Inventor · disambiguated record
Bruno Albert Beutin
Also filed as: BEUTIN BRUNO · BEUTIN BRUNO A · BEUTIN BRUNO ALBERT
33 granted patents·3 pending applications·613 citations·filing 1996–2022
97Inventor score
Top patents by PatentIndex Score
36 records- 0197US7552591B2Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engineSNECMA·Filed 2006·Granted Jun 30, 2009·79 cites·11 claims
- 0297US6282881B1Cooling system for a turbomachine speed reducerSNECMA·Filed 2000·Granted Sep 4, 2001·148 cites·3 claims
- 0392US7412819B2Turbojet architecture with two fans at the frontSNECMA·Filed 2005·Granted Aug 19, 2008·33 cites·10 claims
- 0490US10054001B2V-shaped gearbox for driving turbomachine equipmentSNECMA·Filed 2014·Granted Aug 21, 2018·20 cites·7 claims
- 0587US12258137B2Assembly for supporting an accessory gearbox of an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Mar 25, 2025·2 cites·16 claims
- 0687US11866183B2Aircraft with an offset nacelle aligned with the wake of the wingSAFRAN NACELLES·Filed 2022·Granted Jan 9, 2024·2 cites·15 claims
- 0785US10450079B2Propulsive wing of an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 22, 2019·5 cites·14 claims
- 0881US10634050B2Air circulation device for a turbomachine comprising a hot air bypass system to a heat exchangerSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Apr 28, 2020·4 cites·15 claims
- 0981US8026624B2Turbojet comprising a current generator mounted in the fan and a method of mounting said generator in the fanSNECMA·Filed 2008·Granted Sep 27, 2011·14 cites·13 claims
- 1080US10814989B2Propulsion assembly for an aircraft, comprising a gas generator, two offset fans and an air inlet sleeveSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 27, 2020·3 cites·15 claims
- 1180US5740674AArrangement of gas turbine engine comprising aerodynamic vanes and struts located in the same plane and an intermediate casingSNECMA·Filed 1996·Granted Apr 21, 1998·72 cites·21 claims
- 1280US5615547ASystem for regulating oil and fuel temperatures of a turbojet engineSNECMA·Filed 1996·Granted Apr 1, 1997·86 cites·7 claims
- 1377US7430852B2Turbojet having a large bypass ratioSNECMA·Filed 2005·Granted Oct 7, 2008·17 cites·15 claims
- 1475US7351174B2Twin turbo-shaft engine with accessory gearbox drive meansSNECMA·Filed 2006·Granted Apr 1, 2008·11 cites·6 claims
- 1575US6655920B2Turbomachine rotor assembly with two bladed-discs separated by a spacerSNECMA MOTEURS·Filed 2002·Granted Dec 2, 2003·36 cites·8 claims
- 1669US7966833B2Turbine engine with a power turbine equipped with an electric power generator centered on the axis of the turbine engineSNECMA·Filed 2009·Granted Jun 28, 2011·11 cites·13 claims
- 1764US8136362B2Turbomachine fan ductBEUTIN BRUNO ALBERT·Filed 2007·Granted Mar 20, 2012·11 cites·13 claims
- 1861US7097415B2Low-pressure turbine of a turbomachineSNECMA MOTEURS·Filed 2004·Granted Aug 29, 2006·18 cites·2 claims
- 1961US6938407B2Bleed-off device in a bypass turbojetSNECMA MOTEURS·Filed 2002·Granted Sep 6, 2005·12 cites·20 claims
- 2057US8534077B2Turbine engine with a power turbine equipped with an electric power generatorBEUTIN BRUNO ALBERT·Filed 2009·Granted Sep 17, 2013·6 cites·11 claims
- 2157US7533517B2Exhaust nozzle for an engine of a flying craftSNECMA·Filed 2006·Granted May 19, 2009·4 cites·12 claims
- 2255US7007890B2Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper positionSNECMA MOTEURS·Filed 2004·Granted Mar 7, 2006·15 cites·9 claims
- 2354US12459657B2Structure for linking and supporting a turbine engine on an aircraft pylonSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Nov 4, 2025·0 cites·13 claims
- 2454US10036322B2Electroformed nickel-chromium alloySNECMA·Filed 2014·Granted Jul 31, 2018·0 cites·12 claims
- 2554US7698885B2Closure and locking detection system for turbojet thrust reverserSNECMA·Filed 2006·Granted Apr 20, 2010·3 cites·6 claims
- 2653US10167740B2Turbine engine having an element for deflecting foreign objectsSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Jan 1, 2019·1 cites·8 claims
- 2752US11834187B2Drive unit for an aircraft having lifting points, and carriages for supporting such a unitSAFRAN NACELLES·Filed 2020·Granted Dec 5, 2023·0 cites·15 claims
- 2845US10486819B2Method and device for mounting an engine on an aircraft pylonSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Nov 26, 2019·0 cites·12 claims
- 2942US2024052788A1Aircraft turbine engine assembly comprising a holder for fittingsSAFRAN AIRCRAFT ENGINES·Filed 2021·Application pending·0 cites
- 3040US9957056B2Propulsion unit for an aircraftAIRCELLE SA·Filed 2015·Granted May 1, 2018·0 cites·15 claims
- 3139US11059597B2Aircraft with multiple fan propulsion assembly fixed under the wingSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jul 13, 2021·0 cites·11 claims
- 3239US10400632B2Unducted propeller turboshaft engine provided with a reinforcing shell integrating pipe segmentsSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 3, 2019·0 cites·9 claims
- 3339US8037687B2Bypass turbomachine with reduction of jet noiseSNECMA·Filed 2008·Granted Oct 18, 2011·0 cites·5 claims
- 3439US7549603B2Deflection system for a gas stream in a nozzleSNECMA·Filed 2006·Granted Jun 23, 2009·0 cites·14 claims
- 3536US2021003095A1Jet tube for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2020·Application pending·0 cites
- 3635US2005150970A1Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling systemSNECMA MOTEURS·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →