Inventor · disambiguated record
Pascal Pierre Routier
Also filed as: ROUTIER PASCAL · ROUTIER PASCAL PIERRE NICOLAS · ROUTIER Pascal Pierre
20 granted patents·1 pending application·59 citations·filing 2009–2018
91Inventor score
Top patents by PatentIndex Score
21 records- 0189US8647069B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbineGIRARD PATRICK·Filed 2011·Granted Feb 11, 2014·16 cites·11 claims
- 0288US8672635B2Optimized 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
- 0385US10385697B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 20, 2019·4 cites·10 claims
- 0476US8757968B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbineBLEUZEN JEAN·Filed 2011·Granted Jun 24, 2014·6 cites·11 claims
- 0575US10443393B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 15, 2019·2 cites·11 claims
- 0675US10287888B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fifth stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 14, 2019·2 cites·11 claims
- 0769US10577938B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Mar 3, 2020·1 cites·14 claims
- 0866US10385698B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the sixth stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 20, 2019·1 cites·11 claims
- 0966US10329914B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the sixth stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jun 25, 2019·1 cites·11 claims
- 1058US8794926B2Turbine blade with improved aerodynamic performanceROUTIER PASCAL·Filed 2009·Granted Aug 5, 2014·8 cites·17 claims
- 1151US10619497B2Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Apr 14, 2020·0 cites·13 claims
- 1251US8021113B2Twin-airfoil blade with spacer stripsSNECMA·Filed 2009·Granted Sep 20, 2011·3 cites·14 claims
- 1350US10738631B2Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an armSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Aug 11, 2020·0 cites·17 claims
- 1450US10669871B2Optimized 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
- 1549US10724378B2Optimized 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
- 1648US10519775B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the second stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 31, 2019·0 cites·10 claims
- 1747US10738632B2Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an armSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Aug 11, 2020·0 cites·17 claims
- 1847US10480324B2Optimized 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
- 1947US10458245B2Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 29, 2019·0 cites·11 claims
- 2045US10378384B2Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an armSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 13, 2019·0 cites·13 claims
- 2136US2018016904A1Optimized 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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