发明名称 |
Combustion chamber and nozzle with outer pressure envelope especially for rocket |
摘要 |
The combustion chamber and nozzle have an outer pressure envelope (9), an inner wall (10) with cooling channels (11), and an intermediate layer (2) of a superelastic material with parallel filaments or adjacent strips. In between the cooling channels the inner wall has slits (3) through part of its thickness, lying perpendicular to the intermediate layer.
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申请公布号 |
FR2773850(A1) |
申请公布日期 |
1999.07.23 |
申请号 |
FR19990000370 |
申请日期 |
1999.01.15 |
申请人 |
DAIMLER BENZ AKTIENGESELLSCHAFT |
发明人 |
BEYER STEFFEN;WIEDMANN DIETMAR |
分类号 |
F02C7/00;F02K1/82;F02K9/34;F02K9/64;F02K9/97;F23R3/42;(IPC1-7):F02K9/00;F02K7/10 |
主分类号 |
F02C7/00 |
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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