FIELD: engines and pumps.
SUBSTANCE: pulsejet engine comprises housing with combustion chamber and nozzle, fuel feed and ignition system. Said nozzle is composed of annular slot, either discontinuous or solid closed. Engine housing is composed of, at least, two discs with disc-shape combustion chamber arranged there between. Discs are fixed relative to each other by crossbars arranged in circle. Lower disc is secured to generator while top disc is fitted on axle engaged with generator rotor shaft to revolve relative to bottom disc.
EFFECT: better engine cooling, expanded range of jet engines.
4 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD TO PRODUCE HEAT INSULATING FIREPROOF CONSTRUCTION MATERIAL | 2014 |
|
RU2543845C1 |
COMPOSITION FOR PRODUCTION OF BUILDING COATING AND METHOD OF ITS APPLICATION | 2013 |
|
RU2531176C1 |
SCREW PILE | 2011 |
|
RU2459038C1 |
PULSEJET ENGINE | 2016 |
|
RU2672240C1 |
FUEL-AIR MIX COMBUSTION AND RAMJET ENGINE WITH SPIN DETONATION WAVE | 2014 |
|
RU2573427C2 |
WIND-DRIVEN THERMAL POWER PLANT | 2010 |
|
RU2446310C1 |
STABILIZING ADDITIVE FOR CRUSHED-MASTIC ASPHALT CONCRETE | 2016 |
|
RU2632839C1 |
INTERMITTENT-CYCLE AIR-JET ENGINE (ICAJE) | 2011 |
|
RU2468235C1 |
JET HOVERCRAFT | 2013 |
|
RU2537663C1 |
SCRAMJET WITH PULSE DETONATION COMBUSTION CHAMBER AND HYPERSONIC JET FLOW COMBINED WITH SUPERSONIC DIRECT FLOW IN "ONE-IN-ONE" MANNER | 2012 |
|
RU2524591C1 |
Authors
Dates
2013-07-27—Published
2011-02-14—Filed