WO2009111956A1 - An axial flow fan for decreasing the noise and the energy consumption - Google Patents

An axial flow fan for decreasing the noise and the energy consumption Download PDF

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Publication number
WO2009111956A1
WO2009111956A1 PCT/CN2009/070153 CN2009070153W WO2009111956A1 WO 2009111956 A1 WO2009111956 A1 WO 2009111956A1 CN 2009070153 W CN2009070153 W CN 2009070153W WO 2009111956 A1 WO2009111956 A1 WO 2009111956A1
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WIPO (PCT)
Prior art keywords
blade
axial flow
negative pressure
angle
pressure surface
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PCT/CN2009/070153
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French (fr)
Chinese (zh)
Inventor
韩玮
Original Assignee
Han Wei
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Publication of WO2009111956A1 publication Critical patent/WO2009111956A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps

Definitions

  • the present invention relates to an axial flow fan, and more particularly to a technique for improving the efficiency of an axial flow fan and reducing energy consumption and noise. Background technique
  • PROPELLER This application relates to an axial fan technology having a single-sided curved blade edge paddle structure, which is a further development based on the above techniques.
  • the position, movement trajectory and motion characteristics of the unilateral curved edge are described as follows in the international application specification: "The parts of the rim are basically the same as the center of the propeller, and the same part of the lobes are projected on the same axis of rotation in the axial direction of the propeller. In principle, it is required that the blade edge only generates frictional resistance in the direction of rotation. In the case of the inclination of the blade edge, the blade edge produces a shape force that increases or decreases the pressure at the blade tip end. The blade edge can be rotated in the blade direction as needed. Appropriate expansion in an approximate involute pattern. Summary of the invention
  • the axial fan technology with single-edge curved blade edge paddle structure described above finds a single-sided curved blade edge of the same shape structure in the experiment, and is used on a part of the axial flow fan to save energy and noise reduction effect. Very good, but on another part of the axial fan, there is no energy saving noise reduction effect. Since it is unclear what the reason is, it is impossible to confidently design such an axial flow fan with energy-saving and noise-reducing effects, which seriously hinders the application of this technology.
  • the invention finds that the problem is independent of the unilateral curved blade edge structure, shape, position, spatial motion trajectory, etc. through a large number of research and experiments.
  • the angle between the negative pressure surface of the blade and the radial direction of the axial fan is found. It plays a key role in energy saving effect.
  • the angle ⁇ is positive, the axial fan with single-sided curved blade edge structure has very good energy-saving and noise-reducing effect, as shown in Figure 1;
  • Negative value the axial flow fan with single-sided curved blade edge structure has little energy-saving and noise-reducing effect, and does not even have energy-saving and noise-reducing effects, as shown in Fig. 2.
  • the negative pressure surface of the blade can be fully replenished, and the absolute value of the pressure on the negative pressure surface of the blade is reduced, thereby reducing the pressure resistance of the blade and the resistance of the blade. Energy consumption is reduced. Since the absolute value of the pressure on the negative pressure surface of the blade is reduced, the pressure difference from the surrounding space is reduced, and the flow velocity of the fluid to the negative pressure surface of the blade is lowered, so that the eddy current intensity is also reduced correspondingly, and the noise is also correspondingly reduced. The above effect is most pronounced at the blade end, because it is the fastest fan speed, the most powerful force, the largest pressure gradient, and the paddle speed range used by most fans. The force generated by the negative pressure surface of the blade is much larger than the positive pressure surface, so the absolute value of the negative pressure surface pressure of the blade is reduced, and the energy saving and noise reduction effect is very significant.
  • the technical solution adopted by the present invention to solve the technical problem thereof is: an axial flow fan blade having a single-sided curved blade edge blade structure, and an angle ⁇ between the negative pressure surface of the blade and the radial direction of the axial fan is 0. Between 90 degrees, or an axial fan blade having a single-sided curved blade-edge blade structure, the average angle ⁇ between the negative pressure surface of the blade and the radial direction of the axial fan is between 0 and 90 degrees. Between the studies and experiments, it was found that the angle between the angle ⁇ or the average angle ⁇ is optimally between 6 and 50 degrees.
