Turbine or compressor blade mounting

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

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Details

416219R, F01D 530

Patent

active

046454250

ABSTRACT:
In a turbine or compressor blade and supporting disk assembly in which the assembly is by tangential positioning of the blades, the cooperating blade root and groove in the disk have base surfaces that are held in spaced relation to each other by a rib on the blade root extending toward the base surface of the groove and into contact with it.

REFERENCES:
patent: 2211866 (1940-08-01), Soderberg
patent: 2225769 (1940-12-01), Conrad
patent: 2240742 (1941-05-01), Allen
patent: 2809801 (1957-10-01), Curry
patent: 3216700 (1965-11-01), Bostock, Jr.
patent: 3584971 (1971-06-01), Ortolano
patent: 3610778 (1971-10-01), Suter

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