US Patent 10577955 Airfoil assembly with a scalloped flow surface
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Patent abstract
A stage for a compressor or a turbine in a turbine engine can include an annular row of airfoils radially extending from corresponding platforms, where each platform can include a fore edge and aft edge and each airfoil can include a leading edge and trailing edge. At least one of the platforms can have a scalloped flow surface including a bulge and a trough.
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Patent Inventor Names
Connor Marie Shirley0
Harjit Singh Hura0
Paul Hadley Vitt0
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Patent Jurisdiction
Patent Number
105779550
Date of Patent
March 3, 2020
0Patent Application Number
156377910
Date Filed
June 29, 2017
0Patent Primary Examiner
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US Patent 10577955 Airfoil assembly with a scalloped flow surface
Infobox
Is a
Patent jurisdiction
Patent number
10577955
Date of patent
March 3, 2020
Patent application number
15637791
Date Filed
June 29, 2017
Patent primary examiner
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