  • the invention has the beneficial effects that the technical obstacles are eliminated for the application of the single-sided curved blade edge blade technology, which lays a foundation and provides a feasible implementation scheme for designing and manufacturing a high-efficiency, low-noise axial flow fan, thereby avoiding energy saving.
  • the loss caused by blind design under the condition of reliable implementation technical solution makes the energy-saving and noise-reduction technology of single-sided curved blade edge blade reach the application level.
  • Figure 1 is a graphical representation of the positive angle ⁇ between the negative pressure surface of the blade and the radial direction of the axial fan.
  • Figure 2 is a graphical representation of the negative angle ⁇ between the negative pressure surface of the blade and the radial direction of the axial fan.
  • Fig. 3 is a graphical representation of the average angle ⁇ between the negative pressure surface of the blade and the radial direction of the fan in the case where the surface of the single-sided curved blade edge and the blade negative pressure surface are curved.
  • Figure 4 is a graphical representation of the average angle ⁇ between the negative pressure surface of the blade and the radial direction of the fan in the case where the negative pressure surface of the blade is curved.
  • Figure 5 is a blade with a single-sided curved blade edge and blade forming an integral structure, there is no obvious boundary between the single-sided curved blade edge and the blade, in this case, the blade negative pressure surface and the axial flow fan A graphical representation of the average angle ⁇ between the radial directions.
  • Fig. 6 is a schematic view showing the names and specific positions of the respective portions of the axial flow fan of the single-sided curved blade edge paddle structure.
  • Single-sided curved edge, 6. Axial fan radially flowing toward the negative pressure surface of the blade Fluid, 7. Blade negative pressure surface.
  • the angle between the negative pressure surface (7) of the blade (1) having a single-sided curved blade edge and the radial direction of the axial fan is positive, by the blade Outside the end (4), the fluid (6) flowing radially along the axial fan can reach the boundary layer of the negative pressure surface (7) of the blade, which can reduce the absolute value of the pressure on the negative pressure surface (7) of the blade. , reduce the pressure resistance of the blade, thereby reducing blade resistance, reducing blade energy consumption, and reducing noise.
  • the angle value of the angle ⁇ between the negative pressure surface (7) of the blade and the radial direction of the axial fan is negative. From the outside of the blade end (4), the fluid (6) flowing radially along the axial fan cannot reach the boundary layer of the negative pressure surface (7) of the blade, and the pressure of the negative pressure surface (7) of the blade is substantially absent. Change, so there is no energy saving noise reduction effect.
  • the angle value of the average angle ⁇ between the negative pressure surface (7) of the blade and the radial direction of the axial fan is positive, the edge of the curved edge of the blade (5) and the negative pressure of the blade
  • the surface of the joint surface (7) is a curved surface shape, and the fluid flowing along the negative pressure surface of the blade shape has a small energy loss, a reduced vortex vorticity, and an energy saving and noise reduction effect is further improved.
  • the angle value of the average angle ⁇ between the negative pressure surface of the blade and the radial direction of the axial fan is positive, and the edge of the curved edge of the single side (5) is opposite to the axial direction of the axial fan. Inclination, the fluid flows along the curved surface of the blade with the curved surface of the unilateral curved edge (5) and the unilateral curved edge (5) and the negative pressure surface of the blade, resulting in less energy loss and energy saving. The noise effect is further improved.
  • the blade with the single-sided curved blade edge and the blade forming an integral structure has no obvious boundary line between the single-sided curved blade edge and the blade, and the blade negative pressure surface and the single-sided arc
  • the shape of the shape of the blade is integrally curved, and the angle between the negative pressure surface of the integrated structure and the radial angle of the fan is positive, at the root of the blade (3) near the hub and the middle of the blade, the blade
  • the angle value of the average angle ⁇ between the negative pressure surface and the fan radial direction is a negative value. Since the angle ⁇ is a negative value, the blade linear velocity is low, which has no major effect on the overall energy saving and noise reduction effect.
  • the axial flow fan The overall still has good energy saving and noise reduction effects.
  • This technology is used in axial compressors, especially in the first stage, which increases fluid intake, reduces tip leakage losses, reduces power consumption, and improves compression performance.
