Bruno Albert Beutin

Person

Evry, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Aircraft with an offset nacelle aligned with the wake of the wing
- Patent number 11,866,183
- Issue date Jan 9, 2024
- SAFRAN NACELLES
- Patrick Gonidec
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Drive unit for an aircraft having lifting points, and carriages for...
- Patent number 11,834,187
- Issue date Dec 5, 2023
- SAFRAN NACELLES
- Patrick Boileau
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft with multiple fan propulsion assembly fixed under the wing
- Patent number 11,059,597
- Issue date Jul 13, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Propulsion assembly for an aircraft, comprising a gas generator, tw...
- Patent number 10,814,989
- Issue date Oct 27, 2020
- SAFRAN AIRCRAFT ENGINES
- Christian Sylvain Vessot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Air circulation device for a turbomachine comprising a hot air bypa...
- Patent number 10,634,050
- Issue date Apr 28, 2020
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method and device for mounting an engine on an aircraft pylon
- Patent number 10,486,819
- Issue date Nov 26, 2019
- SAFRAN AIRCRAFT ENGINES
- Mario Lambey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Propulsive wing of an aircraft
- Patent number 10,450,079
- Issue date Oct 22, 2019
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Unducted propeller turboshaft engine provided with a reinforcing sh...
- Patent number 10,400,632
- Issue date Sep 3, 2019
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engine having an element for deflecting foreign objects
- Patent number 10,167,740
- Issue date Jan 1, 2019
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
V-shaped gearbox for driving turbomachine equipment
- Patent number 10,054,001
- Issue date Aug 21, 2018
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Electroformed nickel-chromium alloy
- Patent number 10,036,322
- Issue date Jul 31, 2018
- SNECMA
- Carmen Ancuta
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propulsion unit for an aircraft
- Patent number 9,957,056
- Issue date May 1, 2018
- Aircelle
- Patrick Boileau
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engine with a power turbine equipped with an electric power...
- Patent number 8,534,077
- Issue date Sep 17, 2013
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine fan duct
- Patent number 8,136,362
- Issue date Mar 20, 2012
- SNECMA
- Bruno Albert Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Bypass turbomachine with reduction of jet noise
- Patent number 8,037,687
- Issue date Oct 18, 2011
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbojet comprising a current generator mounted in the fan and a me...
- Patent number 8,026,624
- Issue date Sep 27, 2011
- SNECMA
- Bruno Albert Beutin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Turbine engine with a power turbine equipped with an electric power...
- Patent number 7,966,833
- Issue date Jun 28, 2011
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Closure and locking detection system for turbojet thrust reverser
- Patent number 7,698,885
- Issue date Apr 20, 2010
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Twin spool turbine engine with power take-off means on the low-pres...
- Patent number 7,552,591
- Issue date Jun 30, 2009
- SNECMA
- Jacques Rene Bart
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
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
Turbojet architecture with two fans at the front
- Patent number 7,412,819
- Issue date Aug 19, 2008
- SNECMA
- Jacques Bart
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
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...
Information Patent Grant
Low-pressure turbine of a turbomachine
- Patent number 7,097,415
- Issue date Aug 29, 2006
- SNECMA Moteurs
- Jacques Bart
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbojet designed to be fixed onto the AFT part of the fuselage of...
- Patent number 7,007,890
- Issue date Mar 7, 2006
- SNECMA Moteurs
- Bruno Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Bleed-off device in a bypass turbojet
- Patent number 6,938,407
- Issue date Sep 6, 2005
- SNECMA Moteurs
- Bruno Beutin
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbomachine rotor assembly with two bladed-discs separated by a sp...
- Patent number 6,655,920
- Issue date Dec 2, 2003
- SNECMA Moteurs
- Bruno Beutin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Cooling system for a turbomachine speed reducer
- Patent number 6,282,881
- Issue date Sep 4, 2001
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C....
- Bruno Albert Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Arrangement of gas turbine engine comprising aerodynamic vanes and...
- Patent number 5,740,674
- Issue date Apr 21, 1998
- Societe Nationale d'Etude Et de Construction de Moteurs d'Aviation "Sherma"
- Bruno Beutin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
ASSEMBLY FOR SUPPORTING AN ACCESSORY GEARBOX OF AN AIRCRAFT TURBINE...
- Publication number 20240270396
- Publication date Aug 15, 2024
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
