Didier Vuillamy

Person

Quincampoix, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Tank for a spacecraft engine
- Patent number 11,427,354
- Issue date Aug 30, 2022
- ARIANEGROUP SAS
- Didier Vuillamy
- F17 - STORING OF DISTRIBUTING GASES OR LIQUIDS
Information Patent Grant
Device for pressurizing a propellant tank of a rocket engine
- Patent number 10,371,098
- Issue date Aug 6, 2019
- ARIANEGROUP SAS
- Gérard Roz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propellant feed circuit and a cooling method
- Patent number 10,082,106
- Issue date Sep 25, 2018
- ARIANEGROUP SAS
- Didier Vuillamy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device for heating a fluid
- Patent number 9,803,589
- Issue date Oct 31, 2017
- SNECMA
- Didier Vuillamy
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Cryogenic thruster assembly using regenerative heating from main an...
- Patent number 9,446,862
- Issue date Sep 20, 2016
- SNECMA
- Jean-Luc Barthoulot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rocket engine nozzle system
- Patent number 8,266,887
- Issue date Sep 18, 2012
- SNECMA
- Didier Vuillamy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device for displacing to nozzle outlet or eliminating jet separatio...
- Patent number 6,572,030
- Issue date Jun 3, 2003
- SNECMA Moteurs
- Didier Vuillamy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine nozzle with an engine diffuser
- Patent number 5,490,629
- Issue date Feb 13, 1996
- Societe Europeenne de Propulsion
- Claude Bonniot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine nozzle with selectively smaller outlet cross-section
- Patent number 5,481,870
- Issue date Jan 9, 1996
- Societe Europeenne de Propulsion
- Claude Pacou
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine nozzle having a notched diverging portion
- Patent number 5,450,720
- Issue date Sep 19, 1995
- Societe Europeenne de Propulsion
- Didier Vuillamy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Close combustion gas generator
- Patent number 5,438,834
- Issue date Aug 8, 1995
- Societe Europeenne de Propulsion
- Didier Vuillamy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Liquid propellant rocket engine with parallel auxiliary flow, and a...
- Patent number 5,404,715
- Issue date Apr 11, 1995
- Societe Europeenne de Propulsion
- Didier Vuillamy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
TANK FOR A SPACECRAFT ENGINE
- Publication number 20210403180
- Publication date Dec 30, 2021
- ARIANEGROUP SAS
- Didier VUILLAMY
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PRESSURIZATION DEVICE FOR A LIQUID-OXYGEN TANK OF A ROCKET ENGINE
- Publication number 20180058378
- Publication date Mar 1, 2018
- ARIANEGROUP SAS
- Gérard Roz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THERMAL PROTECTION SYSTEM FOR A CRYOGENIC TANK OF A SPACE VEHICLE
- Publication number 20160341362
- Publication date Nov 24, 2016
- SNECMA
- Didier VUILLAMY
- F17 - STORING OF DISTRIBUTING GASES OR LIQUIDS
Information Patent Application
DEVICE FOR PRESSURIZING A PROPELLANT TANK OF A ROCKET ENGINE
- Publication number 20160169159
- Publication date Jun 16, 2016
- SNECMA
- Gérard ROZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPELLANT FEED CIRCUIT AND A COOLING METHOD
- Publication number 20150354505
- Publication date Dec 10, 2015
- SNECMA
- Didier VUILLAMY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND A METHOD FOR FEEDING A ROCKET ENGINE
- Publication number 20150354503
- Publication date Dec 10, 2015
- SNECMA
- Didier VUILLAMY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
A PROPELLANT FEED CIRCUIT AND A COOLING METHOD
- Publication number 20150337763
- Publication date Nov 26, 2015
- SNECMA
- Didier VUILLAMY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR HEATING A FLUID
- Publication number 20140245717
- Publication date Sep 4, 2014
- SNECMA
- Didier Vuillamy
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
CRYOGENIC THRUSTER ASSEMBLY
- Publication number 20140203148
- Publication date Jul 24, 2014
- SNECMA
- Jean-Luc Barthoulot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET ENGINE NOZZLE SYSTEM
- Publication number 20090145134
- Publication date Jun 11, 2009
- SNECMA
- Didier Vuillamy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Device for reducing or eliminating jet separation in rocket engine...
- Publication number 20020059800
- Publication date May 23, 2002
- SNECMA MOTEURS
- Didier Vuillamy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Didier Vuillamy

Person

Patents Grantslast 30 patents

Tank for a spacecraft engine

Device for pressurizing a propellant tank of a rocket engine

Propellant feed circuit and a cooling method

Device for heating a fluid

Cryogenic thruster assembly using regenerative heating from main an...

Rocket engine nozzle system

Device for displacing to nozzle outlet or eliminating jet separatio...

Rocket engine nozzle with an engine diffuser

Rocket engine nozzle with selectively smaller outlet cross-section

Rocket engine nozzle having a notched diverging portion

Close combustion gas generator

Liquid propellant rocket engine with parallel auxiliary flow, and a...

Patents Applicationslast 30 patents

TANK FOR A SPACECRAFT ENGINE

PRESSURIZATION DEVICE FOR A LIQUID-OXYGEN TANK OF A ROCKET ENGINE

THERMAL PROTECTION SYSTEM FOR A CRYOGENIC TANK OF A SPACE VEHICLE

DEVICE FOR PRESSURIZING A PROPELLANT TANK OF A ROCKET ENGINE

PROPELLANT FEED CIRCUIT AND A COOLING METHOD

SYSTEM AND A METHOD FOR FEEDING A ROCKET ENGINE

A PROPELLANT FEED CIRCUIT AND A COOLING METHOD

DEVICE FOR HEATING A FLUID

CRYOGENIC THRUSTER ASSEMBLY

ROCKET ENGINE NOZZLE SYSTEM

Device for reducing or eliminating jet separation in rocket engine...