Propulsion system for flying machine, particularly for a missile
US9169806B2 · kind B2 · utility
2Cited by
4References
12Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Sep 8, 2011 |
| Grant date | Oct 27, 2015 |
| Priority date | — |
| Expiry date | Oct 25, 2032 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B15/10
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A propulsion system including: a booster; a turbojet engine; the booster including a chamber which is fixed to a rear casing of the turbojet engine by being arranged along the longitudinal axis thereof, which chamber includes at a rear a jet pipe and includes at least one charge and a mechanism initiating the charge; and gas bleed tubes connected to the booster and which are configured either for igniting the combustion chamber of the turbojet engine on for starting the turbine of the turbojet.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.