Jeremy Edmond FERT

Person

Moissy-Cramayel Cedex, FR

People

Patents Grantslast 30 patents

Information Patent Grant
System for controlling an aircraft thrust reversal means
- Patent number 12,065,986
- Issue date Aug 20, 2024
- SAFRAN NACELLES
- Laurent Miralles
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Portion of a fluid drainage conduit for a turbomachine
- Patent number 11,401,836
- Issue date Aug 2, 2022
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond Fert
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft turbomachine comprising a heat exchanger of the precooler...
- Patent number 11,060,462
- Issue date Jul 13, 2021
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond Fert
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Deployable grille with fins for aircraft turbine engine thrust-reve...
- Patent number 10,378,481
- Issue date Aug 13, 2019
- SAFRAN AIRCRAFT ENGINES
- Jeremy Edmond Fert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine engine provided with means for absorbing stresses from the...
- Patent number 10,287,984
- Issue date May 14, 2019
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond Fert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Casing for a propulsion unit
- Patent number 9,981,751
- Issue date May 29, 2018
- SNECMA
- Jeremy Edmond Fert
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Metallisation of an electrically insulating housing of an aeronauti...
- Patent number 9,919,805
- Issue date Mar 20, 2018
- SNECMA
- Julien Sayn-Urpar
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbine engine comprising means for supporting at least one item of...
- Patent number 9,784,135
- Issue date Oct 10, 2017
- SNECMA
- Carmen Gina Ancuta
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Arrangement for a tank between a nacelle cowling and a turbomachine
- Patent number 9,611,047
- Issue date Apr 4, 2017
- SNECMA
- Thierry Kohn
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Mounting an AGB on an intermediate casing for a turbojet fan compar...
- Patent number 8,607,578
- Issue date Dec 17, 2013
- SNECMA
- Jeremy Edmond Fert
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
By-pass turbojet including a thrust reverser
- Patent number 8,468,796
- Issue date Jun 25, 2013
- SNECMA
- Yves Emprin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Deflection system for a gas stream in a nozzle
- Patent number 7,549,603
- Issue date Jun 23, 2009
- SNECMA
- Bruno Albert Beutin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Exhaust nozzle for an engine of a flying craft
- Patent number 7,533,517
- Issue date May 19, 2009
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbofan jet engine with ancillaries distribution support
- Patent number 7,506,499
- Issue date Mar 24, 2009
- SNECMA
- Jeremy Fert
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbojet having a large bypass ratio
- Patent number 7,430,852
- Issue date Oct 7, 2008
- SNECMA
- Bruno Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Twin turbo-shaft engine with accessory gearbox drive means
- Patent number 7,351,174
- Issue date Apr 1, 2008
- SNECMA
- Bruno Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
METHOD AND SYSTEM FOR DETERMINING AIRCRAFT LANDING RUNWAY CONDITIONS
- Publication number 20240105070
- Publication date Mar 28, 2024
- SAFRAN AIRCRAFT ENGINES
- Hakim Maalioune
- G08 - SIGNALLING
Information Patent Application
TURBOMACHINE LUBRICATION SYSTEM COMPRISING A BYPASS FOR PREFERENTIA...
- Publication number 20230407764
- Publication date Dec 21, 2023
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond FERT
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SYSTEM AND METHOD FOR REAL TIME CONTROL OF THE TRAJECTORY OF AN AIR...
- Publication number 20230368683
- Publication date Nov 16, 2023
- SAFRAN LANDING SYSTEMS
- Hakim MAALIOUNE
- G08 - SIGNALLING
Information Patent Application
SYSTEM FOR MANAGING THE DECELERATION OF AN AIRCRAFT ON A RUNWAY ON...
- Publication number 20230137045
- Publication date May 4, 2023
- SAFRAN AIRCRAFT ENGINES
- Hakim MAALIOUNE
- G08 - SIGNALLING
Information Patent Application
SYSTEM FOR CONTROLLING AN AIRCRAFT THRUST REVERSAL MEANS
- Publication number 20220412287
- Publication date Dec 29, 2022
- SAFRAN NACELLES
- Laurent MIRALLES
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT TURBOMACHINE COMPRISING MEANS FOR PRIMING THE LUBRICATING...
- Publication number 20220235708
- Publication date Jul 28, 2022
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond FERT
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PORTION OF A FLUID DRAINAGE CONDUIT FOR A TURBOMACHINE
- Publication number 20210172348
- Publication date Jun 10, 2021
- SAFRAN AIRCRAFT ENGINES
- Jérémy Edmond FERT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEPLOYABLE GRILLE WITH FINS FOR AIRCRAFT TURBINE ENGINE THRUST-REVE...
- Publication number 20170370325
- Publication date Dec 28, 2017
- SAFRAN AIRCRAFT ENGINES
- Jeremy Edmond FERT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT TURBOMACHINE COMPRISING A HEAT EXCHANGER OF THE PRECOOLER...
- Publication number 20170002747
- Publication date Jan 5, 2017
- SNECMA
- Jérémy Edmond Fert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE PROVIDED WITH MEANS FOR ABSORBING STRESSES FROM THE...
- Publication number 20160281605
- Publication date Sep 29, 2016
- SNECMA
- Jeremy Edmond Fert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE COMPRISING MEANS FOR SUPPORTING AT LEAST ONE ITEM OF...
- Publication number 20160215654
- Publication date Jul 28, 2016
- SNECMA
- Carmen Gina ANCUTA
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CASING FOR A PROPULSION UNIT
- Publication number 20150175269
- Publication date Jun 25, 2015
- SNECMA
- Jeremy Edmond FERT
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METALLISATION OF AN ELECTRICALLY INSULATING HOUSING OF AN AERONAUTI...
- Publication number 20150115706
- Publication date Apr 30, 2015
- SNECMA
- Julien SAYN-URPAR
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ARRANGEMENT FOR A TANK BETWEEN A NACELLE COWLING AND A TURBOMACHINE
- Publication number 20150075132
- Publication date Mar 19, 2015
- SNECMA
- Thierry KOHN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MOUNTING AN AGB ON AN INTERMEDIATE CASING FOR A TURBOJET FAN COMPAR...
- Publication number 20120224950
- Publication date Sep 6, 2012
- SNECMA
- Jérémy Edmond Fert
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
BY-PASS TURBOJET INCLUDING A THRUST REVERSER
- Publication number 20080250770
- Publication date Oct 16, 2008
- SNECMA
- Yves EMPRIN
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Exhaust nozzle for an engine of a flying craft
- Publication number 20060230744
- Publication date Oct 19, 2006
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Deflection system for a gas stream in a nozzle
- Publication number 20060226282
- Publication date Oct 12, 2006
- SNECMA
- Bruno Albert Beutin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Twin turbo-shaft engine with accessory gearbox drive means
- Publication number 20060183593
- Publication date Aug 17, 2006
- SNECMA
- Bruno Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Turbofan jet engine with ancillaries distribution support
- Publication number 20050247042
- Publication date Nov 10, 2005
- SNECMA MOTEURS
- Jeremy Fert
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbojet having a large bypass ratio
- Publication number 20050172609
- Publication date Aug 11, 2005
- SNECMA MOTEURS
- Bruno Beutin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Jeremy Edmond FERT

