CN102200405A - Combined triangular curved vortex generator type circular tube fin heat exchanger - Google Patents
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Abstract
本发明提供一种组合式三角形曲面涡产生器式圆管管翅换热器,包括沿着气体流动方向排列的圆管和套在圆管上的翅片,其特征在于所述翅片上设有套装圆管的孔,每个孔前方向上冲压出一个椭圆凸包,椭圆长轴方向沿着主流方向,在翅片背面留下一横向椭圆凹坑;所述翅片上每个孔后部冲压出一对圆弧状三角形曲面涡产生器,同时在翅片上留下一对圆弧状小孔,曲面涡产生器与翅片相连的底边与圆孔位于同心圆上。本发明在翅片上冲压形成的位于圆管前端的椭圆凸包的长轴与流动方向一致,流线性较好,抑制了圆管后侧流体分离,使得圆管后尾流区域减小,改善了翅片与尾流区域相接面上的换热性能,减小了尾流区域的流动阻力损失。
The invention provides a combined triangular curved surface vortex generator type circular tube-fin heat exchanger, which includes circular tubes arranged along the gas flow direction and fins sleeved on the circular tubes, and is characterized in that the fins are provided with For the hole of the round tube, an elliptical convex hull is punched out in front of each hole, and the long axis of the ellipse is along the main flow direction, leaving a transverse elliptical pit on the back of the fin; the back of each hole on the fin is punched out A pair of arc-shaped triangular curved surface vortex generators leave a pair of arc-shaped small holes on the fins, and the bottom edge of the curved surface vortex generators connected to the fins and the circular holes are located on concentric circles. In the present invention, the long axis of the elliptical convex hull at the front end of the round tube formed by stamping on the fins is consistent with the flow direction, and the streamline is better, which suppresses the separation of the fluid at the rear side of the round tube, reduces the wake area behind the round tube, and improves the The heat transfer performance on the joint surface of the fin and the wake region reduces the flow resistance loss in the wake region.
Description
技术领域technical field
本发明涉及换热器技术领域,具体说是一种组合式三角形曲面涡产生器式圆管管翅换热器。The invention relates to the technical field of heat exchangers, in particular to a combined triangular curved surface vortex generator type round tube fin heat exchanger.
背景技术Background technique
圆管管翅换热器的用途非常广泛。随着国民经济生产水平的不断进步和节能减排的要求,圆管管翅换热器的强化传热非常重要。研究者致力于增强圆管管翅换热器换热能力,同时尽可能减少阻力损失的增加,也就是降低圆管管翅换热器的运行费用。通常在管外侧安装翅片以增加换热面积减小热阻,但受到经济性和翅片效率的限制使得翅片的面积不能无限的增加。为了进一步提高圆管管翅换热器传热性能,把翅片表面做成各种各样的结构。其中引入二次流的措施被称为第三代强化传热技术。在翅片表面冲压出的涡产生器在主流中可造成二次流动,能有效地强化翅片表面的换热性能。Round tube fin heat exchangers are very versatile. With the continuous improvement of the production level of the national economy and the requirements of energy saving and emission reduction, it is very important to enhance the heat transfer of the round tube fin heat exchanger. Researchers are committed to enhancing the heat transfer capacity of the tube-fin heat exchanger while reducing the increase in resistance loss as much as possible, that is, reducing the operating cost of the tube-fin heat exchanger. Fins are usually installed on the outside of the tube to increase the heat transfer area and reduce thermal resistance, but the area of the fins cannot be increased indefinitely due to the limitation of economy and fin efficiency. In order to further improve the heat transfer performance of the round tube fin heat exchanger, the fin surface is made into various structures. Among them, the measure of introducing secondary flow is called the third generation enhanced heat transfer technology. The vortex generator punched out on the surface of the fin can cause secondary flow in the main flow, which can effectively enhance the heat transfer performance of the surface of the fin.
圆管管翅换热器的机械加工性能比扁管翅换热器好,制造能耗小。但是流体流经圆管的流线性比流经扁管的流线性差,流体流经圆管前端滞止点附近和流经圆管尾流区域时阻力损失较大,且翅片表面换热能力较差的区域是在与圆管尾流区域相接触的区域。The mechanical processing performance of the round tube fin heat exchanger is better than that of the flat tube fin heat exchanger, and the manufacturing energy consumption is small. However, the flow linearity of the fluid flowing through the circular tube is worse than that of the flat tube, and the resistance loss is large when the fluid flows near the stagnation point at the front end of the circular tube and the wake area of the circular tube, and the heat transfer capacity of the fin surface The poorer area is the area in contact with the wake area of the tube.
