发明授权
US07794201B2 Gas turbine engines including lean stator vanes and methods of assembling the same 有权
包括精密定子叶片的燃气涡轮发动机及其组装方法

Gas turbine engines including lean stator vanes and methods of assembling the same
摘要:
A stator vane that may be used in an engine assembly is provided. The stator vane includes an airfoil that has a first sidewall and a second sidewall, which connects to the first sidewall at a leading edge and at a trailing edge. The airfoil also includes a root portion and a tip portion. The first and second sidewalls both extend from the root portion to the tip portion. The airfoil root portion is formed with a negative lean, and the airfoil tip portion is formed with a positive lean.
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