Thomas Lee Becker
24Patents
6h-index
14Co-inventors
62Inventor score
Filing activity: Jan 17, 2005 → Oct 13, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10578028B2 | Compressor bleed auxiliary turbine | Mechanical Engineering; Lighting; Heating | 19 | Active |
| US9821917B2 | Aft engine for an aircraft | Emerging Cross-Sectional Technologies | 16 | Active |
| US9637217B2 | Aircraft having an aft engine | Emerging Cross-Sectional Technologies | 13 | Active |
| US9957055B2 | Aft engine for an aircraft | Emerging Cross-Sectional Technologies | 8 | Active |
| US10017270B2 | Aft engine for an aircraft | Emerging Cross-Sectional Technologies | 8 | Active |
| US9884687B2 | Non-axis symmetric aft engine | Emerging Cross-Sectional Technologies | 8 | Active |
| US9815560B2 | AFT engine nacelle shape for an aircraft | Emerging Cross-Sectional Technologies | 6 | Active |
| US9938853B2 | Torsional damping for gas turbine engines | Emerging Cross-Sectional Technologies | 6 | Active |
| US11603801B2 | Midshaft rating for turbomachine engines | Emerging Cross-Sectional Technologies | 5 | Active |
| US10358228B2 | AFT engine nacelle shape for an aircraft | Emerging Cross-Sectional Technologies | 3 | Active |
| US11585354B2 | Engine having variable pitch outlet guide vanes | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10060290B2 | Method and system for centrifugal pump | Emerging Cross-Sectional Technologies | 2 | Active |
| US10247017B2 | System and method for gas bearing support of turbine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9995175B2 | System and method for gas bearing support of turbine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11795882B2 | Midshaft rating for turbomachine engines | Emerging Cross-Sectional Technologies | 0 | Active |
| US12215633B2 | Midshaft rating for turbomachine engines | Emerging Cross-Sectional Technologies | 0 | Active |
| US11447259B2 | Aft engine nacelle shape for an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US11346243B2 | Torsional damping for gas turbine engines | Emerging Cross-Sectional Technologies | 0 | Active |
| US12372006B2 | Torsional damping for gas turbine engines | Emerging Cross-Sectional Technologies | 0 | Active |
| US11802492B2 | Torsional damping for gas turbine engines | Emerging Cross-Sectional Technologies | 0 | Active |
| US7383823B2 | Fuel injection system for an internal combustion engine | Mechanical Engineering; Lighting; Heating | 0 | Expired |
| US9998035B2 | Resonant energy harvester, aircraft component comprising the resonant energy harvester and an aircraft comprising the resonant energy harvester or the aircraft component | Electricity | 0 | Active |
| US11391298B2 | Engine having variable pitch outlet guide vanes | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10711702B2 | Mixed flow turbocore | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.