Francois Robert Bellabal

Person

Fontainebleau, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Turbojet engine suspension using a double rear support
- Patent number 10,184,401
- Issue date Jan 22, 2019
- SAFRAN AIRCRAFT ENGINES
- Francois Robert Bellabal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of producing suspension for a structure in a turbojet engine...
- Patent number 10,132,241
- Issue date Nov 20, 2018
- SAFRAN AIRCRAFT ENGINES
- Francois Robert Bellabal
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Suspension structure for suspending a turboprop having two unducted...
- Patent number 10,106,266
- Issue date Oct 23, 2018
- SAFRAN AIRCRAFT ENGINES
- Mathieu Ange Poisson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Isostatic suspension of a turbojet by rear double support
- Patent number 9,863,273
- Issue date Jan 9, 2018
- SNECMA
- Francois Robert Bellabal
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbojet engine cold stream flow path suspended from the exhaust ca...
- Patent number 9,828,877
- Issue date Nov 28, 2017
- SNECMA
- Thomas Gérard Daniel Riviere
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Hyperstatic truss comprising connecting rods
- Patent number 9,429,073
- Issue date Aug 30, 2016
- SNECMA
- Francois Robert Bellabal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Lateral turbojet improved in order to limit the deformation thereof
- Patent number 9,366,186
- Issue date Jun 14, 2016
- SNECMA
- Francois Robert Bellabal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Link between the exhaust casing and a structural ring of the fan du...
- Patent number 9,121,347
- Issue date Sep 1, 2015
- SNECMA
- Francois Robert Bellabal
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turboshaft engine attached to a pylon of the fuselage of an aircraf...
- Patent number 9,067,688
- Issue date Jun 30, 2015
- SNECMA
- Francois Bellabal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbojet engine fan duct suspension using connecting rods with elas...
- Patent number 8,919,723
- Issue date Dec 30, 2014
- SNECMA
- Francois Robert Bellabal
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
SUSPENSION STRUCTURE FOR SUSPENDING A TURBOPROP HAVING TWO UNDUCTED...
- Publication number 20160376016
- Publication date Dec 29, 2016
- SNECMA
- Mathieu Ange POISSON
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT
- Publication number 20160200443
- Publication date Jul 14, 2016
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOJET ENGINE SUSPENSION USING A DOUBLE REAR SUPPORT
- Publication number 20150377136
- Publication date Dec 31, 2015
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD OF PRODUCING SUSPENSION FOR A STRUCTURE IN A TURBOJET ENGINE...
- Publication number 20150007580
- Publication date Jan 8, 2015
- SNECMA
- Francois Robert BELLABAL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COM...
- Publication number 20140311161
- Publication date Oct 23, 2014
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOJET ENGINE COLD STREAM FLOW PATH SUSPENDED FROM THE EXHAUST CA...
- Publication number 20140112770
- Publication date Apr 24, 2014
- SNECMA
- Thomas Gérard, Daniel Riviere
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HYPERSTATIC TRUSS COMPRISING CONNECTING RODS
- Publication number 20130167553
- Publication date Jul 4, 2013
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LATERAL TURBOJET IMPROVED IN ORDER TO LIMIT THE DEFORMATION THEREOF
- Publication number 20130125560
- Publication date May 23, 2013
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOSHAFT ENGINE ATTACHED TO A PYLON OF THE FUSELAGE OF AN AIRCRAF...
- Publication number 20130099051
- Publication date Apr 25, 2013
- SNECMA
- Francois Bellabal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TURBOJET ENGINE FAN DUCT SUSPENSION USING CONNECTING RODS WITH ELAS...
- Publication number 20130037688
- Publication date Feb 14, 2013
- SNECMA
- François Robert BELLABAL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LINK BETWEEN THE EXHAUST CASING AND A STRUCTURAL RING OF THE FAN DU...
- Publication number 20130014515
- Publication date Jan 17, 2013
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Francois Robert Bellabal

Person

Patents Grantslast 30 patents

Turbojet engine suspension using a double rear support

Method of producing suspension for a structure in a turbojet engine...

Suspension structure for suspending a turboprop having two unducted...

Isostatic suspension of a turbojet by rear double support

Turbojet engine cold stream flow path suspended from the exhaust ca...

Hyperstatic truss comprising connecting rods

Lateral turbojet improved in order to limit the deformation thereof

Link between the exhaust casing and a structural ring of the fan du...

Turboshaft engine attached to a pylon of the fuselage of an aircraf...

Turbojet engine fan duct suspension using connecting rods with elas...

Patents Applicationslast 30 patents

SUSPENSION STRUCTURE FOR SUSPENDING A TURBOPROP HAVING TWO UNDUCTED...

ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT

TURBOJET ENGINE SUSPENSION USING A DOUBLE REAR SUPPORT

METHOD OF PRODUCING SUSPENSION FOR A STRUCTURE IN A TURBOJET ENGINE...

METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COM...

TURBOJET ENGINE COLD STREAM FLOW PATH SUSPENDED FROM THE EXHAUST CA...

HYPERSTATIC TRUSS COMPRISING CONNECTING RODS

LATERAL TURBOJET IMPROVED IN ORDER TO LIMIT THE DEFORMATION THEREOF

TURBOSHAFT ENGINE ATTACHED TO A PYLON OF THE FUSELAGE OF AN AIRCRAF...

TURBOJET ENGINE FAN DUCT SUSPENSION USING CONNECTING RODS WITH ELAS...

LINK BETWEEN THE EXHAUST CASING AND A STRUCTURAL RING OF THE FAN DU...