Diffused holes for inter-segment purge and method
AssigneeRtx Corporation
InventorsWinston SMIDDY, Howard LILES, Alex SCHNEIDER
Life of this patent
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AssigneeRtx Corporation
InventorsWinston SMIDDY, Howard LILES, Alex SCHNEIDER
Estimating the term…
A ceramic matrix composite (CMC) component segment forming a portion of a substantially ring-shaped gas turbine engine stage includes a mateface extending axially between an upstream end and a downstream end of the CMC component and configured to form an inter-segment gap with an adjacent CMC component, and a plurality of film cooling holes having diffused openings at the mateface to provide film cooling of the mateface. A method of providing an inter-segment purge flow to such a CMC component includes disposing a first mateface of the CMC component segment next to a second mateface of an adjacent CMC component segment to form an inter-segment gap, and providing first film cooling of the first mateface via the plurality of film cooling holes having diffused openings at the first mateface.
A ceramic matrix composite (CMC) component forming a portion of a substantially ring-shaped gas turbine engine stage, the CMC component comprising:
(canceled)
A ceramic matrix composite (CMC) blade outer air seal (BOAS) segment forming a portion of a substantially ring-shaped BOAS stage, the CMC BOAS segment comprising:
A method of providing an inter-segment purge flow to a ceramic matrix composite (CMC) component segment forming a portion of a substantially ring-shaped gas turbine engine stage, the method comprising:
(canceled)
Dependencies are inferred from the claim text.