CN211178099U - Strip seam-curved surface vortex generator combined type reinforced fin - Google Patents
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Abstract
本实用新型是一种条缝‑曲面涡产生器组合式强化翅片,翅片上布置有套装圆管的圆孔,圆孔上游周向冲压出若干条缝,圆孔下游两侧冲压出一对曲面三角形涡产生器,翅片在管翅式换热器上的间距通过翻边凸台确定。通过在圆管上游周向布置条缝,使得圆管与条缝之间形成流动通道,能对来流起到引流作用,减小了流体流动阻力损失,圆管下游的曲面三角形涡产生器能引导流体流经圆管尾部,有效抑制了流体与管壁的分离,减小了尾流区域的流动阻力损失,另一方面,圆管周向布置的条缝和曲面三角形涡产生器既破坏了边界层的形成和发展,减薄了边界层的厚度,还能诱导出强烈的二次流动,进一步加强冷热流体的混合,有利于强化传热。
The utility model relates to a slot-curved vortex generator combined reinforced fin. The fin is provided with a circular hole for enveloping a circular tube, a plurality of slits are punched out in the circumferential direction at the upstream of the circular hole, and a pair of slots are punched out on both sides of the downstream of the circular hole. For the curved triangular vortex generator, the spacing of the fins on the tube-fin heat exchanger is determined by the flanged bosses. By arranging the slits in the circumferential direction upstream of the circular pipe, a flow channel is formed between the circular pipe and the slits, which can divert the incoming flow and reduce the loss of fluid flow resistance. The curved triangular vortex generator downstream of the circular pipe can It guides the fluid to flow through the tail of the circular tube, which effectively inhibits the separation of the fluid from the tube wall and reduces the flow resistance loss in the wake area. The formation and development of the boundary layer reduces the thickness of the boundary layer and induces a strong secondary flow, which further strengthens the mixing of hot and cold fluids, which is conducive to strengthening heat transfer.
Description
技术领域technical field
本发明涉及换热器技术领域,具体说是一种条缝-曲面涡产生器组合式强化翅片。The invention relates to the technical field of heat exchangers, in particular to a slot-curved vortex generator combined reinforced fin.
背景技术Background technique
管翅式换热器被广泛应用到化工、制冷、空调等领域。该类换热器管外介质大多为空气,以致翅片侧换热系数低,热阻大,极大的影响了换热器的换热效率。为了进一步提高空气侧换热性能,研究人员采取了增大翅片几何尺寸、增强流体扰动强度等措施,但受经济性的限制使得翅片的几何尺寸增大空间有限,因此更多的采用百叶窗式、条缝式和间断环面槽等间断或破口结构以增强流体扰动强度,进而改变翅片管束通道中流体的流动特性。Tube-fin heat exchangers are widely used in chemical, refrigeration, air conditioning and other fields. Most of the medium outside the tube of this type of heat exchanger is air, so that the heat transfer coefficient of the fin side is low and the thermal resistance is large, which greatly affects the heat exchange efficiency of the heat exchanger. In order to further improve the heat transfer performance of the air side, researchers have taken measures such as increasing the geometric size of the fins and enhancing the fluid disturbance intensity. However, due to economic constraints, the space for increasing the geometric size of the fins is limited, so more shutters are used. The discontinuous or broken structures such as type, slot type and discontinuous annular groove can enhance the strength of fluid disturbance, thereby changing the flow characteristics of the fluid in the channel of the finned tube bundle.
