Glenn Levasseur
44Patents
9h-index
54Co-inventors
78Inventor score
Filing activity: Jun 7, 1995 → Jan 31, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8328505B2 | Turbine shroud thermal distortion control | Mechanical Engineering; Lighting; Heating | 26 | Active |
| US7665960B2 | Turbine shroud thermal distortion control | Mechanical Engineering; Lighting; Heating | 26 | Active |
| US8801372B2 | Turbine shroud thermal distortion control | Mechanical Engineering; Lighting; Heating | 24 | Active |
| US9279330B2 | Gas turbine engine component with converging/diverging cooling passage | Emerging Cross-Sectional Technologies | 21 | Active |
| US8092160B2 | Turbine shroud thermal distortion control | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US8834125B2 | Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US9416665B2 | Cooling hole with enhanced flow attachment | Emerging Cross-Sectional Technologies | 15 | Active |
| US8313280B2 | Method and device to avoid turbo instability in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US5913812A | Steam seal air removal system | Emerging Cross-Sectional Technologies | 12 | Expired |
| US8276364B2 | Bladder type variable area fan nozzle | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US8707713B2 | Cooling hole with crenellation features | Emerging Cross-Sectional Technologies | 9 | Active |
| US5941506A | Steam seal air removal system | Emerging Cross-Sectional Technologies | 9 | Expired |
| US5749227A | Steam seal air removal system | Emerging Cross-Sectional Technologies | 8 | Expired |
| US10927843B2 | Plated polymer compressor | Emerging Cross-Sectional Technologies | 7 | Active |
| US11597527B2 | Aircraft hybrid propulsion fan drive gear system DC motors and generators | Emerging Cross-Sectional Technologies | 7 | Active |
| US8936440B2 | Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US9024226B2 | EDM method for multi-lobed cooling hole | Emerging Cross-Sectional Technologies | 5 | Active |
| US8434309B2 | Translating core cowl having aerodynamic flap sections | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US11268526B2 | Plated polymer fan | Emerging Cross-Sectional Technologies | 5 | Active |
| US8851853B2 | Hybrid rotor disk assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8978390B2 | Cooling hole with crenellation features | Emerging Cross-Sectional Technologies | 4 | Active |
| US11091272B2 | Aircraft hybrid propulsion fan drive gear system DC motors and generators | Emerging Cross-Sectional Technologies | 3 | Active |
| US9309771B2 | Film cooling channel array with multiple metering portions | Emerging Cross-Sectional Technologies | 2 | Active |
| US10036276B2 | High durability turbine exhaust case | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11339723B2 | Geared turbofan high gearbox power density | Emerging Cross-Sectional Technologies | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.