Swirl stabilized ram air turbine engine
US4819424A · kind A · utility
5Cited by
4References
1Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 16, 1987 |
| Grant date | Apr 11, 1989 |
| Priority date | — |
| Expiry date | Sep 16, 2007 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02K9/70
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A ramjet combustor operates on a slurry fuel that is atomized to 25 microns or less droplet size. A ram air turbine drives a fuel slinger which injects the fuel into the swirl stabilized ramjet combustor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.