Alexandre Alfred, Gaston Vuillemin

Person

Fontainebleau, FR

People

Patents Grantslast 30 patents

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
Tail cone for a microjet rotary turbine engine
- Patent number 9,885,315
- Issue date Feb 6, 2018
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Bypass turbojet
- Patent number 9,611,865
- Issue date Apr 4, 2017
- SNECMA
- Cedric Morel
- 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 of processing acoustic waves emitted at the outlet of a turb...
- Patent number 9,361,876
- Issue date Jun 7, 2016
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turboshaft engine supporting pylon covered with a porous material a...
- Patent number 8,827,199
- Issue date Sep 9, 2014
- SNECMA
- Sebastien Jean-Paul Aeberli
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbine engine with nonstreamlined impellers
- Patent number 8,701,380
- Issue date Apr 22, 2014
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
TAIL CONE FOR A MICROJET ROTARY TURBINE ENGINE
- Publication number 20140373550
- Publication date Dec 25, 2014
- SNECMA
- Alexandre Alfred Gaston VUILLEMIN
- 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
BYPASS TURBOJET
- Publication number 20130280046
- Publication date Oct 24, 2013
- SNECMA
- Cedric Morel
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TURBINE ENGINE HAVING TWO UNDUCTED PROPELLERS
- Publication number 20130115083
- Publication date May 9, 2013
- SNECMA
- Alexandre Alfred, Gaston Vuillemin
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
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
METHOD OF PROCESSING ACOUSTIC WAVES EMITTED AT THE OUTLET OF A TURB...
- Publication number 20130043343
- Publication date Feb 21, 2013
- SNECMA
- Alexandre Alfred Gaston Vuillemin
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Application
CORE EXHAUST MIXER, HAVING A VARIABLE AREA, FOR TURBO-FAN JET ENGIN...
- Publication number 20070163230
- Publication date Jul 19, 2007
- SNECMA
- Laurent Dussillols
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Alexandre Alfred, Gaston Vuillemin

Person

Patents Grantslast 30 patents

Attachment pylon for a turbine engine

Tail cone for a microjet rotary turbine engine

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

Bypass turbojet

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

Method of processing acoustic waves emitted at the outlet of a turb...

Turboshaft engine supporting pylon covered with a porous material a...

Turbine engine with nonstreamlined impellers

Patents Applicationslast 30 patents

TAIL CONE FOR A MICROJET ROTARY TURBINE ENGINE

ATTACHMENT PYLON FOR A TURBINE ENGINE

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

BYPASS TURBOJET

TURBINE ENGINE HAVING TWO UNDUCTED PROPELLERS

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

METHOD OF PROCESSING ACOUSTIC WAVES EMITTED AT THE OUTLET OF A TURB...

CORE EXHAUST MIXER, HAVING A VARIABLE AREA, FOR TURBO-FAN JET ENGIN...