Inventor · disambiguated record
Etienne Fage
Also filed as: FAGE ETIENNE
15 granted patents·511 citations·filing 1977–1997
95Inventor score
Top patents by PatentIndex Score
15 records- 0188US4424669ASafety device for thrust reverser associated with the jet engine of an aircraftFAGE ETIENNE·Filed 1982·Granted Jan 10, 1984·52 cites·7 claims
- 0287US4422605AReverser for jet engineASTECH SOC·Filed 1981·Granted Dec 27, 1983·46 cites·5 claims
- 0386US5775639AThrust reverser with pivoting doors which can move in translationFiled 1995·Granted Jul 7, 1998·54 cites·29 claims
- 0483US4966327AJet engine provided with a thrust reverserDEE HOWARD CO·Filed 1988·Granted Oct 30, 1990·37 cites·19 claims
- 0582US4212442AThrust reverserASTECH SOC·Filed 1978·Granted Jul 15, 1980·34 cites·9 claims
- 0681US5211008AGas ejection nozzle for a jet engine and a jet engine fitted with this nozzle, in particular an engine of the separate flow typeCONCEPTION AERONAUTIQUE DU SUD·Filed 1991·Granted May 18, 1993·42 cites·11 claims
- 0781US4182501AThrust reverser for jet engine forming active extension of jet tubeASTECH·Filed 1978·Granted Jan 8, 1980·42 cites·6 claims
- 0879US5097661AJet engine having a planar exit openingDEE HOWARD CO·Filed 1989·Granted Mar 24, 1992·34 cites·24 claims
- 0977US5310117AJet engine provided with a thrust reverserDEE HOWARD CO·Filed 1993·Granted May 10, 1994·38 cites·2 claims
- 1075US4129269ASingle-skin thrust reverser for aircraft jet enginesASTECH·Filed 1977·Granted Dec 12, 1978·26 cites·6 claims
- 1171US4362015ADouble jet gas turbine engine equipped with a thrust reverserASTECH·Filed 1980·Granted Dec 7, 1982·24 cites·11 claims
- 1269US5192023AJet engine provided with a thrust reverserDEE HOWARD CO·Filed 1990·Granted Mar 9, 1993·30 cites·1 claims
- 1368US4860956AThrust reverser for aircraft jet engine and aircraft engine equipped with said thrust reverserDEE HOWARD CO·Filed 1987·Granted Aug 29, 1989·22 cites·9 claims
- 1455US5956939ABypass jet engine with confluent nozzle, rotating members which control the bypass air flow and a thrust reverser which controls the variable exhaust areaFiled 1997·Granted Sep 28, 1999·22 cites·11 claims
- 1540US4930308ADouble-flow turboshaft engine with variable confluent nozzleDEE HOWARD CO·Filed 1989·Granted Jun 5, 1990·8 cites·9 claims
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