阅读说明：本技术 具有单件式冲击式涡轮的分离组件 (Separation assembly with single-piece impulse turbine ) 是由 彼得·K·赫尔曼 奇拉格·D·帕里克 于 2019-02-01 设计创作，主要内容包括：一种分离组件,其包括壳体、在壳体内排出流体的喷射器、以及定位在壳体内并定位成以便与从喷射器排出的流体接触的涡轮。流体使得涡轮在壳体内围绕中心旋转轴线旋转。涡轮包括第一轴向端、第二轴向端和相对于中心旋转轴线从第一轴向端轴向地延伸到第二轴向端的多个轮叶。多个轮叶在多个轮叶中的每一个轮叶之间界定轴向地延伸的通道。第一轴向端是轴向地开放的,使得流体可以畅通无阻地轴向地流过第一轴向端并且流入通道中。喷射器被定位成使得流体的至少一部分通过第一轴向端进入涡轮中。(A separator assembly includes a housing, an ejector discharging fluid within the housing, and a turbine positioned within the housing and positioned so as to be in contact with the fluid discharged from the ejector. The fluid causes the turbine to rotate within the housing about a central axis of rotation. The turbine includes a first axial end, a second axial end, and a plurality of buckets extending axially from the first axial end to the second axial end relative to the central axis of rotation. The plurality of vanes define an axially extending channel between each of the plurality of vanes. The first axial end is axially open such that fluid may flow unimpeded axially through the first axial end and into the channel. The ejector is positioned such that at least a portion of the fluid enters the turbine through the first axial end.)