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公开(公告)号:US20210017864A1
公开(公告)日:2021-01-21
申请号:US16876615
申请日:2020-05-18
Applicant: General Electric Company
Inventor: Mark Steven Honkomp , Mark Lawrence Hunt , Frederick Whitfield Dantzler , Yan Cui , Ethan Conrad Schaeffer
IPC: F01D5/18
Abstract: A tip rail cooling insert for attaching into a tip rail pocket in a tip rail of a turbine blade is disclosed. The insert includes a first inner layer defining at least one first insert cooling channel therein, the first inner layer including a pair of spaced legs defining a first coolant collection plenum with at least the tip rail pocket for directing coolant from at least one internal cooling cavity in the turbine blade to the at least one first insert cooling channel. Each of the pair of spaced legs has an angled outer end configured to accommodate rounded inner corners of the tip rail pocket. A first outer layer is on a first side of the first inner layer, and a second outer layer is on a second side of the first inner layer.
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公开(公告)号:US11208902B2
公开(公告)日:2021-12-28
申请号:US16876615
申请日:2020-05-18
Applicant: General Electric Company
Inventor: Mark Steven Honkomp , Mark Lawrence Hunt , Frederick Whitfield Dantzler , Yan Cui , Ethan Conrad Schaeffer
Abstract: A tip rail cooling insert for attaching into a tip rail pocket in a tip rail of a turbine blade is disclosed. The insert includes a first inner layer defining at least one first insert cooling channel therein, the first inner layer including a pair of spaced legs defining a first coolant collection plenum with at least the tip rail pocket for directing coolant from at least one internal cooling cavity in the turbine blade to the at least one first insert cooling channel. Each of the pair of spaced legs has an angled outer end configured to accommodate rounded inner corners of the tip rail pocket. A first outer layer is on a first side of the first inner layer, and a second outer layer is on a second side of the first inner layer.
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