发明名称 Rocket engines
摘要 The nozzle member(10) is formed as a body of revolution about a central axis with a cross section that varies in diameter along this axis. The wall structure has multiple cooling channels(11) for a coolant to flow. The wall structure has a bell shaped continuous sheet metal wall(14) with multiple elongate tubes(15) welded to the wall(14) to provide the cooling channels(11). Each tube runs parallel to the nozzle axis from inlet(12) to exit(13) and is curved to conform to the wall contour.
申请公布号 SE0100079(D0) 申请公布日期 2001.01.11
申请号 SE20010000079 申请日期 2001.01.11
申请人 VOLVO AERO CORP 发明人 JAN *HAEGGANDER;JAN *LUNDGREN;MATS *HALLQVIST
分类号 F02K;F02K9/64;F02K9/97;(IPC1-7):F02K/ 主分类号 F02K
代理机构 代理人
主权项
地址
您可能感兴趣的专利