John James Corrigan
9Patents
4h-index
17Co-inventors
50Inventor score
Filing activity: Dec 8, 2006 → Jul 11, 2017
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9102401B2 | Wing extension control surface | Performing Operations; Transporting | 55 | Active |
| US8523102B2 | Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws | Physics | 17 | Active |
| US9126680B2 | Dual mode rotor hub assembly | Emerging Cross-Sectional Technologies | 12 | Active |
| US8287237B2 | Step-over blade-pitch control system | Performing Operations; Transporting | 7 | Active |
| US9701404B2 | Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws | Physics | 3 | Active |
| US9169012B2 | Coaxial counter-rotating rotor system | Performing Operations; Transporting | 2 | Active |
| US8763950B2 | Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws | Physics | 2 | Active |
| US9550565B2 | Coaxial counter-rotating rotor system | Performing Operations; Transporting | 1 | Active |
| US10183743B2 | Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws | Physics | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.