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United States of America Patent

PATENT NO 10287987
APP PUB NO 20140348630A1
SERIAL NO

14204983

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Abstract

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A gas turbine engine includes a first airflow structure and a second airflow structure disposed aft of the first airflow structure. The second airflow structure includes a leading edge region. A thickness of the leading edge region is based on a thickness of a wake in the airflow produced by the first airflow structure when the airflow passes between the first airflow structure and the second airflow structure.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Atassi, Oliver V Longmeadow, US 27 297
Baltas, Constantine Manchester, US 17 238

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