Inventor · disambiguated record
Damien Merlot
Also filed as: MERLOT DAMIEN
9 granted patents·1 pending application·8 citations·filing 2013–2019
79Inventor score
Top patents by PatentIndex Score
10 records- 0166US10458257B2Blade comprising a shank, provided with a depressed portionSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Oct 29, 2019·2 cites·12 claims
- 0266US9863252B2Single-piece blisk for turbomachine fan comprising an upstream and/or downstream recess making its blades more flexibleSNECMA·Filed 2015·Granted Jan 9, 2018·2 cites·6 claims
- 0363US10619495B2Blisk comprising a hub having a recessed face on which a filling member is mountedSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Apr 14, 2020·1 cites·7 claims
- 0460US11209012B2Fan for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 28, 2021·0 cites·10 claims
- 0558US10502227B2Fan for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Dec 10, 2019·1 cites·13 claims
- 0648US11333164B2Airplane turbojet fan blade of cambered profile in its root sectionsSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted May 17, 2022·1 cites·10 claims
- 0748US9765637B2Blisk with low stresses at blade root, preferably for an aircraft turbine engine fanSNECMA·Filed 2014·Granted Sep 19, 2017·1 cites·11 claims
- 0848US9541002B2Turbine engine cowl capable of covering a fan coneSNECMA·Filed 2013·Granted Jan 10, 2017·0 cites·10 claims
- 0943US10634158B2Blade with a platform and a hollow bumperSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Apr 28, 2020·0 cites·10 claims
- 1035US2015176415A1Blade comprising a support, provided with a portion with a depressionSNECMA·Filed 2014·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →