Invention Grant
US09341065B2 Dual element turbine blade 有权
双元件涡轮叶片

Dual element turbine blade
Abstract:
A method of manufacturing a turbine blade includes providing a core element having a base portion, a tip portion, and an intermediate portion extending between the base portion and the tip portion. The intermediate portion has a non-uniform cross-section and is a high-strength fiber material. The method also includes surrounding the core element with a shell, the volume between the core element and the shell forming a void.
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