US Patent 10584715 Gas turbine engine airfoil
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Patent abstract
An airfoil of a turbine engine 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 stagger angle and span position that defines a curve with a stagger angle that is greater than 35° from 0% span to at least 50% span.
Edits on 22 Mar, 2023
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Patent Jurisdiction
Patent Number
105847150
Date of Patent
March 10, 2020
0Patent Application Number
151149220
Date Filed
February 12, 2015
0Patent Primary Examiner
Edits on 28 Sep, 2022
Golden AI
Infobox
Is a
Patent Jurisdiction
Patent Number
105847150
Date of Patent
March 10, 2020
0Patent Application Number
151149220
Date Filed
February 12, 2015
0Patent Primary Examiner
Edits on 2 Feb, 2022
Golden AI
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US Patent 10584715 Gas turbine engine airfoil
Infobox
Is a
Patent jurisdiction
Patent number
10584715
Date of patent
March 10, 2020
Patent application number
15114922
Date Filed
February 12, 2015
Patent primary examiner
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