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US Patent 7686582 Radial split serpentine microcircuits

Patent 7686582 was granted and assigned to United Technologies on March, 2010 by the United States Patent and Trademark Office.

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Patent
Patent

Patent attributes

Current Assignee
United Technologies
United Technologies
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
7686582
Patent Inventor Names
Francisco J. Cunha2
Date of Patent
March 30, 2010
Patent Application Number
11495131
Date Filed
July 28, 2006
Patent Citations Received
‌
US Patent 11885236 Airfoil tip rail and method of cooling
1
Patent Primary Examiner
‌
Igor Kershteyn
Patent abstract

A turbine engine component, such as a turbine blade has an airfoil portion with an airfoil mean line, a pressure side, and a suction side. A first region on the pressure side of the airfoil portion has a first array of cooling microcircuits embedded in a wall forming the pressure side. A second region on the pressure side has a second array of cooling microcircuits embedded in the wall. The first region is located on a first side of the mean line and the second region is located on a second side of the mean line.

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