Lapergue; Guy

Patent Applications and Registrations

Patent applications and USPTO patent grants for Lapergue; Guy.The latest application filed is for "variable-section turbomachine nozzle".

Company Profile

0.9.9

Lapergue; Guy - Rubelles FR

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Device for lubricating a component in an assembly of parts Grant 7,938,230 - Servant , et al. May 10, 2	2011-05-10
Variable-section turbomachine nozzle Grant 7,520,135 - Dakowski , et al. April 21, 2	2009-04-21
Turbomachine with means for axial retention of the rotor Grant 7,340,882 - Lapergue , et al. March 11, 2	2008-03-11
Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing Grant 7,322,181 - Lapergue , et al. January 29, 2	2008-01-29
Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings Grant 7,322,180 - Lapergue , et al. January 29, 2	2008-01-29
Ventilation system for a convergent divergent exhaust nozzle Grant 7,296,397 - Curtelin , et al. November 20, 2	2007-11-20
Device for supplying cooling air to exhaust nozzle flaps Grant 7,213,393 - Lapergue , et al. May 8, 2	2007-05-08
Variable-section turbomachine nozzle App 20060090470 - Dakowski; Mathieu ; et al.	2006-05-04
Convergent-divergent turbojet nozzle Grant 6,993,914 - Prouteau , et al. February 7, 2	2006-02-07
Turbomachine with means for axial retention of the rotor App 20050276683 - Lapergue, Guy ; et al.	2005-12-15
System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber Grant 6,966,189 - Lapergue , et al. November 22, 2	2005-11-22
Device for lubricating a component in an assembly of parts App 20050247526 - Servant, Regis ; et al.	2005-11-10
Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing App 20050241290 - Lapergue, Guy ; et al.	2005-11-03
Device for supplying cooling air to exhaust nozzle flaps App 20050210864 - Lapergue, Guy ; et al.	2005-09-29
Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings App 20050172608 - Lapergue, Guy ; et al.	2005-08-11
Ventilation system for a convergent divergent exhaust nozzle App 20050091964 - Curtelin, Raphael ; et al.	2005-05-05
Convergent-divergent turbojet nozzle App 20050060984 - Prouteau, Jackie ; et al.	2005-03-24
System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber App 20050005607 - Lapergue, Guy ; et al.	2005-01-13

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