US Patent 9039382 Blade skirt
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Patent abstract
A blade of a gas turbine engine is provided having an airfoil, a platform, a shank, a dovetail, and a skirt. The airfoil may extend distally from the platform, and the shank may extend proximally from the platform. The dovetail may also be provided to extend proximally from the shank. The skirt may be disposed on an aft side of the shank and may extend from the shank in a direction at least partially axially aft from the shank.
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US Patent 09039382 Blade skirt US Patent 9039382 Blade skirt
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Patent Number
0903938200
Patent Number
903938200
Edits on 20 May, 2023
Golden AI
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Official Website
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Patent Jurisdiction
Patent Number
090393820
Date of Patent
May 26, 2015
0Patent Application Number
133064130
Date Filed
November 29, 2011
0Official Website
Patent Primary Examiner
Edits on 27 Sep, 2022
Golden AI
Infobox
Is a
Patent Jurisdiction
Patent Number
090393820
Date of Patent
May 26, 2015
0Patent Application Number
133064130
Date Filed
November 29, 2011
0Official Website
Patent Primary Examiner
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US Patent 09039382 Blade skirt
Infobox
Is a
Patent jurisdiction
Patent number
09039382
Date of patent
May 26, 2015
Patent application number
13306413
Date Filed
November 29, 2011
Patent primary examiner
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