Guillaume BODARD

Person

Verneuil L'etang, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Modified acoustic secondary nozzle
- Patent number 11,149,685
- Issue date Oct 19, 2021
- SAFRAN AIRCRAFT ENGINES
- Jérémy Paul Francisco Gonzalez
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Heating system for convergent-divergent secondary nozzle
- Patent number 10,995,702
- Issue date May 4, 2021
- SAFRAN AIRCRAFT ENGINES
- Guillaume Bodard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Attachment pylon for a turbine engine
- Patent number 9,938,901
- Issue date Apr 10, 2018
- SNECMA
- Guillaume Bodard
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Primary cowl of a turbofan comprising a rotating ring having micro-...
- Patent number 9,617,954
- Issue date Apr 11, 2017
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for reducing the noise emitted by the jet of an aircraft pro...
- Patent number 9,422,887
- Issue date Aug 23, 2016
- SNECMA
- Guillaume Bodard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method for defining the shape of a turbomachine convergent-divergen...
- Patent number 9,249,755
- Issue date Feb 2, 2016
- SNECMA
- Julien Szydlowski
- A45 - HAND OR TRAVELLING ARTICLES
Information Patent Grant
Mixer that performs reciprocating rotary motion for a confluent-flo...
- Patent number 8,881,502
- Issue date Nov 11, 2014
- SNECMA
- Norman Jodet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE
- Publication number 20200378339
- Publication date Dec 3, 2020
- SAFRAN AIRCRAFT ENGINES
- Guillaume BODARD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
MODIFIED ACOUSTIC SECONDARY NOZZLE
- Publication number 20200173396
- Publication date Jun 4, 2020
- SAFRAN AIRCRAFT ENGINES
- Jérémy Paul Francisco GONZALEZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE
- Publication number 20190078534
- Publication date Mar 14, 2019
- SAFRAN AIRCRAFT ENGINES
- Guillaume BODARD
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AFTERBODY FOR A MIXED-FLOW TURBOJET ENGINE COMPRISING A LOBED MIXER...
- Publication number 20160215727
- Publication date Jul 28, 2016
- SNECMA
- Jonathan LANGRIDGE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ATTACHMENT PYLON FOR A TURBINE ENGINE
- Publication number 20140290270
- Publication date Oct 2, 2014
- SNECMA
- Guillaume Bodard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PRIMARY COWL OF A TURBOFAN COMPRISING A ROTATING RING HAVING MICRO-...
- Publication number 20140245715
- Publication date Sep 4, 2014
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MIXER THAT PERFORMS RECIPROCATING ROTARY MOTION FOR A CONFLUENT-FLO...
- Publication number 20140090359
- Publication date Apr 3, 2014
- SNECMA
- Norman JODET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR DEFINING THE SHAPE OF A TURBOMACHINE CONVERGENT-DIVERGEN...
- Publication number 20130206865
- Publication date Aug 15, 2013
- SNECMA
- Julien SZYDLOWSKI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR REDUCING THE NOISE EMITTED BY THE JET OF AN AIRCRAFT PRO...
- Publication number 20130055718
- Publication date Mar 7, 2013
- Guillaume Bodard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE FOR A BYPASS AIRPLANE TURBOJET HAVING A DEPLOYABLE S...
- Publication number 20120192543
- Publication date Aug 2, 2012
- SNECMA
- Sébastien Jean-Paul Aeberli
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Guillaume BODARD

Person

Patents Grantslast 30 patents

Modified acoustic secondary nozzle

Heating system for convergent-divergent secondary nozzle

Attachment pylon for a turbine engine

Primary cowl of a turbofan comprising a rotating ring having micro-...

Device for reducing the noise emitted by the jet of an aircraft pro...

Method for defining the shape of a turbomachine convergent-divergen...

Mixer that performs reciprocating rotary motion for a confluent-flo...

Patents Applicationslast 30 patents

HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE

MODIFIED ACOUSTIC SECONDARY NOZZLE

HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE

AFTERBODY FOR A MIXED-FLOW TURBOJET ENGINE COMPRISING A LOBED MIXER...

ATTACHMENT PYLON FOR A TURBINE ENGINE

PRIMARY COWL OF A TURBOFAN COMPRISING A ROTATING RING HAVING MICRO-...

MIXER THAT PERFORMS RECIPROCATING ROTARY MOTION FOR A CONFLUENT-FLO...

METHOD FOR DEFINING THE SHAPE OF A TURBOMACHINE CONVERGENT-DIVERGEN...

DEVICE FOR REDUCING THE NOISE EMITTED BY THE JET OF AN AIRCRAFT PRO...

EXHAUST NOZZLE FOR A BYPASS AIRPLANE TURBOJET HAVING A DEPLOYABLE S...