首页> 外国专利> Vortex generator for e.g. hydrocyclone or jet engine combustion chamber, comprises inlet part connected to vortex chamber and vortex concentrator

Vortex generator for e.g. hydrocyclone or jet engine combustion chamber, comprises inlet part connected to vortex chamber and vortex concentrator

机译:涡流发生器,例如水力旋流器或喷气发动机燃烧室,包括连接到涡流室和涡流浓缩器的入口部分

摘要

An inlet part (1) is connected to a trumpet-shaped (4a) or oval vortex chamber with a defined length section geometry and to a vortex concentrator which uses an underpressure to draw the medium from the inlet part into the chamber. A vortex generator for a liquid or gas comprises an inlet part connected to a vortex chamber via a rounded lower connection and to a vortex concentrator via a chamfered lower edge so that the concentrator is inserted into the chamber. The medium in which the vortex is to be generated enters the inlet part, passing at least one wing located in this part, before passing through a rotation symmetrical cavity with a curved geometry and at least one helical cone-shaped channel into a trumpet or oval-shaped vortex chamber. The medium begins to rotate just beneath the soft lower connection on the inlet part and is then forced to flow downwards and swirl around the concentrator. The Coanda effect caused by the medium swirling around the outside of the concentrator acts as a brake and generates an underpressure at this surface, creating a vortex travelling downwards towards the outlet opening in the concentrator. The underpressure sucks the medium toward! s the concentrator surface and into at least one central channel and a channel plate containing at least one channel slanting at angle relative to the concentrator, so that the medium flows through the concentrator towards at least one conical nozzle with at least one vortex channel and at least one outlet opening, leading into the vortex chamber. The length section of the inside (401) of the trumpet-shaped chamber is defined by the function f(x) = k x xy. k = 8500-9000, y = -1.1 to -1.0, f(x) = x0 to x0 + 250 length units and x0 = 70-170. The length section of the inside of the oval chamber is defined by the function f(x) = k1 x (x2 + k2) x (y2 - C). C = 18-21, k1 = at least 0.003 when x is less than or equal to zero or at least 0.002 when x is greater than zero, and k2 = at least 0.005 when x is less than or equal to zero or at least 0.005 when x is greater than zero.
机译:入口部分(1)连接到具有规定长度截面几何形状的喇叭形(4a)或椭圆形涡流室,并连接到涡流浓缩器,涡流浓缩器使用负压将介质从入口部分吸入腔室。用于液体或气体的涡流发生器包括入口部分,该入口部分通过圆形下部连接件连接到涡流室,并通过倒角的下边缘连接到涡流集中器,从而将浓缩器插入腔室中。产生涡旋的介质进入入口部分,并通过位于该部分中的至少一个机翼,然后穿过具有弯曲几何形状和至少一个螺旋形锥形通道的旋转对称腔,进入喇叭形或椭圆形形的涡流室。介质刚开始在入口部分的下部软连接下方旋转,然后被迫向下流动并围绕浓缩器旋转。由介质围绕浓缩器外部旋涡引起的柯恩达效应起制动器的作用,并在该表面上产生负压,从而产生向下流向浓缩器出口的涡流。负压将介质吸向!集中器表面进入至少一个中央通道和一个通道板,该通道板包含至少一个相对于集中器倾斜的通道,从而使介质流过集中器流向至少一个带有至少一个涡流通道的锥形喷嘴,并在至少一个至少一个出口通向涡流室。喇叭形腔室内部(401)的长度部分由函数f(x)= k×xy>定义。 k = 8500-9000,y = -1.1至-1.0,f(x)= x0至x0 + 250个长度单位,x0 = 70-170。椭圆形腔室内部的长度部分由函数f(x)= k1 x(x2> + k2)x(y2>-C)定义。 C = 18-21,如果x小于或等于零,则k1 =至少0.003;如果x大于零,则k1 =至少0.002;如果x小于或等于零,或k = 0.005,则k2 =至少0.005。当x大于零时。

著录项

  • 公开/公告号SE528493C2

    专利类型

  • 公开/公告日2006-11-28

    原文格式PDF

  • 申请/专利权人 WATRECO AB;

    申请/专利号SE20050000722

  • 发明设计人 MORTEN OVESEN;CURT HALLBERG;

    申请日2005-04-01

  • 分类号C02F1/00;B04C3/00;B05B1/34;F15C1/16;F15D1/00;

  • 国家 SE

  • 入库时间 2022-08-21 20:55:42

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