Invention Application
- Patent Title: TURBINE BLADE PLATFORM COOLING SYSTEMS
- Patent Title (中): 涡轮叶片平台冷却系统
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Application No.: US12878075Application Date: 2010-09-09
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Publication No.: US20120063916A1Publication Date: 2012-03-15
- Inventor: Bradley Taylor Boyer
- Applicant: Bradley Taylor Boyer
- Applicant Address: US NY Schnectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schnectady
- Main IPC: F01D5/18
- IPC: F01D5/18
Abstract:
The present application provides a turbine blade cooling system. The turbine blade cooling system may include a first turbine blade with a first turbine blade platform having a cooling cavity in communication with a pressure side passage and a second turbine blade with a second turbine blade platform having a platform cooling cavity with a suction side passage. The pressure side passage of the first turbine blade platform is in communication with the suction side passage of the second turbine blade platform.
Public/Granted literature
- US09416666B2 Turbine blade platform cooling systems Public/Granted day:2016-08-16
Information query
