CN110207530B - High-strength heat exchange fin adopting bidirectional discrete protrusions - Google Patents

High-strength heat exchange fin adopting bidirectional discrete protrusions Download PDF

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CN110207530B
CN110207530B CN201910440956.6A CN201910440956A CN110207530B CN 110207530 B CN110207530 B CN 110207530B CN 201910440956 A CN201910440956 A CN 201910440956A CN 110207530 B CN110207530 B CN 110207530B
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heat exchange
fin
raised
convex structure
exchange tube
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CN110207530A (en
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李明佳
汤松臻
王飞龙
何雅玲
陶文铨
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Xian Jiaotong University
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/04Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element
    • F28F3/042Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of local deformations of the element

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  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

一种采用双向离散凸起的高强度换热翅片,所述换热翅片包括翅片基体、折边结构、离散凸起结构和换热管;所述翅片基体上布置双向离散凸起结构;所述凸起结构一和凸起结构四为相同凸起方向,与凸起结构二和凸起结构三的凸起方向相反。所述双向离散凸起的高强度换热翅片,通过设置多组离散凸起可以使流体产生剧烈的扰动,能够显著地强化换热;且将多组离散凸起设置为双向布置,能够有效地作用于整个翅片流道内的流体,也能够降低流动阻力。

Figure 201910440956

A high-strength heat exchange fin using bidirectional discrete protrusions, the heat exchange fin includes a fin base, a folded edge structure, a discrete protrusion structure and a heat exchange tube; the fin base is arranged with bidirectional discrete protrusions structure; the convex structure one and the convex structure four are in the same convex direction, which is opposite to the convex direction of the convex structure two and the convex structure three. For the high-strength heat exchange fins with bidirectional discrete protrusions, by setting multiple groups of discrete protrusions, the fluid can be violently disturbed, and heat exchange can be significantly enhanced; It can also reduce the flow resistance by acting on the fluid in the entire fin flow channel.

Figure 201910440956

Description

一种采用双向离散凸起的高强度换热翅片A high-strength heat exchange fin with two-way discrete protrusions

技术领域technical field

本发明属于换热器技术领域,涉及一种适用于暖通空调、制冷、化工、汽车等各行业的管翅式换热器翅片,特别涉及一种采用双向离散凸起的高强度换热翅片。The invention belongs to the technical field of heat exchangers, and relates to a tube-fin heat exchanger fin suitable for various industries such as heating, ventilation, air conditioning, refrigeration, chemical industry, automobile, etc., in particular to a high-strength heat exchange using bidirectional discrete protrusions fins.

背景技术Background technique

换热器是空调中重要的部件之一,它的性能好坏直接影响到空调的整体效能。随着我国对家用空调能效的要求越来越高,尤其是如何在低成本的情况下,提高换热器的性能更是分析研究的重点。目前空调中主要采用管翅式换热器,由于空气侧传热性能较差,这种换热器的热阻主要集中于管外的空气侧,管外热阻可以占到总热阻的80%~90%,所以,优化管外的翅片结构将会有效改善换热器的传热性能。换热器翅片的形式有多种多样,由最初的平板翅片、波纹翅片,到后来发展的百叶窗翅片、开缝翅片等。这些翅片增加了换热器空气侧的换热面积,同时还增强了对流体的扰动,大大强化了换热器的换热性能。但是,传统的开缝或百叶窗翅片通常适用于非结霜工况的传热强化,因为传统的开缝或百叶窗翅片强化结构常常在结霜工况下容易被霜层堵塞,从而降低了翅片的换热性能。The heat exchanger is one of the important components in the air conditioner, and its performance directly affects the overall efficiency of the air conditioner. With the increasing demand for energy efficiency of household air conditioners in my country, how to improve the performance of heat exchangers at low cost is the focus of analysis and research. At present, tube-fin heat exchangers are mainly used in air conditioners. Due to the poor heat transfer performance on the air side, the thermal resistance of this heat exchanger is mainly concentrated on the air side outside the tubes, and the thermal resistance outside the tubes can account for 80% of the total thermal resistance. % to 90%, therefore, optimizing the fin structure outside the tube will effectively improve the heat transfer performance of the heat exchanger. There are various forms of heat exchanger fins, from the initial flat fins and corrugated fins to the later developed louver fins and slotted fins. These fins increase the heat exchange area on the air side of the heat exchanger, and at the same time increase the disturbance to the fluid, greatly enhancing the heat exchange performance of the heat exchanger. However, traditional slotted or louvered fins are usually suitable for heat transfer enhancement in non-frost conditions, because traditional slotted or louvered fin reinforcement structures are often easily blocked by frost in frosted conditions, thereby reducing the Heat transfer performance of fins.

