Inventor · disambiguated record
Guy Lapergue
Also filed as: LAPERGUE GUY · LAPERGUE GUY J · LAPERGUE GUY J-L · LAPERGUE GUY JEAN-LOUIS
18 granted patents·190 citations·filing 1986–2005
94Inventor score
Top patents by PatentIndex Score
18 records- 0178US7213393B2Device for supplying cooling air to exhaust nozzle flapsSNECMA MOTEURS·Filed 2005·Granted May 8, 2007·14 cites·19 claims
- 0274US6966189B2System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamberSNECMA MOTEURS·Filed 2004·Granted Nov 22, 2005·16 cites·10 claims
- 0366US4730453AAfterburner fuel injection systemSNECMA·Filed 1986·Granted Mar 15, 1988·27 cites·8 claims
- 0462US6327846B1Universal-joint vectoring system for a turbojet-engine exhaust nozzleSNECMA MOTEURS·Filed 2000·Granted Dec 11, 2001·16 cites·8 claims
- 0561US6360527B1Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ringSNECMA MOTEURS·Filed 2000·Granted Mar 26, 2002·16 cites·5 claims
- 0657US7322180B2Turbo-jet engine with fan integral with a drive shaft supported by first and second bearingsSNECMA MOTEURS·Filed 2004·Granted Jan 29, 2008·12 cites·14 claims
- 0756US7938230B2Device for lubricating a component in an assembly of partsSNECMA·Filed 2005·Granted May 10, 2011·1 cites·10 claims
- 0853US7322181B2Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearingSNECMA MOTEURS·Filed 2005·Granted Jan 29, 2008·4 cites·19 claims
- 0951US7296397B2Ventilation system for a convergent divergent exhaust nozzleSNECMA MOTEURS·Filed 2004·Granted Nov 20, 2007·10 cites·9 claims
- 1049US4724671ADevice for connecting a burner ring or flame holder to an afterburner duct of a turbojet engineSNECMA·Filed 1986·Granted Feb 16, 1988·12 cites·9 claims
- 1145US6993914B2Convergent-divergent turbojet nozzleSNECMA MOTEURS·Filed 2004·Granted Feb 7, 2006·7 cites·11 claims
- 1243US6375095B1Swiveling, converging-diverging, axisymmetric exhaust nozzleSNECMA·Filed 2000·Granted Apr 23, 2002·10 cites·5 claims
- 1342US7340882B2Turbomachine with means for axial retention of the rotorSNECMA MOTEURS·Filed 2005·Granted Mar 11, 2008·2 cites·11 claims
- 1440US7520135B2Variable-section turbomachine nozzleSNECMA·Filed 2005·Granted Apr 21, 2009·0 cites·11 claims
- 1540US5676312ASeal for a variable geometry nozzleSNECMA·Filed 1995·Granted Oct 14, 1997·17 cites·20 claims
- 1640US5494221AVariable geometry turbojet engine exhaust nozzleSNECMA·Filed 1995·Granted Feb 27, 1996·13 cites·10 claims
- 1736US6349539B1Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzleSNECMA MOTEURS·Filed 2000·Granted Feb 26, 2002·3 cites·3 claims
- 1833US5359851AVariable geometry exhaust nozzle for a turbojet engineSNECMA·Filed 1993·Granted Nov 1, 1994·10 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →