Inventor
MOUILLE RENE L
25 patents
⚠️ This page may combine multiple inventors who share the name “MOUILLE RENE L”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
AEROSPATIALE
24 patentsUS4639284AJan 27, 1987
Process for manufacturing a variable pitch multi-blade propeller by molding resin-impregnated fails around a preform
AEROSPATIALE42 citations94
US4626172ADec 2, 1986
Variable-pitch multi-blade propeller incorporating individually dismountable blades made of composite materials, process for manufacturing such blades and blades thus produced
AEROSPATIALE95 citations94
US4626173ADec 2, 1986
Variable-pitch multi-blade propeller incorporating individually dismountable blades made of composite materials, process for manufacturing such blades and blades thus produced
AEROSPATIALE61 citations94
US4255084AMar 10, 1981
Device for damping the vibrations of a rotary-wing aircraft rotor
AEROSPATIALE64 citations93
US5316442AMay 31, 1994
Articulated rotor head for gyroplanes
AEROSPATIALE22 citations92
US5242130ASep 7, 1993
Method and device for the reduction of the oscillations of a divergent nature of the fuselage of a helicopter
AEROSPATIALE32 citations92
US5228640AJul 20, 1993
Device for the elastic coupling between two parts, and aircraft with rotating wings comprising said device
AEROSPATIALE50 citations92
US4811627AMar 14, 1989
Main transmission gearbox for a twin-engined helicopter
AEROSPATIALE49 citations92
US4504193AMar 12, 1985
Helicopter rotor with articulation means integrated in the root of the blade
AEROSPATIALE29 citations92
US4431148AFeb 14, 1984
Simplified anti-resonant suspension device for a helicopter
AEROSPATIALE32 citations92
US4304525ADec 8, 1981
Helicopter rotor
AEROSPATIALE44 citations92
US4809931AMar 7, 1989
Directional and stabilizing device having a faired and slanted antitorque rotor and a disymmetric "V" empennage, and a helicopter equipped with such a device
AEROSPATIALE55 citations87
US4458862AJul 10, 1984
Antiresonant suspension device for helicopter
AEROSPATIALE42 citations87
US4273511AJun 16, 1981
Main rotor for a helicopter
AEROSPATIALE42 citations87
US4392781AJul 12, 1983
High performance blade for helicopter rotor
AEROSPATIALE36 citations86
US4732540AMar 22, 1988
Integrated hub-mast and gyroplane rotor head comprising it
AEROSPATIALE24 citations82
US4222709ASep 16, 1980
Variable-pitch rotor, specially for a rotary-wing aircraft
AEROSPATIALE22 citations82
US4281967AAug 4, 1981
Resonator device for damping the vibrations of a rotor of a rotary-wing aircraft
AEROSPATIALE28 citations79
US4458861AJul 10, 1984
Anti-vibratory suspension device for a helicopter
AEROSPATIALE10 citations74
US5007799AApr 16, 1991
Flapping restrainer device for rotorcraft rotor blades, and rotor head comprising said device
AEROSPATIALE16 citations73
US4749339AJun 7, 1988
Integrater hub-mast and gyroplane rotor head comprising it
AEROSPATIALE9 citations72
US4274510AJun 23, 1981
Multi-directional suspension means for rotor aircraft
AEROSPATIALE18 citations72
US4556365ADec 3, 1985
Hub plate for a helicopter rotor, method of manufacturing it, and a helicopter rotor hub equipped with plates
AEROSPATIALE14 citations71
US5242266ASep 7, 1993
Gyrocraft articulated rotor head with intermediate sleeves between hub and blades
AEROSPATIALE1 citations52