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*
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1949-08-24 |
1953-08-18 |
Westinghouse Electric Corp |
Gas turbine engine apparatus designed to burn wet pulverized fuel
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*
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1953-02-10 |
1961-10-10 |
Rolls Royce |
Cooling means for forked exhaust ducts of gas turbine engines
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*
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1954-04-09 |
1958-11-25 |
Douglas Aircraft Co Inc |
Fuel supply means for combustion apparatus
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*
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1955-02-24 |
1960-07-12 |
Thompson Ramo Wooldridge Inc |
Air atomizing spray bar
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1956-07-03 |
1960-06-28 |
Thompson Ramo Wooldridge Inc |
Umbrella spraybar afterburner arrangement
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*
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1972-02-17 |
1973-06-18 |
Gen Electric |
Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air
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*
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1975-12-24 |
1978-01-31 |
General Electric Company |
Low pressure fuel injection system
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*
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1979-12-13 |
1981-06-19 |
Snecma |
Dispositif d'injection pour chambre a combustion de moteur a turbine
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CH666340A5
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1985-05-29 |
1988-07-15 |
Bbc Brown Boveri & Cie |
Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
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1987-12-14 |
1990-09-11 |
Sundstrand Corporation |
Fuel injectors for turbine engines
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1987-12-21 |
1989-01-17 |
United Technologies Corporation |
Augmentor pilot
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(en)
*
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1988-03-18 |
1989-12-19 |
General Electric Company |
Fuel spraybar
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EP0577862B1
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*
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1992-07-03 |
1997-03-12 |
Abb Research Ltd. |
Nachbrenner
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CA2779199C
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*
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2009-11-16 |
2015-08-04 |
Bell Helicopter Textron Inc. |
Dual-path fluid injection jet
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2012-06-22 |
2017-05-02 |
Delavan Inc. |
Active purge mechanism with backflow preventer for gas turbine fuel injectors
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2013-10-07 |
2020-04-08 |
United Technologies Corporation |
Air cooled fuel injector for a turbine engine
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EP3109550B1
(en)
*
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2015-06-19 |
2019-09-04 |
Rolls-Royce Corporation |
Turbine cooled cooling air flowing through a tubular arrangement
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