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US 4,538,331 AGranted
Method of manufacturing an integral bladed turbine disk
AssigneeWilliams International Corporation
InventorsMichael J. Egan, Gary J. Quill
Life of this patent
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Abstract
The disclosure relates to a turbine rotor and method of manufacture thereof. A plurality of blades having dovetails at the radially inner ends thereof are arranged in a circumferentially spaced circular array. A metallic hub is cast about the dovetails of said blades which are metallurgically bonded by the operation. Alternatively, the blades may be joined to the hub thereafter by an electron beam weld that extends axially to the rotor.
Claims1
A method of making a turbine rotor comprising the steps of
- arranging a plurality of blades having dovetails at the radially inner ends thereof in circumferentially spaced circular array,
- coating the dovetails of said blades with a diffusion bonding material comprising an Ni-Cr-B alloy,
- casting a metallic hub about the dovetails of said blades resulting in a diffusion bond between said hub and the dovetails of said blades, and
- directing an electron beam of relatively narrow radial dimension in a direction parallel to the central axis of said hub and through a zone of relatively small radial dimension spaced radially inwardly from the outer perimeter of said hub and encompassing the radially innermost portion only of the diffusion bond between the dovetails of said blades and said hub thereby to modify the grain structure of the diffusion bond in said zone from a granular to a columnar configuration and move any voids in said diffusion bond zone radially outwardly to enhance vibration dampening.
1 more element
Dependencies are inferred from the claim text.