Peter Beck
21Patents
2h-index
19Co-inventors
54Inventor score
Filing activity: Mar 23, 2000 → Aug 12, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6374934B1 | One-seat motor vehicle | Emerging Cross-Sectional Technologies | 9 | Expired |
| US10527003B1 | Rocket engine thrust chamber, injector, and turbopump | Emerging Cross-Sectional Technologies | 5 | Active |
| US11022073B1 | Rocket engine turbopump with coolant passage in impeller central hub | Emerging Cross-Sectional Technologies | 2 | Active |
| US11059609B2 | Satellite deployer with externally adjustable payload restraint | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11408374B1 | Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems | Electricity | 2 | Active |
| US7788893B2 | Apparatus and method for producing composite cable | Electricity | 1 | Active |
| US8156637B2 | Apparatus for forming HTS continuous conductor elements | Emerging Cross-Sectional Technologies | 1 | Active |
| US11415082B1 | Turbopump, thrust chamber, and injector with distribution system and a circular array of support columns to flow liquid from the distribution system into a combustion chamber | Emerging Cross-Sectional Technologies | 1 | Active |
| US11408373B1 | Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems | Electricity | 1 | Active |
| US7980051B2 | Apparatus and method for producing composite cable | Electricity | 1 | Active |
| US10981679B2 | Satellite deployer door release mechanism | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11408375B1 | Rocket engine turbopump with coolant passage in impeller central hub | Emerging Cross-Sectional Technologies | 1 | Active |
| US11066192B2 | Satellite deployer door with clutch bearing | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12196159B1 | Rocket engine injector | Emerging Cross-Sectional Technologies | 0 | Active |
| US11201519B2 | Method for electrically contact-connecting a winding of an electrical machine to a printed circuit board | Electricity | 0 | Active |
| US11794928B2 | Satellite deployer with externally adjustable payload restraint | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10940960B2 | Satellite deployer door release mechanism | General | 0 | Revoked |
| US11148830B2 | Satellite deployer with composite guide rail | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9970740B2 | Viscous liquid monopropellant | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11814194B2 | Satellite deployer with composite guide rail | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12006894B1 | Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems | Electricity | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.