Inventor
MONS CLAUDE MARCEL
FR28 patents
⚠️ This page may combine multiple inventors who share the name “MONS CLAUDE MARCEL”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SNECMA
11 patentsUS7857581B2Dec 28, 2010
Annular wiper for a sealing labyrinth, and its method of manufacture
SNECMA30 citations91
US7695248B2Apr 13, 2010
Method of making a rim situated at the free end of a blade, a blade obtained by the method, and a turbomachine fitted with the blade
SNECMA28 citations91
US7510778B2Mar 31, 2009
Part for protecting the leading edge of a blade
SNECMA38 citations91
US6135712AOct 24, 2000
Turbomachine with mutual braking of concentric shafts
SNECMA23 citations84
US7836572B2Nov 23, 2010
Method of making a wiper for a sealing labyrinth, and a thermomechanical part and a turbomachine including such a wiper
SNECMA20 citations82
US7553130B1Jun 30, 2009
Nozzle ring adhesive bonded blading for aircraft engine compressor
SNECMA6 citations68
US7934367B2May 3, 2011
Method and device for reducing the speed in the event of breakage of a gas turbine engine turbine shaft
SNECMA6 citations63
US7448280B2Nov 11, 2008
Method for evaluating the fatigue strength of welded joints
SNECMA4 citations63
US7597538B2Oct 6, 2009
Thermostructural turbomachine part that is circularly symmetrical about a longitudinal axis, the part including an annular wiper, and a method of manufacture
SNECMA6 citations61
US7685712B2Mar 30, 2010
Method for repairing a rubbing surface of a turbomachine variable-pitch blade
SNECMA6 citations60
US7625176B2Dec 1, 2009
Plain bearing between two parts which are movable with respect to each other
SNECMA1 citations45
MONS CLAUDE MARCEL
5 patentsUS8209834B2Jul 3, 2012
Centering a part inside a shaft
MONS CLAUDE MARCEL26 citations89
US8136999B2Mar 20, 2012
Turbomachine shaft guidance
MONS CLAUDE MARCEL31 citations89
US8561386B2Oct 22, 2013
Wall cooling device
MONS CLAUDE MARCEL12 citations83
US8448446B2May 28, 2013
Actuating device, bypass air bleed system equipped therewith, and turbojet engine comprising these
MONS CLAUDE MARCEL5 citations72
US8322125B2Dec 4, 2012
Turbo-engine compressor tip comprising de-icing means
MONS CLAUDE MARCEL0 citations42
SNECMA MOTEURS
4 patentsUS6336844B1Jan 8, 2002
Method and machine for the ultrasonic peening of parts on a wheel
SNECMA MOTEURS50 citations88
US6289705B1Sep 18, 2001
Method for the ultrasonic peening of large sized annular surfaces of thin parts
SNECMA MOTEURS49 citations88
US7147434B2Dec 12, 2006
Nozzle ring with adhesive bonded blading for aircraft engine compressor
SNECMA MOTEURS32 citations87
US6837085B2Jan 4, 2005
Transverse ultrasound peening of blades on a rotor
SNECMA MOTEURS18 citations82
BART JACQUES RENE
2 patentsFERRER LAURENT
2 patentsUS8662838B2Mar 4, 2014
Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
FERRER LAURENT4 citations71
US8888448B2Nov 18, 2014
Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method
FERRER LAURENT3 citations61
LEBRET YANN PASCAL RAYMOND RENE
2 patentsUS8607456B1Dec 17, 2013
Method of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zone
LEBRET YANN PASCAL RAYMOND RENE3 citations57
US8256116B2Sep 4, 2012
Method of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zone
LEBRET YANN PASCAL RAYMOND RENE0 citations47