Inventor · disambiguated record
Jérémy Guivarc'H
Also filed as: GUIVARC'H JEREMY · GUIVARC'H JÉRÉMY
17 granted patents·1 pending application·41 citations·filing 2016–2022
90Inventor score
Top patents by PatentIndex Score
18 records- 0195US10844725B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 24, 2020·22 cites·8 claims
- 0292US11686203B2Fibrous texture for turbine engine blade made of composite materialSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 27, 2023·3 cites·9 claims
- 0385US11040465B2Preform and one-piece vane for turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 22, 2021·3 cites·13 claims
- 0481US11396820B2Hybridization of fibers of the fibrous reinforcement of a fan bladeSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jul 26, 2022·3 cites·20 claims
- 0576US11105210B2Blade comprising a leading edge shield and method for producing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 31, 2021·2 cites·19 claims
- 0676US11015460B2Blade comprising a blade body made of composite material and a leading-edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 25, 2021·2 cites·26 claims
- 0774US10240463B2Blade made of organic matrix composite material provided with a metal strip, and a method of fastening a metal strip on a blade fiber preformSNECMA·Filed 2016·Granted Mar 26, 2019·1 cites·11 claims
- 0868US11143047B2Fan including a platform and a locking boltSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Oct 12, 2021·2 cites·14 claims
- 0967US10934851B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 2, 2021·1 cites·10 claims
- 1065US10619486B2Blade, associated fan and turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Apr 14, 2020·1 cites·6 claims
- 1162US10883374B2Blade comprising a folded leading edge shield and method of manufacturing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 5, 2021·1 cites·11 claims
- 1258US11795825B2Inter-blade platform with a sacrificial box sectionSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 24, 2023·0 cites·20 claims
- 1356US11254067B2Method for producing a part using a heat-shrinkable sleeveSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 22, 2022·0 cites·17 claims
- 1452US10436036B2Fitted platform for a turbine engine fan, and a method of fabricating itSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 8, 2019·0 cites·9 claims
- 1547US11131196B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 28, 2021·0 cites·11 claims
- 1640US12060811B2Turbomachine fan rotorSAFRAN·Filed 2020·Granted Aug 13, 2024·0 cites·12 claims
- 1739US2024151148A1Composite turbomachine part formed of a core surrounded by two 3d woven fibrous preformsSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 1834US11078918B2Inter-blade platform sealSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 3, 2021·0 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →