Jean-Claude Lacombe

Person

Toulouse, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Aerodynamic/hydrodynamic profile with a composite reinforced oblong...
- Patent number 11,124,285
- Issue date Sep 21, 2021
- Airbus Operations (S.A.S.)
- Rodolphe Trouve
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Device and method for assembling two sections of aircraft fuselage
- Patent number 10,150,553
- Issue date Dec 11, 2018
- Airbus Operations (Societe par Actions Simplifiee)
- Bruno Cacciaguerra
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Stiff panel for aircraft, comprising stiffeners with notched cores
- Patent number 9,126,671
- Issue date Sep 8, 2015
- Airbus Operations SAS
- Jéôme Dubost
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Anti lateral-torsional buckling structural member of an aircraft fu...
- Patent number 8,967,540
- Issue date Mar 3, 2015
- Airbus Operations SAS
- Jean-Claude Lacombe
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method for making a structural part of a composite material having...
- Patent number 8,801,885
- Issue date Aug 12, 2014
- Airbus Operations SAS
- Mathieu Normand
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Method for the orbital assembly of aircraft sections made of compos...
- Patent number 8,484,848
- Issue date Jul 16, 2013
- Airbus Operations SAS
- Guillaume Gallant
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft comprising a window panel
- Patent number 8,286,915
- Issue date Oct 16, 2012
- Airbus Operations SAS
- Alain Depeige
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft structure including stiffener edge junctions
- Patent number 8,215,584
- Issue date Jul 10, 2012
- Airbus Operations SAS
- Helene Cazeneuve
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Stiff panel having composite stiffeners with reduced shock sensitivity
- Patent number 7,814,729
- Issue date Oct 19, 2010
- Airbus France
- Mathieu Normand
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Device for equipping a hole in a panel, and panel thus equipped
- Patent number 7,503,524
- Issue date Mar 17, 2009
- Airbus France
- Ludovic Fournie
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL

Patents Applicationslast 30 patents

Information Patent Application
AERODYNAMIC PROFILE HAVING A ROUNDED OBLONG HOLLOW CORE MADE OF COM...
- Publication number 20190023372
- Publication date Jan 24, 2019
- AIRBUS OPERATIONS (SAS)
- Rodolphe Trouve
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DEVICE AND METHOD FOR ASSEMBLING TWO SECTIONS OF AIRCRAFT FUSELAGE
- Publication number 20130181092
- Publication date Jul 18, 2013
- AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
- Bruno Cacciaguerra
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ANTI LATERAL-TORSIONAL BUCKLING STRUCTURAL MEMBER OF AN AIRCRAFT FU...
- Publication number 20130164465
- Publication date Jun 27, 2013
- Airbus Operation S.A.S
- Jean-Claude Lacombe
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
STIFF PANEL FOR AIRCRAFT, COMPRISING STIFFENERS WITH NOTCHED CORES
- Publication number 20130026292
- Publication date Jan 31, 2013
- AIRBUS OPERATIONS S.A.S.
- Jérôme Dubost
- E04 - BUILDING
Information Patent Application
METHOD FOR THE ORBITAL ASSEMBLY OF AIRCRAFT SECTIONS MADE OF COMPOS...
- Publication number 20110185555
- Publication date Aug 4, 2011
- AIRBUS OPERATIONS (inc as a Societe par Act Simpl)
- Guillaume Gallant
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
AIRCRAFT STRUCTURE INCLUDING STIFFENER EDGE JUNCTIONS
- Publication number 20100264272
- Publication date Oct 21, 2010
- AIRBUS OPERATIONS (SAS)
- Helene Cazeneuve
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
METHOD FOR MAKING A STRUCTURAL PART OF A COMPOSITE MATERIAL HAVING...
- Publication number 20100136309
- Publication date Jun 3, 2010
- AIRBUS FRANCE
- Mathieu Normand
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
WINDOW PANEL AND METHOD OF MANUFACTURING SUCH A WINDOW, AIRCRAFT C...
- Publication number 20090230246
- Publication date Sep 17, 2009
- AIRBUS FRANCE
- Alain Depeige
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Stiff panel having composite stiffeners with reduced shock sensitivity
- Publication number 20080010942
- Publication date Jan 17, 2008
- AIRBUS FRANCE
- Mathieu Normand
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
Device for equipping a hole in a panel, and panel thus equipped
- Publication number 20050121554
- Publication date Jun 9, 2005
- Ludovic Fournie
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL

Jean-Claude Lacombe

Person

Patents Grantslast 30 patents

Aerodynamic/hydrodynamic profile with a composite reinforced oblong...

Device and method for assembling two sections of aircraft fuselage

Stiff panel for aircraft, comprising stiffeners with notched cores

Anti lateral-torsional buckling structural member of an aircraft fu...

Method for making a structural part of a composite material having...

Method for the orbital assembly of aircraft sections made of compos...

Aircraft comprising a window panel

Aircraft structure including stiffener edge junctions

Stiff panel having composite stiffeners with reduced shock sensitivity

Device for equipping a hole in a panel, and panel thus equipped

Patents Applicationslast 30 patents

AERODYNAMIC PROFILE HAVING A ROUNDED OBLONG HOLLOW CORE MADE OF COM...

DEVICE AND METHOD FOR ASSEMBLING TWO SECTIONS OF AIRCRAFT FUSELAGE

ANTI LATERAL-TORSIONAL BUCKLING STRUCTURAL MEMBER OF AN AIRCRAFT FU...

STIFF PANEL FOR AIRCRAFT, COMPRISING STIFFENERS WITH NOTCHED CORES

METHOD FOR THE ORBITAL ASSEMBLY OF AIRCRAFT SECTIONS MADE OF COMPOS...

AIRCRAFT STRUCTURE INCLUDING STIFFENER EDGE JUNCTIONS

METHOD FOR MAKING A STRUCTURAL PART OF A COMPOSITE MATERIAL HAVING...

WINDOW PANEL AND METHOD OF MANUFACTURING SUCH A WINDOW, AIRCRAFT C...

Stiff panel having composite stiffeners with reduced shock sensitivity

Device for equipping a hole in a panel, and panel thus equipped