Eric Durocher
98Patents
16h-index
50Co-inventors
87Inventor score
Filing activity: Aug 27, 2004 → Oct 17, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8091371B2 | Mid turbine frame for gas turbine engine | Mechanical Engineering; Lighting; Heating | 134 | Active |
| US8061969B2 | Mid turbine frame system for gas turbine engine | Mechanical Engineering; Lighting; Heating | 129 | Active |
| US8371127B2 | Cooling air system for mid turbine frame | Mechanical Engineering; Lighting; Heating | 74 | Active |
| US8245518B2 | Mid turbine frame system for gas turbine engine | Mechanical Engineering; Lighting; Heating | 68 | Active |
| US7217089B2 | Gas turbine engine shroud sealing arrangement | Mechanical Engineering; Lighting; Heating | 64 | Expired |
| US7229249B2 | Lightweight annular interturbine duct | Mechanical Engineering; Lighting; Heating | 47 | Expired |
| US8099962B2 | Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine | Emerging Cross-Sectional Technologies | 39 | Active |
| US7374395B2 | Turbine shroud segment feather seal located in radial shroud legs | Mechanical Engineering; Lighting; Heating | 36 | Active |
| US8500392B2 | Sealing for vane segments | Mechanical Engineering; Lighting; Heating | 30 | Active |
| US9279341B2 | Air system architecture for a mid-turbine frame module | Emerging Cross-Sectional Technologies | 26 | Active |
| US9079245B2 | Turbine shroud segment with inter-segment overlap | Mechanical Engineering; Lighting; Heating | 25 | Active |
| US8784041B2 | Turbine shroud segment with integrated seal | Emerging Cross-Sectional Technologies | 24 | Active |
| US7229247B2 | Duct with integrated baffle | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US8182204B2 | Deflector for a gas turbine strut and vane assembly | Mechanical Engineering; Lighting; Heating | 18 | Active |
| US7625415B2 | Strainer for a gas turbine engine | Emerging Cross-Sectional Technologies | 17 | Active |
| US8944749B2 | Oil purge system for a mid turbine frame | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US8347500B2 | Method of assembly and disassembly of a gas turbine mid turbine frame | Emerging Cross-Sectional Technologies | 16 | Active |
| US8347635B2 | Locking apparatus for a radial locator for gas turbine engine mid turbine frame | Emerging Cross-Sectional Technologies | 16 | Active |
| US8157511B2 | Turbine shroud gas path duct interface | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US7300246B2 | Integrated turbine vane support | Mechanical Engineering; Lighting; Heating | 15 | Expired |
| US7950236B2 | Exhaust duct and tail cone attachment of aircraft engines | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US9151164B2 | Dual-use of cooling air for turbine vane and method | Emerging Cross-Sectional Technologies | 13 | Active |
| US7520715B2 | Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US7452184B2 | Airfoil platform impingement cooling | Mechanical Engineering; Lighting; Heating | 13 | Expired |
| US7836702B2 | Gas turbine combustor exit duct and HP vane interface | Emerging Cross-Sectional Technologies | 12 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.