COMPOSITE VANE FOR A TURBINE ENGINE
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United States of America Patent
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app pub date -
Oct 29, 2014
filing date -
Oct 31, 2013
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Abstract
A composite vane for a turbine engine, the vane having a pressure side face (12) and a suction side face (14) that define the aerodynamic profile of the vane, the vane (10) comprising: a metallic core (20) forming the pressure side face (12) or the suction side face (14) of the vane; and an organic matrix (30) associated with the metallic core (20).
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