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1976-11-29 |
1979-04-17 |
United Technologies Corporation |
Lobe mixer for gas turbine engine
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1979-11-01 |
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1980-09-26 |
1983-08-30 |
United Technologies Corporation |
Lobe mixer for gas turbine engine
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1983-05-05 |
1985-10-22 |
Rolls-Royce Limited |
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1983-09-14 |
1987-12-23 |
Rolls Royce |
Exhaust mixer for turbofan aeroengine
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1999-03-05 |
2000-09-14 |
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2000-02-24 |
2002-07-02 |
Honeywell International, Inc. |
Deep lobed deswirling diffuser tailpipe
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2001-07-18 |
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General Electric Company |
Serrated fan blade
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2002-12-07 |
2006-03-28 |
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Jet nozzle mixer
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2002-02-06 |
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ジェット噴流用ローブミキサ
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2003-11-28 |
Mitsubishi Heavy Ind Ltd |
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Tuyere de turbomachine a motifs a reduction de bruit de jet
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Snecma Propulsion Solide Sa |
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United Technologies Corporation |
Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts
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2006-06-19 |
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Snecma |
Melangeur a lobes munis de motifs pour tuyere a flux confluents de turbomachine
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2006-06-26 |
2008-10-24 |
Snecma Sa |
Capot pour tuyere de turbomachine muni de motifs triangulaires a point d'inflexion pour reduire le bruit de jet
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2007-02-12 |
2009-05-08 |
Snecma Propulsion Solide Sa |
Procede de fabrication d'une structure a lobes de melangeur de flux en cmc pour moteur aeronautique a turbine de gaz.
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2007-07-09 |
2011-12-27 |
General Electric Company |
Rotary airfoils and method for fabricating same
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2007-09-28 |
2009-04-03 |
Snecma Sa |
Capot pour tuyere de turbomachine a motifs a reduction de bruit de jet
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2009-11-30 |
2011-06-02 |
Honeywell International Inc. |
Turbofan gas turbine engine aerodynamic mixer
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2010-04-29 |
2014-01-28 |
Pratt & Whitney Canada Corp. |
Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs
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