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Method and apparatus for cooling a wall within a gas turbine engine

  • US 6,514,042 B2
  • Filed: 09/26/2001
  • Issued: 02/04/2003
  • Est. Priority Date: 10/05/1999
  • Status: Expired due to Term
First Claim
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1. A cooling circuit disposed between a first wall portion and a second wall portion of a wall for use in a gas turbine engine, comprising:

  • a plurality of first pedestals extending between said first wall portion and said second wall portion, and arranged in rows, and wherein adjacent said first pedestals in the same said row are separated from one another by an intra-row distance;

    wherein said first pedestals in adjacent said rows are separated by an inter-row distance, and said intra-row distance is equal to or greater than one and one-half times said inter-row distance;

    one or more inlet apertures disposed in said wall providing a cooling air flow path into said cooling circuit; and

    one or more exit apertures disposed in said wall providing a cooling air flow path out of said cooling circuit.

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