Dominique GUITTARD

Person

Toulouse, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Self-stiffened composite panel and method of producing same
- Patent number 10,105,938
- Issue date Oct 23, 2018
- Airbus Operations (S.A.S.)
- Dominique Guittard
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Method for producing a central wing box
- Patent number 9,114,582
- Issue date Aug 25, 2015
- Airbus Operations SAS
- Philippe Blot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Automated drape-forming device
- Patent number 8,871,050
- Issue date Oct 28, 2014
- Airbus Operations SAS
- Philippe Blot
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Connection of a fuselage to an aircraft wing
- Patent number 8,770,518
- Issue date Jul 8, 2014
- Airbus Operations SAS
- Dominique Guittard
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Oblique panel at the rear of a central box of an aircraft fuselage
- Patent number 8,672,268
- Issue date Mar 18, 2014
- Airbus Operations SAS
- Julien Guillemaut
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Three-dimensional surface weaving
- Patent number 8,561,649
- Issue date Oct 22, 2013
- Airbus Operations SAS
- Xavier Legrand
- D03 - WEAVING
Information Patent Grant
Three-dimensional surface weaving
- Patent number 8,361,911
- Issue date Jan 29, 2013
- Airbus Operations SAS
- Xavier Legrand
- D03 - WEAVING

Patents Applicationslast 30 patents

Information Patent Application
SELF-STIFFENED COMPOSITE PANEL AND METHOD OF PRODUCING SAME
- Publication number 20150165744
- Publication date Jun 18, 2015
- AIRBUS OPERATIONS (SAS)
- Dominique Guittard
- B32 - LAYERED PRODUCTS
Information Patent Application
THREE-DIMENSIONAL SURFACE WEAVING
- Publication number 20130263966
- Publication date Oct 10, 2013
- Airbus Operations (S.A.S.)
- Xavier LEGRAND
- D03 - WEAVING
Information Patent Application
Method for producing a central wing box
- Publication number 20130206324
- Publication date Aug 15, 2013
- Philippe Blot
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING
- Publication number 20120286090
- Publication date Nov 15, 2012
- AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
- Dominique GUITTARD
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
AUTOMATED DRAPE-FORMING DEVICE
- Publication number 20120261069
- Publication date Oct 18, 2012
- AIRBUS OPERATIONS (SAS)
- Philippe Blot
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
OBLIQUE PANEL AT THE REAR OF A CENTRAL BOX OF AN AIRCRAFT FUSELAGE
- Publication number 20120138746
- Publication date Jun 7, 2012
- AIRBUS OPERATIONS (SAS)
- Julien GUILLEMAUT
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
THREE-DIMENSIONAL SURFACE WEAVING
- Publication number 20100269948
- Publication date Oct 28, 2010
- AIRBUS FRANCE
- Xavier Legrand
- D03 - WEAVING
Information Patent Application
Method for making a laminated structure and aircraft provided with...
- Publication number 20050224655
- Publication date Oct 13, 2005
- Dominique Guittard
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Dominique GUITTARD

Person

Patents Grantslast 30 patents

Self-stiffened composite panel and method of producing same

Method for producing a central wing box

Automated drape-forming device

Connection of a fuselage to an aircraft wing

Oblique panel at the rear of a central box of an aircraft fuselage

Three-dimensional surface weaving

Three-dimensional surface weaving

Patents Applicationslast 30 patents

SELF-STIFFENED COMPOSITE PANEL AND METHOD OF PRODUCING SAME

THREE-DIMENSIONAL SURFACE WEAVING

Method for producing a central wing box

CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING

AUTOMATED DRAPE-FORMING DEVICE

OBLIQUE PANEL AT THE REAR OF A CENTRAL BOX OF AN AIRCRAFT FUSELAGE

THREE-DIMENSIONAL SURFACE WEAVING

Method for making a laminated structure and aircraft provided with...