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Tapered-ring vortex chamber for extreme acceleration of the vortex medium

机译:锥形环涡流室,可极大加速涡流介质

摘要

The side walls of the tapered-ring vortex chamber extend inwards in a funnel shape, so that they form a tapered ring with the circular outer wall. The vortex material injected through the outer wall at an angle to form a vortex can flow out in the vicinity of the vortex core, because the funnel walls are open at that point. Conventionally, the vortex chamber narrows towards the vortex centre with the square of the approach. Due to the tapered-ring shape, the chamber space tapers inwards also in the width of flow, so that the inward narrowing of the space goes with the cube. As a result, the vortex medium in the tapered-ring vortex chamber is subjected to an extremely high acceleration. Industrial utilisation in: 1. centrifugal separation equipment, 2. pre-acceleration of the propellant medium for liquid turbines and pre- and re-acceleration for gas turbines, 3. pulsed combustion chambers with vortex acceleration, 4. pulsed combustion turbines, 5. ultrahigh-speed small turbines and 6. extreme high-speed water turbines with a blade drive for cutting by vortex water. The drawing shows the tapered-ring vortex chamber with an air cushion antechamber for liquids, to reduce the inflow resistance. Tapered-ring vortex chamber with air cushion antechamber for high-speed liquid turbines: 1. Vortex liquid in the tapered-ring vortex chamber and in the air cushion antechamber with the centrifugal force rising outwards. 2. Injection orifice into the air cushion antechamber. 3. Air cushion antechamber. 4. Air cushion buffer space. 5. Compressed-air feed, if necessary. 6. Overflow ring orifice. 7. Vortex outflow orifice. 8. Turbine shaft. 9. Open outflow chamber. IMAGE
机译:锥形环涡流室的侧壁以漏斗形向内延伸,从而它们与圆形外壁形成锥形环。通过外壁以一定角度注入以形成旋涡的旋涡材料可以在旋涡芯附近流出,因为漏斗壁在该点处是敞开的。按照惯例,涡流室朝着涡流中心的方向逐渐变窄。由于锥形环的形状,腔室空间在流动的宽度上也向内逐渐变细,使得空间的向内变窄与立方体一致。结果,锥形环涡旋室中的涡旋介质受到极高的加速度。在以下方面的工业利用:1.离心分离设备; 2.液体涡轮机的推进剂介质的预加速;以及燃气涡轮机的预加速和再加速; 3.具有涡旋加速的脉冲燃烧室; 4.脉冲燃烧涡轮; 5。超高速小型水轮机和带有叶片驱动装置的超高速水轮机6.用于涡流切割。该图显示了锥形环涡流室,该室带有用于液体的气垫前室,以减小流入阻力。用于高速液体涡轮机的带有气垫前室的锥形环涡室:1.在锥形环涡室和气垫室中使液体涡旋,并且离心力向外上升。 2.将孔口注入空气垫前室。 3.气垫前室。 4.气垫缓冲空间。 5.如有必要,使用压缩空气。 6.溢流环孔。 7.涡流流出孔。 8.涡轮轴。 9.打开流出室。 <图像>

著录项

  • 公开/公告号DE3202358A1

    专利类型

  • 公开/公告日1983-08-18

    原文格式PDF

  • 申请/专利权人 REIBERKURT;

    申请/专利号DE19823202358

  • 发明设计人 REIBERKURT;

    申请日1982-01-26

  • 分类号F15D1/00;F02C3/14;F03B11/00;B04C1/00;F23R3/58;

  • 国家 DE

  • 入库时间 2022-08-22 10:05:44

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