Inventor · disambiguated record
Renaud Gabriel Constant Royan
Also filed as: ROYAN RENAUD · ROYAN RENAUD GABRIEL · ROYAN RENAUD GABRIEL CONSTANT
18 granted patents·67 citations·filing 2009–2018
91Inventor score
Top patents by PatentIndex Score
18 records- 0188US8672635B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the first stage of a turbineBLEUZEN JEAN·Filed 2011·Granted Mar 18, 2014·15 cites·10 claims
- 0286US10781706B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Sep 22, 2020·4 cites·12 claims
- 0381US8734096B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbineGUIMBARD JEAN-MICHEL·Filed 2011·Granted May 27, 2014·8 cites·11 claims
- 0478US8734113B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbineGIRARD PATRICK·Filed 2011·Granted May 27, 2014·7 cites·11 claims
- 0573US9752506B2Device for connecting a fixed portion of a turbine engine and a distributor foot of a turbine engine turbineSNECMA·Filed 2014·Granted Sep 5, 2017·5 cites·15 claims
- 0673US9328618B2High-pressure turbine nozzle for a turbojetGROHENS RÉGIS·Filed 2011·Granted May 3, 2016·7 cites·7 claims
- 0772US9022744B2Turbine engine bladeROYAN RENAUD GABRIEL CONSTANT·Filed 2012·Granted May 5, 2015·6 cites·6 claims
- 0869US8342803B2Blade with a cooling groove for a bladed wheel of a turbomachineSNECMA·Filed 2009·Granted Jan 1, 2013·12 cites·13 claims
- 0965US10465561B2Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an armSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Nov 5, 2019·1 cites·12 claims
- 1053US10544692B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jan 28, 2020·0 cites·14 claims
- 1151US10738633B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Aug 11, 2020·0 cites·12 claims
- 1251US10619485B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Apr 14, 2020·0 cites·13 claims
- 1351US10533423B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jan 14, 2020·0 cites·13 claims
- 1451US10526895B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jan 7, 2020·0 cites·13 claims
- 1550US10683767B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 16, 2020·0 cites·12 claims
- 1650US10669871B2Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an armSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 2, 2020·0 cites·17 claims
- 1749US10724378B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jul 28, 2020·0 cites·12 claims
- 1840US9353634B2Turbine blade equipped with means of adjusting its cooling fluid flow rateGROHENS REGIS·Filed 2009·Granted May 31, 2016·2 cites·15 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →