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Turbine engine shroud assembly including axially floating shroud segment

  • US 6,884,026 B2
  • Filed: 09/30/2002
  • Issued: 04/26/2005
  • Est. Priority Date: 09/30/2002
  • Status: Expired due to Term
First Claim
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1. A turbine engine shroud segment for assembly circumferentially about an axial flow engine axis, separate and spaced apart from any blading member, the shroud segment comprising a shroud segment body including a radially inner surface arcuate at least circumferentially, a radially outer surface, and at least one shroud segment support integral with the shroud segment body for carrying the shroud segment body, the segment support projecting generally radially outwardly from the shroud segment body radially outer surface, wherein:

  • the shroud segment is separate and spaced apart from any blading member;

    the radially inner surface defines a part of a turbine engine flowpath boundary over rotating blading members; and

    , the shroud segment support includes therein a support wall surface extending generally axially into and at least partially through the segment support.

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