CN101092964A - Axial flow cooling blower fan - Google Patents
Axial flow cooling blower fan Download PDFInfo
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- CN101092964A CN101092964A CN 200710119141 CN200710119141A CN101092964A CN 101092964 A CN101092964 A CN 101092964A CN 200710119141 CN200710119141 CN 200710119141 CN 200710119141 A CN200710119141 A CN 200710119141A CN 101092964 A CN101092964 A CN 101092964A
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- blade
- guide plate
- aerofoil profile
- blower fan
- paddle components
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Abstract
This invention discloses an axial cooling blower with large diameter of 8-10m, low pressure head of 70-130Pa and high blast volume of 440-550m3/s composed of a motor, a bustle pipe, a deflector vane component and a blade component, in which the outer circle of the deflector vane component is connected with one end of the bustle pipe, the vane component is assembled in the pipe, the output shaft of the motor passes through the inner circle of the deflector vane and connects to the rim of the vane, which applies a theory of free vortex blade lattice, applies low Renault number and high lift aerofoil and increases torsion angle of the vane to increase chord length of the tine to manufacture a new type of blower and installs a deflector vane to recover rotation energy of the outlet and increase hydrostatic lifting of the blower so as to increase speed of the output of an air cooler.
Description
Technical field
The present invention relates to a kind of axial flow cooling blower fan, this cooling blower has major diameter 8～10m, low-head 70～130Pa, high air quantity 440～550m
3/ s.
Background technique
Because the important function that the forced-convection heat transfer of large axial flow fan in the direct air cooling system of thermal power plant has, so the quality of fan performance is directly determining the important symbol of the height of air cooling condenser radiating effect.Because air cooling condenser needs big air quantity in the heat radiation process, but pressure head is little, so the blower fan of air cooling system often adopts low-head, big air quantity, low noise axial fan.Yet in the season of sweltering heat in summer; ambient temperature is very high; particularly natural wind blew side from the boiler room; when under air cooling tower, forming hot refluence; the air quantity that existing blower fan blasts can not satisfy the heat radiation requirement of the air cooling condenser under the actual high temperature condition, has a strong impact on the radiating effect of air cooling condenser, even causes the shutdown of system; bring very big influence for the safety in production and the operation of power plant, caused enormous economic loss.
Summary of the invention
The purpose of this invention is to provide a kind of have major diameter 8～10m, low-head 70～130Pa, high air quantity 440～550m
3The axial flow cooling blower fan of/s, the blade of this cooling blower adopt free vortex flow Theories of Cascades, aerofoil profile to adopt low reynolds number Re, high-lift aerofoil profile C
L, thereby its structure optimization is obtained preferable blade profile, realized the increase of blower fan rate of discharge; Simultaneously in order to improve the flow field structure in blower fan outlet port, and then the radiating effect of raising air cooling condenser, guide plate is installed in outlet at blower fan, be used to reclaim the rotation function of blower fan outlet, increased the static pressure liter of blower fan, the wind speed of air cooling condenser outlet is improved, thereby strengthened convection heat exchange ability air cooling condenser.
The present invention is a kind of have major diameter 8～10m, low-head 70～130Pa, high air quantity 440～550m
3The axial flow cooling blower fan of/s, form by motor, solar or lunar halo, guide plate assembly and paddle components, the outer toroid of guide plate assembly is connected with the smooth section of solar or lunar halo, and paddle components is assemblied in the solar or lunar halo, and the interior annulus that the output shaft of motor passes the guide plate assembly is connected with the wheel hub of paddle components.
The lift coefficient of the blade aerofoil profile in the paddle components of the present invention
The resistance coefficient of blade aerofoil profile
The advantage of axial flow cooling blower fan of the present invention is: low reynolds number Re=1.5 * 10 of (1) blade aerofoil profile
6～3.9 * 10
6, high-lift aerofoil profile C
L=0.479+0.0895 α, the resistance coefficient C of blade aerofoil profile
d=0.0286-0.0039 α+0.0009 α
2(2) after the employing high-lift aerofoil profile, the wind flow of blower fan outlet obviously increases, and helps improving the radiating effect of air cooling condenser; (3) blade in the paddle components adopts independent design, regulates established angle when helping installing between each blade and is consistent; (4) blade aerofoil profile configuration adopts Fluent software to carry out the optimal design of two-dimensional gas dynamic response, improved the flow field structure of blower fan outlet, reclaim the rotation function of blower fan outlet, help improving the flow velocity of air cooling condenser outlet, strengthen the convection heat exchange ability of cool air and air cooling condenser, thereby improved the radiating effect of air cooling condenser.
Description of drawings
Fig. 1 is the external structure of axial flow cooling blower fan of the present invention.
