GAS TURBINE ENGINE OUTLET GUIDE VANES
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United States of America
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Issued Date -
Jan 16, 2020
app pub date -
Jun 25, 2019
filing date -
Jun 25, 2019
priority date (Note) -
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Abstract
The present disclosure relates to outlet guide vanes in a gas turbine engine, and in particular to such vanes with particular ranges of relative dimensions. Example embodiments include a gas turbine engine (10) comprising a plurality of outlet guide vanes (31) each having a length extending across a bypass duct (22) of the gas turbine engine (10), wherein for each outlet guide vane a minimum thickness to chord ratio is less than 80% of a maximum thickness to chord ratio.
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