Gas-path leakage seal for a turbine

Seal for a joint or juncture – Seal between fixed parts or static contact against... – Contact seal for other than internal combustion engine – or...

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277643, 277644, 277649, 277651, 277653, F16J 1502

Patent

active

059346876

ABSTRACT:
A gas-path leakage seal for generally sealing a gas-path leakage-gap between spaced-apart first and second members of a turbine (such as combustor casing segments of a gas turbine). The seal includes a flexible and generally imperforate metal sheet assemblage having opposing first and second surfaces and two opposing raised edges extending a generally identical distance above and below the surfaces. A first cloth layer assemblage has a thickness generally equal to the previously-defined identical distance and is superimposed on the first surface between the raised edges. A second cloth layer assemblage is generally identical to the first cloth layer assemblage and is superimposed on the second surface between the raised edges.

REFERENCES:
patent: 2249127 (1941-07-01), Goetze
patent: 2687909 (1954-08-01), Blackman et al.
patent: 2764311 (1956-09-01), Blackman
patent: 4063845 (1977-12-01), Allen
patent: 5125796 (1992-06-01), Cromer
patent: 5509669 (1996-04-01), Wolfe et al.
patent: 5586773 (1996-12-01), Bagepalli
patent: 5607167 (1997-03-01), Franckx
Application entitled, "Gas-Path Leakage Seal For a Gas Turbine", filed Dec. 14, 1995, Serial No. 08/572,355.

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