Inventor
PINTAT LUDOVIC
FR22 patents
⚠️ This page may combine multiple inventors who share the name “PINTAT LUDOVIC”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SAFRAN AIRCRAFT ENGINES
16 patentsUS11466578B2Oct 11, 2022
Turbine nozzle for a turbine engine, comprising a passive system for reintroducing blow-by gas into a gas jet
SAFRAN AIRCRAFT ENGINES2 citations72
US10781706B2Sep 22, 2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbine
SAFRAN AIRCRAFT ENGINES4 citations70
US10577938B2Mar 3, 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbine
SAFRAN AIRCRAFT ENGINES1 citations58
US11473435B2Oct 18, 2022
Turbine vane comprising a passive system for reducing vortex phenomena in an air flow flowing over said vane
SAFRAN AIRCRAFT ENGINES0 citations57
US10738633B2Aug 11, 2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US10683767B2Jun 16, 2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US10619485B2Apr 14, 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US10544692B2Jan 28, 2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US10533423B2Jan 14, 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US10526895B2Jan 7, 2020
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of a turbine
SAFRAN AIRCRAFT ENGINES0 citations49
US11788436B2Oct 17, 2023
Exhaust casing of a turbomachine with improved aerodynamics
SAFRAN AIRCRAFT ENGINES0 citations46
US10619497B2Apr 14, 2020
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of a turbine
SAFRAN AIRCRAFT ENGINES0 citations45
US12595739B2Apr 7, 2026
Gas turbine engine blading comprising a blade and a platform which has an internal flow-intake and flow-ejection canal
SAFRAN AIRCRAFT ENGINES0 citations44
US10738631B2Aug 11, 2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an arm
SAFRAN AIRCRAFT ENGINES0 citations38
US10738632B2Aug 11, 2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an arm
SAFRAN AIRCRAFT ENGINES0 citations35
US10711627B2Jul 14, 2020
Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural casing having such an arm
SAFRAN AIRCRAFT ENGINES0 citations35
GUIMBARD JEAN-MICHEL
2 patentsGIRARD PATRICK
2 patentsUS8647069B2Feb 11, 2014
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbine
GIRARD PATRICK16 citations80
US8757983B2Jun 24, 2014
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the second stage of a turbine
GIRARD PATRICK4 citations69