首页> 外国专利> TURBOMACHINE INLET NOZZLE ASSEMBLY FOR ASYMMETRIC FLOW WITH BLADES OF DIFFERENT SHAPE

TURBOMACHINE INLET NOZZLE ASSEMBLY FOR ASYMMETRIC FLOW WITH BLADES OF DIFFERENT SHAPE

机译:不同形状叶片的不对称流动的涡轮机入口喷嘴组件

摘要

FIELD: non-displacement compressors and pumps.;SUBSTANCE: in some embodiments, the suction chamber of the power transmission device between the rotating member and the fluid can comprise a through hole, inlet guide vanes passing near the peripheral edge of the through hole and comprising a first group of inlet guide vanes having a symmetrical profile, second group of inlet guide vanes and third group of inlet guide vanes, wherein all inlet guide vanes of second and third group have curved profile, and bent profile of every inlet guide vane of third group differs from bent profile of other vanes of third group.;EFFECT: embodiments of an apparatus for transferring energy between a rotating element and a fluid are provided herein.;20 cl, 8 dwg
机译:领域:在一些实施例中,在旋转构件和流体之间的动力传递装置的吸入室可以包括通孔,在通孔的外围边缘附近通过的进口导向叶片和包括具有对称轮廓的第一组进气导流叶片,第二组进气导流叶片和第三组进气导流叶片,其中第二组和第三组的所有进气导流叶片均具有弯曲轮廓,并且每个进气导流叶片的弯曲轮廓第三组不同于第三组其他叶片的弯曲轮廓。效果:本文提供了用于在旋转元件和流体之间传递能量的装置的实施方式。20 cl,8 dwg

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