发明名称 |
METHOD FOR MANUFACTURING COMBUSTOR OF ROCKET ENGINE, COMBUSTOR OF ROCKET ENGINE, AND ROCKET ENGINE |
摘要 |
In the present invention, a method for manufacturing a combustor of a rocket engine comprises: a step for preparing a combustor inner tube (20) having a cooling groove (24); a step for providing an outer layer (30) on an outer circumferential surface of the combustor inner tube (20) so as to cover the cooling groove (24); and a step for layering an LMD layer (50) by LMD processing on an outer circumferential surface of the outer layer (30). |
申请公布号 |
WO2016117202(A1) |
申请公布日期 |
2016.07.28 |
申请号 |
WO2015JP80612 |
申请日期 |
2015.10.29 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
TAKAHASHI TAKAYUKI;TSUZUKI TAMAKI;KAJIMA KAZUHIRO |
分类号 |
F02K9/64;B22F3/105;B22F3/16;B22F7/04;C23C26/00;C23C28/00;C25D7/04;F02K9/62;F02K9/97 |
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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