Inventor
BART JACQUES RENE
FR19 patents
⚠️ This page may combine multiple inventors who share the name “BART JACQUES RENE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SNECMA
9 patentsUS7552591B2Jun 30, 2009
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
SNECMA79 citations97
US8051952B2Nov 8, 2011
Deoiling device and turbomachine comprising this device
SNECMA16 citations83
US7828521B2Nov 9, 2010
Turbine module for a gas-turbine engine
SNECMA8 citations83
US7596938B2Oct 6, 2009
Turbomachine with a deflector system
SNECMA8 citations81
US7661928B2Feb 16, 2010
Device for rotationally locking a clamping nut for a component on a shaft, clamping nut and shaft comprising it, and aircraft engine equipped therewith
SNECMA8 citations76
US10036277B2Jul 31, 2018
Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing device
SNECMA2 citations72
US7743598B2Jun 29, 2010
Sealing system for the rear lubricating chamber of a jet engine
SNECMA2 citations62
US7507072B2Mar 24, 2009
Turbine module for a gas-turbine engine with rotor that includes a monoblock body
SNECMA2 citations62
US9366183B2Jun 14, 2016
System for attaching a turbojet engine spinner
SNECMA2 citations57
BART JACQUES RENE
8 patentsUS8312702B2Nov 20, 2012
Oil recovery device
BART JACQUES RENE7 citations83
US8127525B2Mar 6, 2012
System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine
BART JACQUES RENE8 citations83
US8172509B2May 8, 2012
Device for detecting breakage of a turbomachine shaft
BART JACQUES RENE7 citations82
US9429030B2Aug 30, 2016
Device for locking a root of a rotor blade
BART JACQUES RENE2 citations62
US8182202B2May 22, 2012
Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewith
BART JACQUES RENE5 citations62
US8161727B2Apr 24, 2012
System providing braking in a gas turbine engine in the event of the turbine shaft breaking
BART JACQUES RENE4 citations62
US8157506B2Apr 17, 2012
Device for supplying ventilation air to the low pressure blades of a gas turbine engine
BART JACQUES RENE3 citations62
US8057160B2Nov 15, 2011
Device for limiting turbine overspeed in a turbomachine
BART JACQUES RENE6 citations62