发明名称 |
Method for manufacturing an outlet nozzle for a liquid fuel rocket engine |
摘要 |
The outlet nozzle(10) is formed as a body of revolution around a longitudinal axis with a cross section varying in diameter along this axis. The wall structure is made up of multiple mutually adjacent cooling channels(11) extending from nozzle inlet(12) to nozzle outlet(13). Multiple pre-processed profile members are produced each having a web and flanges extending from the web. Each member is milled to have a gradually tapering width in the longitudinal direction and then curved to conform to the desired bell-shaped profile. All the members are then joined by welding to form the bell-shaped nozzle(10) with the cooling channels(11) formed by adjacent member webs and pairs of flanges. |
申请公布号 |
SE520261(C2) |
申请公布日期 |
2003.06.17 |
申请号 |
SE20010000077 |
申请日期 |
2001.01.11 |
申请人 |
VOLVO AERO CORP |
发明人 |
JAN HAEGGANDER;JAN LUNDGREN |
分类号 |
F02K;F02K9/64;F02K9/97;(IPC1-7):F02K9/64 |
主分类号 |
F02K |
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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