Michael John Layland
24Patents
10h-index
20Co-inventors
75Inventor score
Filing activity: Oct 2, 1989 → Mar 12, 2015
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7923668B2 | Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein | Performing Operations; Transporting | 51 | Active |
| US7921966B2 | Linear acoustic liner | Physics | 43 | Active |
| US5083426A | Integrated engine shroud for gas turbine engines | Emerging Cross-Sectional Technologies | 38 | Expired |
| US8197191B2 | Inlet section of an aircraft engine nacelle | Emerging Cross-Sectional Technologies | 27 | Active |
| US7798285B2 | Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers | Emerging Cross-Sectional Technologies | 26 | Active |
| US7469862B2 | Aircraft engine nacelle inlet having access opening for electrical ice protection system | Emerging Cross-Sectional Technologies | 21 | Active |
| US7513458B2 | Aircraft engine nacelle inlet having electrical ice protection system | Emerging Cross-Sectional Technologies | 19 | Active |
| US7837150B2 | Ice protection system for a multi-segment aircraft component | Emerging Cross-Sectional Technologies | 17 | Active |
| US8402765B2 | Translating variable area fan nozzle providing an upstream bypass flow exit | Emerging Cross-Sectional Technologies | 16 | Active |
| US9403599B2 | Inlet section of an aircraft engine nacelle | Emerging Cross-Sectional Technologies | 13 | Active |
| US8267642B2 | Inlet section of an aircraft engine nacelle | Emerging Cross-Sectional Technologies | 8 | Active |
| US8025499B2 | Multi-segment tool and method for composite formation | Emerging Cross-Sectional Technologies | 6 | Active |
| US7631838B2 | Aircraft engine nacelle inlet having access opening for electrical ice protection system | Emerging Cross-Sectional Technologies | 6 | Active |
| US8196704B2 | Linear acoustic liner | Physics | 6 | Active |
| US9567089B2 | Hybrid hinge and latch beam | Performing Operations; Transporting | 6 | Active |
| US9016042B2 | Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure | Emerging Cross-Sectional Technologies | 5 | Active |
| US7681838B2 | Aircraft engine nacelle inlet having access opening for electrical ice protection system | Emerging Cross-Sectional Technologies | 4 | Active |
| US9233757B2 | Nacelle | Emerging Cross-Sectional Technologies | 4 | Active |
| US9551298B2 | Variable area fan nozzle with one or more integrated blocker doors | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9759087B2 | Translating variable area fan nozzle providing an upstream bypass flow exit | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8394315B2 | Multi-segment tool and method for composite formation | Emerging Cross-Sectional Technologies | 2 | Active |
| US9897007B2 | Thrust reverser-integrated track beam and inner fixed structure | Emerging Cross-Sectional Technologies | 2 | Active |
| USRE46321E1 | Multi-segment tool and method for composite formation | General | 0 | Active |
| US10184398B2 | Acoustic structural panel with slanted core | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.