Inventor · disambiguated record
Olivier Belmonte
Also filed as: BELMONTE OLIVIER
67 granted patents·5 pending applications·264 citations·filing 2007–2023
98Inventor score
Top patents by PatentIndex Score
72 records- 0193US11572889B2Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hubSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Feb 7, 2023·6 cites·11 claims
- 0292US9708926B2Turbine engine comprising a means for measuring the speed and torque of a shaft of the turbine engine and method for monitoring said shaftSNECMA·Filed 2013·Granted Jul 18, 2017·16 cites·18 claims
- 0391US12006844B2Radial locking of a blade pivot with adjustable orientation for a turbomachine fan hubSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jun 11, 2024·2 cites·11 claims
- 0491US9926944B2Device for guiding variable pitch diffuser vanes of a turbine engineSNECMA·Filed 2014·Granted Mar 27, 2018·11 cites·8 claims
- 0590US10302187B2Reduction gear having an epicyclic gear train for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 28, 2019·6 cites·13 claims
- 0687US10280941B2Guide device for variable pitch stator vanes of a turbine engine, and a method of assembling such a deviceSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted May 7, 2019·10 cites·11 claims
- 0785US8215910B2Aircraft turbomachine fan comprising a balancing flange concealed by the inlet coneBELMONTE OLIVIER·Filed 2008·Granted Jul 10, 2012·25 cites·8 claims
- 0884US12078072B2Turbomachine module provided with a propeller and offset stator vanesSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Sep 3, 2024·1 cites·15 claims
- 0984US7959408B2Device for attaching a stator vane to a turbomachine annular casing, turbojet engine incorporating the device and method for mounting the vaneSNECMA·Filed 2007·Granted Jun 14, 2011·16 cites·10 claims
- 1083US12000344B2Aircraft turbine engine with an off-axis propellerSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Jun 4, 2024·1 cites·10 claims
- 1183US9884675B2System for changing the pitch of the blades of a propellerSNECMA·Filed 2014·Granted Feb 6, 2018·7 cites·10 claims
- 1281US10730608B2Variable pitch blade pivot for a turbine engine fan hubSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 4, 2020·3 cites·9 claims
- 1380US8696779B2Deoiler layoutBELMONTE OLIVIER·Filed 2010·Granted Apr 15, 2014·5 cites·6 claims
- 1479US11933230B2Modularity of an aircraft turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Mar 19, 2024·1 cites·11 claims
- 1579US11708148B2Blade pivot with adjustable orientation and protected integrity for a turbomachine fan hubSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jul 25, 2023·1 cites·10 claims
- 1679US8864470B2Unducted propeller with variable pitch blades for a turbomachineBELMONTE OLIVIER·Filed 2010·Granted Oct 21, 2014·7 cites·7 claims
- 1778US11415045B2Aircraft turbomachine with mechanical reducer and contrarotative turbineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Aug 16, 2022·2 cites·10 claims
- 1878US9759088B2Device for de-icing a turbomachine separatorBELMONTE OLIVIER·Filed 2012·Granted Sep 12, 2017·6 cites·12 claims
- 1977US10280795B2Device for recovering lubrication oil ejected by centrifugal effect in a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted May 7, 2019·2 cites·12 claims
- 2076US11885265B2Recovery of lubricating oil from a reduction gear of an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 30, 2024·1 cites·12 claims
- 2176US11828183B2Pressurising of lubrication chambers in a turbomachine with counter-rotating turbineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Nov 28, 2023·1 cites·15 claims
- 2276US9708917B2Turbine engine part forming a compressor stator or a turbine nozzle, and method for fabricating sameBELMONTE OLIVIER·Filed 2012·Granted Jul 18, 2017·6 cites·18 claims
- 2376US8845294B2Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mountedSNECMA·Filed 2013·Granted Sep 30, 2014·3 cites·17 claims
