Invention Grant
US07918653B2 Rotor blade trailing edge assemby and method of use 有权
转子叶片后缘总成及使用方法

Rotor blade trailing edge assemby and method of use
Abstract:
A method of assembling a rotor blade for a turbine is provided that includes forming a rotor blade trailing edge by coupling a suction side terminus to a pressure side terminus and positioning a trailing edge assembly between the suction side terminus and the pressure side terminus, the trailing edge assembly having a varying cross-section.
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