Person

Patents Grantslast 30 patents

System for controlling an aircraft thrust reversal means

Portion of a fluid drainage conduit for a turbomachine

Aircraft turbomachine comprising a heat exchanger of the precooler...

Deployable grille with fins for aircraft turbine engine thrust-reve...

Turbine engine provided with means for absorbing stresses from the...

Casing for a propulsion unit

Metallisation of an electrically insulating housing of an aeronauti...

Turbine engine comprising means for supporting at least one item of...

Arrangement for a tank between a nacelle cowling and a turbomachine

Mounting an AGB on an intermediate casing for a turbojet fan compar...

By-pass turbojet including a thrust reverser

Deflection system for a gas stream in a nozzle

Exhaust nozzle for an engine of a flying craft

Turbofan jet engine with ancillaries distribution support

Turbojet having a large bypass ratio

Twin turbo-shaft engine with accessory gearbox drive means

Patents Applicationslast 30 patents

METHOD AND SYSTEM FOR DETERMINING AIRCRAFT LANDING RUNWAY CONDITIONS

TURBOMACHINE LUBRICATION SYSTEM COMPRISING A BYPASS FOR PREFERENTIA...

SYSTEM AND METHOD FOR REAL TIME CONTROL OF THE TRAJECTORY OF AN AIR...

SYSTEM FOR MANAGING THE DECELERATION OF AN AIRCRAFT ON A RUNWAY ON...

SYSTEM FOR CONTROLLING AN AIRCRAFT THRUST REVERSAL MEANS

AIRCRAFT TURBOMACHINE COMPRISING MEANS FOR PRIMING THE LUBRICATING...

PORTION OF A FLUID DRAINAGE CONDUIT FOR A TURBOMACHINE

DEPLOYABLE GRILLE WITH FINS FOR AIRCRAFT TURBINE ENGINE THRUST-REVE...

AIRCRAFT TURBOMACHINE COMPRISING A HEAT EXCHANGER OF THE PRECOOLER...

TURBINE ENGINE PROVIDED WITH MEANS FOR ABSORBING STRESSES FROM THE...

TURBINE ENGINE COMPRISING MEANS FOR SUPPORTING AT LEAST ONE ITEM OF...

CASING FOR A PROPULSION UNIT

METALLISATION OF AN ELECTRICALLY INSULATING HOUSING OF AN AERONAUTI...

ARRANGEMENT FOR A TANK BETWEEN A NACELLE COWLING AND A TURBOMACHINE

MOUNTING AN AGB ON AN INTERMEDIATE CASING FOR A TURBOJET FAN COMPAR...

BY-PASS TURBOJET INCLUDING A THRUST REVERSER

Exhaust nozzle for an engine of a flying craft

Deflection system for a gas stream in a nozzle

Twin turbo-shaft engine with accessory gearbox drive means

Turbofan jet engine with ancillaries distribution support

Turbojet having a large bypass ratio