Methods and apparatus for missile air inlet
US8344304B2 · kind B2 · utility
2Cited by
14References
18Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 10, 2010 |
| Grant date | Jan 1, 2013 |
| Priority date | — |
| Expiry date | Jan 29, 2031 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B15/10
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.