US Patent 7967570 Low transient thermal stress turbine engine components
Patent 7967570 was granted and assigned to United Technologies on June, 2011 by the United States Patent and Trademark Office.
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Patent abstract
A turbine vane includes a platform; and at least one airfoil mounted to the platform and having a trailing edge and a leading edge, wherein the vane is composed of a functionally graded material having a first material and a second material, wherein the trailing edge includes a greater amount of the first material than the second material, and the leading edge includes a greater amount of the second material than the first material.
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US Patent 07967570 Low transient thermal stress turbine engine components US Patent 7967570 Low transient thermal stress turbine engine components
Infobox
Patent Number
0796757000
Patent Number
796757000
Edits on 26 Apr, 2023
Golden AI
Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
079675700
Date of Patent
June 28, 2011
0Patent Application Number
118293910
Date Filed
July 27, 2007
0Patent Primary Examiner
Edits on 23 Sep, 2022
Golden AI
Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
079675700
Date of Patent
June 28, 2011
0Patent Application Number
118293910
Date Filed
July 27, 2007
0Patent Primary Examiner
Edits on 8 Dec, 2021
Golden AI
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US Patent 07967570 Low transient thermal stress turbine engine components
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07967570
Date of patent
June 28, 2011
Patent application number
11829391
Date Filed
July 27, 2007
Patent primary examiner
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