翅片开缝是一种有效强化空气侧传热的方法,其强化传热机理是开缝的存在改善了平直翅片中流场和温度场的协同性。一般开缝翅片缝的位置接近“X”形,“X”形开缝翅片可以使流体边界层间断发展,但流体流经圆管尾流区域时阻力损失较大,采取在圆管尾流区布置一对曲面三角形涡产生器能引导更多的流体流经圆管尾部,有效抑制了流体与管壁的分离,减小了尾流区域的流动阻力损失,另一方面,曲面三角形涡产生器还能诱导出强烈的二次流动,进一步加强冷热流体的混合,有利于强化传热,可以实现强化传热和减小阻力损失的双重作用。Slitting of fins is an effective method to enhance heat transfer on the air side. The mechanism of heat transfer enhancement is that the existence of slits improves the synergy of flow field and temperature field in flat fins. Generally, the position of the slotted fins is close to the "X" shape. The "X"-shaped slotted fins can make the fluid boundary layer develop intermittently, but the resistance loss is large when the fluid flows through the wake region of the circular tube. The arrangement of a pair of curved triangular vortex generators in the flow area can guide more fluid to flow through the tail of the circular tube, effectively inhibiting the separation of the fluid from the tube wall and reducing the flow resistance loss in the wake region. On the other hand, the curved triangular vortex The generator can also induce a strong secondary flow, which further strengthens the mixing of cold and hot fluids, which is conducive to strengthening heat transfer, and can achieve the dual effects of strengthening heat transfer and reducing resistance loss.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题是为了进一步改善圆管管翅式换热器的换热性能,提供一种能减小流体流经圆管尾流区域的阻力损失,并在不断破坏边界层的形成和发展的同时诱导产生二次流动以加强冷热流体的混合的一种条缝-曲面涡产生器组合式强化翅片。The technical problem to be solved by the present invention is to further improve the heat exchange performance of the circular tube, tube and fin heat exchanger, to provide a method that can reduce the resistance loss of fluid flowing through the wake region of the circular tube, and continuously destroy the formation of the boundary layer. A slot-curved vortex generator combined reinforced fin that induces secondary flow to enhance the mixing of hot and cold fluids while developing and developing.
本发明采用下述技术方案解决其技术问题:提供一种条缝-曲面涡产生器组合式强化翅片,包括翅片、平行四边形条缝、矩形条缝、曲面三角形涡产生器、等腰梯形条缝和翻边凸台,所述翅片上开有若干套装圆管的圆孔,错排或者顺排布置的圆孔周围布置有平行四边形条缝、矩形条缝、曲面三角形涡产生器、等腰梯形条缝和翻边凸台。The present invention solves its technical problems by adopting the following technical solutions: providing a combined reinforced fin with a slit-curved vortex generator, including a fin, a parallelogram slit, a rectangular slit, a curved triangular vortex generator, an isosceles trapezoid Slots and flanging bosses, the fins are provided with a number of circular holes for fitting round tubes, and parallelogram slits, rectangular slits, curved triangular vortex generators, etc. are arranged around the circular holes arranged in staggered or sequential rows. Trapezoidal seam and cuff boss at waist.
所述翅片上每两个圆孔中心上游冲压出若干平行四边形条缝和若干矩形条缝,平行四边形条缝和矩形条缝在圆孔一侧的边线与圆孔同圆心的圆弧相切,平行四边形条缝和矩形条缝在圆孔两侧对称分布。A number of parallelogram slits and a number of rectangular slits are punched out in the upstream of the center of each two circular holes on the fin, and the edge of the parallelogram slits and the rectangular slits on one side of the circular hole is tangent to the circular arc concentric with the circular hole, Parallelogram slits and rectangular slits are symmetrically distributed on both sides of the circular hole.
所述翅片在每个圆孔中心下游两侧冲压出一对曲面三角形涡产生器,并在翅片上留下一对曲边三角形孔,所述曲面三角形涡产生器的圆弧所在圆心与圆孔的圆心重合。The fins punch out a pair of curved triangular vortex generators on the downstream sides of the center of each circular hole, and leave a pair of curved triangular holes on the fins. The centers of the holes coincide.
所述翅片在每两个圆孔中心下游冲压出1~2个等腰梯形条缝,所述等腰梯形条缝的腰所在边线与以圆孔同圆心的圆弧相切。One to two isosceles trapezoid slits are punched out of the fin at the downstream of the center of each two circular holes, and the side line where the waist of the isosceles trapezoidal slit is located is tangent to the arc concentric with the circular holes.
