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SEAL SEGMENT FOR A GAS TURBINE ENGINE

  • US 20170022840A1
  • Filed: 07/25/2016
  • Published: 01/26/2017
  • Est. Priority Date: 07/24/2015
  • Status: Active Grant
First Claim
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1. A gas turbine engine, comprising:

  • a housing;

    at least one compressor positioned within the housing;

    at least one turbine operably coupled to the at least one compressor and including a plurality of blades extending radially from a longitudinal axis of the engine; and

    a seal segment positioned along a portion of the housing and comprising;

    a radially outer wall having a first length extending annularly around a portion of the engine;

    a radially inner wall positioned intermediate the outer wall and the portion of the engine and having a second length; and

    a rib member extending between the outer wall and the inner wall and along the first and second lengths.

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