- 2475US10408069B2Radial control shaft for a device for controlling the pitch of fan blades of a turbine engine having an unducted fan, and a method of mounting such a shaftSNECMA·Filed 2016·Granted Sep 10, 2019·2 cites·12 claims
- 2575US9995176B2Device for transferring oil between two repositories rotating relative to each other, and propeller turbomachine for an aircraft with such a deviceSNECMA·Filed 2014·Granted Jun 12, 2018·3 cites·12 claims
- 2674US9284041B2Stationary actuator device for controlling the pitch of fan blades of a turbopropBELMONTE OLIVIER·Filed 2010·Granted Mar 15, 2016·7 cites·7 claims
- 2773US9518472B2Turbine engine stator wheel and a turbine or a compressor including such a stator wheelBELMONTE OLIVIER·Filed 2012·Granted Dec 13, 2016·4 cites·16 claims
- 2873US8529209B2Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mountedBELMONTE OLIVIER·Filed 2008·Granted Sep 10, 2013·11 cites·2 claims
- 2972US8277188B2Turbomachine rotor diskBELMONTE OLIVIER·Filed 2008·Granted Oct 2, 2012·11 cites·11 claims
- 3070US8864466B2Cooling device for cooling the slots of a turbomachine rotor disk downstream from the drive coneBELMONTE OLIVIER·Filed 2011·Granted Oct 21, 2014·5 cites·6 claims
- 3169US8257023B2Fan bladeBELMONTE OLIVIER·Filed 2008·Granted Sep 4, 2012·9 cites·17 claims
- 3268US11225317B2Radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 18, 2022·2 cites·7 claims
- 3367US8985952B2Turbine engine fan comprising a balancing system with blind holes for accommodating massesBELMONTE OLIVIER·Filed 2009·Granted Mar 24, 2015·11 cites·14 claims
- 3467US8727719B2Annular flange for fastening a rotor or stator element in a turbomachineBELMONTE OLIVIER·Filed 2009·Granted May 20, 2014·11 cites·11 claims
- 3565US10479514B2Assembly for turbine machine with open rotor contra-rotating propellers, comprising a small duct for the passage of ancillariesSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Nov 19, 2019·1 cites·10 claims
- 3665US8932020B2Low-pressure turbineBELMONTE OLIVIER·Filed 2010·Granted Jan 13, 2015·3 cites·8 claims
- 3765US8757980B2Rotor for a gas turbine engine comprising a rotor spool and a rotor ringBELMONTE OLIVIER·Filed 2011·Granted Jun 24, 2014·3 cites·7 claims
- 3864US10279889B2Device for supplying hydraulic fluid to a ram and mechanism for controlling the pitch of the blades of a turbine engine propeller comprising the ramSNECMA·Filed 2014·Granted May 7, 2019·1 cites·19 claims
- 3964US9988937B2Hydraulic and electrical interface ring for a turbine engineSNECMA·Filed 2013·Granted Jun 5, 2018·2 cites·14 claims
- 4064US9284847B2Retaining ring assembly and supporting flange for said ringBELMONTE OLIVIER·Filed 2010·Granted Mar 15, 2016·3 cites·7 claims
- 4163US9371742B2Set of rotor disks for a turbine engineBELMONTE OLIVIER·Filed 2011·Granted Jun 21, 2016·3 cites·10 claims
- 4262US9957896B2Unlockable device for axially arresting a sealing ring with which an aircraft turbomachine module rotor wheel makes contactSNECMA·Filed 2012·Granted May 1, 2018·2 cites·10 claims
- 4361US9616992B2Device for supplying and distributing fluidSNECMA·Filed 2013·Granted Apr 11, 2017·3 cites·9 claims
- 4460US9664117B2Guidance of turbine engine shaftsSNECMA·Filed 2013·Granted May 30, 2017·2 cites·4 claims
- 4560US8162616B2Turbomachine fanBELMONTE OLIVIER·Filed 2008·Granted Apr 24, 2012·6 cites·15 claims
- 4658US9518687B2Device for the blind coupling of fluidic, electrical or similar supplies, to a receiving control mechanismSNECMA·Filed 2013·Granted Dec 13, 2016·1 cites·12 claims
- 4757US12497901B2Variable pitch fanSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Dec 16, 2025·0 cites·11 claims
- 4857US8998579B2Blade retention diskBELMONTE OLIVIER·Filed 2011·Granted Apr 7, 2015·2 cites·12 claims
- 4955US9726039B2Oil transfer system on rotating shaftSNECMA·Filed 2014·Granted Aug 8, 2017·1 cites·9 claims
- 5055US9017016B2Balancing device and methodBELMONTE OLIVIER·Filed 2010·Granted Apr 28, 2015·1 cites·7 claims
Showing the top 50 of 72 patent records by PatentIndex Score.
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