSTION ENGINE ADAPTED FOR OPERATION ON LIQUEFIED NATURAL GAS | 1995 |
|
RU2095611C1 |
WINDMILL | 1995 |
|
RU2074981C1 |
FLIGHT VEHICLE | 2009 |
|
RU2421376C1 |
Authors
Dates
1999-03-20—Published
1997-06-23—Filed