Christopher M. Dye
97Patents
16h-index
46Co-inventors
80Inventor score
Filing activity: Dec 6, 2006 → Nov 5, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8075261B2 | Gas turbine engine compressor case mounting arrangement | Mechanical Engineering; Lighting; Heating | 65 | Active |
| US8511967B2 | Gearbox assembly | Emerging Cross-Sectional Technologies | 43 | Active |
| US9234481B2 | Shared flow thermal management system | Emerging Cross-Sectional Technologies | 38 | Active |
| US8602717B2 | Compression system for turbomachine heat exchanger | Emerging Cross-Sectional Technologies | 37 | Active |
| US8905711B2 | Ceramic matrix composite vane structures for a gas turbine engine turbine | Mechanical Engineering; Lighting; Heating | 33 | Active |
| US8347637B2 | Accessory gearbox with internal layshaft | Emerging Cross-Sectional Technologies | 24 | Active |
| US8337149B1 | Gas turbine engine compressor arrangement | Mechanical Engineering; Lighting; Heating | 23 | Active |
| US8128021B2 | Engine mount system for a turbofan gas turbine engine | Performing Operations; Transporting | 22 | Active |
| US8256707B2 | Engine mounting configuration for a turbofan gas turbine engine | Emerging Cross-Sectional Technologies | 21 | Active |
| US8210800B2 | Integrated actuator module for gas turbine engine | Emerging Cross-Sectional Technologies | 20 | Active |
| US9412017B1 | Methods systems and computer program products for motion initiated document capture | Physics | 19 | Active |
| US8490410B2 | Axial accessory gearbox | Mechanical Engineering; Lighting; Heating | 18 | Active |
| US8118251B2 | Mounting system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US8904805B2 | Environmental control system for aircraft utilizing turbo-compressor | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US9097137B2 | Integrated actuator module for gas turbine engine | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US7942632B2 | Variable-shape variable-stagger inlet guide vane flap | Emerging Cross-Sectional Technologies | 16 | Active |
| US9470153B2 | Combined pump system for engine TMS AOC reduction and ECS loss elimination | Emerging Cross-Sectional Technologies | 16 | Active |
| US8834125B2 | Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US8449247B1 | Gas turbine engine compressor arrangement | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US8277174B2 | Gas turbine engine compressor arrangement | Mechanical Engineering; Lighting; Heating | 14 | Active |
| US7594405B2 | Catenary mid-turbine frame design | Emerging Cross-Sectional Technologies | 14 | Active |
| US7762087B2 | Rotatable integrated segmented mid-turbine frames | Emerging Cross-Sectional Technologies | 13 | Active |
| US8490411B2 | Axial accessory gearbox | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US8113768B2 | Actuated variable geometry mid-turbine frame design | Emerging Cross-Sectional Technologies | 13 | Active |
| US9163562B2 | Constant speed pump system for engine ECS loss elimination | Emerging Cross-Sectional Technologies | 13 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.