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公开(公告)号：US20180291752A1
公开(公告)日：2018-10-11
申请号：US15481935
申请日：2017-04-07
Applicant: General Electric Company
Inventor： David Allen Flodman , Robert Francis Manning
Abstract: An apparatus and method relating to an airfoil for a turbine engine and cooling channels within the airfoil. The airfoil includes an outer wall defining an interior bound by a pressure side and a suction side extending axially between a leading edge and a trailing edge defining a chord-wise direction and extending radially between a root and a tip defining a span-wise direction. Further, the airfoil includes ribs located within the interior and a flow enhancer extending between the ribs.
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公开(公告)号：US10724391B2
公开(公告)日：2020-07-28
申请号：US15481935
申请日：2017-04-07
Applicant: General Electric Company
Inventor： David Allen Flodman , Robert Francis Manning
Abstract: An apparatus and method relating to an airfoil for a turbine engine and cooling channels within the airfoil. The airfoil includes an outer wall defining an interior bound by a pressure side and a suction side extending axially between a leading edge and a trailing edge defining a chord-wise direction and extending radially between a root and a tip defining a span-wise direction. Further, the airfoil includes ribs located within the interior and a flow enhancer extending between the ribs.
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