GAS TURBINE ENGINE COMPONENT
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United States of America
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Issued Date -
Jan 23, 2020
app pub date -
Feb 12, 2019
filing date -
Feb 12, 2019
priority date (Note) -
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status (Latency Note)
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Abstract
There is disclosed a component arranged to extend across a bypass duct (22) of a gas turbine engine (10), comprising: an outlet guide vane (24); and a structural support (26) arranged to structurally support a radially inner component of the gas turbine engine (10). The outlet guide vane (24) and the structural support (26) are contiguous at a merged portion (32) which is at a radially outer region of the component.
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