Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Circumferentially spaced nozzle or stator segments
Patent
1993-11-08
1995-01-10
Brown, David
Rotary kinetic fluid motors or pumps
Including thermal expansion joint
Circumferentially spaced nozzle or stator segments
415116, F01D 1108, F01D 900, F02C 712
Patent
active
053801504
ABSTRACT:
A turbine shroud segment includes a center hook along one edge which retains the segment to the turbine structure while permitting thermal distortion of the segment. In a particular embodiment, a segment includes a pair of spaced center hooks, a first lateral hook, and a second lateral hook disposed oppositely of the first lateral hook. The spaced center hooks retain the segment and prevent radially inward movement of the center region of the segment. The lateral hooks provide supplemental retention while permitting the lateral edges of the segment to move radially outward in response to thermal distortion of the segment.
REFERENCES:
patent: 3365172 (1968-01-01), McDonough et al.
patent: 3583824 (1971-06-01), Smuland et al.
patent: 3728039 (1973-04-01), Plemmons et al.
patent: 4013376 (1977-03-01), Bisson et al.
patent: 4311432 (1982-01-01), Kildea
patent: 4497610 (1985-02-01), Richardson et al.
patent: 4573865 (1986-03-01), Hsia et al.
patent: 4642024 (1987-02-01), Weidner
patent: 4752184 (1988-06-01), Liang
patent: 4992025 (1991-02-01), Stroud et al.
patent: 5088888 (1992-02-01), Bobo
patent: 5165847 (1992-11-01), Proctor et al.
patent: 5167485 (1992-12-01), Starkweather
patent: 5167487 (1992-12-01), Rock
patent: 5167488 (1992-12-01), Ciokajlo et al.
patent: 5169287 (1992-12-01), Proctor et al.
patent: 5318402 (1994-06-01), Bailey et al.
Brown David
United Technologies Corporation
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