COOLED POLYMER GAS TURBINE ENGINE COMPONENT AND CORRESPONDING MANUFACTURING METHOD
A polymer gas turbine engine component, e.g. an airfoil assembly, is disclosed and includes at least one cooling passage (50) for circulating coolant to remove heat from the polymer component. A corresponding method of manufacturing is also provided.
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Published patent application
Disclosure date: 12-12-2018
Publication date: 06-19-2019
Applicant: HAMILTON SUNDSTRAND CORP, US
Inventor: PEARSON MATTHEW ROBERT PEARSON, US
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