cross flow fan
A cross-flow fan and cross-flow wind wheel technology, applied in mechanical equipment, radial flow pumps, machines/engines, etc., can solve problems such as large gap between wind wheel and volute, poor flow field characteristics, and large eccentric worm scale
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specific Embodiment 1
[0032] Such as Figure 3-4 As shown, the structural parameters of this embodiment mainly include the following points, the tangent point between the sectional curve of the rear volute tongue 2 and the horizontal plane is point A, and the end point of the sectional curve of the front volute tongue 3 near the end of the air inlet is point F, Through the central point O of the cross-flow wind wheel 1, a tangent line that is tangent to the cross-sectional curve of the front volute tongue 3 intersects the cross-sectional curve of the front volute tongue 3 at point H, and the point A and the center vertical line of the cross-flow wind wheel 1 have The included angle θ=45°, the radius of curvature R=2.76mm of the section curve of the rear cochlear tongue 2. Angle θ between point A and point F with ∠AOF 1 =155°, the included angle θ of ∠AOH between point A and point H 2 =176°.
[0033] The angle θ between the line connecting the terminal point F of the anterior cochlear tongue 3 an...
specific Embodiment 2
[0038] Such as Figure 3-4 As shown, the structural parameters of this embodiment on the basis of Embodiment 1 have the following changes: the included angle θ=50° between the point A at the rear volute tongue 2 and the vertical line of the center of the cross-flow wind wheel 1, and the rear The radius of curvature R of the section curve of the volute tongue 2 is 3.49mm, and the included angle θ between point A and point H is ∠AOH 2 =177°; ∠BOA angle θ between the end point B and point A of the BC curve section near the air inlet side 6 =5°; the radius of curvature R of the boss 1 = 1.2 mm.
[0039] The CFD simulation speed vector diagram of the present embodiment is Figure 7 , the velocity distribution of the flow field is marked in the form of contour lines in the figure, and the number marks represent the flow velocity. It can be seen that the flow field is similar to that of Example 1, but the scale of the eccentric worm is relatively smaller than that of the prior art...
specific Embodiment 3
[0040] Such as Figure 3-4 As shown, the structural parameters of this embodiment have the following changes on the basis of Embodiment 1. The included angle θ=55° between the point A at the 2 points of the rear volute tongue and the vertical line of the center of the cross-flow wind wheel 1 is 55°. The curvature radius R of the volute tongue 2 section curve is 5.27mm, and the AOH angle θ between point A and point H 2 =177°; ∠BOA angle θ between the end point B and point A of the BC curve section near the air inlet side 6 =5°; the radius of curvature R of the boss 1 = 1.15 mm.
[0041] The CFD simulation speed vector diagram of the present embodiment is Figure 8 , the velocity distribution of the flow field is marked in the form of contour lines in the figure, and the numerical marks represent the flow velocity. It can be seen that the scale of the eccentric worm is relatively smaller, the effective flow area of the cross-flow rotor 1 is increased, and the flow field at ...
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