- Patent Title: Turbine blade tip cooling system including tip rail cooling insert
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Application No.: US16208001Application Date: 2018-12-03
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Publication No.: US10934852B2Publication Date: 2021-03-02
- Inventor: Mark Steven Honkomp , Mehmet Suleyman Ciray , Mark Lawrence Hunt
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Hoffman Warnick LLC
- Agent James Pemrick
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D25/12 ; F01D5/20

Abstract:
A turbine blade tip cooling system includes a turbine blade having a tip cavity, a tip rail surrounding at least a portion of the tip cavity and at least one internal cooling cavity. The tip rail has an inner rail surface, an outer rail surface, an end surface and at least one tip rail pocket open at the end surface and fluidly connected to the at least one internal cooling cavity that carries a coolant. A tip rail cooling insert attaches to the at least one tip rail pocket, and has insert cooling channel(s) and a coolant collection plenum for directing coolant from the at least one internal cooling cavity to the insert cooling channel(s).
Public/Granted literature
- US20200173288A1 TURBINE BLADE TIP COOLING SYSTEM INCLUDING TIP RAIL COOLING INSERT Public/Granted day:2020-06-04
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