但是开缝翅片能够有效地强化换热,因此,本发明中尽量在不开窗和不开缝的条件下对翅片进行改进,并满足加工工艺的翅片对称性和高强度要求,采用双向开缝的思想,提出了双向离散凸起结构翅片,能够有效降低结霜问题对翅片换热能力的影响。However, slotted fins can effectively strengthen heat exchange. Therefore, in the present invention, the fins are improved as far as possible without opening windows and slots, and to meet the requirements of fin symmetry and high strength in the processing technology. The idea of two-way slits is proposed, and the two-way discrete convex structure fins are proposed, which can effectively reduce the effect of frosting on the heat transfer capacity of the fins.

发明内容SUMMARY OF THE INVENTION

为了克服上述现有技术的缺点,本发明的目的在于提供一种采用双向离散凸起的高强度换热翅片,In order to overcome the above-mentioned shortcomings of the prior art, the purpose of the present invention is to provide a high-strength heat exchange fin using two-way discrete protrusions,

为了实现上述目的,本发明采用的技术方案是:In order to achieve the above object, the technical scheme adopted in the present invention is:

一种采用双向离散凸起的高强度换热翅片,包括翅片基体1,在翅片基体1上有供换热管穿过的换热管孔7,其特征在于,在翅片基体1上环绕换热管孔7设置有双向离散凸起结构。翅片通过双向离散凸起结构实现流体的剧烈扰动,破坏流动边界层,并具有引流效果,减少管后流动滞止区。A high-strength heat exchange fin using two-way discrete protrusions, including a fin base 1, and a heat exchange tube hole 7 for the heat exchange tube to pass through on the fin base 1, characterized in that the fin base 1 The upper periphery of the heat exchange tube hole 7 is provided with a bidirectional discrete convex structure. The fins achieve violent disturbance of the fluid through the bidirectional discrete convex structure, destroy the flow boundary layer, and have a drainage effect to reduce the flow stagnation area behind the tube.

所述双向离散凸起结构包括若干段关于换热管孔7中心对称的凸起结构一3和凸起结构二4,以及位于相邻换热管孔7之间的凸起结构三5和凸起结构四6,其中,凸起结构一3、凸起结构二4、凸起结构三5、凸起结构四6均位于翅片基体1上且各不相连。The two-way discrete convex structures include several sections of convex structures one 3 and two convex structures 4 symmetrical about the center of the heat exchange tube hole 7, and convex structures three 5 and two convex structures located between adjacent heat exchange tube holes 7. A structure four 6 is formed, wherein the convex structure one 3, the convex structure two 4, the convex structure three 5, and the convex structure four 6 are all located on the fin base 1 and are not connected to each other.

所述凸起结构一3和凸起结构四6的凸起方向相同,且均与凸起结构二4和凸起结构三5的凸起方向相反。The protruding structure 1 3 and the protruding structure 4 6 have the same protruding direction, and are opposite to the protruding direction of the protruding structure 2 4 and the protruding structure 3 5 .

其中,关于同一换热管孔7中心对称的各段凸起结构一3和凸起结构二4位于同一圆周上,所述凸起结构四6布置在相邻换热管孔7的连线上,凸起结构三5为多个,沿相邻换热管孔7的连线对称布置,所述凸起结构三5和凸起结构四6均位于所述圆周之外。Among them, each section of raised structure 1 3 and raised structure 2 4 that are symmetrical with respect to the center of the same heat exchange tube hole 7 are located on the same circumference, and the raised structure 4 6 is arranged on the connecting line of the adjacent heat exchange tube holes 7 There are multiple protruding structures 5 , which are symmetrically arranged along the connecting line of the adjacent heat exchange tube holes 7 , and the protruding structures 3 5 and the protruding structures 4 6 are both located outside the circumference.

