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    • 5. 发明专利
    • DE102004036598A1
    • 2006-03-23
    • DE102004036598
    • 2004-07-28
    • MTU AERO ENGINES GMBHDAIMLER CHRYSLER AG
    • BAYER ERWINBUSSMANN MARTINPLATZ ALBINSTEINWANDEL JUERGENKRAENZLER THOMAS
    • B23H9/10B23H3/00B23H3/02F01D5/02
    • The invention relates to a method for the production of aero-dynamic structures during the production of integrally bladed gas turbine rotors. Aerodynamic structures of an integrally bladed gas turbine rotor are produced on a rotor disk base body, whereon the end contours are precise, by removing material according to an electrochemical removal process, i.e. by means of an electrochemical machining (ECM)-process. The method comprises the following steps: a) preparing a rotor disk base body which is made of a material which is difficult to machine; b) removing the material which is between the blade wings until a specific dimension is obtained, according to a removal process; c) preparing at least one working electrode in order to finish at least one aerodynamic structure of an integrally bladed gas turbine rotor. The contours of the or each of the working electrodes are adapted to the contours of the aerodynamic structure, which are produced by means of the respective working electrode, such that a gap between the rotor disk base body and a working electrode are produced in an approximately identical manner during the removal process of the material; d) electrochemically machining the or each aerodynamic structure in an electrochemical sinking by placing the rotor disk base body and the or each working electrode in an electrolyte and by applying voltage and/or current, whereby the applied current and/or voltage is temporally pulsed; e) pressure-rinsing the gap which is filled with electrolytes between the aero-dynamic structure and the or each working electrode by a pulsed movement of the or each working electrode.
    • 10. 发明申请
    • METHOD FOR REMOVING MATERIAL FROM A COMPONENT, AND ELECTRODE
    • 法测量材料从一个组成部分,除铅
    • WO2009074141A3
    • 2010-09-23
    • PCT/DE2008002040
    • 2008-12-05
    • MTU AERO ENGINES GMBHBAYER ERWINBUSSMANN MARTINPLATZ ALBIN
    • BAYER ERWINBUSSMANN MARTINPLATZ ALBIN
    • B23H3/00B23H3/10
    • B23H3/00B23H1/04B23H3/04B23H3/06B23H3/10B23H5/10B23H7/26
    • Disclosed is a method for removing material from a component (10, 10') that is connected as an anode. In said method, an electrode (12) that is connected as a cathode is guided to the component such that a gap (16) is formed, an electrolyte is introduced into the gap, and a closed system is formed for the electrolyte by forming a duct. The electrolyte is continuously conducted from an inlet to an outlet of the duct. Forming the duct, e.g. by means of conducting elements (18) that are mounted on the electrode (12), ensures that only those surface parts of the component (10) to be machined from which material is to be removed enter in contact with the electrode while the other surface parts do not enter in contact with the electrolyte. Since the electrolyte is continuously conducted across said surface, used electrolyte is continuously discharged along with residual matter while fresh electrolyte is delivered such that the method can be carried out in a particularly trouble-free and expedient manner.
    • 在用于从连接作为阳极的部件(10,10“)去除材料,和一种方法,其中一个切换作为阴极电极(12)被引导到该组件,从而形成一间隙(16),和 其中,电解质被引入间隙通过形成通道用于电解质的封闭系统形成。 这是连续地从进料口向信道的排出口供给。 通过形成的通道,例如,通过在电极(12)上的导向元件(18)是固定的,它保证了仅由组分的那些表面部分被加工(10)接触的电解质加入到从材料烧蚀 并且,剩余的表面部分不接触到与电解质接触。 通过不断地使电解质随时间废电解质的表面被连续残基一起排出和新鲜电解质供应,因此该方法特别平滑且迅速地进行。