Self-cooling joint connection for abutting segments in a gas tur

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

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415138, 415139, F01D 904

Patent

active

051674858

ABSTRACT:
A joint connection for abutting, circumferentially extending segments in a gas turbine engine, such as turbine nozzle segments, includes a sealing member which is insertable between longitudinally extending slots formed in the abutting side edges of two adjacent segments. The segments are each formed with a number of grooves which are longitudinally spaced along the length of the slots therein, and which extend beneath the sealing member carried within the slots. A cooling air flow path is thus formed extending from one side of the sealing member, into the longitudinal slot of each segment and then through the grooves to the opposite side of the sealing member so that the entire joint connection or seal region between the abutting side edges of the segments is cooled.

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patent: 4688988 (1987-08-01), Olsen
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