P

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 patents
US4639284AJan 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

IND AERO SOC NAT

1 patent