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US08784037B2 Turbine shroud segment with integrated impingement plate 有权
具有集成冲击板的涡轮机护罩段

Turbine shroud segment with integrated impingement plate
摘要:
A turbine shroud segment is metal injection molded (MIM) about an insert having a cooling air cavity covered by an impingement plate. The insert is held in position in an injection mold and then the MIM material is injected in the mold to form the body of the shroud segment about the insert.
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