Inventor · disambiguated record
Thierry Kohn
Also filed as: KOHN THIERRY
12 granted patents·8 citations·filing 2014–2022
81Inventor score
Top patents by PatentIndex Score
12 records- 0178US10906667B2Transport and hoisting structure for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Feb 2, 2021·5 cites·1 claims
- 0273US9611047B2Arrangement for a tank between a nacelle cowling and a turbomachineSNECMA·Filed 2014·Granted Apr 4, 2017·3 cites·9 claims
- 0355US11384650B2Servitude passage arm for a turbo machineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jul 12, 2022·0 cites·17 claims
- 0447US11433336B2Drive pinion of an air-oil separator of a turbomachine accessory gearboxSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 6, 2022·0 cites·20 claims
- 0545US12018628B2Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing wallsSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 25, 2024·0 cites·8 claims
- 0644US11199203B2Jet pump comprising an internal nozzleSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Dec 14, 2021·0 cites·7 claims
- 0744US9919805B2Metallisation of an electrically insulating housing of an aeronautic engineSNECMA·Filed 2014·Granted Mar 20, 2018·0 cites·8 claims
- 0839US10689992B2Aerodynamic link in part of a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 23, 2020·0 cites·11 claims
- 0936US11248487B2Turbomachine including a cooling and turbine clearance control system having an air supply scoopSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Feb 15, 2022·0 cites·6 claims
- 1033US12429012B2Turbojet engine rear portion having an augmented A9/A8 nozzle area ratioSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Sep 30, 2025·0 cites·3 claims
- 1133US11713730B2Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfacesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 1, 2023·0 cites·9 claims
- 1229US11739712B2Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle, the flaps of which each comprise a cooling air circulation ductSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 29, 2023·0 cites·9 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →