JB

Jacques Rene Bart

SN Snecma: 22 patents #17 of 1,717Top 1%
SM Snecma Moteurs: 2 patents #99 of 501Top 20%
SE Safran Aircraft Engines: 1 patents #914 of 1,821Top 55%
Overall (All Time): #146,376 of 4,157,543Top 4%
27
Patents All Time

Issued Patents All Time

Showing 25 most recent of 27 patents

Patent #TitleCo-InventorsDate
10385872 Variable pitch rectifier for a turbomachine compressor comprising two inner rings Nadege Hugon 2019-08-20
10036277 Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing device Antoine Jean-Philippe Beaujard 2018-07-31
9897004 Oil discharge device and turbomachine comprising such a device Amandine Roche, Gerard Philippe Gauthier 2018-02-20
9759088 Device for de-icing a turbomachine separator Olivier Belmonte 2017-09-12
9429030 Device for locking a root of a rotor blade Antoine Jean-Philippe Beaujard 2016-08-30
9366183 System for attaching a turbojet engine spinner Emmanuel Pierre Dimitri Patsouris 2016-06-14
8919133 Double-body gas turbine engine provided with an inter-shaft bearing Didler René André Escure, Ornella Gastineau 2014-12-30
8794922 Assembly between a compressor shaft trunnion and a bevel gear for driving an accessory gearbox of a turbomachine Didier Rene Andre Escure 2014-08-05
8312702 Oil recovery device Serge Rene Morreale, Jean-Luc Soupizon 2012-11-20
8182202 Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewith Didier Rene Andre Escure, Stephane Rousselin 2012-05-22
8172509 Device for detecting breakage of a turbomachine shaft Didier Rene Andre Escure, Cedric Magret, Stephane Rousselin 2012-05-08
8161727 System providing braking in a gas turbine engine in the event of the turbine shaft breaking Didier Rene Andre Escure, Claude Marcel Mons, Stephane Rousselin 2012-04-24
8157506 Device for supplying ventilation air to the low pressure blades of a gas turbine engine Didier Rene Andre Escure, Stephane Rousselin 2012-04-17
8127525 System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine Didier Rene Andre Escure, Claude Marcel Mons, Stephane Rousselin 2012-03-06
8057160 Device for limiting turbine overspeed in a turbomachine Didier Rene Andre Escure, Stephane Rousselin 2011-11-15
8051952 Deoiling device and turbomachine comprising this device Jacky Raphael Michel Derenes, Stephane Rousselin 2011-11-08
7828521 Turbine module for a gas-turbine engine 2010-11-09
7743598 Sealing system for the rear lubricating chamber of a jet engine Stephane Rousselin 2010-06-29
7661928 Device for rotationally locking a clamping nut for a component on a shaft, clamping nut and shaft comprising it, and aircraft engine equipped therewith Laurent Michel Andre Berbiguier 2010-02-16
7596938 Turbomachine with a deflector system Laurent Donatien Behaghel, Stephane Rousselin 2009-10-06
7552591 Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine Bruno Albert Beutin, Patrick Morel 2009-06-30
7507072 Turbine module for a gas-turbine engine with rotor that includes a monoblock body 2009-03-24
7412819 Turbojet architecture with two fans at the front Bruno Albert Beutin, Yann Lebret 2008-08-19
7299621 Three-spool by-pass turbojet with a high by-pass ratio Fabienne Lacorre, Yann Lebret, Vanessa Le Rousseau, Patrick Morel 2007-11-27
7097415 Low-pressure turbine of a turbomachine Bruno Albert Beutin, Philippe Pierre Vincent Bouiller 2006-08-29