STRUCTURE FOR LINKING AND SUPPORTING A TURBINE ENGINE ON AN AIRCRAF...
- Publication number 20240239502
- Publication date Jul 18, 2024
- SAFRAN AIRCRAFT ENGINES
- Guillaume GLEMAREC
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING A HOLDER FOR FITTINGS
- Publication number 20240052788
- Publication date Feb 15, 2024
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT WITH AN OFFSET NACELLE ALIGNED WITH THE WAKE OF THE WING
- Publication number 20220242583
- Publication date Aug 4, 2022
- SAFRAN NACELLES
- Patrick Gonidec
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
JET TUBE FOR A TURBOMACHINE
- Publication number 20210003095
- Publication date Jan 7, 2021
- SAFRAN AIRCRAFT ENGINES
- Antonin Etienne Diego Tessiereau
- B22 - CASTING POWDER METALLURGY
Information Patent Application
DRIVE UNIT FOR AN AIRCRAFT HAVING LIFTING POINTS, AND CARRIAGES FOR...
- Publication number 20200377221
- Publication date Dec 3, 2020
- SAFRAN NACELLES
- Patrick BOILEAU
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT WITH MULTIPLE FAN PROPULSION ASSEMBLY FIXED UNDER THE WING
- Publication number 20180281978
- Publication date Oct 4, 2018
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR CIRCULATION DEVICE FOR A TURBOMACHINE COMPRISING A HOT AIR BYPA...
- Publication number 20170314465
- Publication date Nov 2, 2017
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND DEVICE FOR MOUNTING AN ENGINE ON AN AIRCRAFT PYLON
- Publication number 20170259928
- Publication date Sep 14, 2017
- SAFRAN AIRCRAFT ENGINES
- Mario LAMBEY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A GAS GENERATOR, TW...
- Publication number 20170137134
- Publication date May 18, 2017
- SAFRAN AIRCRAFT ENGINES
- Christian Sylvain Vessot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PROPULSIVE WING OF AN AIRCRAFT
- Publication number 20170137136
- Publication date May 18, 2017
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
UNDUCTED PROPELLER TURBOSHAFT ENGINE PROVIDED WITH A REINFORCING SH...
- Publication number 20170002688
- Publication date Jan 5, 2017
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Aircraft Turbomachine Comprising a Heat Exchanger and a Gearbox in...
- Publication number 20160376990
- Publication date Dec 29, 2016
- SNECMA
- Carmen ANCUTA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
V-SHAPED GEARBOX FOR DRIVING TURBOMACHINE EQUIPMENT
- Publication number 20160032755
- Publication date Feb 4, 2016
- SNECMA
- Bruno Albert BEUTIN
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
PROPULSION UNIT FOR AN AIRCRAFT
- Publication number 20150367946
- Publication date Dec 24, 2015
- Aircelle
- Patrick BOILEAU
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TURBINE ENGINE HAVING AN ELEMENT FOR DEFLECTING FOREIGN OBJECTS
- Publication number 20150300208
- Publication date Oct 22, 2015
- SNECMA
- Bruno Albert BEUTIN
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE ENGINE WITH A POWER TURBINE EQUIPPED WITH AN ELECTRIC POWER...
- Publication number 20110167835
- Publication date Jul 14, 2011
- SNECMA
- Bruno Albert BEUTIN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE ENGINE WITH A POWER TURBINE EQUIPPED WITH AN ELECTRIC POWER...
- Publication number 20100186418
- Publication date Jul 29, 2010
- SNECMA
- Bruno Albert BEUTIN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BYPASS TURBOMACHINE WITH REDUCTION OF JET NOISE
- Publication number 20090064658
- Publication date Mar 12, 2009
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOJET COMPRISING A CURRENT GENERATOR MOUNTED IN THE FAN AND A ME...
- Publication number 20090039653
- Publication date Feb 12, 2009
- SNECMA
- Bruno Albert BEUTIN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBOMACHINE FAN DUCT
- Publication number 20080072572
- Publication date Mar 27, 2008
- SNECMA
- Bruno Albert BEUTIN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CLOSURE AND LOCKING DETECTION SYSTEM FOR TURBOJET THRUST REVERSER
- Publication number 20070084191
- Publication date Apr 19, 2007
- SNECMA
- Bruno Albert BEUTIN
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TWIN SPOOL TURBINE ENGINE WITH POWER TAKE-OFF MEANS ON THE LOW-PRES...
- Publication number 20060277920
- Publication date Dec 14, 2006
- SNECMA
- Jacques Rene BART
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Turbojet architecture with two fans at the front
- Publication number 20050198941
- Publication date Sep 15, 2005
- SNECMA MOTEURS
- Jacques Bart
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbojet designed to be fixed onto the AFT part of the fuselage of...
- Publication number 20050178887
- Publication date Aug 18, 2005
- SNECMA MOTEURS
- Bruno Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Information Patent Application
Cooling system for hot parts of an aircraft engine, and aircraft en...
- Publication number 20050150970
- Publication date Jul 14, 2005
- SNECMA MOTEURS
- Bruno Beutin
- F28 - HEAT EXCHANGE IN GENERAL

Bruno Albert Beutin

Person

Patents Grantslast 30 patents

Aircraft with an offset nacelle aligned with the wake of the wing

Drive unit for an aircraft having lifting points, and carriages for...

