Air cooler for gas turbine engine
Number of patents in Portfolio can not be more than 2000
United States of America
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Mar 15, 2022
Grant Date -
Nov 26, 2020
app pub date -
May 24, 2019
filing date -
May 24, 2019
priority date (Note) -
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Abstract
A turbofan engine comprising an outer bypass duct, an annular bypass flow path between the outer bypass duct and a core engine, an engine component forming an airflow obstruction adjacent the outer bypass duct, an air cooler having a tube, the tube having at least a sinuous portion extending in the annular bypass flow path, the sinuous portion extending along the outer bypass duct, downstream of the airflow obstruction, the sinuous portion configured for exchanging heat between a fluid circulating in the tube and air circulating in the bypass flow path during operation of the turbofan engine.
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