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Combustion apparatus

  • US 6,708,499 B2
  • Filed: 02/22/2002
  • Issued: 03/23/2004
  • Est. Priority Date: 03/12/2001
  • Status: Expired due to Term
First Claim
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1. A wall element for use as part of a gas turbine engine combustor wall structure, the wall element including inner and outer walls defining a space therebetween, the inner wall being of cast construction and including a plurality of cooling apertures provided therethrough and formed during the casting process.

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