Inventor · disambiguated record
Christophe Marcel Lucien Perdrigeon
Also filed as: PERDRIGEON CHRISTOPHE · PERDRIGEON CHRISTOPHE MARCEL LUCIEN
24 granted patents·1 pending application·46 citations·filing 2012–2022
93Inventor score
Top patents by PatentIndex Score
25 records- 0193US11015468B2Outlet guide vane for turbomachine, comprising a lubricant cooling passage equipped with a thermal conducting matrix compressed between the intrados and extrados wallsSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted May 25, 2021·9 cites·6 claims
- 0291US10723476B2Ring of turbojet vanes including an acoustic treatment structureSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jul 28, 2020·7 cites·15 claims
- 0390US11125091B2Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved designSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Sep 21, 2021·5 cites·12 claims
- 0486US10830076B2Outlet guide vane for turbomachine, made from several parts assembled together by attachment means outside the flow streamSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Nov 10, 2020·4 cites·10 claims
- 0582US11686249B2Turbine engine comprising a heat exchanger in the secondary pathSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jun 27, 2023·3 cites·11 claims
- 0681US11346247B2Turbine engine including a heat exchanger formed in a platformSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 31, 2022·2 cites·10 claims
- 0777US11143045B2Intermediate case for an aircraft turbomachine made from a single casting with a lubricant ductSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Oct 12, 2021·2 cites·9 claims
- 0876US11639665B2Turbomachine comprising a heat exchanger in the secondary pathSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 2, 2023·1 cites·8 claims
- 0976US9540935B2Fan rotor and associated turbojet enginePERDRIGEON CHRISTOPHE·Filed 2012·Granted Jan 10, 2017·5 cites·5 claims
- 1074US10697312B2Outlet guide vane for aircraft turbomachine, with improved lubricant cooling functionSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 30, 2020·2 cites·15 claims
- 1173US9429031B2Hub for radial housing of a helical ring of a turbomachine with variable-pitch blades and assembly comprising such a hubSNECMA·Filed 2013·Granted Aug 30, 2016·4 cites·6 claims
- 1267US10669872B2Intermediate case for an aircraft turbomachine comprising a lubricant passage end-piece connected to a case vane by a connection pieceSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 2, 2020·1 cites·11 claims
- 1360US11209012B2Fan for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 28, 2021·0 cites·10 claims
- 1458US11982316B2Device for distributing oil from a rolling bearing for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted May 14, 2024·0 cites·10 claims
- 1558US10502227B2Fan for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Dec 10, 2019·1 cites·13 claims
- 1656US12247498B2System for changing the pitch of the blades of a turbomachine propellerSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Mar 11, 2025·0 cites·5 claims
- 1752US11982197B2Device for distributing oil from a rolling bearing for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted May 14, 2024·0 cites·10 claims
- 1850US12071865B2Air flow straightening stage for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Aug 27, 2024·0 cites·14 claims
- 1950US10604235B2Pitch change module for turbine engine and corresponding turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Mar 31, 2020·0 cites·12 claims
- 2047US12460550B2Fan module equipped with an oil transfer deviceSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Nov 4, 2025·0 cites·20 claims
- 2145US12180912B2Turbine engine comprising a heat exchanger consisting of at least one deck between vanesSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 31, 2024·0 cites·7 claims
- 2244US10436212B2Fan, in particular for a turbine engineSNECMA·Filed 2014·Granted Oct 8, 2019·0 cites·16 claims
- 2344US2025178294A1Method for manufacturing a part made of composite materialSAFRAN·Filed 2022·Application pending·0 cites
- 2442US11946381B2Stator support for a fan shaft driven by a reduction gearbox in a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Apr 2, 2024·0 cites·15 claims
- 2540US10711643B2Turbine engine with an oil guiding device and method for disassembling the turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jul 14, 2020·0 cites·10 claims
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