Inventor · Navan, ON, CA

Daniel Lecuyer

20Patents
5h-index
34Co-inventors
65Inventor score

Filing activity: Sep 22, 2005 → Jun 14, 2024

Most-cited inventions

PatentTitleAreaCited byStatus
US8246305B2 Gas turbine engine balancing Emerging Cross-Sectional Technologies 27 Active
US9062556B2 High pressure turbine blade cooling hole distribution Emerging Cross-Sectional Technologies 9 Active
US9581029B2 High pressure turbine blade cooling hole distribution Emerging Cross-Sectional Technologies 8 Active
US8186939B2 Turbine disc and retaining nut arrangement Emerging Cross-Sectional Technologies 8 Active
US7140952B1 Oxidation protected blade and method of manufacturing Emerging Cross-Sectional Technologies 5 Expired
US9650914B2 Turbine blade for a gas turbine engine Emerging Cross-Sectional Technologies 4 Active
US9458723B2 Power turbine blade airfoil profile Emerging Cross-Sectional Technologies 3 Active
US11867081B1 Turbine blade airfoil profile Mechanical Engineering; Lighting; Heating 1 Active
US11371359B2 Turbine blade for a gas turbine engine Mechanical Engineering; Lighting; Heating 1 Active
US10876429B2 Shroud segment assembly intersegment end gaps control Mechanical Engineering; Lighting; Heating 1 Active
US11578607B2 Airfoil having a spline fillet Emerging Cross-Sectional Technologies 1 Active
US12345174B1 Turbine engine airfoil Mechanical Engineering; Lighting; Heating 1 Active
US11603763B1 Turbine blade airfoil profile Emerging Cross-Sectional Technologies 1 Active
US10174626B2 Partially coated blade Emerging Cross-Sectional Technologies 0 Active
US11199096B1 Turbomachine blade Emerging Cross-Sectional Technologies 0 Active
US12305533B2 Turbine rotor dovetail structure with splines Mechanical Engineering; Lighting; Heating 0 Active
US12070811B2 Method of manufacturing a rotor disc for a turbine engine Emerging Cross-Sectional Technologies 0 Active
US11572790B1 Turbine blade airfoil profile Emerging Cross-Sectional Technologies 0 Active
US10975714B2 Rotor assembly with blade sealing tab Emerging Cross-Sectional Technologies 0 Active
US11536141B1 Turbine vane airfoil profile Emerging Cross-Sectional Technologies 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.