Baghdad Achbari

Person

Nangis, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Fire resistance device designed to be placed between one end of a m...
- Patent number 11,851,200
- Issue date Dec 26, 2023
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier Jacon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air-sealing device intended to be inserted between an aircraft dual...
- Patent number 11,746,706
- Issue date Sep 5, 2023
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier Jacon
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Outer shroud of an intermediate casing for a dual flow turbine engi...
- Patent number 11,585,292
- Issue date Feb 21, 2023
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier Jacon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine comprising an exhaust cone attached to the exhau...
- Patent number 9,897,011
- Issue date Feb 20, 2018
- SNECMA
- Mario Cesar De Sousa
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooling device for the casing of an aircraft jet engine comprising...
- Patent number 9,732,885
- Issue date Aug 15, 2017
- SNECMA
- Arthur Cohin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method for assembling a nozzle and an exhaust case of a turbomachine
- Patent number 9,399,952
- Issue date Jul 26, 2016
- SNECMA
- Mario Cesar De Sousa
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
IMPROVED AIR-SEALING DEVICE INTENDED TO BE INSERTED BETWEEN AN AIRC...
- Publication number 20210332762
- Publication date Oct 28, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier JACON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
IMPROVED FIRE RESISTANCE DEVICE DESIGNED TO BE PLACED BETWEEN ONE E...
- Publication number 20210122482
- Publication date Apr 29, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier JACON
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FIRE RESISTANCE DEVICE INTENDED TO BE INTERPOSED BETWEEN AN UPSTREA...
- Publication number 20210095569
- Publication date Apr 1, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexander Didier JACON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
OUTER SHROUD OF AN INTERMEDIATE CASING FOR A DUAL FLOW TURBINE ENGI...
- Publication number 20210003098
- Publication date Jan 7, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier JACON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COOLING DEVICE FOR THE CASING OF AN AIRCRAFT JET ENGINE COMPRISING...
- Publication number 20160003088
- Publication date Jan 7, 2016
- SNECMA
- Arthur Cohin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPRISING AN EXHAUST CONE ATTACHED TO THE EXHAU...
- Publication number 20150152788
- Publication date Jun 4, 2015
- SNECMA
- Mario Cesar De Sousa
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR ASSEMBLING A NOZZLE AND AN EXHAUST CASE OF A TURBOMACHINE
- Publication number 20140053563
- Publication date Feb 27, 2014
- SNECMA
- Mario Cesar DE SOUSA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Baghdad Achbari

Person

Patents Grantslast 30 patents

Fire resistance device designed to be placed between one end of a m...

Air-sealing device intended to be inserted between an aircraft dual...

Outer shroud of an intermediate casing for a dual flow turbine engi...

Gas turbine engine comprising an exhaust cone attached to the exhau...

Cooling device for the casing of an aircraft jet engine comprising...

Method for assembling a nozzle and an exhaust case of a turbomachine

Patents Applicationslast 30 patents

IMPROVED AIR-SEALING DEVICE INTENDED TO BE INSERTED BETWEEN AN AIRC...

IMPROVED FIRE RESISTANCE DEVICE DESIGNED TO BE PLACED BETWEEN ONE E...

FIRE RESISTANCE DEVICE INTENDED TO BE INTERPOSED BETWEEN AN UPSTREA...

OUTER SHROUD OF AN INTERMEDIATE CASING FOR A DUAL FLOW TURBINE ENGI...

COOLING DEVICE FOR THE CASING OF AN AIRCRAFT JET ENGINE COMPRISING...

GAS TURBINE ENGINE COMPRISING AN EXHAUST CONE ATTACHED TO THE EXHAU...

METHOD FOR ASSEMBLING A NOZZLE AND AN EXHAUST CASE OF A TURBOMACHINE