Ceramic blade attachment system

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received by continuous circumferential channel

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416214R, 416205, F01D 530

Patent

active

054315417

ABSTRACT:
A turbine blade having a preestablished rate of thermal expansion is attached to a turbine disc having a preestablished rate of thermal expansion being greater than the preestablished rate of thermal expansion of the turbine blade and forms a turbine assembly. The turbine blade has a root portion defining a pair of sides having a pair of grooves therein. The turbine assembly includes a pair of flanges between which the turbine blades are positioned. Each of the pair of flanges has a plurality of grooves defined therein. The grooves within the pair of flanges are aligned with the grooves in the blades and have a space formed therebetween. A plurality of spherical balls are positioned within the space. The plurality of spherical balls has a preestablished rate of thermal expansion being equal to the preestablished rate of thermal expansion of the turbine blade.

REFERENCES:
patent: 3490537 (1970-01-01), Quenneville
patent: 4717312 (1988-01-01), Seeley
patent: 4850801 (1989-07-01), Valentine
patent: 5118256 (1992-06-01), Violette et al.

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