Inventor · disambiguated record
Laurent Patrick Robert Coudert
Also filed as: COUDERT LAURENT PATRICK · COUDERT LAURENT PATRICK ROBERT
7 granted patents·1 pending application·7 citations·filing 2015–2020
74Inventor score
Files withSAFRAN AIRCRAFT ENGINES8
Top patents by PatentIndex Score
8 records- 0174US10822961B2Turbine blade comprising an improved trailing-edgeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 3, 2020·2 cites·9 claims
- 0272US10753215B2Turbine vane comprising a blade with a tub including a curved pressure side in a blade apex regionSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 25, 2020·2 cites·8 claims
- 0369US10260361B2Turbomachine vane including an antivortex finSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Apr 16, 2019·2 cites·9 claims
- 0466US10443392B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 15, 2019·1 cites·11 claims
- 0547US10655484B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 19, 2020·0 cites·10 claims
- 0647US10480324B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 19, 2019·0 cites·8 claims
- 0741US11946387B2Turbine engine blade with improved coolingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Apr 2, 2024·0 cites·11 claims
- 0836US2018016904A1Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the first stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →