Method and apparatus for etching the surfaces of integrally bladed rotors

摘要

For electrolytically etching the surfaces of integrally bladed rotors (blisks) (6) made of nickel-base material for aircraft gas turbines, auxiliary cathodes (10), in addition to the main cathodes (3) provided in the electrolyte (1), are arranged in the area of the blades (9) remote from the electric contact points at the rotor disk (7). The auxiliary cathodes are adaptable in shape, arrangement and size to the blade and disk geometry, so that a uniform current flow from all parts of the rotor connected as anode via the electrolyte to the main and auxiliary cathodes is produced and an intense and uniform etching effect is achieved. This ensures a reliable structural assessment in all rotor areas and in particular also in the area of the integral blading.

主权项

1. An apparatus for etching surfaces of an integrally bladed rotor made of a nickel-base material for an aircraft gas turbine, comprising:
an electrical source; a container containing an electrolyte; at least one main cathode positioned in the electrolyte and connected to the electrical source; a holding device for holding an integrally bladed rotor to be subjected to surface etching in the electrolyte, the holding device including a contacting and retaining device for contacting a rotor disk of the integrally bladed rotor and connecting the integrally bladed rotor to the electrical source as an anode; at least one auxiliary cathode positioned in the electrolyte in an area of the blades integrally formed onto the rotor disk and connected to the electrical source, and the at least one auxiliary cathode being adapted in form, size and arrangement to a blade geometry, to create a generally uniform current flow from all parts of the rotor via the electrical source, the integrally bladed rotor as the anode and the electrolyte to the at least one main and auxiliary cathode and produce an intense and generally uniform etching effect on the rotor; the at least one main cathode extending in a radial direction of the rotor from a blade tip of the rotor to an opposite blade tip of the rotor to extend across an entirety of a diameter of the rotor, the at least one auxiliary cathode being an annual disc having an outer radius positioned generally adjacent a blade tip region of the rotor and an inner radius positioned before reaching a center axis of the integrally bladed rotor to leave a central portion of the integrally bladed rotor uncovered by the at least one auxiliary cathode, the at least one auxiliary cathode extending in a radial direction of the rotor from the outer radius to the inner radius to substantially correspond to at least a radial height of the blades of the rotor; wherein at least a portion of the at least one auxiliary cathode is positioned between a position of the integrally bladed rotor and the at least one main cathode such that a straight line of shortest distance extending from the position of the integrally bladed rotor in at least one portion of the area of the blades must pass through the at least one auxiliary cathode before touching the at least one main cathode.