Supersonic revolving nozzle
US6981365B1 · kind B1 · utility
9Cited by
16References
10Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 26, 2002 |
| Grant date | Jan 3, 2006 |
| Priority date | — |
| Expiry date | Dec 26, 2022 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02K7/075
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The disclosed device is directed toward a periodic combustion propulsion system. The periodic combustion propulsion system comprises at least one periodic combustion chamber configured to contain periodic combustion and at least one supersonic exhaust nozzle coupled to the at least one periodic combustion chamber. The supersonic exhaust nozzle is configured with a variable exhaust expansion ratio.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.