US Patent 10352177 Airfoil having impingement openings
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Patent abstract
An airfoil for a turbine engine having a perimeter wall bounding an interior and defining a pressure side and a suction side, a radially extending rib located within the interior and spaced from the leading edge to define a radially extending leading edge chamber, and at least one impingement opening in the rib defining a flow path aligned with the leading edge.
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Patent Inventor Names
Robert David Briggs0
Ronald Scott Bunker0
Timothy Deryck Stone0
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Patent Citations Received
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Patent Jurisdiction
Patent Number
103521770
Date of Patent
July 16, 2019
0Patent Application Number
150446970
Date Filed
February 16, 2016
0Official Website
Patent Citations Received
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US Patent 10352177 Airfoil having impingement openings
Infobox
Is a
Patent jurisdiction
Patent number
10352177
Date of patent
July 16, 2019
Patent application number
15044697
Date Filed
February 16, 2016
Patent primary examiner
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