  • the technology of the present invention can be applied to fluid machines such as propellers, axial flow fans, axial flow blowers, axial flow compressors, fans, axial flow pumps, wind fire extinguishers, and the like, or various fluid machines for agitating fluids.
  • fluid machines such as propellers, axial flow fans, axial flow blowers, axial flow compressors, fans, axial flow pumps, wind fire extinguishers, and the like, or various fluid machines for agitating fluids.
  • the blade of the present invention can be produced by casting, die casting, injection molding, stamping, mechanical cutting, welding, and the like. Description:
  • Average angle ⁇ The angle between the line connecting the two ends of the curve and the radial direction of the axial fan is the average angle ⁇ ; or the average value of the angle between the tangent of each point of the curve and the radial direction of the axial fan is the average angle ⁇ .
  • the invention sets the radial direction of the axial flow fan and the axial direction of the axial flow fan to be perpendicular to each other.

Abstract

An axial flow fan comprises a hub (2) and a plurality of blades(1) extending radially outwardly from the hub(2),a single-side arc brim(5) is provided at the tip each blade. The axial flow fan characterizes in that the angle or the average angle between the negative pressure face of the blades and the radial directions of the axial flow fan is 0o-90o, the optimum scope of the angle or the average angle is 6 o -50 o. The fan can decrease the noise and the energy consumption,and can be used widely in varieties of fields such as all kinds of the axial flow fans,the axial flow motors and the fluidtransportation and stir machine.

Description

一种降低能耗和噪音的轴流风扇 所属技术领域  Axial flow fan for reducing energy consumption and noise
本发明涉及一种轴流风扇, 尤其是能提高轴流风扇的效率, 降低能耗和噪音的技术。 背景技术  The present invention relates to an axial flow fan, and more particularly to a technique for improving the efficiency of an axial flow fan and reducing energy consumption and noise. Background technique
本发明人与其他发明人合作于 2000年向中国知识产权局提交了一项专利申请, 发明名称 《高性能螺旋桨》, 专利申请号 CN00111209.0, 2001年提交国际专利申请, 国际申请号: pet /cnOl/00112,在美国的申请已经得到授权,专利号 US6866482 B2,名称: HIGN-PERFORMENCE The inventor cooperated with other inventors in 2000 to submit a patent application to the Chinese Intellectual Property Office, the title of the invention "High Performance Propeller", Patent Application No. CN00111209.0, International Patent Application submitted in 2001, International Application No.: pet /cnOl/00112, the application in the United States has been authorized, patent number US6866482 B2, name: HIGN-PERFORMENCE
PROPELLER。该申请涉及一种具有单边弧形叶边桨叶结构的轴流风扇技术,本申请技术是在 上述技术基础上的进一步发展。 PROPELLER. This application relates to an axial fan technology having a single-sided curved blade edge paddle structure, which is a further development based on the above techniques.
国际申请说明书中对单边弧形叶边的位置、 运动轨迹、 运动特性有如下描述: "叶边各部 分基本与螺旋桨同圆心, 叶边功能相同部分在螺旋桨轴向投影基本在相同旋转半径上, 原则 上要求叶边在旋转方向只产生摩擦阻力。 在叶边有倾角情况下, 叶边会产生增加或减小桨叶 叶端压力的形状力。 根据需要, 叶边可以在桨叶旋转方向以近似渐开线型式适当展开"。 发明内容  The position, movement trajectory and motion characteristics of the unilateral curved edge are described as follows in the international application specification: "The parts of the rim are basically the same as the center of the propeller, and the same part of the lobes are projected on the same axis of rotation in the axial direction of the propeller. In principle, it is required that the blade edge only generates frictional resistance in the direction of rotation. In the case of the inclination of the blade edge, the blade edge produces a shape force that increases or decreases the pressure at the blade tip end. The blade edge can be rotated in the blade direction as needed. Appropriate expansion in an approximate involute pattern. Summary of the invention
前面所述的具有单边弧形叶边桨叶结构的轴流风扇技术, 在实验中发现完全相同形状结 构的单边弧形叶边, 在一部份轴流风扇上使用, 节能降噪效果非常好, 而在另一部分轴流风 扇上, 却没有节能降噪效果。 由于不清楚是什么原因, 因此无法有把握的设计这种具有节能 降噪效果的的轴流风扇, 严重阻碍了这项技术的应用。  The axial fan technology with single-edge curved blade edge paddle structure described above finds a single-sided curved blade edge of the same shape structure in the experiment, and is used on a part of the axial flow fan to save energy and noise reduction effect. Very good, but on another part of the axial fan, there is no energy saving noise reduction effect. Since it is unclear what the reason is, it is impossible to confidently design such an axial flow fan with energy-saving and noise-reducing effects, which seriously hinders the application of this technology.
