US Patent 7887929 Oriented fiber ceramic matrix composite abradable thermal barrier coating
Patent 7887929 was granted and assigned to United Technologies on February, 2011 by the United States Patent and Trademark Office.
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Patent abstract
A method of manufacturing a gas turbine engine component includes the steps of forming a ceramic workpiece having oriented ceramic reinforcement, and severing the ceramic workpiece to produce a ceramic member having a desired orientation of the ceramic reinforcement. The ceramic member is then attached to a turbine engine component as a thermal barrier layer for the turbine engine component.
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US Patent 07887929 Oriented fiber ceramic matrix composite abradable thermal barrier coating US Patent 7887929 Oriented fiber ceramic matrix composite abradable thermal barrier coating
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Patent Number
0788792900
Patent Number
788792900
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Official Website
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
078879290
Date of Patent
February 15, 2011
0Patent Application Number
118458100
Date Filed
August 28, 2007
0Official Website
Patent Primary Examiner
Edits on 27 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
078879290
Date of Patent
February 15, 2011
0Patent Application Number
118458100
Date Filed
August 28, 2007
0Official Website
Patent Primary Examiner
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US Patent 07887929 Oriented fiber ceramic matrix composite abradable thermal barrier coating
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07887929
Date of patent
February 15, 2011
Patent application number
11845810
Date Filed
August 28, 2007
Patent primary examiner
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