Turbine engine vane with asymmetrical profile
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United States of America Patent
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Oct 10, 2017
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N/A
app pub date -
Oct 10, 2014
filing date -
Oct 11, 2013
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Abstract
The invention relates to a turbine engine vane comprising a main body made of composite material, a leading edge, a trailing edge, and at least one metal structural reinforcement, the structural reinforcement comprising a junction surface portion connected to the main body, the structural reinforcement extending between the junction surface portion and one of the leading or trailing edges, the vane being characterized in that the profile of the junction surface portion of the structural reinforcement has a camber less than 30%.
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