Seal for a joint or juncture – Seal between relatively movable parts – Relatively rotatable radially extending sealing face member
Patent
1978-03-14
1979-07-17
Ward, Jr., Robert S.
Seal for a joint or juncture
Seal between relatively movable parts
Relatively rotatable radially extending sealing face member
277 74, 277134, 415110, 415172A, 60 3966, F01D 1104, F16J 1540
Patent
active
041613180
ABSTRACT:
Turbine blade shrouds are sealed by injecting air on to the shroud immediately upstream of a shroud seal. This air serves two purposes: it creates a turbulent flow immediately upstream of the shroud seal, thus spoiling and reducing the leakage flow over the seal, and the hot gases which would otherwise leak over the seal are replaced by the cooler air, thus reducing energy wastage and improving S.F.C. (specific fuel consumption).
REFERENCES:
patent: 2685429 (1954-08-01), Auyer
patent: 2963268 (1960-12-01), Smile et al.
patent: 2988325 (1961-06-01), Dawson
patent: 3189320 (1965-06-01), Beldecos et al.
patent: 3239193 (1966-03-01), Kerensky
patent: 3279378 (1966-10-01), Sproule
patent: 3437313 (1969-04-01), Moore
patent: 3756740 (1973-09-01), Deich et al.
patent: 3927951 (1975-12-01), Mitsuhashi
Stratford Brian S.
Stuart Alan R.
Rolls-Royce Limited
Ward, Jr. Robert S.
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