Mathieu POISSON

Person

Melun, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Turboprop air intake
- Patent number 10,428,733
- Issue date Oct 1, 2019
- SNECMA
- Mathieu Ange Poisson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
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
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
Suspension structure with variable geometry of a turboprop engine o...
- Patent number 9,738,392
- Issue date Aug 22, 2017
- SNECMA
- Antoine Hellegouarch
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Structure for suspending a turboprop having two unducted propellers...
- Patent number 9,637,239
- Issue date May 2, 2017
- SNECMA
- Mathieu Ange Alexis Poisson
- B64 - AIRCRAFT AVIATION COSMONAUTICS

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
TURBOPROP AIR INTAKE
- Publication number 20160237898
- Publication date Aug 18, 2016
- SNECMA
- Mathieu Ange Poisson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
A STRUCTURE FOR SUSPENDING A TURBOPROP HAVING TWO UNDUCTED PROPELLE...
- Publication number 20160159486
- Publication date Jun 9, 2016
- SNECMA
- Mathieu Ange Alexis POISSON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SUSPENSION STRUCTURE WITH VARIABLE GEOMETRY OF A TURBOPROP ENGINE O...
- Publication number 20150360788
- Publication date Dec 17, 2015
- SNECMA
- Antoine HELLEGOUARCH
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
BICONICAL EXHAUST CONE FOR A CIVIL AVIATION JET ENGINE
- Publication number 20150028129
- Publication date Jan 29, 2015
- SNECMA
- Pierrick MOUCHOUX
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Mathieu POISSON

Person

Patents Grantslast 30 patents

Turboprop air intake

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

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

Isostatic suspension of a turbojet by rear double support

Suspension structure with variable geometry of a turboprop engine o...

Structure for suspending a turboprop having two unducted propellers...

Patents Applicationslast 30 patents

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

TURBOPROP AIR INTAKE

ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT

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

SUSPENSION STRUCTURE WITH VARIABLE GEOMETRY OF A TURBOPROP ENGINE O...

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

BICONICAL EXHAUST CONE FOR A CIVIL AVIATION JET ENGINE