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
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