The invention relates to a cascade impactor with several stages.
A cascade impactor is a serial connection of nozzle plates. The nozzle diameter, which is reduced from stage to stage, usually causes the gas velocity to increase. Between the individual nozzle plates, there are baffles covered with filter disks. A gas flow loaded with solids (particles) or liquids impinges on the filter and is deflected there. While fine loads follow the flow for low gas velocities, larger particles or droplets are deposited on the filter. The increasing gas velocity from cascade to cascade thereby separates the individual grain or liquid fractions. Cascade impactors may also be employed immediately in hot and chemically aggressive gases.
EP 2 378 090 A1 relates to an oil mist separator (1) for a crankcase ventilation means. It includes a first separator unit (2), which has at least one filter body (10) which is arranged in a blow-by gas path (11) in such a manner that blow-by gas can pass through it. A second separator unit (3) is provided, which is connected in parallel to said first separator unit (2) and arranged in a bypass path (18) that bypasses the first separator unit (2). Using a bypass valve (4), the bypass path (18) can be opened as soon as a differential pressure at the first separator unit (2) exceeds a predefined value.
The gas flows through two or more impactor stages arranged behind each other. The impactor as a separator and also an impactor cascade consisting of several stages are known. However, these individual stages are not variable. This means that the bore diameters and plate distances have a fixed design.
It is the object of the present invention to provide a variable cascade impactor in which the separating performance can be adapted to the required circumstances.
A cascade impactor through which gas flows, comprising a first stage having a plate (2) with at least one bore as gas inlets, a first baffle (4) variably spaced away from said plate (2) along the gas flow path, and a second stage arranged downstream of the gas flow and downstream of the first baffle (4), comprising a fixed second baffle (5).
The above object is achieved by a cascade impactor comprising a first stage including a plate 2 with fixed bores as a gas inlet and at least one first baffle 4 with a variable distance to the plate 2, and at least one second stage arranged downstream of the first baffle 4 and comprising a fixed second baffle 5.
According to
The special feature of the cascade impactor according to the invention is the fact that a second impactor stage follows after the first stage. Thus, the gas velocity in the variable gap of the first stage is utilized to throw the droplets or solid particles present in the gas with a high velocity onto a second baffle 5, which now has a fixed distance. Because of the optional spring bias 3, a high gas velocity is achieved for low and high volume flows.
At the second fixed baffle 5, the gas can escape downwards and upwards, so that the jet can impinge vertically onto the baffle 5. This jet division is important because the gas thereby can escape in two opposite directions, and the droplets or solid particles are enabled to reach the second baffle 5. Upon contact with the baffle 5, the droplets or solid particles are separated.
In a preferred embodiment of the present invention, the cascade impactor only consists of first and second stages. Although basically several impactor stages may be present, in the vast majority of cases, the above mentioned two stages are sufficient to remove a sufficient amount of droplets or solid particles from a gas flow because of the present invention.
The angle of the mutual arrangement of the baffle surfaces can be varied arbitrari-ly. However, the closer the angle corresponds to a value of 90°, the greater is its separation performance. Accordingly, it is particularly preferred according to the present invention to orient the baffle surfaces of the first and second baffles 4, 5 mutually at an angle of 60 to 120°, especially from 85 to 95°. It is even more preferred according to the present invention if the baffle surfaces of the first and second baffles 4, 5 are at an angle of 90° to one another. Naturally, the same applies to further subsequent baffles, if required.
According to the invention, the baffle 4 may be installed with a variable distance to the plate 2 by the action of a force acting against the gas flow. In principle, this is possible by using a mechanical or electric control. However, according to the present invention, it is particularly preferred if the baffle 4 is pressed against plate 2 by a spring 3. Thus, the distance is varied by the pressure of the gas flow. As the volume flow increases, the baffle 4 is pressed against the spring 3, and thus, the distance to plate 2 is increased, opening a corresponding flow gap.
More particularly, the gas is directed against the baffle 5 at a high velocity through this flow gap.
Because of this gas flow, the gas can flow off the baffle 5 in both directions.
In another preferred embodiment of the present invention, the baffle 4 and the spring 3 may be designed integrally as a spring plate. This results in further structural simplifications of the cascade impactor according to the invention.
Instead of a single bore 2 as represented in
Number | Date | Country | Kind |
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10 2014 214 973 | Jul 2014 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/065844 | 7/10/2015 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2016/015976 | 2/4/2016 | WO | A |
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Number | Date | Country |
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103764252 | Apr 2014 | CN |
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Entry |
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International Search Report for International Application No. PCT/EP2015/065844 dated Sep. 17, 2015. |
Number | Date | Country | |
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20170225107 A1 | Aug 2017 | US |