所述凸起结构一3的高度为0.5~1.0mm,底面为直角梯形,底边长度为1.5~2.5mm,底面的高为1.5~3.0mm,底角为60~70°;所述凸起结构二4的高度为0.5~1.0mm,底面的内半径为5.6mm,外半径为7.0~8.0mm,凸起的两个弧面与翅片表面的夹角均为45~60°,其余两个侧面与翅片表面的夹角为30~45°;所述凸起结构三5的高度为0.5~1.0mm,底面为等腰梯形,顶边长度为1.5~3.0mm,底边长度为2.5~4.0mm,底面的高为2.5~3.5mm,靠近和远离翅片边缘的两侧面与翅片表面的夹角均为30~45°,其余两个侧面与翅片表面的夹角为45~60°;所述凸起结构四6的高度为0.5~1.0mm,两个弧面与与翅片表面的夹角为45~60°,其余两个侧面与翅片表面的夹角为30~45°,沿片宽方向底面的长度为2.5~4.0mm,底面弧线的半径为8.5~9.5mm。The height of the raised structure one 3 is 0.5-1.0 mm, the bottom surface is a right-angled trapezoid, the length of the bottom side is 1.5-2.5 mm, the height of the bottom surface is 1.5-3.0 mm, and the bottom angle is 60-70°; The height of the structure 24 is 0.5-1.0mm, the inner radius of the bottom surface is 5.6mm, and the outer radius is 7.0-8.0mm. The angle between each side and the surface of the fin is 30-45°; the height of the raised structure 5 is 0.5-1.0mm, the bottom surface is an isosceles trapezoid, the length of the top side is 1.5-3.0mm, and the length of the bottom side is 2.5mm ~4.0mm, the height of the bottom surface is 2.5~3.5mm, the angle between the two sides near and far from the edge of the fin and the surface of the fin is 30~45°, and the angle between the other two sides and the surface of the fin is 45~ 60°; the height of the raised structure 6 is 0.5-1.0mm, the angle between the two arc surfaces and the surface of the fin is 45-60°, and the angle between the other two sides and the surface of the fin is 30- 45°, the length of the bottom surface along the sheet width direction is 2.5 to 4.0 mm, and the radius of the arc of the bottom surface is 8.5 to 9.5 mm.

所述翅片基体1为平直结构,换热管孔7在翅片基体1宽度方向位于对称线上,所述双向离散凸起高强度换热翅片为对称翅片。The fin base 1 has a straight structure, the heat exchange tube holes 7 are located on a symmetrical line in the width direction of the fin base 1, and the bidirectionally discrete raised high-strength heat exchange fins are symmetrical fins.

所述翅片基体1厚度为0.09~0.11mm,宽度为18.19~21.65mm;相邻翅片基体1的间距为1.3~1.6mm;所述换热管的管径为7mm或7.94mm;相邻换热管孔7的孔距为21~23mm。The thickness of the fin base body 1 is 0.09-0.11mm, and the width is 18.19-21.65mm; the distance between the adjacent fin base bodies 1 is 1.3-1.6mm; the diameter of the heat exchange tube is 7mm or 7.94mm; The hole spacing of the heat exchange tube holes 7 is 21-23 mm.

所述翅片基体1的长边两侧设置有折边结构2。Folding structures 2 are provided on both sides of the long side of the fin base 1 .

与现有技术相比,本发明的有益效果是:Compared with the prior art, the beneficial effects of the present invention are:

1)在换热管的圆周设置离散凸起结构,能够增强流体的扰动,增加流体与换热管和翅片表面的换热强度,且减小流体在换热管后的流动滞止区。而且,采用双向凸起,能够地整个翅片流道内的流体进行扰动,可以显著地强化换热。1) Discrete convex structures are arranged on the circumference of the heat exchange tube, which can enhance the disturbance of the fluid, increase the heat exchange intensity between the fluid and the heat exchange tube and the surface of the fins, and reduce the flow stagnation area of the fluid behind the heat exchange tube. Moreover, the use of bidirectional protrusions can disturb the fluid in the entire fin flow channel, which can significantly enhance heat exchange.