本发明通过大量研究试验发现问题与单边弧形叶边结构、 形状、 位置、 空间运动轨迹等 无关, 通过大量试验和研究发现桨叶负压力面与轴流风扇径向之间的夹角 β对节能作用效果 有着关键作用, 当夹角 β为正值, 单边弧形叶边桨叶结构的轴流风扇具有非常好的节能降噪 效果, 如附图 1所示; 当夹角 β为负值, 单边弧形叶边桨叶结构的轴流风扇节能降噪效果很 小, 甚至不具有节能降噪效果, 如附图 2所示。  The invention finds that the problem is independent of the unilateral curved blade edge structure, shape, position, spatial motion trajectory, etc. through a large number of research and experiments. Through a large number of experiments and studies, the angle between the negative pressure surface of the blade and the radial direction of the axial fan is found. It plays a key role in energy saving effect. When the angle β is positive, the axial fan with single-sided curved blade edge structure has very good energy-saving and noise-reducing effect, as shown in Figure 1; Negative value, the axial flow fan with single-sided curved blade edge structure has little energy-saving and noise-reducing effect, and does not even have energy-saving and noise-reducing effects, as shown in Fig. 2.
研究发现, 在夹角 β为正值情况下, 桨叶负压力面能够得到充分的流体补充, 使桨叶负 压力面的压强绝对值降低, 从而降低了桨叶压力抵抗、 使桨叶阻力和能耗都得到降低。 由于 桨叶负压力面的压强绝对值减小, 与周围空间的压力差减小, 流体向桨叶负压力面流动速度 降低, 因此产生的涡流强度也相应降低, 噪音也得到相应降低。 上述作用在桨叶叶端效果最 显著, 因为这里是风扇线速度最快, 产生的各项作用力最大, 压力梯度也最大的位置, 而且 在绝大部分风扇使用的旋转线速度范围内, 桨叶负压力面产生的作用力远大于正压力面, 因 此降低桨叶负压力面压强绝对值, 节能降噪效果非常显著。  It is found that when the angle β is positive, the negative pressure surface of the blade can be fully replenished, and the absolute value of the pressure on the negative pressure surface of the blade is reduced, thereby reducing the pressure resistance of the blade and the resistance of the blade. Energy consumption is reduced. Since the absolute value of the pressure on the negative pressure surface of the blade is reduced, the pressure difference from the surrounding space is reduced, and the flow velocity of the fluid to the negative pressure surface of the blade is lowered, so that the eddy current intensity is also reduced correspondingly, and the noise is also correspondingly reduced. The above effect is most pronounced at the blade end, because it is the fastest fan speed, the most powerful force, the largest pressure gradient, and the paddle speed range used by most fans. The force generated by the negative pressure surface of the blade is much larger than the positive pressure surface, so the absolute value of the negative pressure surface pressure of the blade is reduced, and the energy saving and noise reduction effect is very significant.
本发明解决其技术问题所采用的技术方案是: 具有单边弧形叶边桨叶结构的轴流风扇桨 叶, 该桨叶负压力面与轴流风扇径向之间的夹角 β在 0度至 90度之间, 或具有单边弧形叶边桨 叶结构的轴流风扇桨叶, 该桨叶负压力面与轴流风扇径向之间的平均夹角 β在 0度至 90度之 间, 研究和试验发现夹角 β或平均夹角 β角度数值最佳范围在 6度至 50度之间。  The technical solution adopted by the present invention to solve the technical problem thereof is: an axial flow fan blade having a single-sided curved blade edge blade structure, and an angle β between the negative pressure surface of the blade and the radial direction of the axial fan is 0. Between 90 degrees, or an axial fan blade having a single-sided curved blade-edge blade structure, the average angle β between the negative pressure surface of the blade and the radial direction of the axial fan is between 0 and 90 degrees Between the studies and experiments, it was found that the angle between the angle β or the average angle β is optimally between 6 and 50 degrees.