发明内容Contents of the invention
本着进一步提高圆管管翅片型的换热性能,同时减小流动阻力损失的目的,本发明涉及减小圆管尾流区域大小的一三角形曲面涡产生器和减小上游圆管前端附近流动阻力损失的在翅片上冲压形成的椭圆凸包。本发明提供一种能减小圆管前端附近流动阻力损失,增强换热性能的组合式曲面涡产生器式圆管管翅换热器。In order to further improve the heat transfer performance of the round tube fin type and reduce the loss of flow resistance, the present invention relates to a triangular curved surface vortex generator that reduces the size of the wake region of the round tube and reduces the size of the upstream round tube near the front end. Elliptical convex hull stamped on fins for flow resistance loss. The invention provides a combined curved surface vortex generator type round tube fin heat exchanger which can reduce the flow resistance loss near the front end of the round tube and enhance the heat exchange performance.
本发明采用下述技术方案解决其技术问题:The present invention adopts following technical scheme to solve its technical problem:
一种组合式三角形曲面涡产生器式圆管管翅换热器,包括沿着气体流动方向排列的圆管和套在圆管上的翅片,其特征在于所述翅片上设有套装圆管的孔,每个孔前方向上冲压出一个椭圆凸包,椭圆长轴方向沿着主流方向,在翅片背面留下一横向椭圆凹坑;所述翅片上每个孔后部冲压出一对圆弧状三角形曲面涡产生器, 同时在翅片上留下一对圆弧状小孔,曲面涡产生器与翅片相连的底边与圆孔位于同心圆上。A combined triangular curved surface vortex generator type round tube fin heat exchanger, including round tubes arranged along the gas flow direction and fins sleeved on the round tubes, characterized in that the fins are equipped with sleeved round tubes punch out an elliptical convex hull in the front direction of each hole, and the long axis direction of the ellipse is along the main flow direction, leaving a transverse elliptical pit on the back of the fin; a pair of circles are punched out in the rear of each hole The arc-shaped triangular curved surface vortex generator leaves a pair of arc-shaped small holes on the fins, and the bottom edge of the curved surface vortex generator connected to the fins and the circular holes are located on the concentric circle.
所述涡产生器与圆管的纵向中心线上下对称分布,涡产生器底边中点位于以孔为同心的圆弧上,且圆弧的半径与孔的半径之比为r 1/r=1.15~1.35,圆弧角的范围为θ=50°~60°,所述涡产生器底边起始点与孔中心的连线和来流方向的角β=90°~115° 。The vortex generator is symmetrically distributed up and down with the longitudinal center line of the circular tube, the midpoint of the bottom edge of the vortex generator is located on the circular arc concentric with the hole, and the ratio of the radius of the circular arc to the radius of the hole is r1 / r = 1.15~1.35, the range of the arc angle is θ =50°~60°, the angle between the starting point of the bottom edge of the vortex generator and the center of the hole and the incoming flow direction is β=90°~115°.
所述三角形曲面涡产生器与底边垂直的边位于前端,且垂直于翅片。The side perpendicular to the base of the triangular curved surface vortex generator is located at the front end and is perpendicular to the fins.
所述曲面涡产生器与底边垂直的边的高度为翅片间距的0.6~0.95倍。The height of the side perpendicular to the bottom side of the curved vortex generator is 0.6-0.95 times the pitch of the fins.
所述椭圆凸包的长轴与流动方向一致,椭圆凸包的中心在孔的纵向中心线上,并且位于以孔为同心的圆弧上,且圆弧的半径与孔的半径之比为r 2/r=1.3~1.6;所述椭圆凸包在翅片上的投影为一椭圆,长轴和短轴之比为2,长轴为圆管外径的0.3~0.4倍,椭圆凸包高度为翅片间距的0.5~0.8倍。The major axis of the elliptical convex hull is consistent with the flow direction, the center of the elliptical convex hull is on the longitudinal centerline of the hole, and is located on an arc concentric with the hole, and the ratio of the radius of the arc to the radius of the hole is r 2 / r = 1.3~1.6; the projection of the elliptical convex hull on the fin is an ellipse, the ratio of the major axis to the minor axis is 2, the major axis is 0.3~0.4 times the outer diameter of the circular tube, and the height of the elliptical convex hull is 0.5~0.8 times of the fin pitch.