所述翅片上套装圆管的圆孔上设有翻边凸台,翻边凸台的高度等于翅片安装在管翅式换热器后翅片之间的间距。The fins are provided with flanging bosses on the circular holes of the round tubes sleeved on the fins, and the height of the flanging bosses is equal to the spacing between the fins after the fins are installed in the tube-fin heat exchanger.
本发明在圆孔上游周向布置条缝,条缝可以使流体流动边界层间断发展,同时形成间断发展的热边界层来强化传热,在圆管尾流区布置一对曲面三角形涡产生器能引导更多的流体流经圆管尾部,有效抑制了流体与管壁的分离,减小了尾流区域的流动阻力损失,另一方面,条缝和曲面三角形涡产生器还能诱导出强烈的二次流动,进一步加强冷热流体的混合,有利于强化传热,可以实现强化传热和减小阻力损失的双重作用。The invention arranges slits in the circumferential direction upstream of the circular hole, the slits can make the fluid flow boundary layer develop intermittently, and at the same time form a thermal boundary layer with discontinuous development to strengthen heat transfer, and a pair of curved triangular vortex generators are arranged in the wake region of the circular tube It can guide more fluid to flow through the tail of the round tube, effectively suppress the separation of the fluid and the tube wall, and reduce the flow resistance loss in the wake region. On the other hand, the slit and curved triangular vortex generators can also induce strong The secondary flow can further strengthen the mixing of cold and hot fluids, which is conducive to strengthening heat transfer, and can achieve the dual effects of strengthening heat transfer and reducing resistance loss.
附图说明Description of drawings
图1为本发明三维结构示意图;Fig. 1 is the three-dimensional structure schematic diagram of the present invention;
图2为本发明二维结构示意图;2 is a schematic diagram of a two-dimensional structure of the present invention;
图3为图2的A-A局部放大图;Fig. 3 is a partial enlarged view of A-A of Fig. 2;
图4为图2的B-B局部放大图;Fig. 4 is a partial enlarged view of B-B of Fig. 2;
图5为案例计算的流体流动阻力系数f与雷诺数Re的关系。Figure 5 shows the relationship between the fluid flow resistance coefficient f and the Reynolds number Re calculated for the case.
图6为案例计算的强化传热因子JF与雷诺数Re的关系。Figure 6 shows the relationship between the enhanced heat transfer factor JF and the Reynolds number Re calculated for the case.
具体实施方式Detailed ways
为了说明本实用新型的目的及优点,结合以下数值计算实例对本实用新型做进一步说明。应当理解,此处所描述的具体实例仅仅用以解释本实用新型,并不用于限定本实用新型。In order to illustrate the purpose and advantages of the present utility model, the present utility model will be further described in conjunction with the following numerical calculation examples. It should be understood that the specific examples described herein are only used to explain the present invention, and are not intended to limit the present invention.
选取的计算域主要参数为:翅片管的纵向管间距S1=13.64mm,横向管间距S2=21mm,肋片间距为1.34mm,肋片厚度为0.11mm,净翅片间距Tp=1.24mm,圆管外径D=7.61mm,圆管厚度δt=0.21mm,条缝宽度W=1.26mm,条缝净高度为0.93mm,条缝间距S=1.07mm,条缝所在圆弧与圆管直径比为1.55,条缝倾角为α=35°,曲面三角形涡产生器的高度是 H=1.05mm,弧长L=4.21mm,厚度δ=0.11mm。The main parameters of the selected computational domain are: longitudinal tube spacing S 1 =13.64mm, transverse tube spacing S 2 =21mm, fin spacing 1.34mm, fin thickness 0.11mm, net fin spacing T p = 1.24mm, the outer diameter of the round tube D = 7.61mm, the thickness of the round tube δ t = 0.21mm, the width of the slot W = 1.26mm, the net height of the slot is 0.93mm, the slot spacing S = 1.07mm, the arc where the slot is located The ratio to the diameter of the circular tube is 1.55, the inclination angle of the slit is α=35°, the height of the curved triangular vortex generator is H=1.05mm, the arc length L=4.21mm, and the thickness δ=0.11mm.
