Exhaust duct of gas turbine engine
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United States of America
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Mar 29, 2022
Grant Date -
Mar 17, 2022
app pub date -
Sep 17, 2020
filing date -
Sep 17, 2020
priority date (Note) -
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Abstract
An exhaust duct of a gas turbine engine comprises a hub defining a radially-inner surface of a substantially annular exhaust gas path, and a strut extending into the exhaust gas path. The strut is attached to the hub via a first fastener at a forward fastening location closer to a leading edge of the strut than to a trailing edge of the strut, and via a second fastener at an aft fastening location closer to the trailing edge than to the leading edge. The second fastener is engaged with an appendage of the strut. The appendage is received into a receptacle formed in the hub open to the radially-inner surface.
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