2)在相邻换热管的对称轴方向上,设置三个交替反向凸起结构,可以有效增强流体在主流方向上的扰动,进一步地强化换热。2) In the direction of the symmetry axis of the adjacent heat exchange tubes, three alternately reversed convex structures are arranged, which can effectively enhance the disturbance of the fluid in the main flow direction and further strengthen the heat exchange.

3)在每个凸起的侧面均采用一定的倾角,可以增强流体换热的同时并不产生较大的流体阻力。3) A certain inclination angle is adopted on the side surface of each protrusion, which can enhance the fluid heat exchange without generating large fluid resistance.

4)在翅片前缘和后缘设置折边结构,能够有效增强翅片强度。4) The folding structure is arranged on the leading edge and the trailing edge of the fin, which can effectively enhance the strength of the fin.

附图说明Description of drawings

下面结合附图所描述的实施方式对本发明进一步说明。The present invention will be further described below with reference to the embodiments described in the accompanying drawings.

图1为本发明的实施例的俯视图。FIG. 1 is a top view of an embodiment of the present invention.

图2为本发明的实施例的A-A剖面视图。Figure 2 is an A-A cross-sectional view of an embodiment of the present invention.

图3为本发明的实施例的B-B剖面视图。3 is a B-B cross-sectional view of an embodiment of the present invention.

图4为本发明的实施例的C-C剖面视图。4 is a C-C cross-sectional view of an embodiment of the present invention.

图5为本发明的实施例的轴测图。Figure 5 is an isometric view of an embodiment of the present invention.

具体实施方式Detailed ways

下面结合附图和实施例详细说明本发明的实施方式。The embodiments of the present invention will be described in detail below with reference to the accompanying drawings and examples.

参见图1至图5,是本发明的双向离散凸起高强度换热翅片的实施例,该翅片的主要特征包括:翅片基体1、折边结构2、凸起结构一3、凸起结构二4、凸起结构三5、凸起结构四6和换热管孔7。1 to 5, it is an embodiment of the bidirectional discrete convex high-strength heat exchange fin of the present invention. The main features of the fin include: a fin base 1, a folded edge structure 2, a convex structure one 3, a convex structure Lifting structure two 4 , raised structure three 5 , raised structure four 6 and heat exchange tube hole 7 .

翅片基体1为平直翅片,其长边两侧设置有折边结构2,供换热管穿过的换热管孔7在翅片基体1宽度方向位于对称线上。在翅片基体1上环绕换热管孔7设置有双向离散凸起结构,双向离散凸起结构主要由若干段关于换热管孔7中心对称的上述凸起结构一3和凸起结构二4,以及位于相邻换热管孔7之间的上述凸起结构三5和凸起结构四6组成,其中凸起结构一3、凸起结构二4、凸起结构三5、凸起结构四6均位于翅片基体1上且各不相连。且凸起结构一3和凸起结构四6的凸起方向相同,且均与凸起结构二4和凸起结构三5的凸起方向相反。The fin base 1 is a straight fin, and the two sides of the long side are provided with a folding structure 2 , and the heat exchange tube holes 7 for the heat exchange tubes to pass through are located on the symmetry line in the width direction of the fin base 1 . The fin base 1 is provided with a bidirectional discrete convex structure surrounding the heat exchange tube hole 7 , and the bidirectional discrete convex structure is mainly composed of several sections of the above-mentioned convex structure 1 3 and the convex structure 2 4 that are symmetrical about the center of the heat exchange tube hole 7 . , and the above-mentioned raised structures three 5 and four raised structures 6 between the adjacent heat exchange tube holes 7 are composed of raised structures one 3, raised structures two 4, raised structures three 5, raised structures four 6 are all located on the fin base 1 and are not connected to each other. Moreover, the protruding direction of the protruding structure 1 3 and the protruding structure 4 6 is the same, and both are opposite to the protruding direction of the protruding structure 2 4 and the protruding structure 3 5 .

整个双向离散凸起高强度换热翅片为对称翅片,翅片通过双向离散凸起结构实现流体的剧烈扰动,破坏流动边界层,并具有引流效果,减少管后流动滞止区。The entire bidirectional discrete raised high-strength heat exchange fins are symmetrical fins. The fins achieve violent disturbance of the fluid through the bidirectional discrete raised structure, destroy the flow boundary layer, and have a drainage effect to reduce the flow stagnation area behind the tube.

