US Patent 11585223 Gas turbine blade arrangement
Patent 11585223 was granted and assigned to MTU Aero Engines on February, 2023 by the United States Patent and Trademark Office.
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Edits on 25 Apr, 2023
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
115852230
Date of Patent
February 21, 2023
0Patent Application Number
177187100
Date Filed
April 12, 2022
0Patent Citations
Patent Primary Examiner
Edits on 6 Apr, 2023
Golden AI
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Edits on 22 Feb, 2023
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US Patent 11585223 Gas turbine blade arrangement
Article
A curved contour of the lateral surface of a blade arrangement includes in at least one meridian section on mutually opposite sides of a blade airfoil an intersection point that is closer to the blade airfoil front edge, and an intersection point that is closer to the blade airfoil rear edge, and a best-fit line of least square distances from the curved contour. The curved contour includes first and/or the second contour section which meet specified conditions.
Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
115852230
Date of Patent
February 21, 2023
0Patent Application Number
177187100
Date Filed
April 12, 2022
0Patent Citations
Patent Primary Examiner
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