Jean-Romain BIHEL

Person

Le Rove, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Hydroelastic damper, and an aircraft
- Patent number 11,518,503
- Issue date Dec 6, 2022
- Airbus Helicopters
- Jean-Romain Bihel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Hydro-elastic damper and an aircraft
- Patent number 11,161,601
- Issue date Nov 2, 2021
- Airbus Helicopters
- Jean-Romain Bihel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Lead-lag damper integrated inside a blade of a rotor
- Patent number 11,142,307
- Issue date Oct 12, 2021
- Airbus Helicopters
- Stephane Mazet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotorcraft having a rotary wing and at least two propellers, and a...
- Patent number 10,836,482
- Issue date Nov 17, 2020
- Airbus Helicopters
- Jacques Gaffiero
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Servo control, rotor and aircraft
- Patent number 10,738,803
- Issue date Aug 11, 2020
- Airbus Helicopters
- Clement Coiec
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Control member, a rotary wing aircraft, and a method
- Patent number 10,737,775
- Issue date Aug 11, 2020
- Airbus Helicopters
- Jean-Romain Bihel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Electric control member, a rotary wing aircraft, and a method
- Patent number 10,518,870
- Issue date Dec 31, 2019
- Airbus Helicopters
- Marc Salesse-Lavergne
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adaptive flight control system for the yaw and thrust flight contro...
- Patent number 10,507,905
- Issue date Dec 17, 2019
- Airbus Helicopters
- Jean-Romain Bihel
- G05 - CONTROLLING REGULATING
Information Patent Grant
Ball-bearing control cable, a mechanical system, and an aircraft
- Patent number 9,950,783
- Issue date Apr 24, 2018
- Airbus Helicopters
- Jean-Romain Bihel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Servo-control and an aircraft having such a servo-control
- Patent number 9,732,769
- Issue date Aug 15, 2017
- Airbus Helicopters
- Jean-Romain Bihel
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Pressure-balance valve for balancing fluid feed to actuator cylinde...
- Patent number 9,670,940
- Issue date Jun 6, 2017
- Airbus Helicopters
- Thibaut Marger
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Double hydraulic valve of a servo-control for feathering the blades...
- Patent number 9,624,946
- Issue date Apr 18, 2017
- Airbus Helicopters
- Jean-Romain Bihel
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Aircraft hydraulic system comprising at least one servo-control, an...
- Patent number 9,428,262
- Issue date Aug 30, 2016
- Airbus Helicopters
- Jean-Romain Bihel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hydraulic actuator with a limit force detector device
- Patent number 9,115,733
- Issue date Aug 25, 2015
- Airbus Helicopters
- Jean-Romain Bihel
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Method of determining the static force developed by a servo-control
- Patent number 9,115,735
- Issue date Aug 25, 2015
- Airbus Helicopters
- Jean-Romain Bihel
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL

Patents Applicationslast 30 patents

Information Patent Application
HYDROELASTIC DAMPER, AND AN AIRCRAFT
- Publication number 20190367163
- Publication date Dec 5, 2019
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTORCRAFT HAVING A ROTARY WING AND AT LEAST TWO PROPELLERS, AND A...
- Publication number 20190329881
- Publication date Oct 31, 2019
- AIRBUS HELICOPTERS
- Jacques GAFFIERO
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HYDRO-ELASTIC DAMPER AND AN AIRCRAFT
- Publication number 20190300163
- Publication date Oct 3, 2019
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SERVO CONTROL, ROTOR AND AIRCRAFT
- Publication number 20190178266
- Publication date Jun 13, 2019
- AIRBUS HELICOPTERS
- Clement COIEC
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Application
CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD
- Publication number 20180148167
- Publication date May 31, 2018
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
LEAD-LAG DAMPER INTEGRATED INSIDE A BLADE OF A ROTOR
- Publication number 20180105265
- Publication date Apr 19, 2018
- AIRBUS HELICOPTERS
- Stephane MAZET
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTRIC CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD
- Publication number 20180099739
- Publication date Apr 12, 2018
- AIRBUS HELICOPTERS
- Marc SALESSE-LAVERGNE
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ADAPTIVE FLIGHT CONTROL SYSTEM FOR THE YAW AND THRUST FLIGHT CONTRO...
- Publication number 20170144747
- Publication date May 25, 2017
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
BALL-BEARING CONTROL CABLE, A MECHANICAL SYSTEM, AND AN AIRCRAFT
- Publication number 20170066526
- Publication date Mar 9, 2017
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SERVO-CONTROL AND AN AIRCRAFT HAVING SUCH A SERVO-CONTROL
- Publication number 20160195113
- Publication date Jul 7, 2016
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT HYDRAULIC SYSTEM COMPRISING AT LEAST ONE SERVO-CONTROL, AN...
- Publication number 20150298796
- Publication date Oct 22, 2015
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PRESSURE-BALANCE VALVE FOR BALANCING FLUID FEED TO ACTUATOR CYLINDE...
- Publication number 20150292527
- Publication date Oct 15, 2015
- AIRBUS HELICOPTERS
- Thibaut MARGER
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DOUBLE HYDRAULIC VALVE OF A SERVO-CONTROL FOR FEATHERING THE BLADES...
- Publication number 20150176612
- Publication date Jun 25, 2015
- AIRBUS HELICOPTERS
- Jean-Romain BIHEL
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD OF DETERMINING THE STATIC FORCE DEVELOPED BY A SERVO-CONTROL
- Publication number 20120303296
- Publication date Nov 29, 2012
- EUROCOPTER
- Jean-Romain Bihel
- G01 - MEASURING TESTING
Information Patent Application
SERVO-CONTROL PROVIDED WITH A LIMIT FORCE DETECTOR DEVICE
- Publication number 20120011840
- Publication date Jan 19, 2012
- EUROCOPTER
- Jean-Romain Bihel
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL

Jean-Romain BIHEL

Person

Patents Grantslast 30 patents

Hydroelastic damper, and an aircraft

Hydro-elastic damper and an aircraft

Lead-lag damper integrated inside a blade of a rotor

Rotorcraft having a rotary wing and at least two propellers, and a...

Servo control, rotor and aircraft

Control member, a rotary wing aircraft, and a method

Electric control member, a rotary wing aircraft, and a method

Adaptive flight control system for the yaw and thrust flight contro...

Ball-bearing control cable, a mechanical system, and an aircraft

Servo-control and an aircraft having such a servo-control

Pressure-balance valve for balancing fluid feed to actuator cylinde...

Double hydraulic valve of a servo-control for feathering the blades...

Aircraft hydraulic system comprising at least one servo-control, an...

Hydraulic actuator with a limit force detector device

Method of determining the static force developed by a servo-control

Patents Applicationslast 30 patents

HYDROELASTIC DAMPER, AND AN AIRCRAFT

ROTORCRAFT HAVING A ROTARY WING AND AT LEAST TWO PROPELLERS, AND A...

HYDRO-ELASTIC DAMPER AND AN AIRCRAFT

SERVO CONTROL, ROTOR AND AIRCRAFT

CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD

LEAD-LAG DAMPER INTEGRATED INSIDE A BLADE OF A ROTOR

ELECTRIC CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD

ADAPTIVE FLIGHT CONTROL SYSTEM FOR THE YAW AND THRUST FLIGHT CONTRO...

BALL-BEARING CONTROL CABLE, A MECHANICAL SYSTEM, AND AN AIRCRAFT

SERVO-CONTROL AND AN AIRCRAFT HAVING SUCH A SERVO-CONTROL

AIRCRAFT HYDRAULIC SYSTEM COMPRISING AT LEAST ONE SERVO-CONTROL, AN...

PRESSURE-BALANCE VALVE FOR BALANCING FLUID FEED TO ACTUATOR CYLINDE...

DOUBLE HYDRAULIC VALVE OF A SERVO-CONTROL FOR FEATHERING THE BLADES...

METHOD OF DETERMINING THE STATIC FORCE DEVELOPED BY A SERVO-CONTROL

SERVO-CONTROL PROVIDED WITH A LIMIT FORCE DETECTOR DEVICE