Beutin; Bruno

Patent Applications and Registrations

Patent applications and USPTO patent grants for Beutin; Bruno.The latest application filed is for "aircraft with an offset nacelle aligned with the wake of the wing".

Company Profile

0.9.11

Beutin; Bruno - Moissy Cramayel FR
Beutin; Bruno - Evry FR
Beutin; Bruno - Corbeil-Essonnes FR

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Aircraft With An Offset Nacelle Aligned With The Wake Of The Wing App 20220242583 - Gonidec; Patrick ; et al.	2022-08-04
Drive Unit For An Aircraft Having Lifting Points, And Carriages For Supporting Such A Unit App 20200377221 - BOILEAU; Patrick ; et al.	2020-12-03
Propulsion unit for an aircraft Grant 9,957,056 - Boileau , et al. May 1, 2	2018-05-01
Propulsion Unit For An Aircraft App 20150367946 - BOILEAU; Patrick ; et al.	2015-12-24
Turbojet having a large bypass ratio Grant 7,430,852 - Beutin , et al. October 7, 2	2008-10-07
Turbojet architecture with two fans at the front Grant 7,412,819 - Bart , et al. August 19, 2	2008-08-19
Twin turbo-shaft engine with accessory gearbox drive means Grant 7,351,174 - Beutin , et al. April 1, 2	2008-04-01
Low-pressure turbine of a turbomachine Grant 7,097,415 - Bart , et al. August 29, 2	2006-08-29
Twin turbo-shaft engine with accessory gearbox drive means App 20060183593 - Beutin; Bruno ; et al.	2006-08-17
Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position Grant 7,007,890 - Beutin , et al. March 7, 2	2006-03-07
Turbojet architecture with two fans at the front App 20050198941 - Bart, Jacques ; et al.	2005-09-15
Bleed-off device in a bypass turbojet Grant 6,938,407 - Beutin , et al. September 6, 2	2005-09-06
Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position App 20050178887 - Beutin, Bruno ; et al.	2005-08-18
Turbojet having a large bypass ratio App 20050172609 - Beutin, Bruno ; et al.	2005-08-11
Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system App 20050150970 - Beutin, Bruno ; et al.	2005-07-14
Low-pressure turbine of a turbomachine App 20050089399 - Bart, Jacques ; et al.	2005-04-28
Turbomachine rotor assembly with two bladed-discs separated by a spacer Grant 6,655,920 - Beutin , et al. December 2, 2	2003-12-02
Bleed-off device in a bypass turbojet App 20030079465 - Beutin, Bruno ; et al.	2003-05-01
Turbomachine rotor assembly with two bladed-discs separated by a spacer App 20020187046 - Beutin, Bruno ; et al.	2002-12-12
Arrangement of gas turbine engine comprising aerodynamic vanes and struts located in the same plane and an intermediate casing Grant 5,740,674 - Beutin , et al. April 21, 1	1998-04-21

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