Benoît Carrere

Person

Le Taillan Medoc, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Ejection cone having a flexible aerodynamic attachment
- Patent number 11,821,387
- Issue date Nov 21, 2023
- SAFRAN CERAMICS
- Eric Conete
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust cone with flexible fitting
- Patent number 11,519,361
- Issue date Dec 6, 2022
- SAFRAN CERAMICS
- Eric Conete
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Acoustic treatment structure for an aircraft propulsion unit nacelle
- Patent number 11,512,666
- Issue date Nov 29, 2022
- Safan Nacelles
- Florent Bouillon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Structure for fastening after-body parts of an aeroengine
- Patent number 10,066,581
- Issue date Sep 4, 2018
- SAFRAN NACELLES
- Gautier Mecuson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Assembly providing a connection that is self tightening with temper...
- Patent number 9,267,531
- Issue date Feb 23, 2016
- Herakles
- Thomas Revel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Assembly providing a connection that is self tightening with temper...
- Patent number 9,121,428
- Issue date Sep 1, 2015
- Herakles
- Thomas Revel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
CMC mixer with structural outer cowling
- Patent number 8,590,316
- Issue date Nov 26, 2013
- Snecma Propulsion Solide
- Eric Conete
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine combustion chamber having inner and outer walls subdivi...
- Patent number 8,146,372
- Issue date Apr 3, 2012
- SNECMA Propulsion Solide
- Benoit Carrere
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine combustion chamber made of CMC material and subdivided...
- Patent number 8,141,371
- Issue date Mar 27, 2012
- SNECMA Propulsion Solide
- Georges Habarou
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
High temperature heat exchanger structure
- Patent number 7,013,964
- Issue date Mar 21, 2006
- SNECMA Propulsion Solide
- Roger Pays
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Resilient mount for a CMC combustion chamber of a turbomachine in a...
- Patent number 6,732,532
- Issue date May 11, 2004
- SNECMA Moteurs
- Pierre Camy
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Patents Applicationslast 30 patents

Information Patent Application
TURBOMACHINE TURBINE ASSEMBLY
- Publication number 20230407816
- Publication date Dec 21, 2023
- SAFRAN CERAMICS
- Eric CONETE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE TURBINE
- Publication number 20230407814
- Publication date Dec 21, 2023
- SAFRAN CERAMICS
- Thomas VANDELLOS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT
- Publication number 20220341373
- Publication date Oct 27, 2022
- SAFRAN CERAMICS
- Eric CONETE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST CONE WITH FLEXIBLE ATTACHMENT
- Publication number 20210293201
- Publication date Sep 23, 2021
- SAFRAN CERAMICS
- Eric Conete
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACOUSTIC TREATMENT STRUCTURE FOR AN AIRCRAFT PROPULSION UNIT NACELLE
- Publication number 20200339243
- Publication date Oct 29, 2020
- SAFRAN NACELLES
- Florent BOUILLON
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INTEGRATING AFTER-BODY PARTS OF AN AEROENGINE
- Publication number 20150083822
- Publication date Mar 26, 2015
- HERAKLES
- Gautier Mecuson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ASSEMBLY PROVIDING A CONNECTION THAT IS SELF TIGHTENING WITH TEMPER...
- Publication number 20140369785
- Publication date Dec 18, 2014
- Thomas REVEL
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
ASSEMBLY PROVIDING A CONNECTION THAT IS SELF TIGHTENING WITH TEMPER...
- Publication number 20140356094
- Publication date Dec 4, 2014
- HERAKLES
- Thomas REVEL
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
GAS TURBINE COMBUSTION CHAMBER MADE OF CMC MATERIAL AND SUBDIVIDED...
- Publication number 20120073306
- Publication date Mar 29, 2012
- SNECMA PROPULSION SOLIDE
- Georges Habarou
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
CMC MIXER WITH STRUCTURAL OUTER COWLING
- Publication number 20100126183
- Publication date May 27, 2010
- SNECMA PROPULSION SOLIDE
- Eric Conete
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE COMBUSTION CHAMBER HAVING INNER AND OUTER WALLS SUBDIVI...
- Publication number 20090249790
- Publication date Oct 8, 2009
- SNECMA PROPULISION SOLIDE
- Benoit Carrere
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
High temperature heat exchanger structure
- Publication number 20030188856
- Publication date Oct 9, 2003
- Roger Pays
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
Resilient mount for a CMC combustion of a turbomachine in a metal c...
- Publication number 20020184890
- Publication date Dec 12, 2002
- SNECMA MOTEURS
- Pierre Camy
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Benoît Carrere

Person

Patents Grantslast 30 patents

Ejection cone having a flexible aerodynamic attachment

Exhaust cone with flexible fitting

Acoustic treatment structure for an aircraft propulsion unit nacelle

Structure for fastening after-body parts of an aeroengine

Assembly providing a connection that is self tightening with temper...

Assembly providing a connection that is self tightening with temper...

CMC mixer with structural outer cowling

Gas turbine combustion chamber having inner and outer walls subdivi...

Gas turbine combustion chamber made of CMC material and subdivided...

High temperature heat exchanger structure

Resilient mount for a CMC combustion chamber of a turbomachine in a...

Patents Applicationslast 30 patents

TURBOMACHINE TURBINE ASSEMBLY

FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE TURBINE

EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT

EXHAUST CONE WITH FLEXIBLE ATTACHMENT

ACOUSTIC TREATMENT STRUCTURE FOR AN AIRCRAFT PROPULSION UNIT NACELLE

INTEGRATING AFTER-BODY PARTS OF AN AEROENGINE

ASSEMBLY PROVIDING A CONNECTION THAT IS SELF TIGHTENING WITH TEMPER...

ASSEMBLY PROVIDING A CONNECTION THAT IS SELF TIGHTENING WITH TEMPER...

GAS TURBINE COMBUSTION CHAMBER MADE OF CMC MATERIAL AND SUBDIVIDED...

CMC MIXER WITH STRUCTURAL OUTER COWLING

GAS TURBINE COMBUSTION CHAMBER HAVING INNER AND OUTER WALLS SUBDIVI...

High temperature heat exchanger structure

Resilient mount for a CMC combustion of a turbomachine in a metal c...