本实施例中,关于同一换热管孔7中心对称的各段凸起结构一3和凸起结构二4位于同一圆周上,凸起结构四6布置在相邻换热管孔7的连线上,凸起结构三5为多个,沿相邻换热管孔7的连线对称布置,凸起结构三5和凸起结构四6均位于上述的圆周之外。In this embodiment, each segment of raised structure 1 3 and raised structure 2 4 that are symmetrical with respect to the center of the same heat exchange tube hole 7 are located on the same circumference, and the raised structure 4 6 is arranged on the connecting line of adjacent heat exchange tube holes 7 Above, there are a plurality of raised structures 5 , which are symmetrically arranged along the connecting line of the adjacent heat exchange tube holes 7 , and the raised structures 3 5 and the raised structures 4 6 are both located outside the above-mentioned circumference.

下面介绍实施例的具体结构参数,在介绍中,以翅片宽度方向为纵向,翅片长度方向为横向,以靠近换热管孔7方向为内侧,远离换热管孔7的方向为外侧。The specific structural parameters of the embodiment are described below. In the introduction, the width direction of the fins is the longitudinal direction, the length direction of the fins is the transverse direction, the direction close to the heat exchange tube hole 7 is the inner side, and the direction away from the heat exchange tube hole 7 is the outer side.

翅片宽度(也即翅片基体1的宽度)为21.65mm,相邻换热管孔7的孔距为21mm,翅片厚度(也即翅片基体1的厚度)为0.1mm,换热管管径为7mm。所有凸起结构的高度均为0.7mm。凸起结构一3的底面为直角梯形,底边长度为2.0mm,底面的高为3.0mm,底角为70°。凸起结构二4底面的内半径为5.6mm,外半径为7.4mm,凸起的两个弧面与翅片表面的夹角均为60°,其余两个侧面与翅片表面的夹角为45°。凸起结构三5的底面为等腰梯形,顶边长度为2.5mm,底边长度为4.0mm,底面的高为2.5mm,靠近和远离翅片边缘的两侧面与翅片表面的夹角均为45°,其余两个侧面与翅片表面的夹角为60°。凸起结构四6的两个弧面与与翅片表面的夹角为60°,其余两个侧面与翅片表面的夹角为45°,沿片宽方向底面的长度为4.0mm,底面弧线的半径为9.0mm。折边结构2的垂直高度为0.3mm,坡度为20°,斜坡下边线与翅片边缘的距离为1.0mm。The width of the fins (that is, the width of the fin base 1) is 21.65 mm, the distance between the adjacent heat exchange tube holes 7 is 21 mm, and the thickness of the fins (that is, the thickness of the fin base 1) is 0.1 mm. The pipe diameter is 7mm. The height of all raised structures is 0.7mm. The bottom surface of the raised structure 1 3 is a right-angled trapezoid, the length of the bottom side is 2.0mm, the height of the bottom surface is 3.0mm, and the bottom angle is 70°. The inner radius of the bottom surface of the convex structure 24 is 5.6mm, the outer radius is 7.4mm, the angle between the two convex arc surfaces and the surface of the fin is 60°, and the angle between the other two sides and the surface of the fin is 45°. The bottom surface of the raised structure 35 is an isosceles trapezoid, the length of the top side is 2.5mm, the length of the bottom side is 4.0mm, the height of the bottom surface is 2.5mm, and the angles between the two sides near and far from the edge of the fin and the surface of the fin are equal. is 45°, and the angle between the remaining two sides and the surface of the fin is 60°. The angle between the two arc surfaces of the raised structure 46 and the surface of the fin is 60°, the angle between the other two side surfaces and the surface of the fin is 45°, the length of the bottom surface along the width direction of the fin is 4.0mm, and the arc of the bottom surface is 4.0 mm. The radius of the wire is 9.0mm. The vertical height of the folding structure 2 is 0.3mm, the slope is 20°, and the distance between the lower edge of the slope and the edge of the fin is 1.0mm.

