发明名称 METHOD AND TOOL FOR USE WITH TURBOMACHINES
摘要 A tool for drilling, tapping, and back spot facing at least one hole in a turbomachine includes a servo motor cutting device configured for use with a cutting tool. A drill unit skid is adapted to engage a hook fit slot in a case of the turbomachine, and for supporting the servo motor cutting device, and the drill unit skid including hook fit slides. The hook fit slides guide the drill unit skid along the hook fit slot and act as a stop in a radial direction with respect to the turbomachine. A laser positioning device detects the position of the cutting tool. A micro switch stops the servo motor cutting device when the micro switch activates. The servo motor cutting device rotates the cutting tool to create the hole, while a rotor of the turbomachine is left in place during drilling, tapping and back spot facing.
申请公布号 US2016375498(A1) 申请公布日期 2016.12.29
申请号 US201615257260 申请日期 2016.09.06
申请人 General Electric Company 发明人 Holmes James Bradford;Herbold John William;Corn Randall Stephen
分类号 B23B39/14;B23G1/18;B23B49/00 主分类号 B23B39/14
代理机构 代理人
主权项 1. A tool for drilling, tapping, and back spot facing at least one hole in a turbomachine, the tool comprising: a servo motor cutting device configured for use with a cutting tool; a drill unit skid adapted to engage a hook fit slot in a case of the turbomachine and for supporting the servo motor cutting device, the drill unit skid including hook fit slides, the hook fit slides configured to guide the drill unit skid along the hook fit slot and act as a stop in a radial direction with respect to the turbomachine; a laser positioning device configured to detect the position of the cutting tool; a micro switch configured to stop the servo motor cutting device when the micro switch activates; and wherein the servo motor cutting device rotates the cutting tool to create the at least one hole, and wherein a rotor of the turbomachine is left in place during drilling, tapping and back spot facing.
地址 Schenectady NY US