Seal assembly

Rotary kinetic fluid motors or pumps – Including thermal expansion joint

Reexamination Certificate

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Details

C415S136000, C415S137000, C415S138000, C415S139000

Reexamination Certificate

active

07445425

ABSTRACT:
A seal arrangement32between a turbine shroud seal segments38,40in a gas turbine engine. The arrangement32comprises facing slots34, 36provided respectively in the segments38,40with offset spaces42, 44provided between the segments38,40. A strip46is cemented into the slot36such that the flow path50passes through the space42, around the free end of the strip46, and out through the offset space44, thereby providing a longer flow path.

REFERENCES:
patent: 3970318 (1976-07-01), Tuley
patent: 4688988 (1987-08-01), Olsen
patent: 5167485 (1992-12-01), Starkweather
patent: 5531457 (1996-07-01), Tibbott et al.
patent: 5997247 (1999-12-01), Arraitz et al.
patent: 6439844 (2002-08-01), Turnquist et al.
patent: 1047208 (1966-11-01), None
patent: A 10-274003 (1998-10-01), None
patent: A 2003-129803 (2003-05-01), None

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