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GAS TURBINE ENGINE HAVING A MISTURNED STAGE

  • US 20160017796A1
  • Filed: 02/13/2014
  • Published: 01/21/2016
  • Est. Priority Date: 02/21/2013
  • Status: Active Grant
First Claim
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1. A stage of a gas turbine engine, comprising:

  • a row of flow directing components circumferentially disposed about a centerline axis; and

    at least one flow directing component of said row having at least one design characteristic that is dissimilar from a corresponding design characteristic of at least one other flow directing component of said row.

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