Integral bladed disk

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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170/72

F02C 7/00 (2006.01)

Patent

CA 1229797

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 opera- tion. Alternatively, the blades may be joined to the hub thereafter by an electron beam weld that extends axially to the rotor.

491973

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