首页> 外国专利> TURBOMACHINE INLET NOZZLE FOR ASYMMETRIC FLOW, WITH VANES OF DIFFERENT SHAPES

TURBOMACHINE INLET NOZZLE FOR ASYMMETRIC FLOW, WITH VANES OF DIFFERENT SHAPES

机译:带有不同形状叶片的不对称流动的涡轮机入口喷嘴

摘要

In some embodiments, a plenum of an apparatus for transferring energy between a rotating element and a fluid may include a through hole disposed through the plenum; a plurality of inlet guide vanes disposed proximate a peripheral edge of the through hole, the plurality of inlet guide vanes comprising a first group of inlet guide vanes having a symmetrical profile, a second group of inlet guide vanes, and a third group of inlet guide vanes, wherein each inlet guide vane of the second group and third group have a cambered profile, and wherein each inlet guide vane of the third group has a different cambered profile from each other inlet guide vane of the third group.
机译:在一些实施例中,用于在旋转元件和流体之间传递能量的设备的气室可包括穿过该气室设置的通孔。多个入口导向叶片设置在通孔的周缘附近,多个入口导向叶片包括具有对称轮廓的第一组入口导向叶片,第二组入口导向叶片和第三组入口导向叶片。叶片,其中第二组和第三组的每个入口导向叶片均具有弧形轮廓,并且其中第三组的每个入口导向叶片均具有不同于第三组的每个入口导向叶片的弧形轮廓。

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