本发明的有益效果是, 为单边弧形叶边桨叶技术的应用扫除了技术障碍, 为设计制造高 效率、 低噪音轴流风扇奠定了基础和提供了可行的实施方案, 避免了在节能降噪原理不清楚 的情况下, 没有可靠的实施技术方案条件下, 盲目设计造成的损失, 使单边弧形叶边桨叶这 项节能降噪技术达到了应用水平。  The invention has the beneficial effects that the technical obstacles are eliminated for the application of the single-sided curved blade edge blade technology, which lays a foundation and provides a feasible implementation scheme for designing and manufacturing a high-efficiency, low-noise axial flow fan, thereby avoiding energy saving. Under the condition that the principle of noise reduction is not clear, the loss caused by blind design under the condition of reliable implementation technical solution makes the energy-saving and noise-reduction technology of single-sided curved blade edge blade reach the application level.
附图说明 DRAWINGS
下面结合附图和实施例对本发明进一步说明。  The invention will now be further described with reference to the drawings and embodiments.
图 1是桨叶负压力面与轴流风扇径向之间的夹角 β为正值的图示。  Figure 1 is a graphical representation of the positive angle β between the negative pressure surface of the blade and the radial direction of the axial fan.
图 2是桨叶负压力面与轴流风扇径向之间的夹角 β为负值的图示。  Figure 2 is a graphical representation of the negative angle β between the negative pressure surface of the blade and the radial direction of the axial fan.
图 3 是单边弧形叶边与桨叶负压力面连接位置的表面为曲面形状情况下, 桨叶负压力面 与风扇径向之间的平均夹角 β的图示。 图 4是桨叶负压力面为曲面形状情况下, 桨叶负压力面与风扇径向之间的平均夹角 β的 图示。 Fig. 3 is a graphical representation of the average angle β between the negative pressure surface of the blade and the radial direction of the fan in the case where the surface of the single-sided curved blade edge and the blade negative pressure surface are curved. Figure 4 is a graphical representation of the average angle β between the negative pressure surface of the blade and the radial direction of the fan in the case where the negative pressure surface of the blade is curved.
图 5是采用单边弧形叶边与桨叶形成一体结构的桨叶, 单边弧形叶边与桨叶之间没有明 显分界线, 在此情况下, 桨叶负压力面与轴流风扇径向之间的平均夹角 β的图示。  Figure 5 is a blade with a single-sided curved blade edge and blade forming an integral structure, there is no obvious boundary between the single-sided curved blade edge and the blade, in this case, the blade negative pressure surface and the axial flow fan A graphical representation of the average angle β between the radial directions.
图 6是描述单边弧形叶边桨叶结构的轴流风扇各部分采用的名称与具体对应位置示意图。 图中 1.桨叶 , 2.桨毂, 3.桨叶根部, 4.桨叶端部, 5.单边弧形叶边, 6.由轴流风扇径向向 桨叶负压力面流动的流体, 7.桨叶负压力面。  Fig. 6 is a schematic view showing the names and specific positions of the respective portions of the axial flow fan of the single-sided curved blade edge paddle structure. 1. Blade, 2. Hub, 3. Blade root, 4. Blade end, 5. Single-sided curved edge, 6. Axial fan radially flowing toward the negative pressure surface of the blade Fluid, 7. Blade negative pressure surface.
