A heat transfer apparatus for a gas turbine engine includes: a component having a wall structure defining a flow bounding surface; a chamber formed in the component, the chamber including a wicking structure, a vapor channel, and a working fluid.

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Patent Inventor Names

James Michael Kostka0

Jeffrey Douglas Rambo0

John William Moores0

William Dwight Gerstler0

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Patent Citations Received

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US Patent 11765871 Aircraft and method for thermal management

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US Patent 09909448 Gas turbine engine component with integrated heat pipe US Patent 9909448 Gas turbine engine component with integrated heat pipe

Infobox

Patent Number

09909448

Patent Number

9909448

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US Patent 09909448 Gas turbine engine component with integrated heat pipe

Infobox

Is a

Patent

Patent jurisdiction

United States Patent and Trademark Office

Patent number

09909448

Date of patent

March 6, 2018

Patent application number

14686799

Date Filed

April 15, 2015

Patent primary examiner

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Igor Kershteyn

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