Peter Townsend
36Patents
9h-index
38Co-inventors
75Inventor score
Filing activity: May 8, 2002 → Jun 10, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6589015B1 | Discrete passage diffuser | Mechanical Engineering; Lighting; Heating | 49 | Expired |
| US10378554B2 | Gas turbine engine with partial inlet vane | Emerging Cross-Sectional Technologies | 22 | Active |
| US9726084B2 | Compressor bleed self-recirculating system | Mechanical Engineering; Lighting; Heating | 21 | Active |
| US10837361B2 | Gas turbine engine inlet | Emerging Cross-Sectional Technologies | 17 | Active |
| US10690146B2 | Turbofan nacelle assembly with flow disruptor | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US10145301B2 | Gas turbine engine inlet | Emerging Cross-Sectional Technologies | 16 | Active |
| US10215194B2 | Mistuned fan | Emerging Cross-Sectional Technologies | 15 | Active |
| US9303589B2 | Low hub-to-tip ratio fan for a turbofan gas turbine engine | Emerging Cross-Sectional Technologies | 9 | Active |
| US7628583B2 | Discrete passage diffuser | Mechanical Engineering; Lighting; Heating | 9 | Expired |
| US9004850B2 | Twisted variable inlet guide vane | Emerging Cross-Sectional Technologies | 8 | Active |
| US8490408B2 | Continuous slot in shroud | Emerging Cross-Sectional Technologies | 7 | Active |
| US11118601B2 | Gas turbine engine with partial inlet vane | Emerging Cross-Sectional Technologies | 7 | Active |
| US9803652B2 | Centrifugal compressor diffuser and method for controlling same | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9810157B2 | Compressor shroud reverse bleed holes | Emerging Cross-Sectional Technologies | 4 | Active |
| US10865806B2 | Mistuned rotor for gas turbine engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US10865807B2 | Mistuned fan | Emerging Cross-Sectional Technologies | 4 | Active |
| US10107307B2 | Gas turbine engine rotor casing treatment | Emerging Cross-Sectional Technologies | 4 | Active |
| US11041388B2 | Blade cutback distribution in rotor for noise reduction | Emerging Cross-Sectional Technologies | 4 | Active |
| US9879540B2 | Compressor stator with contoured endwall | Emerging Cross-Sectional Technologies | 2 | Active |
| US10087764B2 | Airfoil for gas turbine engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9709070B2 | Low hub-to-tip ratio fan for a turbofan gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US11033992B2 | Double row compressor stators | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10408223B2 | Low hub-to-tip ratio fan for a turbofan gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10670041B2 | Compressor rotor for supersonic flutter and/or resonant stress mitigation | Emerging Cross-Sectional Technologies | 1 | Active |
| US10408231B2 | Rotor with non-uniform blade tip clearance | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.