STATOR VANE
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United States of America Patent
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Issued Date -
Jul 27, 2017
app pub date -
Jan 19, 2017
filing date -
Jan 21, 2016
priority date (Note) -
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status (Latency Note)
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Abstract
Stator vane for a turbine engine and including at least one portion made from material suitable for superelasticity. The portion made from material suitable for superelasticity is arranged so as to start to resonate at a predetermined speed of the turbine engine, in particular during a speed of the turbine engine typical of the cruising phase of the aircraft.
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