Michel Labrecque
25Patents
6h-index
32Co-inventors
69Inventor score
Filing activity: Jun 4, 2002 → Mar 14, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6996880B2 | Fastener elements and methods of manufacture | Emerging Cross-Sectional Technologies | 69 | Expired |
| US6991843B2 | Fasteners engageable with loops of nonwoven fabrics and with other open structures, and methods and machines for making fasteners | Emerging Cross-Sectional Technologies | 26 | Expired |
| US7727440B2 | Methods of making fastener products | Emerging Cross-Sectional Technologies | 12 | Active |
| US6977055B2 | Securing electrical conductors | Emerging Cross-Sectional Technologies | 11 | Expired |
| US10221764B2 | Variable geometry inlet system | Mechanical Engineering; Lighting; Heating | 11 | Active |
| US10054050B2 | Low noise aeroengine inlet system | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US7670639B2 | Forming electrical cables | Emerging Cross-Sectional Technologies | 5 | Active |
| USRE42475E1 | Fasteners engageable with loops of nonwoven fabrics and with other open structures, and methods and machines for making fasteners | General | 4 | Active |
| US11066993B2 | Variable geometry inlet system | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9951690B2 | Low noise aeroengine inlet system | Emerging Cross-Sectional Technologies | 2 | Active |
| US7181812B2 | Fastener elements and methods of manufacture | Emerging Cross-Sectional Technologies | 1 | Expired |
| US11661887B2 | Variable geometry inlet system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10683099B2 | Methods and systems for controlling operation of aircraft engines | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9957889B2 | Low noise aeroengine inlet system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US12116937B1 | Boosting gas turbine engine power with fluid motor | General | 0 | Revoked |
| US11180259B2 | Synthesized low-pressure bleed air scheme for aircraft bleed air network | Emerging Cross-Sectional Technologies | 0 | Active |
| US12409940B2 | Electric motor propulsion system for an aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12365473B1 | Air inlet barrier filter for a helicopter | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11739696B2 | System and method for synthesizing engine output power | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12071252B1 | Aircraft and associated method of controlling an electric aircraft powerplant | Performing Operations; Transporting | 0 | Active |
| US11828248B1 | Rotatably driven exhaust mixer | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12103695B2 | Exhaust nozzle assembly for an aircraft propulsion system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12146443B2 | Boosting gas turbine engine power with fluid motor | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11674450B1 | System and method for synthesizing engine thrust | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10829235B2 | Methods and systems for controlling operation of aircraft engines | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.