FIELD: engines and pumps.
SUBSTANCE: proposed method comprises, in particular, cyclic ejection of combustion products and suction of atmospheric air. Two circular vortices are generated at a time in intake channel in suction cycle. This intensifies mass transfer and combustion to up pressure pulse amplitude and engine thrust.
EFFECT: increased thrust of pulse duct.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF INCREASING VALVELESS PULSE DUCT THRUST | 2007 |
|
RU2429367C2 |
PULSEJET ENGINE | 2005 |
|
RU2300005C2 |
PULSEJET ENGINE | 2005 |
|
RU2300004C2 |
INTERMITTENT-CYCLE AIR-JET ENGINE | 2010 |
|
RU2435977C1 |
METHOD OF PULSE JET ENGINE DOUBLE-FLOW BLOWING AND DOUBLE-FLOW PULSE JET ENGINE | 2015 |
|
RU2608427C1 |
METHOD OF INCREASING VERTICAL TAKE-OFF PULSE JET ENGINE THRUST (VERSIONS) | 2006 |
|
RU2333378C2 |
METHOD TO IMPLEMENT CYCLIC DETONATION BURNING IN INTERMITTENT AIR JET ENGINE | 2011 |
|
RU2493399C2 |
INTERMITTENT-CYCLE AIR-JET ENGINE | 2010 |
|
RU2435978C1 |
METHOD FOR FORCING A DUAL-FLOW EJECTOR PULSE JET ENGINE AND FORCED DUAL-FLOW EJECTOR PULSE JET ENGINE | 2020 |
|
RU2765672C1 |
PULSATING AIR-BREATHING DETONATION ENGINE | 2010 |
|
RU2443893C1 |
Authors
Dates
2011-09-20—Published
2007-08-06—Filed