Christophe Bourdeau

Person

Toulouse, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Deflector provided with faces with different curvatures for a thrus...
- Patent number 12,012,911
- Issue date Jun 18, 2024
- Airbus Operations (S.A.S.)
- Lauren Davis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Grating for the formation of a reverse flow of an aircraft turbofan...
- Patent number 11,028,801
- Issue date Jun 8, 2021
- Airbus Operations SAS
- Christophe Bourdeau
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet nacelle and method for controlling separation in a turboje...
- Patent number 8,640,986
- Issue date Feb 4, 2014
- Airbus Operations SAS
- Thierry Surply
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Air outlet system for aircraft leading edge
- Patent number 8,434,724
- Issue date May 7, 2013
- Airbus Operations SAS
- Frédéric Chelin
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...
- Publication number 20240418137
- Publication date Dec 19, 2024
- Airbus Operations SAS
- Frédéric CHELIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...
- Publication number 20240360801
- Publication date Oct 31, 2024
- Airbus Operations SAS
- Frédéric CHELIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...
- Publication number 20240360802
- Publication date Oct 31, 2024
- Airbus Operations SAS
- Frédéric CHELIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MO...
- Publication number 20240124148
- Publication date Apr 18, 2024
- AIRBUS OPERATIONS (SAS)
- Frédéric Chelin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEFLECTOR PROVIDED WITH A SPOILER FOR A THRUST REVERSER OF AN AIRCR...
- Publication number 20230340929
- Publication date Oct 26, 2023
- Airbus Operations SAS
- Frédéric CHELIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEFLECTOR PROVIDED WITH FACES WITH DIFFERENT CURVATURES FOR A THRUS...
- Publication number 20230340928
- Publication date Oct 26, 2023
- AIRBUS OPERATIONS (SAS)
- Lauren DAVIS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GRATING FOR THE FORMATION OF A REVERSE FLOW OF AN AIRCRAFT TURBOFAN...
- Publication number 20200025138
- Publication date Jan 23, 2020
- Airbus Operations SAS
- Christophe BOURDEAU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR OUTLET SYSTEM FOR AIRCRAFT LEADING EDGE
- Publication number 20100327120
- Publication date Dec 30, 2010
- Airbus Operations SAS
- Frederic Chelin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
TURBOJET NACELLE AND METHOD FOR CONTROLLING SEPARATION IN A TURBOJE...
- Publication number 20090140104
- Publication date Jun 4, 2009
- AIRBUS FRANCE
- Thierry Surply
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Christophe Bourdeau

Person

Patents Grantslast 30 patents

Deflector provided with faces with different curvatures for a thrus...

Grating for the formation of a reverse flow of an aircraft turbofan...

Turbojet nacelle and method for controlling separation in a turboje...

Air outlet system for aircraft leading edge

Patents Applicationslast 30 patents

AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...

AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...

AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE...

AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MO...

DEFLECTOR PROVIDED WITH A SPOILER FOR A THRUST REVERSER OF AN AIRCR...

DEFLECTOR PROVIDED WITH FACES WITH DIFFERENT CURVATURES FOR A THRUS...

GRATING FOR THE FORMATION OF A REVERSE FLOW OF AN AIRCRAFT TURBOFAN...

AIR OUTLET SYSTEM FOR AIRCRAFT LEADING EDGE

TURBOJET NACELLE AND METHOD FOR CONTROLLING SEPARATION IN A TURBOJE...