Michael David Trantham
7Patents
2h-index
14Co-inventors
40Inventor score
Filing activity: Nov 2, 2012 → Nov 1, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8825342B2 | System and method of protecting an engine and other aircraft components from damage that may otherwise occur from a fuel control unit failure | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US11174015B2 | Multimode clutch assemblies having engagement status sensors | Emerging Cross-Sectional Technologies | 3 | Active |
| US11505309B2 | Control method for preventing differences between rotor tilt angles in a fly-by-wire tiltrotor aircraft | Performing Operations; Transporting | 1 | Active |
| US11604059B2 | Blade flap measurement process | Physics | 0 | Active |
| US10745123B2 | Rotorcraft swashplate actuator control | Performing Operations; Transporting | 0 | Active |
| US11708155B2 | Multimode clutch assemblies having engagement status sensors | Emerging Cross-Sectional Technologies | 0 | Active |
| US11027821B2 | Control method for preventing differences between rotor tilt angles in a fly-by-wire tiltrotor aircraft | Performing Operations; Transporting | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.