采用ANSYS FLUENT软件对该实施例和行业已经采用的折边平直翅片的流动换热性能进行数值计算。计算条件为:空气流速1.597m/s,进口温度308K,换热管壁面温度318.5K,采用稳态、常物性的SST k-w模型。通过有限容积法对控制方程进行离散,压力与速度的耦合采用SIMPLE算法。模拟考虑翅片厚度的影响,换热翅片壁面为速度无滑移固体边界,翅片表面温度由流固换热耦合计算得出。对于动量以及能量方程,扩散项采用中心差分格式,对流项采用二阶迎风差分格式。当连续性方程、动量方程以及能量方程的残差均低于10-6时,认为数值结果收敛。ANSYS FLUENT software is used to numerically calculate the flow heat transfer performance of this embodiment and the folded straight fins that have been used in the industry. The calculation conditions are as follows: the air velocity is 1.597m/s, the inlet temperature is 308K, and the wall temperature of the heat exchange tube is 318.5K. The SST kw model of steady state and constant physical properties is adopted. The governing equations are discretized by the finite volume method, and the SIMPLE algorithm is used for the coupling of pressure and velocity. The simulation considers the influence of the thickness of the fin, the wall of the heat exchange fin is a velocity-free solid boundary, and the surface temperature of the fin is calculated by the fluid-solid heat transfer coupling. For the momentum and energy equations, the diffusion term uses the central difference format, and the convection term uses the second-order upwind difference format. The numerical results are considered convergent when the residuals of the continuity equation, momentum equation and energy equation are all below 10 -6 .

通过提取计算区域进出口的压力和温度,可以计算出不同翅片的换热量和压降,同时考虑风机自身所损耗的压降,即可获得相同功率下换热量的变化情况。数据计算结果表明,与行业已经采用的折边平直翅片相比,本实施例的换热系数得到大幅提高,在相同功率条件下换热量提升9.3%,可以保证在不开窗和不开缝的情况下实现综合性能的显著提升。By extracting the pressure and temperature at the inlet and outlet of the calculation area, the heat exchange and pressure drop of different fins can be calculated, and the change of heat exchange under the same power can be obtained by considering the pressure drop lost by the fan itself. The data calculation results show that compared with the folded and straight fins that have been used in the industry, the heat transfer coefficient of this embodiment is greatly improved, and the heat transfer is increased by 9.3% under the same power condition, which can ensure that the window is not opened and In the case of slitting, the overall performance is significantly improved.

Claims (2)

