Ramjet engine combustion chamber and ramjet engine equipped with same
US7000398B2 · kind B2 · utility
2Cited by
10References
7Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Feb 27, 2003 |
| Grant date | Feb 21, 2006 |
| Priority date | — |
| Expiry date | May 8, 2023 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The invention concerns a combustion chamber whereof the inner wall (17)is made at least partly of a thermostructural composite material, which is porous to the fuel passing through the double wall (14); and the porosity of said inner wall (17) is adjusted so that the proportion of said fuel passing through said inner skin ranges between 5% and 15% of the total amount of fuel input in said ramjet engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.