Sideplates for rotor disk and rotor blades

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received in well or slot

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Details

F01D 518, F01D 530

Patent

active

042795729

ABSTRACT:
A rotor sideplate for inhibiting the leakage of fluid mediums across a blade and disk assembly of a gas turbine engine is disclosed. Techniques for preventing the leakage of working medium gases across the assembly beneath the platforms and for preventing the leakage of turbine cooling air are developed. Various construction details which enhance the fatigue performance of the sideplate are developed. The sideplate is supported from the rotor disk at more than one support point.

REFERENCES:
patent: 3181835 (1965-05-01), Davis
patent: 3395891 (1968-08-01), Burge et al.
patent: 3501249 (1970-03-01), Scalzo et al.
patent: 3644058 (1972-02-01), Barnabel
patent: 3728042 (1973-04-01), Hugoson
patent: 3748060 (1973-07-01), Hugoson
patent: 3751183 (1973-08-01), Nichols
patent: 3752598 (1973-08-01), Bowers
patent: 3841792 (1974-10-01), Amos
patent: 4021138 (1977-05-01), Scalzo et al.
patent: 4171930 (1979-10-01), Brisken et al.

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