Urea supersonic jet ejector structure and engine SCR tail gas emission aftertreatment system
An exhaust emission, supersonic technology, applied in the direction of machine/engine, exhaust treatment, engine components, etc., can solve problems such as affecting the effect of exhaust treatment, and achieve the effect of shortening the injection stroke, reducing the output pressure, and improving the conversion efficiency.
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[0065] figure 1 An embodiment of the structure of a urea supersonic jet injector of the present invention is shown, including:
[0066] Primary injection mechanism 202 for urea metering injection;
[0067] The secondary injection mechanism 203 that atomizes the metered urea;
[0068] An airtight mixing chamber 201 is constructed between the primary injection mechanism 202 and the secondary injection mechanism 203, and the mixing chamber 201 is configured to allow additional fluid to mix with the urea injected by the primary injection mechanism to form a mixed fluid that is directly sprayed by the secondary injection mechanism. out.
[0069] In order to allow fluid to flow into the mixing chamber, the mixing chamber is generally provided with a fluid inlet 207. The function of the mixing chamber is mainly to provide space for the mixing of metered urea and fluid. Therefore, under the premise of ensuring the mixing, the injection port of the primary injection mechanism It is ...
Embodiment 2
[0072] On the basis of Example 1, such as figure 1 and 3 As shown in ~9, further, in the structure of the urea supersonic jet injector, the distance between the end surface of the injection port 2021 of the primary injection mechanism 202 and the end surface of the inlet 2031 of the secondary injection mechanism 203 is -50mm~50mm , no matter how the primary spraying mechanism and the secondary spraying mechanism are arranged in space, as long as the distance between the end surface of the injection port of the primary spraying mechanism and the inlet end surface of the secondary spraying mechanism is -50mm ~ 50mm.
Embodiment 3
[0074] On the basis of Example 1, such as figure 1 and 3 As shown in ~9, in the structure of the urea supersonic jet injector, the arrangement of the primary injection mechanism and the secondary injection mechanism is: coaxial arrangement or axial parallel arrangement or axial cross arrangement or axial space intersect set up. image 3 The middle is the axial vertical cross setting; Figure 4 Set for axial cross but not perpendicular angles; Figure 5 is perpendicular to the axial space; Figure 6 is axially parallel; Figure 7 The axes are parallel but in opposite directions; Figure 8 It is set coaxially but the entrance of the secondary injection mechanism is concave, and the injection port of the primary injection mechanism is inserted into it; Figure 9 The middle injection port sinks into the entrance of the secondary injection mechanism, and the distance to the entrance of the secondary injection mechanism is a negative value. Of course, there are other arrangem...
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