FIELD: engines and pumps.
SUBSTANCE: system of plasma-enriched fast expansion duct comprises gas turbine engine transition duct and conical plasma generator to generate comical plasma along duct outer wall. Said transition duct has inlet and outlet downstream of duct inlet, duct conical radially inner and outer walls arranged in axil direction between duct inlet and outlet.
EFFECT: ruled out detachment of boundary layer.
11 cl, 6 dwg
| Title |
Year |
Author |
Number |
| AIRCRAFT COUNTER ROTATION GAS-TURBINE ENGINE WITH COMPRESSOR WITH HIGH COMMON DEGREE OF PRESSURE RISE |
2003 |
- Seda Dzhordzh F.
- Danbar Lorens V.
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- Brauehr Dzhon S.
- Dzhonson Dzhejms E.
|
RU2302545C2 |
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2002 |
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- Danbar Lorens V.
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- Brauehr Dzhon S.
- Dzhonson Dzhejms E.
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- Shtajnmetts Gregori T.
|
RU2295046C2 |
| GAS TURBINE ENGINE WITH A RADIAL DIFFUSER AND A SHORT-TERM MEDIUM PART |
2013 |
- Charron Richard K.
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|
RU2631181C2 |
| CONTINUOUS TRANSIENT CHANNEL BETWEEN HIGH-PRESSURE TURBINE AND LOW-PRESSURE TURBINE OF DOUBLE-FLOW AIRCRAFT ENGINE |
2011 |
- Gladkov Jurij Igorevich
- Baranovskij Boris Viktorovich
|
RU2484264C2 |
| GEAR DRIVE SYSTEM OF GAS TURBINE ENGINE FAN AND GAS TURBINE ENGINE CONTAINING SUCH SYSTEM |
2013 |
|
RU2608511C2 |
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2005 |
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|
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| INJECTOR HEAD FOR GAS TURBINE ENGINE CONTAINING PRIMARY FUEL CIRCUIT AROUND SECONDARY FUEL CIRCUIT |
2019 |
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- Bernard, Clement, Yves, Emile
- Loval, Sebastien, Christophe
|
RU2798404C2 |
| SWIRLER FOR MIXING FUEL WITH AIR IN COMBUSTION ENGINE |
2017 |
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|
RU2716951C1 |
| GAS TURBINE ENGINE (VERSIONS) |
2014 |
- Finneran Dzhon U.
- Graber Deril Dzh.
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- Munshi Mrinal
- Porter Mettyu R.
- Shtejman Evgenij P.
|
RU2639921C2 |
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2003 |
- Kertli Kevin
- Gratsiozi Paolo
|
RU2331776C2 |
