FIELD: mechanical engineering; internal combustion engine.
SUBSTANCE: proposed internal combustion engine contains reaction turbine made in form of solid of revolution with reaction nozzle installed tangentially to peripheral surface of turbine, combustion chamber made in volume of reaction turbine, diffuser and ejector. Diffuser outlet is connected with inlet of combustion chamber. Nozzle of ejector is connected to combustion chamber, and ejected inlet communicates with atmosphere. Diffused and ejector are made in turbine volume. Outlet of elector is completely connected with inlet of diffuser.
EFFECT: simplified design, increased efficiency.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
ENGINE UTILIZING ENERGY OF HEATED VAPOR OF FUEL | 1995 |
|
RU2095606C1 |
GAS TURBINE PLANT OPERATING ON HIGH-PRESSURE GASEOUS FUEL | 1996 |
|
RU2149273C1 |
JET-TYPE POWER PLANT | 2011 |
|
RU2467188C2 |
COMPRESSED AIR OR GAS COOLING METHOD AND COMPRESSOR PLANT FOR IMPLEMENTING THIS METHOD | 1999 |
|
RU2172854C2 |
VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE | 2019 |
|
RU2766496C2 |
ELECTROGASODYNAMIC CO-LASER | 1993 |
|
RU2065240C1 |
TURBO-EJECTOR ENGINE | 1999 |
|
RU2190772C2 |
PULSE GAS-TURBINE EJECTOR ENGINE (VERSIONS) | 2005 |
|
RU2362033C2 |
ELECTRIC DETONATION TURBINE UNIT AND UNIVERSAL COMBINED-CYCLE PLANT (EMBODIMENTS) | 2018 |
|
RU2693353C1 |
METHOD OF USING GAS-AIR THERMODYNAMIC CYCLE FOR INCREASING EFFICIENCY OF SMALL TURBO-ENGINE | 2019 |
|
RU2735880C1 |
Authors
Dates
2006-06-10—Published
2005-01-14—Filed