发明名称 METHOD FOR FABRICATING CASE WITH BOSS OF AIRCRAFT ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a method for fabricating a turbine engine casing (34) having at least one boss (38). SOLUTION: The method includes a step for forming an engine casing (40) having an outer wall (48), a step for penetrating a casing outer wall and machining a tapered opening portion (46), and a step for machining within a metal plug (42) a tapered portion (44) that has attained such dimension as to fit into the tapered opening portion within the casing outer wall. The method further includes a step for inserting the metal plug into the tapered opening portion within the casing outer wall, and a step for welding the metal plug to the casing. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006125399(A) 申请公布日期 2006.05.18
申请号 JP20050307936 申请日期 2005.10.24
申请人 GENERAL ELECTRIC CO <GE> 发明人 CARRIER CHARLES W
分类号 F02C7/00;F01D25/00;F01D25/28 主分类号 F02C7/00
代理机构 代理人
主权项
地址