发明名称 |
Ramjet engine combustion chamber and ramjet engine equipped with same |
摘要 |
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.
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申请公布号 |
US2004134195(A1) |
申请公布日期 |
2004.07.15 |
申请号 |
US20030476648 |
申请日期 |
2003.11.04 |
申请人 |
BOUCHEZ MARC;FALEMPIN FRANCOIS |
发明人 |
BOUCHEZ MARC;FALEMPIN FRANCOIS |
分类号 |
F02K7/10;F02K9/64;(IPC1-7):F02K7/10 |
主分类号 |
F02K7/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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