发明名称 Method for closing core printout holes in superalloy gas turbine blades
摘要 A hole (3) formed in a superalloy turbine blade (12) is sealed by providing a superalloy plug (4), machining the hole to be of a configuration can receive the plug therein, and bonding the plug to the turbine blade. The plug can be of a threaded or unthreaded configuration and can be of a tapered or straight configuration. The plug is bonded to the hole by applying a bonding catalyst to one or both of the plug and the hole or by positioning the bonding catalyst therebetween, and providing appropriate treatment to the bonding catalyst, such as heating or other treatment, to cause the bonding catalyst to form a bond between the plug and the turbine blade to form a joint therebetween. Any of a variety of known bonds can be employed to form the joint. The plug additionally may be pre-cooled prior to insertion thereof into the hole in the turbine blade, or alternatively may be of a coefficient of thermal expansion that is greater than that of the turbine blade.
申请公布号 US6454156(B1) 申请公布日期 2002.09.24
申请号 US20000602215 申请日期 2000.06.23
申请人 SIEMENS WESTINGHOUSE POWER CORPORATION 发明人 TARAS, JR. MICHAEL A.;SABOL STEPHEN M.
分类号 B23K20/16;B23P6/00;F01D5/18;(IPC1-7):B23P6/00 主分类号 B23K20/16
代理机构 代理人
主权项
地址