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IMPINGEMENT COOLING BAFFLE

  • US 20170175578A1
  • Filed: 12/21/2015
  • Published: 06/22/2017
  • Est. Priority Date: 12/21/2015
  • Status: Active Grant
First Claim
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1. A component for a gas turbine engine, comprising:

  • a first component end;

    a second component end;

    a cavity extending from the first component end to the second component end; and

    a baffle assembly located in the cavity including;

    a first baffle portion inserted into the cavity; and

    a second baffle portion inserted into the cavity;

    the first baffle portion overlapping the second baffle portion.

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