US Patent 10590775 Gas turbine engine airfoil
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Patent abstract
An airfoil of a turbine engine includes pressure and suction sides and extends in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a stagger angle and span position that defines a curve with a stagger angle that is greater than 32° from 90% span to 100% span.
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Patent Inventor Names
Edward J. Gallagher0
Joseph C. Straccia0
Kate Hudon0
Lisa I. Brilliant0
Mark A. Stephens0
Stanley J. Balamucki0
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US Patent 10590775 Gas turbine engine airfoil
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Is a
Patent jurisdiction
Patent number
10590775
Date of patent
March 17, 2020
Patent application number
15115501
Date Filed
February 12, 2015
Patent primary examiner
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