发明名称 Method for the manufacture of the blade tips of rotor wheels made in BLISK design
摘要 With a method for finish-machining the blade tips of rotor wheels made in BLISK design, the rotor wheel or multi-stage compressor rotor (1), is machined—blade by blade and stage by stage—at the blade tips (2) by a conical cutter (5) whose cutting edge (6) is oriented tangentially to the outside surface of the rotor wheel/compressor rotor and routed on the blade tip essentially along the centerline thereof, with the cutting force being introduced perpendicular to the tool axis and in the stiffest direction of the blade (3), i.e. the centerline (11) of the blade cross-section and the perpendicular axis extending from the centerline. The cutting action and the force introduction of the conical cutter at the blade tip allow production of blade tips with a geometrically precisely defined edge without setting the respective blades into vibration.
申请公布号 US8850703(B2) 申请公布日期 2014.10.07
申请号 US201012685813 申请日期 2010.01.12
申请人 Rolls-Royce Deutschland Ltd & Co KG 发明人 Zhu Leping;Riedel Gregor
分类号 B23P15/02;F04D29/32;F01D5/34;B23C3/18;F04D29/64;B23P15/00;B23P13/02 主分类号 B23P15/02
代理机构 Shuttleworth & Ingersoll, PLC 代理人 Klima Timothy J.;Shuttleworth & Ingersoll, PLC
主权项 1. A method for machining blade tips of BLISK type rotor wheels, comprising: machining blade tips of at least one chosen from a rotor wheel and a compressor rotor, the at least one chosen from a rotor wheel and a compressor rotor restrained in a clamping fixture by: orienting a cutting edge of a conical cutter of a rotary cutting tool tangentially to an outside surface of the at least one chosen from the rotor wheel and the compressor rotor; routing the cutting edge on a radially outer surface of one of the blade tips essentially on a centerline of the blade tip, the centerline extending from a leading edge to a trailing edge of the blade tip and bisecting a distance perpendicular to the centerline between opposing suction and pressure sides of the blade tip to follow a curvature of the blade tip from the leading edge to the trailing edge of the blade tip, the routing of the cutting edge on the centerline extending from the leading edge to the trailing edge of the blade tip; introducing a cutting force by the cutting edge onto the blade tip in a stiffest direction of the blade by maintaining the axis of the cutting tool at a 90° angle with respect to the centerline, as viewed in a projection plane tangential to an outside surface of the at least one chosen from the rotor wheel and the compressor rotor, as the cutting edge is moved along the centerline.
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