Jean Bertucchi

Person

Thiais, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Discharge system of a separated twin-flow turbojet for an aircraft,...
- Patent number 9,915,227
- Issue date Mar 13, 2018
- SNECMA
- Matthieu Leyko
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Discharge system of a separated twin-flow turbojet for an aircraft,...
- Patent number 9,726,111
- Issue date Aug 8, 2017
- SNECMA
- Matthieu Leyko
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Pylon for fixing an aircraft engine having unducted pusher propellers
- Patent number 9,682,783
- Issue date Jun 20, 2017
- SNECMA
- Stéphane Emmanuel Daniel Bensilum
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Convergent-divergent nozzle for a turbine engine
- Patent number 9,683,516
- Issue date Jun 20, 2017
- SNECMA
- Matthieu Leyko
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine comprising a device for the cooling of a pylon
- Patent number 9,540,109
- Issue date Jan 10, 2017
- SNECMA
- Matthieu Leyko
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Assembly formed by a turbine engine and a system for attaching it t...
- Patent number 9,488,106
- Issue date Nov 8, 2016
- SNECMA
- Mathieu Gaillot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Pipe having an upstream core having a sharp curvature
- Patent number 9,341,082
- Issue date May 17, 2016
- SNECMA
- Stephane Emmanuel Daniel Bensilum
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
TURBOMACHINE COMPRISING A DEVICE FOR THE COOLING OF A PYLON
- Publication number 20150284098
- Publication date Oct 8, 2015
- SNECMA
- Matthieu LEYKO
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CONVERGENT-DIVERGENT NOZZLE FOR A TURBINE ENGINE
- Publication number 20150033747
- Publication date Feb 5, 2015
- SNECMA
- Matthieu Leyko
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ASSEMBLY FORMED BY A TURBINE ENGINE AND A SYSTEM FOR ATTACHING IT T...
- Publication number 20140202169
- Publication date Jul 24, 2014
- SNECMA
- Mathieu Gaillot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DISCHARGE SYSTEM OF A SEPARATED TWIN-FLOW TURBOJET FOR AN AIRCRAFT,...
- Publication number 20140061331
- Publication date Mar 6, 2014
- SNECMA
- Matthieu LEYKO
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PIPE HAVING AN UPSTREAM CORE HAVING A SHARP CURVATURE
- Publication number 20130336772
- Publication date Dec 19, 2013
- SNECMA
- Stéphane Emmanuel Daniel Bensilum
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SECONDARY-AIR NOZZLE OF A TWO-FLOW JET ENGINE HAVING SEPARATED FLOW...
- Publication number 20130032642
- Publication date Feb 7, 2013
- SNECMA
- Stephane Bensilum
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PYLON FOR FIXING AN AIRCRAFT ENGINE HAVING UNDUCTED PUSHER PROPELLERS
- Publication number 20120145824
- Publication date Jun 14, 2012
- SNECMA
- Stéphane Emmanuel Daniel Bensilum
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Jean Bertucchi

Person

Patents Grantslast 30 patents

Discharge system of a separated twin-flow turbojet for an aircraft,...

Discharge system of a separated twin-flow turbojet for an aircraft,...

Pylon for fixing an aircraft engine having unducted pusher propellers

Convergent-divergent nozzle for a turbine engine

Turbomachine comprising a device for the cooling of a pylon

Assembly formed by a turbine engine and a system for attaching it t...

Pipe having an upstream core having a sharp curvature

Patents Applicationslast 30 patents

TURBOMACHINE COMPRISING A DEVICE FOR THE COOLING OF A PYLON

CONVERGENT-DIVERGENT NOZZLE FOR A TURBINE ENGINE

ASSEMBLY FORMED BY A TURBINE ENGINE AND A SYSTEM FOR ATTACHING IT T...

DISCHARGE SYSTEM OF A SEPARATED TWIN-FLOW TURBOJET FOR AN AIRCRAFT,...

PIPE HAVING AN UPSTREAM CORE HAVING A SHARP CURVATURE

SECONDARY-AIR NOZZLE OF A TWO-FLOW JET ENGINE HAVING SEPARATED FLOW...

PYLON FOR FIXING AN AIRCRAFT ENGINE HAVING UNDUCTED PUSHER PROPELLERS