US Patent 9212560 CMC blade with integral 3D woven platform
Patent 9212560 was granted and assigned to United Technologies on December, 2015 by the United States Patent and Trademark Office.
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Patent abstract
A method of forming a component for use in a gas turbine engine includes the steps of forming an airfoil/root assembly; creating a platform assembly structure having an opening; inserting the airfoil/root assembly into the opening; and bonding the platform assembly structure to the airfoil/root assembly to form the component.
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US Patent 09212560 CMC blade with integral 3D woven platform US Patent 9212560 CMC blade with integral 3D woven platform
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Patent Number
092125600
Patent Number
92125600
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Current Assignee
Patent Jurisdiction
Patent Number
092125600
Date of Patent
December 15, 2015
0Patent Application Number
131733080
Date Filed
June 30, 2011
0Official Website
Patent Primary Examiner
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US Patent 09212560 CMC blade with integral 3D woven platform
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
09212560
Date of patent
December 15, 2015
Patent application number
13173308
Date Filed
June 30, 2011
Patent primary examiner
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