Summary of the invention:
The objective of the invention is to consider the problems referred to above and a kind of optimum blade tilt that has is provided, air quantity is promoted greatly, the through-flow fan impeller that noise also reduces.
Structural representation of the present invention as shown in Figure 1, include impeller left end cap (1), impeller right end cap (4), in several spacer ring (3) and be located between the middle spacer ring (3) or middle spacer ring (3) and left end cap (1), right end cap (4) between some blades (2), wherein blade (2) is pressed blade tilt beta=21 ± 2 ° distribution.
On the cross section of above-mentioned blade (2), width of blade L is 12 ± 2 millimeters, and blade action h is 2.5 ± 0.8 millimeters, and maximum blade thickness t is 1.3 ± 0.5 millimeters.
Above-mentioned blade (2) is by every in the axial direction prolongations H=100 millimeter, with regard to deflection angle along the circumferential direction
Ratio prolong deflection angle
Satisfy:
The blade quantity that above-mentioned blade (2) distributes on circumference of impeller is 30~40, and the circumference spacing λ between adjacent two blades satisfies: λ ∈ [6 °, 15 °].
The diameter D of above-mentioned through-flow fan impeller is 88 ± 4 millimeters.
The present invention is because employing has the structure of optimum blade tilt, and therefore, it not only makes the air quantity of fan promote greatly, and also reduces the noise in the fan running.The present invention is that a kind of design is ingenious, function admirable, convenient and practical through-flow fan impeller.
Embodiment:
Embodiment:
The structural representation of through-flow fan impeller of the present invention as shown in Figure 1, Fig. 2 is the cross-sectional view of through-flow fan impeller, λ is the circumference spacing of two blades, to be blade tilt: Fig. 3 be the partial enlarged drawing at A place among Fig. 2 at the beta angle.Include impeller left end cap 1, impeller right end cap 4, spacer ring 3 and not between the middle spacer ring 3 or the some blades 2 between middle spacer ring 3 and left end cap 1, the right end cap 4 in several, wherein blade 2 is pressed blade tilt beta=21 ± 2 ° distribution.On the cross section of above-mentioned blade 2, width of blade L is 12 ± 2 millimeters, and blade action h is 2.5 ± 0.8 millimeters, and maximum blade thickness t is 1.3 ± 0.5 millimeters.The diameter D of above-mentioned through-flow fan impeller is 88 ± 4 millimeters.
In the present embodiment, through-flow fan impeller diameter D is: 88.8 millimeters, and during blade 2 is distributed in by beta=21 ° between the spacer ring 3 or between spacer ring 3 and left end cap 1, the right end cap 4.Above-mentioned blade 2 width of blade L values are 12 millimeters, and the maximum action h of blade value is 2.5 millimeters, and maximum blade thickness t value is 1.2 millimeters.
When Fig. 4 prolonged H=100mm vertically for blade, the blade while is deflection angle along the circumferential direction
Schematic representation.Wherein, p
1Be the circumferential position of vane end faces on a spacer ring 3 place face f, p
2For vane end faces prolongs H vertically, and deflection angle along the circumferential direction simultaneously
After the position, P
2' be p
2Projection on face f, p
2With P
2' the fillet spacing at angle be deflection angle just
Above-mentioned blade 2 is by every in the axial direction prolongations H=100 millimeter, with regard to deflection angle along the circumferential direction
Ratio prolong deflection angle
Satisfy:
。In the present embodiment, the every in the axial direction overtime of above-mentioned blade 2, the angle of blade deflection along the circumferential direction
, be the prismatic blade impeller.
The blade quantity that above-mentioned blade 2 distributes on circumference of impeller is 30~40, and the circumference spacing λ between adjacent two blades satisfies: λ ∈ [6 °, 15 °].In the present embodiment, the blade quantity that above-mentioned blade 2 distributes on circumference of impeller is 35, wherein blade between distribution mode for being equally spaced circumference spacing λ=360 °/35=10.2857 °.
In numerical simulation, blade tilt beta variation from 16 ° to 29 °, axial-flow fan air quantity and efficient respective change situation are seen accompanying drawing 5 and accompanying drawing 6.Fig. 5 is the different blade tilt Beta figure that influences to the axial-flow fan air quantity, and abscissa is blade tilt Beta, and y coordinate is an air quantity, and unit is: kg
3/ h.Fig. 6 abscissa is an air quantity, and unit is: kg
3/ h, y coordinate are efficient, and under the different blade tilt Beta, the optimum efficiency of axial-flow fan and corresponding flow are determined a location point in this figure system of coordinates.
Can see that from accompanying drawing 5 it is that parabolic curve changes that outflow and blade tilt close, it is on the summit near 21 °.In accompanying drawing 6 efficient flow diagrams, can find out more obviously that blade tilt beta has a best region [19 ° ~ 23 °], in this interval, axial-flow fan efficient height, flow is big.
According to numerical simulation result, we have manufactured the impeller of 17 °, 21 °, 26 ° three different blade tilts in true test, record air quantity, noise number such as the following table 1 of each impeller.
Air quantity noise under the different impeller different rotating speeds of table 1
From the true test result of last table 1, improve nearly 30m than 26 ° of blade tilt impellers with the following 21 ° of blade tilt impeller air quantity of rotating speed
3/ h, and noise level is approaching.
Through interpolation processing, can calculate with air quantity 455m
3Under/the h, 26 ° of blade tilt impeller noises are 36.6dB, and 21 ° of blade tilt impeller noises are 35.1dB, 21 ° of blade tilt impeller noises than 26 ° of little 1.5dB of blade tilt impeller about.
In addition, 17 ° of blade tilt impellers slightly improve than 26 ° of blade tilt impeller air quantity in the table, and noise also slightly improves.
By last analysis as can be known, beta=21 ± 2 ° blade tilt really is optimum blade tilt.