具体实施方式 detailed description
在图 1 所示实施例中, 有单边弧形叶边的桨叶 (1 ) 的负压力面 (7) 与轴流风扇径向之 间夹角 β的角度数值为正值, 由桨叶端部 (4) 的外部, 沿轴流风扇径向流动的流体 (6) 能 够到达桨叶负压力面 (7) 的附面层, 能够减小桨叶负压力面 (7) 的压强绝对值, 减小桨叶 的压力抵抗, 从而减少桨叶阻力, 减小桨叶能耗, 降低噪音。  In the embodiment shown in Fig. 1, the angle between the negative pressure surface (7) of the blade (1) having a single-sided curved blade edge and the radial direction of the axial fan is positive, by the blade Outside the end (4), the fluid (6) flowing radially along the axial fan can reach the boundary layer of the negative pressure surface (7) of the blade, which can reduce the absolute value of the pressure on the negative pressure surface (7) of the blade. , reduce the pressure resistance of the blade, thereby reducing blade resistance, reducing blade energy consumption, and reducing noise.
在图 2所示, 桨叶负压力面 (7) 与轴流风扇径向之间夹角 β的角度数值为负值。 由桨叶 端部 (4) 的外部, 沿轴流风扇径向流动的流体 (6) 不能到达桨叶负压力面 (7) 的附面层, 桨叶负压力面 (7) 的压力基本没有变化, 因此没有节能降噪效果。  In Fig. 2, the angle value of the angle β between the negative pressure surface (7) of the blade and the radial direction of the axial fan is negative. From the outside of the blade end (4), the fluid (6) flowing radially along the axial fan cannot reach the boundary layer of the negative pressure surface (7) of the blade, and the pressure of the negative pressure surface (7) of the blade is substantially absent. Change, so there is no energy saving noise reduction effect.
在图 3所示实施例中, 桨叶负压力面 (7) 与轴流风扇径向之间平均夹角 β的角度数值为 正值, 单边弧形叶边(5 ) 与桨叶负压力面 (7)连接位置表面为曲面形状, 沿这曲面形状向 桨叶负压力面流动的流体, 能量损失小, 涡流涡度减小, 节能降噪效果进一步提高。  In the embodiment shown in Fig. 3, the angle value of the average angle β between the negative pressure surface (7) of the blade and the radial direction of the axial fan is positive, the edge of the curved edge of the blade (5) and the negative pressure of the blade The surface of the joint surface (7) is a curved surface shape, and the fluid flowing along the negative pressure surface of the blade shape has a small energy loss, a reduced vortex vorticity, and an energy saving and noise reduction effect is further improved.
在图 4所示实施例中, 桨叶负压力面与轴流风扇径向之间平均夹角 β的角度数值为正值, 单边弧形叶边 (5 ) 相对轴流风扇轴向有外倾角, 流体沿单边弧形叶边 (5 ) 和单边弧形叶边 ( 5 )与桨叶负压力面连接位置表面构成的曲面向桨叶负压力面流动, 能量损失更小, 节能降 噪效果进一步提高。  In the embodiment shown in Fig. 4, the angle value of the average angle β between the negative pressure surface of the blade and the radial direction of the axial fan is positive, and the edge of the curved edge of the single side (5) is opposite to the axial direction of the axial fan. Inclination, the fluid flows along the curved surface of the blade with the curved surface of the unilateral curved edge (5) and the unilateral curved edge (5) and the negative pressure surface of the blade, resulting in less energy loss and energy saving. The noise effect is further improved.
在图 5所示实施例中, 单边弧形叶边与桨叶形成一体结构的桨叶, 单边弧形叶边与桨叶 之间没有明显分界线, 桨叶负压力面与单边弧形叶边整体成曲面形状, 一体结构桨叶负压力 面与风扇径向之间平均夹角 β的角度数值为正值, 在靠近桨毂的桨叶根部 (3 ) 和桨叶中部, 桨叶负压力面与风扇径向之间平均夹角 β的角度数值为负值, 由于夹角 β为负值部分桨叶线 速度较低, 对整体节能降噪效果影响不起主要作用, 轴流风扇整体仍有较好的节能降噪效果。  In the embodiment shown in FIG. 5, the blade with the single-sided curved blade edge and the blade forming an integral structure has no obvious boundary line between the single-sided curved blade edge and the blade, and the blade negative pressure surface and the single-sided arc The shape of the shape of the blade is integrally curved, and the angle between the negative pressure surface of the integrated structure and the radial angle of the fan is positive, at the root of the blade (3) near the hub and the middle of the blade, the blade The angle value of the average angle β between the negative pressure surface and the fan radial direction is a negative value. Since the angle β is a negative value, the blade linear velocity is low, which has no major effect on the overall energy saving and noise reduction effect. The axial flow fan The overall still has good energy saving and noise reduction effects.
