FIELD: jet facilities. SUBSTANCE: proposed ejector has active and passive gas nozzles and mixing chamber. Ring receiver to supply higher temperature passive gas enclosed lower temperature passive gas nozzle. Higher temperature passive gas nozzles are found in receiver wall on cut of passive nozzle. EFFECT: reduced overall dimensions and weight. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
RING COMBUSTION CHAMBER | 1993 |
|
RU2099640C1 |
EJECTOR | 1996 |
|
RU2116521C1 |
FAN | 1995 |
|
RU2133382C1 |
PROCESS TESTING GAS-TURBINE ENGINE | 1995 |
|
RU2162593C2 |
WATER-JET GAS-LIQUID EJECTOR | 1997 |
|
RU2137948C1 |
COMBUSTION CHAMBER OF GAS-TURBINE ENGINE WITH CONTROLLER DISTRIBUTION OF AIR | 1995 |
|
RU2163991C2 |
GAS LIQUEFACTION PLANT | 1995 |
|
RU2119134C1 |
LIQUID-PROPELLANT ROCKET ENGINE | 1986 |
|
RU2083859C1 |
AIR-GAS BURNER | 1997 |
|
RU2146788C1 |
METHOD OF CYCLIC ELECTROCHEMICAL TREATMENT | 1992 |
|
RU2071883C1 |
Authors
Dates
2001-03-10—Published
1995-11-22—Filed