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

F - Mech Eng,Light,Heat,Weapons – 01 – D

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F01D 9/02 (2006.01) F01D 11/00 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2024721

13DV-9093 SELF-COOLING JOINT CONNECTION FOR ABUTTING SEGMENTS IN A GAS Abstract of the Disclosure A joint connection for abutting, circumfer- entially 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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