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THERMOELECTRIC GENERATOR IN TURBINE ENGINE NOZZLES

  • US 20130205798A1
  • Filed: 02/15/2012
  • Published: 08/15/2013
  • Est. Priority Date: 02/15/2012
  • Status: Active Grant
First Claim
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1. A core nozzle for a gas turbine engine, comprising:

  • a core nozzle wall defining a core through which a core stream flows; and

    a cowling assembly coupled to the core nozzle wall, wherein the core nozzle wall and the cowling assembly define a plenum to receive a portion of the core stream flow from the core nozzle; and

    a thermoelectric generator assembly positioned in the plenum.

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