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COMPOSITE RETENTION FEATURE

  • US 20150044054A1
  • Filed: 12/02/2013
  • Published: 02/12/2015
  • Est. Priority Date: 03/15/2013
  • Status: Active Grant
First Claim
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1. A retention feature for use in a gas turbine engine comprisinga ceramic post including a body adapted to be coupled to a turbine engine component and a head coupled to the body, the head formed to include a space,a first insert arranged in the space, anda first braze layer extending from the ceramic post to the first insert to bond the first insert to the ceramic post.

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