Inventor · disambiguated record
Thierry Georges Paul Papin
Also filed as: PAPIN THIERRY · PAPIN THIERRY GEORGES PAUL
24 granted patents·4 pending applications·79 citations·filing 2009–2024
94Inventor score
Files withSAFRAN AIRCRAFT ENGINES20PAPIN THIERRY GEORGES PAUL3SNECMA3DUCHATELLE THIERRY FRANCOIS MAURICE2
Top patents by PatentIndex Score
28 records- 0195US12012201B2Assembly comprising a vane and a vane pitch setting systemSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 18, 2024·4 cites·15 claims
- 0293US10392952B2Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vaneSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 27, 2019·9 cites·11 claims
- 0392US10907489B2Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pinSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 2, 2021·7 cites·14 claims
- 0491US10723476B2Ring of turbojet vanes including an acoustic treatment structureSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jul 28, 2020·7 cites·15 claims
- 0588US10378556B2Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling functionSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 13, 2019·6 cites·12 claims
- 0686US11780562B2Turbomachine module for a propeller having variable-pitch blades and turbomachine comprising sameSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 10, 2023·2 cites·13 claims
- 0785US8740556B2Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a modulePAPIN THIERRY GEORGES PAUL·Filed 2011·Granted Jun 3, 2014·12 cites·13 claims
- 0881US9556745B2Turbine engine vane plate sealPAPIN THIERRY GEORGES PAUL·Filed 2012·Granted Jan 31, 2017·8 cites·5 claims
- 0978US11428199B2Turbomachine module for a variable pitch blade propeller and turbomachine comprising itSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 30, 2022·1 cites·15 claims
- 1077US12448110B2Assembly comprising a vane and a vane pitch setting systemSAFRAN AIRCRAFT ENGINES·Filed 2024·Granted Oct 21, 2025·0 cites·15 claims
- 1177US11143045B2Intermediate 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
- 1274US10697312B2Outlet guide vane for aircraft turbomachine, with improved lubricant cooling functionSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 30, 2020·2 cites·15 claims
- 1370US9771968B2Turbine engine drive shaft deviceDUCHATELLE THIERRY FRANCOIS MAURICE·Filed 2012·Granted Sep 26, 2017·5 cites·11 claims
- 1467US8646744B2Structural frame for a turbomachineDUCHATELLE THIERRY FRANCOIS MAURICE·Filed 2009·Granted Feb 11, 2014·11 cites·16 claims
- 1560US9528441B2Aircraft turbofan comprising an intermediate ring with simplified downstream supportSNECMA·Filed 2014·Granted Dec 27, 2016·2 cites·9 claims
- 1658US10131073B2Monobloc blade preform and module for a turbo machine intermediate casingSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Nov 20, 2018·1 cites·13 claims
- 1748US11753143B2Turbomachine module equipped with a system for changing the pitch of the blades of a propeller and with a device for feathering the bladesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 12, 2023·0 cites·14 claims
- 1847US2025297554A1Aircraft turbomachine having variable-pitch propeller vanesSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
- 1946US9797266B2Turbine engine guide vane attachment orifice closerSNECMA·Filed 2015·Granted Oct 24, 2017·0 cites·10 claims
- 2044US12098690B2Assembly for an aircraft turbine engine, comprising means for the axial and radial retention of a fanSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Sep 24, 2024·0 cites·12 claims
- 2142US12270348B2Sealing device for a discharge valve of a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Apr 8, 2025·0 cites·5 claims
- 2242US10662974B2Turbine engine flow guide vane with removable attachmentSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted May 26, 2020·0 cites·15 claims
- 2342US10648356B2Bypass turbomachine fitted with bleed systemSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted May 12, 2020·0 cites·12 claims
- 2442US10392955B2Turbomachine fan frame comprising improved attachment meansSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 27, 2019·0 cites·10 claims
- 2542US9945261B2Casing support structureSNECMA·Filed 2015·Granted Apr 17, 2018·0 cites·12 claims
- 2642US2013164145A1Method for manufacturing a hollow vanePAPIN THIERRY GEORGES PAUL·Filed 2012·Application pending·0 cites
- 2739US2022099022A1Noise reducing device having an obliquely pierced honeycomb structureSAFRAN AIRCRAFT ENGINES·Filed 2020·Application pending·0 cites
- 2838US2019071989A1Flow stator for turbomachine with integrated and attached platformsSAFRAN AIRCRAFT ENGINES·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →