发明名称 Method of drilling aircraft gas turbine rotor blades uses multiple electrodes to form simultaneous bores in blade surface
摘要 The method of drilling aircraft gas turbine blades (10) involves forming multiple bores using electrochemical machining. For each bore, a separate boring electrode (14) is used, with all electrodes having the same spacing from the surface of the vane. The electrodes can be slidable in their holders for adjustment of the spacing.
申请公布号 DE10255455(A1) 申请公布日期 2004.06.24
申请号 DE20021055455 申请日期 2002.11.28
申请人 MTU AERO ENGINES GMBH 发明人 SCHWAIGER, SIXTUS;PLATZ, ALBIN
分类号 B23H7/26;B23H9/10;B23H9/14;(IPC1-7):B23H9/14 主分类号 B23H7/26
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