FIELD: air transport.
SUBSTANCE: aircraft contains frame for effective load and device for ejector gas acceleration, which nozzles are interconnected and vacuum cavity. In the first example behind the last air-tight nozzles interconnected in rigid or flexible way there is a loose mounted ejecting nozzle with critical cross-section bigger in comparison with critical cross-section nozzle defining consumption for the same air-tight interconnected nozzles. In the second example for air-tight interconnected nozzles one nozzle is introduced into resonance cavity so that gas-dynamic flow leaving the nozzle could collide with gas-dynamic flow in resonance cavity equipped with at least one outlet nozzle. In the third example air-tight interconnected nozzles are installed so that they could rotate relative to rotative axis to which they are fixed by the arm.
EFFECT: efficiency upgrading of energy use of active pulse jet.
3 cl, 8 dwg
Title | Year | Author | Number |
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|
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|
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THERMAL HEAD | 2006 |
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RU2313403C2 |
SHESTERENKO SUPERNOZZLE (VERSIONS) | 2004 |
|
RU2361679C2 |
SHESTERENKO MOUTHPIECE | 2005 |
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RU2354459C2 |
SHESTERENKO'S SUPERNOZZLE (VERSIONS) | 2005 |
|
RU2361680C2 |
NOZZLE DEVICE | 2004 |
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RU2303491C2 |
NOZZLE ASSEMBLY | 2004 |
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RU2277441C2 |
SHESTERENKO(S SUPERSONIC NOZZLE | 2011 |
|
RU2574788C2 |
Authors
Dates
2010-03-20—Published
2006-12-22—Filed