Figure 1B is the external structure at another visual angle of axial flow cooling blower fan of the present invention.
Fig. 1 C is the front view of axial flow cooling blower fan of the present invention.
Fig. 1 D is the plan view of axial flow cooling blower fan of the present invention.
Fig. 2 is the external structure of guide plate assembly of the present invention.
Fig. 2 A is the front view of A guide plate.
Fig. 3 is the external structure of paddle components of the present invention.
Fig. 3 A is the blade external structure.
Fig. 3 B is the lateral plan of blade.
Fig. 3 C is the incoming flow angle of attack, lift coefficient and the resistance coefficient coordinate graph of a relation of blade aerofoil profile.
Among the figure: 1. guide plate assembly 101.A guide plate 102.B guide plate 103.C guide plate
104.D guide plate 105.E guide plate 106.F guide plate 107.G guide plate 108.H guide plate
109.I annulus in guide plate 110. outer toroid 111.
2. paddle components 201.A blade 202.B blade 203.C blade 204.D blade
205.E blade 206.F blade 207.G blade 208.H blade 209. wheel hubs
221. top airfoil 222. upper-end surfaces 223. attachment posts, 224. front-end faces, 225. lower aerofoils
226. blade-span axis 227. blade tips
3. solar or lunar halo 301. extending sections 302. smooth section
Embodiment
The present invention is described in further detail below in conjunction with accompanying drawing.
The present invention is a kind of have major diameter 8～10m, low-head 70～130Pa, high air quantity 440～550m
3The axial flow cooling blower fan of/s, form (shown in Fig. 1, Figure 1A, Figure 1B) by motor (not shown), solar or lunar halo 3, guide plate assembly 1 and paddle components 2, the outer toroid 110 of guide plate assembly 1 is connected with the smooth section 302 of solar or lunar halo 3, paddle components 2 is assemblied in the solar or lunar halo 3, and the interior annulus 111 that the output shaft of motor passes guide plate assembly 1 is connected with the wheel hub 209 of paddle components 2.(shown in Fig. 1 C) solar or lunar halo 3 profiles are provided with smooth section 302, extending section 301 from top to bottom, and the expansion ratio of extending section 301 ends is 3～10 degree.In the present invention, when motor driving paddle components 2 is rotated along clockwise direction, the cool air of air cooling condenser below is upwards taken out, when motor driving paddle components 2 when counterclockwise direction is rotated, the hot air of air cooling condenser top is inhaled downwards, thereby made air cooling condenser have preferable radiating effect.The output power of motor is 120～160KW.
Referring to shown in Figure 2, between interior annulus 111 and outer toroid 110, be connected with A guide plate 101, B guide plate 102, C guide plate 103, D guide plate 104, E guide plate 105, F guide plate 106, G guide plate 107, H guide plate 108, I guide plate 109 in turn.In the present invention, nine flow deflector structures are identical, are wide circular arc aerofoil profile, aerofoil profile chord length b
sBe 500mm, aerofoil profile width b
wBe 2.5～5mm (shown in Fig. 2 A).
In the present invention, evenly be provided with on the cylindrical of wheel hub 209 a plurality of domes hole (dome hole length 10～50mm), symmetry has A through hole, B through hole (being used for pin passes) on the dome hole; The front-end face of each blade is provided with attachment post, and symmetry has C through hole, D through hole (being used for pin passes) on the attachment post; In when assembling, attachment post is installed in the dome hole, and after passing A through hole, C through hole, D through hole, B through hole with pin both is fixed, thereby realizes the flexible assembly of wheel hub 209 and eight blades.Referring to shown in Figure 3, on the cylindrical of wheel hub 209 by attachment post being installed in the dome hole and being equipped with A blade 201, B blade 202, C blade 203, D blade 204, E blade 205, F blade 206, G blade 207, H blade 208 in turn.In the present invention, A blade 201, B blade 202, C blade 203, D blade 204, E blade 205, F blade 206, G blade 207, H blade 208 structures are identical, and the established angle γ between two blades is 15～30 degree.In order to describe the concrete structure of blade of the present invention in detail, shown in Fig. 3 A, Fig. 3 B, front-end face 224 central positions of A blade 201 are provided with attachment post 223, and the end symmetry of attachment post 223 has C through hole, D through hole (not shown), the length 10～50mm of attachment post 223.The blade torsional angle β of top airfoil 225 is 10～15 degree.
