Peter M. Munsell
29Patents
10h-index
13Co-inventors
72Inventor score
Filing activity: Jan 17, 2002 → Mar 8, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6663346B2 | Compressor stator inner diameter platform bleed system | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US8167545B2 | Self-balancing face seals and gas turbine engine systems involving such seals | Mechanical Engineering; Lighting; Heating | 21 | Active |
| US9004849B2 | Gas turbine engine forward bearing compartment architecture | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US8109717B2 | Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US8109716B2 | Gas turbine engine systems involving hydrostatic face seals with anti-fouling provisioning | Mechanical Engineering; Lighting; Heating | 19 | Active |
| US7797941B2 | Gas turbine engine systems involving hydrostatic face seals | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US9416677B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 15 | Active |
| US10415468B2 | Gas turbine engine buffer system | Emerging Cross-Sectional Technologies | 14 | Active |
| US8459040B2 | Rear hub cooling for high pressure compressor | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US8105021B2 | Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US10487734B2 | Gas turbine engine buffer system | Emerging Cross-Sectional Technologies | 6 | Active |
| US8256229B2 | Rear hub cooling for high pressure compressor | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10087782B2 | Engine mid-turbine frame transfer tube for low pressure turbine case cooling | Emerging Cross-Sectional Technologies | 6 | Active |
| US9885249B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 5 | Active |
| US10731563B2 | Compressed air bleed supply for buffer system | Emerging Cross-Sectional Technologies | 2 | Active |
| US11499476B2 | Gas turbine engine buffer system | Emerging Cross-Sectional Technologies | 1 | Active |
| US9879602B2 | Compressed air bleed supply for buffer system | Emerging Cross-Sectional Technologies | 1 | Active |
| US10465549B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 1 | Active |
| US11098644B2 | Gas turbine engine buffer system | Emerging Cross-Sectional Technologies | 1 | Active |
| US9410483B2 | Gas turbine engine forward bearing compartment architecture | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10920603B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 1 | Active |
| US11286852B2 | Gas turbine engine buffer system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11549387B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 0 | Active |
| US10550713B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 0 | Active |
| US11293299B2 | Gas turbine engine forward bearing compartment architecture | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.