GL

Guy Lapergue

SM Snecma Moteurs: 9 patents #5 of 501Top 1%
SN Snecma: 2 patents #478 of 1,717Top 30%
📍 Le Mée-sur-Seine, FR: #5 of 89 inventorsTop 6%
Overall (All Time): #258,799 of 4,157,543Top 7%
18
Patents All Time

Issued Patents All Time

Showing 1–18 of 18 patents

Patent #TitleCo-InventorsDate
7938230 Device for lubricating a component in an assembly of parts Regis Eugene Henri Servant, Gael Bouchy 2011-05-10
7520135 Variable-section turbomachine nozzle Mathieu Dakowski, Romain Nicolas Lunel, Guillaume Sevi 2009-04-21
7340882 Turbomachine with means for axial retention of the rotor Regis Servant, Gael Bouchy, Alain Baum 2008-03-11
7322181 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing Regis Servant, Gael Bouchy 2008-01-29
7322180 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings Regis Servant, Gael Bouchy 2008-01-29
7296397 Ventilation system for a convergent divergent exhaust nozzle Raphael Curtelin, Marc Doussinault, Didier Noël Durand 2007-11-20
7213393 Device for supplying cooling air to exhaust nozzle flaps Raphael Curtelin, Didier Feder 2007-05-08
6993914 Convergent-divergent turbojet nozzle Jackie Raymond Julien Prouteau, Raphael Curtelin, Didier Feder 2006-02-07
6966189 System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber Guillaume Sevi, Jacques Roche 2005-11-22
6375095 Swiveling, converging-diverging, axisymmetric exhaust nozzle Didier Feder, Bertrand Pierre Renaud Monville, Laurent Claude Patrick Salperwick 2002-04-23
6360527 Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring Didier Feder, Bertrand Pierre Renaud Monville, Laurent Claude Patrick Salperwyck 2002-03-26
6349539 Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzle Didier Feder, Daniel Kettler, Bertrand Pierre Renaud Monville, Jacky Naudet, Laurent Claude Patrick Salperwyck 2002-02-26
6327846 Universal-joint vectoring system for a turbojet-engine exhaust nozzle Didier Feder 2001-12-11
5676312 Seal for a variable geometry nozzle Claude Lejars 1997-10-14
5494221 Variable geometry turbojet engine exhaust nozzle Fabrice Michel Olivier Cot 1996-02-27
5359851 Variable geometry exhaust nozzle for a turbojet engine Pierre A. L. M. Bannerot, Eric Maingre, Xavier J. Pasquali, Jean-Claude H. Reghezza 1994-11-01
4730453 Afterburner fuel injection system Rene A. Benoist, Jacques A. Legueux 1988-03-15
4724671 Device for connecting a burner ring or flame holder to an afterburner duct of a turbojet engine Marc G. Loubet, Marcel R. Soligny 1988-02-16