Invention Application
US20020162220A1 Method of repairing a turbine blade tip 失效
修复涡轮叶片尖端的方法

Method of repairing a turbine blade tip
Abstract:
A blade tip cap of a turbine blade is repaired by restoring the tip rail and attaching a strengthening rib across the blade tip cap connecting the concave wall to the convex wall of the tip rail.
Public/Granted literature
Information query
Patent Agency Ranking
0/0