Method for the repair of a compressor rotor designed in blisk technology
With a method for the repair of compressor rotors designed in blisk technology the damaged stage is severed from the rotor, and a new blisk is joined to the rotor by electron-beam welding. For stress relieving the rotor is subjected to local thermal treatment by means of a current produced in the weld area by electro-magnetic induction.
1. A method for repairing a compressor rotor designed in blisk technology and having a plurality of blisks joined together to form a one-piece assembly, comprising:
severing from the rotor and removing an entire damaged stage of a blisk having integral blades, the severing being performed away from the integral blades;
replacing the entire damaged stage of the blisk with an undamaged blisk stage;
joining the undamaged blisk stage to the rotor by electron-beam welding; and
subsequently to the electron-beam welding and not before or during the electron-beam welding, subjecting only a weld joint and a locally confined area adjacent to the weld joint which has been affected by a heat of the weld to local stress-relieving thermal treatment by a current induced into the component by electro-magnetic induction for heat generation, the current induced into the component for heat generation being confined to the weld joint and the locally confined area adjacent to the weld joint such that a temperature required for the stress-relieving thermal treatment is produced only in the weld joint and locally confined area adjacent to the weld joint, peripherally along the weld joint, away from the integral blades.
2. A method in accordance with claim 1 , wherein the weld joint is inspected and subjected to mechanical rework, if necessary.
3. A method for manufacturing blisk rotors designed in blisk technology and having a plurality of blisks joined together to form a one-piece assembly, comprising:
joining an entire stage of a blisk having integral blades to a rotor sub-assembly by electron-beam welding along a peripheral joint away from the integral blades; and
subsequently to the electron-beam welding and not before or during the electron-beam welding, subjecting only a weld joint and a locally confined area adjacent to the weld joint which has been affected by a heat of the weld to local stress-relieving thermal treatment by a current induced into the component by electro-magnetic induction for heat generation, the current induced into the component for heat generation being confined to the weld joint and the locally confined area adjacent to the weld joint such that a temperature required for the stress-relieving thermal treatment is produced only in the weld joint and locally confined area adjacent to the weld joint, peripherally along the weld joint, away from the integral blades.
4. A method for repairing a compressor rotor designed in blisk technology and having a plurality of blisks joined together to form a one-piece assembly, comprising:
severing from the rotor and removing an entire damaged stage of a blisk having integral blades, the severing being performed away from the integral blades;
replacing the entire damaged stage of the blisk with an undamaged blisk stage;
joining the undamaged blisk stage to the rotor by electron-beam welding; and
only after the electron-beam welding, subjecting only a weld joint and a locally confined area adjacent to the weld joint which has been affected by a heat of the weld to local stress-relieving thermal treatment by a current induced into the component by electro-magnetic induction for heat generation, the current induced into the component for heat generation being confined to the weld joint and the locally confined area adjacent to the weld joint such that a temperature required for the stress-relieving thermal treatment is produced only in the weld joint and locally confined area adjacent to the weld joint, peripherally along the weld joint, away from the integral blades.