Philippe Beauchesne-Martel
36Patents
3h-index
33Co-inventors
59Inventor score
Filing activity: Jan 29, 2013 → Mar 8, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9322341B2 | System and method for engine transient power response | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US9382010B2 | Aircraft power outtake management | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US11236681B2 | Systems and methods for operating gas turbine engines | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10961919B2 | Corrected parameters control logic for variable geometry mechanisms | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10822104B2 | Variable geometries transient control logic | Emerging Cross-Sectional Technologies | 2 | Active |
| US10808624B2 | Turbine rotor with low over-speed requirements | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11668249B2 | System and method for operating a multi-engine aircraft | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11168621B2 | Method and system for operating an engine in a multi-engine aircraft | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11408352B2 | Reverse-flow gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10280788B2 | Aircraft power outtake management | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11299286B2 | System and method for operating a multi-engine aircraft | Performing Operations; Transporting | 1 | Active |
| US11352900B2 | Method and system for operating a rotorcraft engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11713723B2 | Method and system for operating an engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11760500B2 | Systems and methods for filling a fuel manifold of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11719165B2 | Air inlet strut for aircraft engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11663863B2 | Methods and systems for operating a rotorcraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11549446B1 | Method and apparatus for measuring compressor bleed flow | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11867129B2 | System and method for operating a multi-engine aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12116940B2 | Corrected parameters control logic for variable geometry mechanisms | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11643965B2 | System and method for operating multi-engine rotorcraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US11674456B1 | System and method of operating multi-engine system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11761385B2 | Turbine engine shaft shear detection | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11781476B2 | System and method for operating a multi-engine rotorcraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11859554B2 | Fast engine re-start for multi-engine system and method | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12031489B2 | System and method for variable geometry mechanism configuration | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.