US Patent 11391294 Gas turbine engine airfoil
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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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Patent Number
113912940
Date of Patent
July 19, 2022
0Patent Application Number
167221640
Date Filed
December 20, 2019
0Patent Citations
Patent Primary Examiner
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US Patent 11391294 Gas turbine engine airfoil
Article
A compressor airfoil of a turbine engine having a geared architecture includes pressure and suction sides that extend in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a tangential stacking offset and span position that defines a curve that is non-linear.
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Patent jurisdiction
Patent number
11391294
Date of patent
July 19, 2022
Patent application number
16722164
Date Filed
December 20, 2019
Patent citations
Patent primary examiner
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