发明名称 |
Keel-rib coolant channels for rocket combustors |
摘要 |
The present invention provides a regeneratively cooled rocket combustor comprising a combustor wall, a plurality of coolant channels extending through the combustor wall and at least one keel-rib extending into each coolant channel from the channel roof and which is bounded on both of its sides by arcuate flutes for providing smooth and continuous surface transition between the keel-rib and adjoining interior surfaces of the coolant channel.
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申请公布号 |
US4781019(A) |
申请公布日期 |
1988.11.01 |
申请号 |
US19870070638 |
申请日期 |
1987.07.08 |
申请人 |
ROCKWELL INTERNATIONAL CORPORATION |
发明人 |
WAGNER, WILLIAM R. |
分类号 |
F02K9/64;F02K9/97;(IPC1-7):F02K9/00 |
主分类号 |
F02K9/64 |
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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