所述翅片上孔的边缘设有翻边凸台,翻边凸台的高度等于翅片的间距。The edges of the upper holes of the fins are provided with flanging bosses whose height is equal to the distance between the fins.
本发明在翅片上冲压形成的位于圆管前端的椭圆凸包的长轴与流动方向一致,流线性较好,当流体流经凸包时,流体改变流动方向沿着凸包流动,这样在圆管前部就减小了因流体直接垂直冲刷圆管而引起的流动阻力损失。在圆管中线下游两侧冲压的三角形曲面涡产生器使得在圆管与涡产生器之间形成一流体通道,部分流体经该通道到达圆管尾流区,抑制了圆管后侧流体分离,使得圆管后尾流区域减小,改善了翅片与尾流区域相接面上的换热性能,且减小了尾流区域的流动阻力损失。涡产生器和凸台冲压在同一个方向,冲压模具制造比较简单。In the present invention, the long axis of the elliptical convex hull at the front end of the circular tube formed by stamping on the fins is consistent with the flow direction, and the flow is relatively good. The front of the tube reduces the flow resistance loss caused by the fluid directly scouring the round tube vertically. The triangular curved vortex generators stamped on both sides of the downstream of the center line of the circular tube form a fluid channel between the circular tube and the vortex generator, and part of the fluid reaches the wake area of the circular tube through this channel, which inhibits the separation of the fluid at the back of the circular tube. The wake area behind the circular tube is reduced, the heat transfer performance on the joint surface of the fin and the wake area is improved, and the flow resistance loss in the wake area is reduced. The vortex generator and the boss are stamped in the same direction, and the stamping die is relatively simple to manufacture.
附图说明Description of drawings
图1为本发明结构示意图;Fig. 1 is a structural representation of the present invention;
图2为翅片结构示意图。Figure 2 is a schematic diagram of the fin structure.
具体实施方式Detailed ways
下面结合附图对本发明做进一步详细说明:Below in conjunction with accompanying drawing, the present invention is described in further detail:
一种组合式三角形曲面涡产生器式圆管管翅换热器,包括沿着气体流动方向排列的圆管3和套在圆管3上的翅片4,圆管可以是叉排或顺排排列方式,翅片4上每个孔8后部冲压出一对三角形曲面涡产生器1,并在翅片4上留下一对三角形小孔5。涡产生器底边中点位于以孔8为同心的圆弧上,三角形曲面涡产生器1与底边垂直的边位于前端,且垂直于翅片4。涡产生器1与圆管3的纵向中心线上下对称分布,涡产生器底边中点位于以孔8为同心的圆弧上,且圆弧的半径与孔8的半径之比为r 1/r=1.15~1.35,圆弧角的范围为θ=50°~60°,涡产生器1底边起始点与孔8中心的连线和来流方向的角β=90°~115° 。A combined triangular curved surface vortex generator type circular tube-fin heat exchanger, including circular tubes 3 arranged along the direction of gas flow and fins 4 sleeved on the circular tubes 3, the circular tubes can be arranged in a fork row or in a straight row In the arrangement, a pair of triangular curved surface vortex generators 1 are punched out at the rear of each hole 8 on the fin 4 , and a pair of triangular small holes 5 are left on the fin 4 . The midpoint of the bottom edge of the vortex generator is located on the concentric circular arc with the hole 8 , and the side perpendicular to the bottom edge of the triangular curved surface vortex generator 1 is located at the front end and is perpendicular to the fins 4 . The longitudinal center line of the vortex generator 1 and the circular tube 3 is distributed symmetrically up and down, the midpoint of the bottom edge of the vortex generator is located on the arc concentric with the hole 8, and the ratio of the radius of the arc to the radius of the hole 8 is r 1 / r =1.15~1.35, the range of the arc angle is θ =50°~60°, the angle between the line connecting the starting point of the base of the vortex generator 1 and the center of the hole 8 and the incoming flow direction β=90°~115°.
