The invention relates to a work station for electrochemically machining a workpiece, having a number of recesses, including a base structure; a module which is fastened to the base structure and is configured to electrochemically machine the workpiece. A workpiece holder is fastened to the base structure. The workpiece holder is movable relative to the base structure along a feed axis which is parallel to the axis of rotation of the module. The module includes an electrode carrier arrangement, which is coupled to the module base body so the electrode carrier arrangement can be rotated together with the module base body about the axis of rotation of the module. The electrode carrier arrangement has a carrier frame and an electrode frame, where at least one electrode is detachably fastened to the electrode frame.

The invention relates to a work station for electrochemically machining a workpiece, having a number of recesses, including a base structure; a module which is fastened to the base structure and is configured to electrochemically machine the workpiece. A workpiece holder is fastened to the base structure. The workpiece holder is movable relative to the base structure along a feed axis which is parallel to the axis of rotation of the module. The module includes an electrode carrier arrangement, which is coupled to the module base body so the electrode carrier arrangement can be rotated together with the module base body about the axis of rotation of the module. The electrode carrier arrangement has a carrier frame and an electrode frame, where at least one electrode is detachably fastened to the electrode frame.

The present invention relates to a method for the production of drill holes in difficult to machine materials, in which a removal of material takes place in order to produce a drill hole by electrochemical erosion of material by an electrode that is moved in the longitudinal direction of the drill hole being produced in the direction onto the material to be processed at a feed rate, wherein the drilling has at least two steps, wherein, in the first step, the electrochemical processing takes place, and wherein, in a second step, the further processing of the drill hole to the final diameter takes place by machining processing or by erosion or by an electrochemical processing.

An electrolyte solution is provided for an electrochemical machining process. The electrolyte solution includes a substantially water free ionic solvent, an ionisable material in the form of an inorganic salt; and a viscosity modifier. The electrolyte has a viscosity in the range of 1 to 50 mPa.Math.s at 20° C.

An electrolyte solution is provided for an electrochemical machining process. The electrolyte solution includes a substantially water free ionic solvent, an ionisable material in the form of an inorganic salt; and a viscosity modifier. The electrolyte has a viscosity in the range of 1 to 50 mPa.Math.s at 20° C.

A discretized-flow electrode for use in electrochemical machining (ECM) and a corresponding method and system for using the discretized-flow cathode are disclosed. The machining face of the discretized-flow cathode is divided into a plurality of discrete sections. The discrete sections may be geometrically shaped, and they are separated at the machining face by an electrolyte flow outlet channel, and each discrete section includes an electrolyte flow inlet local to the discrete section. The plurality of discrete sections of the machining face of the discretized-flow electrode divide the electrolyte flow into approximately equal portions for even electrolyte flow across the machining face.

A method of forming a gas turbine engine component including an airfoil and at least one shroud includes the steps of (1) machining a gas path surface of the at least one shroud utilizing a non-electrochemical machining (ECM) process, and (2) then utilizing ECM on at least the airfoil.

A method of forming a gas turbine engine component including an airfoil and at least one shroud includes the steps of (1) machining a gas path surface of the at least one shroud utilizing a non-electrochemical machining (ECM) process, and (2) then utilizing ECM on at least the airfoil.

The present disclosure relates to electrochemical erosion of material from a workpiece. For example, a device for electrochemical erosion of material from a workpiece may include: a holder for the workpiece; an electrolyte carrier material impregnated with electrolyte; a voltage source imposing a negative potential on the electrolyte carrier; and a mechanical connection between the holder and the electrolyte carrier allowing a relative movement with at least one degree of freedom.

The present disclosure relates to electrochemical erosion of material from a workpiece. For example, a device for electrochemical erosion of material from a workpiece may include: a holder for the workpiece; an electrolyte carrier material impregnated with electrolyte; a voltage source imposing a negative potential on the electrolyte carrier; and a mechanical connection between the holder and the electrolyte carrier allowing a relative movement with at least one degree of freedom.