发明名称 Cylindrical drilling tool for drilling casing flange of turbojet of aircraft, has completion part placed behind blank part and covered with abrasive material allowing completion of hole, where blank part comprises ring in extension of axis
摘要 <p>The tool (1) has a blank part (3) positioned at front end of the tool. The blank part is covered with an abrasive material (5) for forming a blank hole. A completion part (4) is placed behind the blank part and covered with another abrasive material (6) allowing completion of the hole by dimensioning. The blank part comprises an abrasive ring (7) in extension of a longitudinal axis (L). The completion part is provided with abrasive grains that are finer than that of the blank part. The ring includes leading edge in straight, beveled or round form. An independent claim is also included for a method for drilling a part.</p>
申请公布号 FR2994871(A1) 申请公布日期 2014.03.07
申请号 FR20120058305 申请日期 2012.09.05
申请人 SNECMA 发明人 GROSBOIS CHRISTOPHE;SEVE MATHIAS
分类号 B23B51/00;B32B43/00 主分类号 B23B51/00
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