Aircraft with multiple fan propulsion assembly fixed under the wing

Propulsion assembly for an aircraft, comprising a gas generator, tw...

Air circulation device for a turbomachine comprising a hot air bypa...

Method and device for mounting an engine on an aircraft pylon

Propulsive wing of an aircraft

Unducted propeller turboshaft engine provided with a reinforcing sh...

Turbine engine having an element for deflecting foreign objects

V-shaped gearbox for driving turbomachine equipment

Electroformed nickel-chromium alloy

Propulsion unit for an aircraft

Turbine engine with a power turbine equipped with an electric power...

Turbomachine fan duct

Bypass turbomachine with reduction of jet noise

Turbojet comprising a current generator mounted in the fan and a me...

Turbine engine with a power turbine equipped with an electric power...

Closure and locking detection system for turbojet thrust reverser

Twin spool turbine engine with power take-off means on the low-pres...

Deflection system for a gas stream in a nozzle

Exhaust nozzle for an engine of a flying craft

Turbojet having a large bypass ratio

Turbojet architecture with two fans at the front

Twin turbo-shaft engine with accessory gearbox drive means

Low-pressure turbine of a turbomachine

Turbojet designed to be fixed onto the AFT part of the fuselage of...

Bleed-off device in a bypass turbojet

Turbomachine rotor assembly with two bladed-discs separated by a sp...

Cooling system for a turbomachine speed reducer

Arrangement of gas turbine engine comprising aerodynamic vanes and...

Patents Applicationslast 30 patents

ASSEMBLY FOR SUPPORTING AN ACCESSORY GEARBOX OF AN AIRCRAFT TURBINE...

STRUCTURE FOR LINKING AND SUPPORTING A TURBINE ENGINE ON AN AIRCRAF...

AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING A HOLDER FOR FITTINGS

AIRCRAFT WITH AN OFFSET NACELLE ALIGNED WITH THE WAKE OF THE WING

JET TUBE FOR A TURBOMACHINE

DRIVE UNIT FOR AN AIRCRAFT HAVING LIFTING POINTS, AND CARRIAGES FOR...

AIRCRAFT WITH MULTIPLE FAN PROPULSION ASSEMBLY FIXED UNDER THE WING

AIR CIRCULATION DEVICE FOR A TURBOMACHINE COMPRISING A HOT AIR BYPA...

METHOD AND DEVICE FOR MOUNTING AN ENGINE ON AN AIRCRAFT PYLON

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A GAS GENERATOR, TW...

PROPULSIVE WING OF AN AIRCRAFT

UNDUCTED PROPELLER TURBOSHAFT ENGINE PROVIDED WITH A REINFORCING SH...

Aircraft Turbomachine Comprising a Heat Exchanger and a Gearbox in...

V-SHAPED GEARBOX FOR DRIVING TURBOMACHINE EQUIPMENT

PROPULSION UNIT FOR AN AIRCRAFT

TURBINE ENGINE HAVING AN ELEMENT FOR DEFLECTING FOREIGN OBJECTS

TURBINE ENGINE WITH A POWER TURBINE EQUIPPED WITH AN ELECTRIC POWER...

TURBINE ENGINE WITH A POWER TURBINE EQUIPPED WITH AN ELECTRIC POWER...

BYPASS TURBOMACHINE WITH REDUCTION OF JET NOISE

TURBOJET COMPRISING A CURRENT GENERATOR MOUNTED IN THE FAN AND A ME...

TURBOMACHINE FAN DUCT

CLOSURE AND LOCKING DETECTION SYSTEM FOR TURBOJET THRUST REVERSER

TWIN SPOOL TURBINE ENGINE WITH POWER TAKE-OFF MEANS ON THE LOW-PRES...

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

Turbojet architecture with two fans at the front

Turbojet designed to be fixed onto the AFT part of the fuselage of...

Turbojet having a large bypass ratio

Cooling system for hot parts of an aircraft engine, and aircraft en...