Jonathan Gilson
22Patents
10h-index
22Co-inventors
71Inventor score
Filing activity: Jun 26, 2008 → Sep 23, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10066548B2 | Acoustic liner with varied properties | Mechanical Engineering; Lighting; Heating | 31 | Active |
| US10184340B2 | Geared turbofan engine having a reduced number of fan blades and improved acoustics | Emerging Cross-Sectional Technologies | 26 | Active |
| US9932933B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 24 | Active |
| US8997497B2 | Gas turbine engine with variable area fan nozzle | Mechanical Engineering; Lighting; Heating | 22 | Active |
| US8800261B2 | Gas turbine engine with noise attenuating variable area fan nozzle | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US8820088B2 | Variable area fan nozzle with acoustic system for a gas turbine engine | Emerging Cross-Sectional Technologies | 14 | Active |
| US10655538B2 | Geared gas turbine engine with reduced fan noise | Mechanical Engineering; Lighting; Heating | 14 | Active |
| US9920653B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 14 | Active |
| US8973364B2 | Gas turbine engine with noise attenuating variable area fan nozzle | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US9745918B2 | Gas turbine engine with noise attenuating variable area fan nozzle | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US10301971B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 9 | Active |
| US10371051B2 | Gas turbine engine noise reducing nose cone | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US11492967B2 | Particulate ingestion sensor for gas turbine engines | Physics | 3 | Active |
| US11286811B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 1 | Active |
| US11015550B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 1 | Active |
| US12060834B2 | Hybrid electric idle and braking for an aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11781505B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10808648B2 | Variable area fan nozzle for gas turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11118507B2 | Geared gas turbine engine with reduced fan noise | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11781447B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 0 | Active |
| US11512631B2 | Geared gas turbine engine with reduced fan noise | Mechanical Engineering; Lighting; Heating | 0 | Active |
| USRE48980E1 | Acoustic liner with varied properties | General | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.