Shown in Fig. 3 C, adopted large-scale general fluid mechanics software for calculation Fluent to carry out the computational analysis of two-dimensional gas dynamic response for the optimization of blade aerofoil profile, in system of coordinates XOY, X-axis is represented aerofoil profile string of a musical instrument direction, Y-axis is represented and the blade-span axis parallel direction, incoming flow angle of attack α=-6～+ 16 degree are the angle that comes between flow path direction and the X-axis (aerofoil profile string of a musical instrument direction), to be positive incoming flow angle of attack α (being negative incoming flow angle of attack α clockwise) counterclockwise.The lift of aerofoil profile with come flow path direction vertical, the resistance of aerofoil profile is parallel with flow path direction, and the lift coefficient C of aerofoil profile is then arranged
lWith resistance coefficient C
dFor:
Has the lift coefficient C of aerofoil profile
lWith resistance coefficient C
dIn the relation, design one have eight blades, nine guide plates, when the motor output power is 132KW, blade chord length 3705mm, blade torsional angle β be that 14.7 °, blade tip chord length 1562mm, front-end face chord length b are that 1910.35mm and established angle γ are 28.5 °, and low reynolds number Re=1.79 * 10 of blade aerofoil profile are then arranged
6, high-lift aerofoil profile C
L=0.479+0.0895 α, the resistance coefficient C of blade aerofoil profile
d=0.0286-0.0039 α+0.0009 α
2
By blade aerofoil profile configuration is optimized design, and adopt the blade computational analysis of low reynolds number, high-lift aerofoil profile to compare, increase established angle γ, the increase blade torsional angle β (shown in Fig. 3 B) between two blades and increase blade tip 227 chord lengths, can improve the static pressure of blower fan, increase the flow of blower fan outlet.Practice shows, during the broiling summer, when ambient temperature is higher than 30 ℃, adopts the blower fan of high-lift aerofoil profile can increase the blower fan rate of discharge, improves the air cooling condenser radiating effect, makes the air cooling system safe production in summer.
In the present invention, guide plate assembly 1 is set, under blower fan rated speed 67.6rpm condition, the fluid structure in blower fan outlet port is obviously improved in the upper end of paddle components 2.The rotational speed in blower fan outlet port reduces greatly simultaneously, the flow of blower fan, stagnation pressure, dynamic pressure all reduce, static pressure and air horsepower increase, caused the air velocity of air cooling condenser outlet to increase thus, strengthen the convection heat exchange ability of air and air cooling condenser, improved the radiating effect of air cooling condenser.
The axial flow cooling blower fan of the present invention's design has following technical requirement:
(1) under the rated speed of paddle components 2,, can make maximum 10% air quantity or the pressure increment of increasing of blower fan by changing blade installation angle β (pitch);
(2) blower fan is an axial flow, and in order to control the noise of blower fan, the tip speed of blower fan blade must not surpass 60m/s;
(3) minimum area of rotary fans should be not less than 40% of air cooling condenser outlet wind-exposuring area.Blower fan is not more than 45 ° to the diffusion angle of air cooling condenser outlet;
(4) the radial spacing 9～19mm between the inwall of the blade tip of blade and solar or lunar halo;
(5) blade adopts independent design, is installed on the wheel hub by attachment post, and blade has interchangeability;
(6) the blower fan total acoustic power level noise of the present invention's design is no more than 110dB.
Axial flow cooling blower fan of the present invention goes for the thermal power plant direct air cooling system and other are large diameter, the design of the axial flow cooling blower of low-head, high air quantity.
Claims (5)
1, a kind of axial flow cooling blower fan, it is characterized in that: form by motor, solar or lunar halo (3), guide plate assembly (1) and paddle components (2), the outer toroid (110) of guide plate assembly (1) is connected with the smooth section (302) of solar or lunar halo (3), paddle components (2) is assemblied in the solar or lunar halo (3), and the interior annulus (111) that the output shaft of motor passes guide plate assembly (1) is connected with the wheel hub (209) of paddle components (2);
Be connected with A guide plate (101), B guide plate (102), C guide plate (103), D guide plate (104), E guide plate (105), F guide plate (106), G guide plate (107), H guide plate (108), I guide plate (109) between the interior annulus (111) of described guide plate assembly (1) and the outer toroid (110) in turn; A guide plate (101), B guide plate (102), C guide plate (103), D guide plate (104), E guide plate (105), F guide plate (106), G guide plate (107), H guide plate (108) are identical with I guide plate (109) structure, and be wide circular arc aerofoil profile, aerofoil profile chord length b
sBe 500mm, aerofoil profile width b
wBe 2.5～5mm;
Evenly be provided with a plurality of domes hole on the cylindrical of the wheel hub (209) of described paddle components (2), the front-end face of each blade is provided with attachment post; Be installed in the dome hole by attachment post on the cylindrical of wheel hub (209), and be equipped with A blade (201), B blade (202), C blade (203), D blade (204), E blade (205), F blade (206), G blade (207), H blade (208) in turn; A blade (201), B blade (202), C blade (203), D blade (204), E blade (205), F blade (206), G blade (207) are identical with H blade (208) structure, and the established angle γ between two blades is 15～30 degree;
Described solar or lunar halo (3) is provided with smooth section (302), extending section (301) from top to bottom, and the expansion ratio of extending section (301) end is 3～10 degree.
