Inventor
MAZEAUD GEORGES
FR23 patents
⚠️ This page may combine multiple inventors who share the name “MAZEAUD GEORGES”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SNECMA
19 patentsUS5524430AJun 11, 1996
Gas-turbine engine with detachable combustion chamber
SNECMA100 citations96
US4805398AFeb 21, 1989
Turbo-machine with device for automatically controlling the rate of flow of turbine ventilation air
SNECMA107 citations93
US5163285ANov 17, 1992
Cooling system for a gas turbine
SNECMA75 citations92
US5052176AOct 1, 1991
Combination turbojet-ramjet-rocket propulsion system
SNECMA74 citations91
US4500143AFeb 19, 1985
Means for controlling clearance in an intershaft bearing journal of a multi-spool gas turbine
SNECMA39 citations91
US7506499B2Mar 24, 2009
Turbofan jet engine with ancillaries distribution support
SNECMA22 citations90
US4378197AMar 29, 1983
Inter-shaft bearing for multibody turbojet engines with damping by a film of oil
SNECMA38 citations90
US5347807ASep 20, 1994
Combined jet engine with RAM jet and turbojet
SNECMA24 citations89
US5806793ASep 15, 1998
Cooling device for a turboshaft engine on an aircraft
SNECMA27 citations88
US5193980AMar 16, 1993
Hollow turbine blade with internal cooling system
SNECMA51 citations88
US5410870AMay 2, 1995
Aircraft engine layout
SNECMA24 citations87
US6129509AOct 10, 2000
Particle traps for turbo-prop engine
SNECMA16 citations80
US7543442B2Jun 9, 2009
Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems
SNECMA18 citations77
US5275532AJan 4, 1994
Axial compressor and method of carrying out maintenance on the axial compressor
SNECMA10 citations71
US5284014AFeb 8, 1994
Turbojet-ramjet hypersonic aircraft engine
SNECMA19 citations70
US5343695ASep 6, 1994
Combined jet engine provided with means for switching between two operating states
SNECMA9 citations63
US7805949B2Oct 5, 2010
Device for supporting and housing auxiliaries in a bypass turbojet
SNECMA4 citations61
US5305600AApr 26, 1994
Propulsion engine
SNECMA5 citations57
US7461813B2Dec 9, 2008
Air input device for a turboprop engine
SNECMA0 citations42
SNECMA MOTEURS
3 patentsUS6474596B1Nov 5, 2002
Suspension system with intrinsic safety features for aircraft powerplants
SNECMA MOTEURS47 citations90
US7007890B2Mar 7, 2006
Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position
SNECMA MOTEURS15 citations77
US7100869B2Sep 5, 2006
Turboprop carrier structure and an assembly including such a carrier structure
SNECMA MOTEURS6 citations62