US Patent 9422815 Gas turbine engine component with compound cusp cooling configuration
Patent 9422815 was granted and assigned to United Technologies on August, 2016 by the United States Patent and Trademark Office.
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Patent abstract
A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.
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US Patent 09422815 Gas turbine engine component with compound cusp cooling configuration US Patent 9422815 Gas turbine engine component with compound cusp cooling configuration
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Patent Number
0942281500
Patent Number
942281500
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
094228150
Date of Patent
August 23, 2016
0Patent Application Number
135442270
Date Filed
July 9, 2012
0Official Website
Patent Primary Examiner
Edits on 24 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
094228150
Date of Patent
August 23, 2016
0Patent Application Number
135442270
Date Filed
July 9, 2012
0Official Website
Patent Primary Examiner
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US Patent 09422815 Gas turbine engine component with compound cusp cooling configuration
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
09422815
Date of patent
August 23, 2016
Patent application number
13544227
Date Filed
July 9, 2012
Patent primary examiner
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