2, axial flow cooling blower fan according to claim 1 is characterized in that: the lift coefficient of the blade aerofoil profile on the paddle components (2)
In the formula, L represents the lift of blade aerofoil profile, and ρ represents the density of air, V
∞The expression speed of incoming flow, b represents the chord length of blade aerofoil profile, unit: mm; The resistance coefficient of the blade aerofoil profile on the paddle components (2)
In the formula, D represents the resistance of blade aerofoil profile, and ρ represents the density of air, V
∞Expression air speed of incoming flow, b represents the chord length of blade aerofoil profile, unit: mm.
3, axial flow cooling blower fan according to claim 1 is characterized in that: the torsional angle β of the top airfoil of the blade on the paddle components (2) is 10～15 degree.
4, axial flow cooling blower fan according to claim 1 is characterized in that: the incoming flow angle of attack α of the blade aerofoil profile on the paddle components (2) is-6～+ 16 degree.
5, axial flow cooling blower fan according to claim 1 is characterized in that: the low reynolds number Re of the blade aerofoil profile on the paddle components (2) is 1.5 * 10
6～3.9 * 10
6, high-lift aerofoil profile C
LBe 0.479+0.0895 α, the resistance coefficient C of blade aerofoil profile
dBe 0.0286-0.0039 α+0.0009 α
2, α represents the angle of the incoming flow angle of attack.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007101191415A CN100497950C (en) | 2007-07-17 | 2007-07-17 | Axial flow cooling blower fan |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007101191415A CN100497950C (en) | 2007-07-17 | 2007-07-17 | Axial flow cooling blower fan |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101092964A true CN101092964A (en) | 2007-12-26 |
| CN100497950C CN100497950C (en) | 2009-06-10 |
Family
ID=38991361
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2007101191415A Expired - Fee Related CN100497950C (en) | 2007-07-17 | 2007-07-17 | Axial flow cooling blower fan |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100497950C (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104069759A (en) * | 2014-07-07 | 2014-10-01 | 刘海 | Air mixed type high-energy-saving material mixer provided with HZJH paddles |
| CN104454639A (en) * | 2014-11-28 | 2015-03-25 | 南阳防爆集团股份有限公司 | Novel generator rotor axial fan |
| CN105065302A (en) * | 2015-08-06 | 2015-11-18 | 浙江上风高科专风实业有限公司 | Efficient sweepforward-type subway tunnel axial flow fan |
| CN105358839A (en) * | 2013-07-02 | 2016-02-24 | 株式会社Ihi | Stator vane structure and turbofan jet engine using same |
| CN107084154A (en) * | 2017-06-19 | 2017-08-22 | 苏州前川机电有限公司 | Axial flow blower carbon fiber impeller |
| CN113294357A (en) * | 2020-03-29 | 2021-08-24 | 苏州市臻湖流体技术有限公司 | Intelligent movement high compression pump |
-
2007
- 2007-07-17 CN CNB2007101191415A patent/CN100497950C/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105358839A (en) * | 2013-07-02 | 2016-02-24 | 株式会社Ihi | Stator vane structure and turbofan jet engine using same |
| CN104069759A (en) * | 2014-07-07 | 2014-10-01 | 刘海 | Air mixed type high-energy-saving material mixer provided with HZJH paddles |
| CN104454639A (en) * | 2014-11-28 | 2015-03-25 | 南阳防爆集团股份有限公司 | Novel generator rotor axial fan |
| CN105065302A (en) * | 2015-08-06 | 2015-11-18 | 浙江上风高科专风实业有限公司 | Efficient sweepforward-type subway tunnel axial flow fan |
| CN105065302B (en) * | 2015-08-06 | 2018-01-16 | 浙江上风高科专风实业有限公司 | A kind of efficiently sweepforward type subway tunnel axial flow blower |
| CN107084154A (en) * | 2017-06-19 | 2017-08-22 | 苏州前川机电有限公司 | Axial flow blower carbon fiber impeller |
| CN113294357A (en) * | 2020-03-29 | 2021-08-24 | 苏州市臻湖流体技术有限公司 | Intelligent movement high compression pump |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100497950C (en) | 2009-06-10 |
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
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Granted publication date: 20090610 Termination date: 20120717 |