发明名称 |
ROCKET ENGINE MEMBER AND A METHOD FOR MANUFACTURING A ROCKET ENGINE MEMBER |
摘要 |
The invention relates to a liquid fuel rocket engine member (10). The member forms a body of revolution having an axis of revolution having an axis of revolution and a cross section that varies in diameter along said axis. The wall structure comprises a plurality of cooling channels (11). The outside of the wall structure includes a continuous sheet metal wall (14). The cooling channels (11) are longitudinally attached to the inside of the sheet metal wall. A method for manufacturing the rocket engine member (10) includes the steps of forming a sheet metal wall (14) having a wall section corresponding to the desired nozzle section, providing a plurality of channel members (15), and attaching the channel members (15) to the inside of the sheet metal wall (14). |
申请公布号 |
WO02055863(A1) |
申请公布日期 |
2002.07.18 |
申请号 |
WO2002SE00026 |
申请日期 |
2002.01.09 |
申请人 |
VOLVO AERO CORPORATION;HAEGGANDER, JAN;LUNDGREN, JAN;HALLQVIST, MATS |
发明人 |
HAEGGANDER, JAN;LUNDGREN, JAN;HALLQVIST, MATS |
分类号 |
F02K1/00;F02K9/48;F02K9/64;F02K9/97;(IPC1-7):F02K9/64 |
主分类号 |
F02K1/00 |
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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