结合图1至图4,本发明提供一种条缝-曲面涡产生器组合式强化翅片,包括翅片1、平行四边形条缝(3、4)、矩形条缝5、曲面三角形涡产生器6、等腰梯形条缝7和翻边凸台 8。所述翅片1上开有若干套装圆管的圆孔2,根据换热管布置圆孔2的位置和数量,圆孔2 上设有翻边凸台8,所述翻边凸台8用于固定翅片1安装在管翅式换热器后翅片之间的间距。在圆孔2的一周冲压有平行四边形条缝(3、4)和矩形条缝5,平行四边形条缝(3、4)和矩形条缝5在圆孔一侧的边线与以圆孔2同圆心的圆弧相切,平行四边形条缝(3、4)和矩形条缝5 在圆孔2两侧对称分布。在每个圆孔2中心下游两侧冲压出一对曲面三角形涡产生器6,并在翅片1上留下一对曲边三角形孔9,曲面三角形涡产生器6的圆弧所在圆心与圆孔2的圆心重合。在每两个圆孔2中心下游冲压出1~2个等腰梯形条缝7,所述等腰梯形条缝7的腰所在边线与以圆孔2同圆心的圆弧相切。1 to 4, the present invention provides a slot-curved vortex generator combined reinforced fin, including
在雷诺数Re为250~1600的范围内对条缝-曲面涡产生器组合式强化翅片管内流体流动与传热进行了数值模拟,并与普通“X”形条缝翅片管的计算结果进行了对比,对比结果如图5、6所示。In the range of Reynolds number Re from 250 to 1600, the numerical simulation of fluid flow and heat transfer in the slot-curved vortex generator combined enhanced finned tube was carried out, and the results were compared with the calculation results of the ordinary "X"-shaped slotted finned tube. The comparison was carried out, and the comparison results are shown in Figures 5 and 6.
图5所示为翅片管束通道中的流动阻力系数f与雷诺数Re的关系,从图中可以明显看出,条缝-曲面涡产生器组合式强化翅片的流体流动阻力小于普通条缝翅片,说明圆管后置一对曲面三角形涡产生器能有效抑制流体与管壁的分离,减小尾流区域的流动阻力损失。Figure 5 shows the relationship between the flow resistance coefficient f and the Reynolds number Re in the channel of the finned tube bundle. It can be clearly seen from the figure that the fluid flow resistance of the slot-curved vortex generator combined reinforced fin is smaller than that of the ordinary slot. The fins indicate that a pair of curved triangular vortex generators behind the circular tube can effectively inhibit the separation of the fluid from the tube wall and reduce the flow resistance loss in the wake region.
图6所示为翅片管束通道中的强化传热因子JF与雷诺数Re的关系,强化传热因子JF的定义式为JF=(Nu/Nuref)/(f/fref)1/3,其中Nuref和fref分别为普通“X”形条缝翅片管的努塞尔数和阻力系数,从图中可以看出,条缝-曲面涡产生器组合式强化翅片在Re为250~1600 的范围内强化传热因子均大于1,说明其综合强化传热效果较好。Figure 6 shows the relationship between the enhanced heat transfer factor JF and the Reynolds number Re in the channel of the finned tube bundle. The definition formula of the enhanced heat transfer factor JF is JF=(Nu/Nu ref )/(f/f ref ) 1/3 , where Nu ref and f ref are the Nusselt number and drag coefficient of the ordinary "X"-shaped slotted fin tube, respectively. It can be seen from the figure that the slot-curved vortex generator combined reinforced fin has a Re of In the range of 250-1600, the enhanced heat transfer factors are all greater than 1, indicating that the comprehensive heat transfer enhancement effect is better.
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