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Wall elements for gas turbine engine combustors

  • US 6,408,628 B1
  • Filed: 11/02/2000
  • Issued: 06/25/2002
  • Est. Priority Date: 11/06/1999
  • Status: Expired due to Term
First Claim
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1. A wall element for a wall structure of a gas turbine engine combustor with the engine having a principal axis, the wall element comprising a base portion having an axis which in use, extends generally parallel to the principal axis of the engine, wherein the dimension of said wall element parallel to said axis thereof is greater then substantially 20% of the dimension of the wall element transverse to said axis of the wall element, and the base portion includes a plurality of rows of mixing ports to allow gas to enter the combustor in use.

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