1.一种采用双向离散凸起的高强度换热翅片,包括翅片基体(1),在翅片基体(1)上有供换热管穿过的换热管孔(7),在翅片基体(1)上环绕换热管孔(7)设置有双向离散凸起结构,其特征在于:所述双向离散凸起结构包括若干段关于换热管孔(7)中心对称的凸起结构一(3)和凸起结构二(4),以及位于相邻换热管孔(7)之间的凸起结构三(5)和凸起结构四(6),其中,凸起结构一(3)、凸起结构二(4)、凸起结构三(5)、凸起结构四(6)均位于翅片基体(1)上且各不相连,所述翅片基体(1)为平直结构,换热管孔(7)在翅片基体(1)宽度方向位于对称线上,所述双向离散凸起高强度换热翅片为对称翅片,所述翅片基体(1)的长边两侧设置有折边结构(2),所述凸起结构一(3)的高度为0.5~1.0mm,底面为直角梯形,底边长度为1.5~2.5mm,底面的高为1.5~3.0mm,底角为60~70°;所述凸起结构二(4)的高度为0.5~1.0mm,底面的内半径为5.6mm,外半径为7.0~8.0mm,凸起的两个弧面与翅片表面的夹角均为45~60°,其余两个侧面与翅片表面的夹角为30~45°;所述凸起结构三(5)的高度为0.5~1.0mm,底面为等腰梯形,顶边长度为1.5~3.0mm,底边长度为2.5~4.0mm,底面的高为2.5~3.5mm,靠近和远离翅片边缘的两侧面与翅片表面的夹角均为30~45°,其余两个侧面与翅片表面的夹角为45~60°;所述凸起结构四(6)的高度为0.5~1.0mm,两个弧面与翅片表面的夹角为45~60°,其余两个侧面与翅片表面的夹角为30~45°,沿片宽方向底面的长度为2.5~4.0mm,底面弧线的半径为8.5~9.5mm,所述凸起结构一(3)和凸起结构四(6)的凸起方向相同,且均与凸起结构二(4)和凸起结构三(5)的凸起方向相反,关于同一换热管孔(7)中心对称的各段凸起结构一(3)和凸起结构二(4)位于同一圆周上,所述凸起结构四(6)布置在相邻换热管孔(7)的连线上,凸起结构三(5)为多个,沿相邻换热管孔(7)的连线对称布置,所述凸起结构三(5)和凸起结构四(6)均位于所述圆周之外。1. A high-strength heat exchange fin using two-way discrete protrusions, comprising a fin base (1), and a heat exchange tube hole (7) for the heat exchange tube to pass through on the fin base (1). The fin base (1) is provided with a bidirectional discrete convex structure surrounding the heat exchange tube hole (7), characterized in that: the bidirectional discrete convex structure includes several sections of protrusions symmetrical about the center of the heat exchange tube hole (7). Structure one (3) and convex structure two (4), as well as convex structure three (5) and convex structure four (6) located between adjacent heat exchange tube holes (7), wherein convex structure one (3) The second raised structure (4), the third raised structure (5), and the fourth raised structure (6) are all located on the fin base (1) and are not connected to each other, and the fin base (1) is Straight structure, the heat exchange tube holes (7) are located on a symmetrical line in the width direction of the fin base (1), the bidirectionally discrete raised high-strength heat exchange fins are symmetrical fins, and the fin base (1) A folding structure (2) is arranged on both sides of the long side, the height of the raised structure one (3) is 0.5-1.0mm, the bottom is a right-angled trapezoid, the length of the bottom is 1.5-2.5mm, and the height of the bottom is 1.5 mm. ~3.0mm, the bottom angle is 60~70°; the height of the second raised structure (4) is 0.5~1.0mm, the inner radius of the bottom surface is 5.6mm, the outer radius is 7.0~8.0mm, the two raised The angle between the arc surface and the surface of the fin is 45-60°, and the angle between the other two side surfaces and the surface of the fin is 30-45°; the height of the raised structure three (5) is 0.5-1.0mm, The bottom surface is an isosceles trapezoid, the length of the top side is 1.5~3.0mm, the length of the bottom side is 2.5~4.0mm, and the height of the bottom surface is 2.5~3.5mm. The angle between the other two sides and the surface of the fin is 45-60°; the height of the raised structure four (6) is 0.5-1.0mm, and the two arc surfaces and the surface of the fin are clamped. The angle is 45-60°, the angle between the other two sides and the surface of the fin is 30-45°, the length of the bottom surface along the width direction of the fin is 2.5-4.0mm, and the radius of the arc of the bottom surface is 8.5-9.5mm. The convex structure one (3) and the convex structure four (6) have the same convex direction, and are opposite to the convex structure two (4) and the convex structure three (5) in the opposite direction. For the same heat exchange tube The convex structure one (3) and convex structure two (4) of each section with symmetrical center of the hole (7) are located on the same circumference, and the convex structure four (6) are arranged on the adjacent heat exchange tube holes (7). On the connection line, there are a plurality of raised structures three (5), which are symmetrically arranged along the connection line of the adjacent heat exchange tube holes (7), and the raised structures three (5) and the raised structures four (6) are both located in the connecting line. outside the circumference. 2.根据权利要求1所述采用双向离散凸起的高强度换热翅片,其特征在于,所述翅片基体(1)厚度为0.09~0.11mm,宽度为18.19~21.65mm;相邻翅片基体(1)的间距为1.3~1.6mm;所述换热管的管径为7mm或7.94mm;相邻换热管孔(7)的孔距为21~23mm。2 . The high-strength heat exchange fin using bidirectional discrete protrusions according to claim 1 , wherein the fin base body ( 1 ) has a thickness of 0.09-0.11 mm and a width of 18.19-21.65 mm; adjacent fins The spacing between the sheet bases (1) is 1.3-1.6 mm; the diameter of the heat exchange tubes is 7 mm or 7.94 mm; the hole spacing between adjacent heat-exchanging tube holes (7) is 21-23 mm.
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