Invention Grant
- Patent Title: Turbine blade tip cooling
- Patent Title (中): 涡轮叶片尖端冷却
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Application No.: US13419729Application Date: 2012-03-14
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Publication No.: US09200523B2Publication Date: 2015-12-01
- Inventor: Daniel Cregg Crites , Mark C. Morris , Steve Halfmann
- Applicant: Daniel Cregg Crites , Mark C. Morris , Steve Halfmann
- Applicant Address: unknown Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: unknown Morris Plains
- Agency: Ingrassia Fisher & Lorenz, PC
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A turbine blade includes a blade portion, the blade portion comprising a tip outer wall and a trailing edge, an internal cooling circuit, the internal cooling circuit being configured for directing cooling air within the blade portion, and a tip trailing edge slot positioned adjacent to the tip outer wall and the trailing edge, the tip trailing edge slot being fluidly connected to the internal cooling circuit. The tip outer wall is recessed at the tip trailing edge slot such that the tip outer wall is not provided over the trailing edge slot, thereby allowing cooling air to flow from the cooling circuit, into the trailing edge slot, and radially over the tip outer wall.
Public/Granted literature
- US20130243606A1 TURBINE BLADE TIP COOLING Public/Granted day:2013-09-19
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