轴流压气机采用这项技术, 特别是第一级, 能够增加流体吸入量, 减少叶端泄漏损失, 减少功耗, 提高压缩性能。  This technology is used in axial compressors, especially in the first stage, which increases fluid intake, reduces tip leakage losses, reduces power consumption, and improves compression performance.
本发明技术可以应用于各种流体输送用途的螺旋桨、 轴流风机、 轴流鼓风机、 轴流压气 机、 风扇、 轴流泵、 风力灭火机等流体机械, 或各种搅拌流体的流体机械。  The technology of the present invention can be applied to fluid machines such as propellers, axial flow fans, axial flow blowers, axial flow compressors, fans, axial flow pumps, wind fire extinguishers, and the like, or various fluid machines for agitating fluids.
本发明桨叶可以采用铸造、 压铸、 注塑、 冲压、 机械切削、 焊接等方法制造。 说明: The blade of the present invention can be produced by casting, die casting, injection molding, stamping, mechanical cutting, welding, and the like. Description:
平均夹角 β: 取曲线两端的连线与轴流风扇径向的夹角为平均夹角 β; 或取曲线各点的 切线与轴流风扇径向的夹角的平均值为平均夹角 β 。  Average angle β: The angle between the line connecting the two ends of the curve and the radial direction of the axial fan is the average angle β; or the average value of the angle between the tangent of each point of the curve and the radial direction of the axial fan is the average angle β .
本发明设定轴流风扇径向与轴流风扇轴向是相互垂直的。  The invention sets the radial direction of the axial flow fan and the axial direction of the axial flow fan to be perpendicular to each other.

Claims

权 利 妥 豕 Right
1. 一种降低能耗和噪音的轴流风扇, 在桨毂 (2) 上安装有若干桨叶 (1 ), 在桨叶 (1 ) 上有 单边弧形叶边 (5 ), 或在桨毂 (2) 上安装有若干单边弧形叶边 (5 ) 与桨叶 (1 ) 形成一体结 构的桨叶,其特征是: 桨叶负压力面与轴流风扇径向之间的夹角 β在 0度至 90度之间, 或桨 叶负压力面与轴流风扇径向之间的平均夹角 β在 0度至 90度之间。  1. An axial fan that reduces energy consumption and noise, with a plurality of blades (1) mounted on the hub (2) and a single curved edge (5) on the blade (1), or The hub (2) is provided with a plurality of single-sided curved edge (5) and a blade formed integrally with the blade (1), characterized by: a clamp between the negative pressure surface of the blade and the radial direction of the axial fan The angle β is between 0 and 90 degrees, or the average angle β between the negative pressure surface of the blade and the radial direction of the axial fan is between 0 and 90 degrees.
2.根据权利要求 1所述的轴流风扇, 其特征是: 桨叶负压力面与轴流风扇径向之间的夹角 β 在 6度至 50度之间,或桨叶负压力面与轴流风扇径向之间的平均夹角 β在 6度至 50度之间。  The axial flow fan according to claim 1, wherein: an angle β between the negative pressure surface of the blade and the radial direction of the axial fan is between 6 degrees and 50 degrees, or a negative pressure surface of the blade The average angle β between the radial directions of the axial fans is between 6 and 50 degrees.
PCT/CN2009/070153 2008-03-12 2009-01-15 An axial flow fan for decreasing the noise and the energy consumption WO2009111956A1 (en)

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CN104139849B (en) * 2014-08-07 2015-02-25 西北工业大学 High-altitude propeller and propeller tip winglet capable of improving efficiency of high-altitude propeller
CN104329276A (en) * 2014-11-28 2015-02-04 德清振达电气有限公司 Efficient mute axial flow fan
CN104358712A (en) * 2014-11-28 2015-02-18 德清振达电气有限公司 Fan blade of safe and high-efficiency axial flow fan
CN104389821A (en) * 2014-11-28 2015-03-04 德清振达电气有限公司 Silent axial fan blade

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