在翅片4上每孔8前端中线处冲出一椭圆凸包6,椭圆长轴方向沿着主流方向,在翅片4背面相应的留下一椭圆凹坑7。椭圆凸包6的长轴与流动方向一致,椭圆凸包6的中心在孔8的纵向中心线上,并且位于以孔8为同心的圆弧上,圆弧的半径与孔8的半径之比为r 2/r=1.3~1.6。椭圆凸包6在翅片4上的投影为一椭圆,长轴和段轴之比为2,长轴为0.3~0.4倍的圆管3外径,椭圆凸包6的高度为翅片4间距的0.5~0.8倍。An elliptical convex hull 6 is punched out at the midline of the front end of each hole 8 on the fin 4 , the long axis of the ellipse is along the main flow direction, and an elliptical pit 7 is correspondingly left on the back of the fin 4 . The long axis of the elliptical convex hull 6 is consistent with the flow direction, the center of the elliptical convex hull 6 is on the longitudinal centerline of the hole 8, and is located on the arc concentric with the hole 8, the ratio of the radius of the arc to the radius of the hole 8 It is r 2 / r =1.3~1.6. The projection of the elliptical convex hull 6 on the fin 4 is an ellipse, the ratio of the major axis to the segment axis is 2, the major axis is 0.3~0.4 times the outer diameter of the circular tube 3, and the height of the elliptical convex hull 6 is the distance between the fins 4 0.5~0.8 times of that.
翅片4上孔8的边缘设有翻边凸台2,翻边凸台2的高度等于翅片4的间距,翻边凸台2起到翅片定位的作用,同时圆管与管板间胀接时,翻边凸台2可以紧密的和圆管3连接在一起,提高管与翅片4的胀紧性。The edge of the hole 8 on the fin 4 is provided with a flanging boss 2. The height of the flanging boss 2 is equal to the distance between the fins 4. The flanging boss 2 plays the role of fin positioning. At the same time, the gap between the round tube and the tube sheet During the expansion joint, the flanging boss 2 can be tightly connected with the round tube 3 to improve the expansion and tightness of the tube and the fin 4 .
本发明在翅片冲压成型后,将翅片4套装在圆管3上,翅片4间通过圆孔翻边凸台2定位,通过胀管、管内试压等一系列工艺之后就完成了整个涡产生器式圆管管翅换热器的制作。In the present invention, after the fins are stamped and formed, the fins 4 are set on the round tube 3, and the fins 4 are positioned through the round hole flanging boss 2, and the whole tube is completed after a series of processes such as tube expansion and pressure test inside the tube. Fabrication of vortex generator type round tube fin heat exchanger.
Claims (6)
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Cited By (4)
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CN103256834A (en) * | 2013-02-22 | 2013-08-21 | 广东美的电器股份有限公司 | Oval tube finned type heat exchanger and upward air outlet air-conditioning outdoor unit |
CN110906778A (en) * | 2019-11-04 | 2020-03-24 | 宁波奥克斯电气股份有限公司 | Fin of heat exchanger, heat exchanger and air conditioner |
CN113758358A (en) * | 2020-06-01 | 2021-12-07 | 广东美的暖通设备有限公司 | Heat Exchangers and Air Conditioners |
CN113834129A (en) * | 2020-06-08 | 2021-12-24 | 青岛海信日立空调系统有限公司 | Air conditioner |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN103256834A (en) * | 2013-02-22 | 2013-08-21 | 广东美的电器股份有限公司 | Oval tube finned type heat exchanger and upward air outlet air-conditioning outdoor unit |
CN110906778A (en) * | 2019-11-04 | 2020-03-24 | 宁波奥克斯电气股份有限公司 | Fin of heat exchanger, heat exchanger and air conditioner |
CN113758358A (en) * | 2020-06-01 | 2021-12-07 | 广东美的暖通设备有限公司 | Heat Exchangers and Air Conditioners |
CN113758358B (en) * | 2020-06-01 | 2025-03-07 | 广东美的暖通设备有限公司 | Heat exchanger and air conditioner |
CN113834129A (en) * | 2020-06-08 | 2021-12-24 | 青岛海信日立空调系统有限公司 | Air conditioner |
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