loadpatents
name:-0.015318870544434
name:-0.015136003494263
name:-0.0032880306243896
BOUCHY; Gael Patent Filings

BOUCHY; Gael

Patent Applications and Registrations

Patent applications and USPTO patent grants for BOUCHY; Gael.The latest application filed is for "production in composite material of a lobed structure of a flow mixer".

Company Profile
0.10.11
  • BOUCHY; Gael - MOISSY-CRAMAYEL FR
  • Bouchy; Gael - La Chapelle Iger FR
  • Bouchy, Gael - La Chappelle Iger 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
PatentDate
Production In Composite Material Of A Lobed Structure Of A Flow Mixer
App 20200254698 - Kind Code
2020-08-13
Device for lubricating a component in an assembly of parts
Grant 7,938,230 - Servant , et al. May 10, 2
2011-05-10
Tension decoupler device
Grant 7,452,152 - Bouchy , et al. November 18, 2
2008-11-18
Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement
Grant 7,448,808 - Bouchy , et al. November 11, 2
2008-11-11
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
Tension decoupler device
Grant 7,318,685 - Bouchy , et al. January 15, 2
2008-01-15
Turbine engine with an uncoupling device, uncoupling device and fusible screw for the uncoupling device
Grant 7,316,538 - Bouchy , et al. January 8, 2
2008-01-08
Breakable coupling system for a turbojet fan shaft
Grant 7,237,959 - Bouchy , et al. July 3, 2
2007-07-03
Tension Decoupler Device
App 20070081852 - BOUCHY; Gael ;   et al.
2007-04-12
Turbomachine with a decoupling device common to first and second bearings of its drive shaft, compressor comprising the decoupling device and decoupling device
Grant 7,195,444 - Brault , et al. March 27, 2
2007-03-27
Turbomachine with a decoupling device common to first and second bearings of its drive shaft, compressor comprising the decoupling device and decoupling device
App 20060110244 - Brault; Michel Gilbert Roland ;   et al.
2006-05-25
Turbine engine with an uncoupling device, uncoupling device and fusible screw for the uncoupling device
App 20060087396 - Bouchy; Gael ;   et al.
2006-04-27
Turbomachine with means for axial retention of the rotor
App 20050276683 - Lapergue, Guy ;   et al.
2005-12-15
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
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
Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement
App 20050129343 - Bouchy, Gael ;   et al.
2005-06-16
Breakable coupling system for a turbojet fan shaft
App 20050117828 - Bouchy, Gael ;   et al.
2005-06-02
Tension decoupler device
App 20040063504 - Bouchy, Gael ;   et al.
2004-04-01

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