FIELD: aero-engine manufacture. SUBSTANCE: needle valve is moved along axis of blind passage. Fuel is fed from the end of needle valve. Flow rate of fuel gas is regulated in accordance with relationship given in the description. EFFECT: enhanced efficiency. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
SUPERSONIC RAMJET ENGINE WITH PULSATING COMBUSTION AND METHOD OF ITS OPERATION | 2010 |
|
RU2446305C2 |
METHOD OF ORGANIZATION OF DETONATION COMBUSTION CHAMBER OF SUPERSONIC RAMJET ENGINE | 2004 |
|
RU2285143C2 |
SEISMIC SOURCE | 1994 |
|
RU2094826C1 |
DEVICE FOR APPLYING COATINGS | 1987 |
|
RU1603581C |
METHOD OF SETTING-UP COMBUSTION IN HYPERSONIC RAMJET ENGINE AND HYPERSONIC RAMJET ENGINE FOR REALIZATION OF THIS METHODS (VERSIONS) | 1994 |
|
RU2082017C1 |
DEVICE FOR GAS-DYNAMIC SPRAYING OF POWDER MATERIALS | 2000 |
|
RU2190695C2 |
NOZZLE UNIT OF GAS-DYNAMIC LASER | 1998 |
|
RU2149487C1 |
SHIPBOARD ENGINE-AND-PROPULSOR COMPLEX AND METHOD OF ITS OPERATION | 2000 |
|
RU2188141C2 |
DEVICE FOR AFFECTING SUPERSONIC FLOW | 1981 |
|
SU1166561A1 |
HIGH-POWER CARBON DIOXIDE LASER | 1998 |
|
RU2143772C1 |
Authors
Dates
1995-02-20—Published
1990-12-17—Filed