Inventor · San Diego, CA, US

Christopher M. Dye

97Patents
16h-index
46Co-inventors
80Inventor score

Filing activity: Dec 6, 2006 → Nov 5, 2024

Most-cited inventions

PatentTitleAreaCited byStatus
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.