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CN104729329B - A kind of non-homogeneous fin radiator for Heller type indirect air cooling system - Google Patents

A kind of non-homogeneous fin radiator for Heller type indirect air cooling system Download PDF

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CN104729329B
CN104729329B CN201510178536.7A CN201510178536A CN104729329B CN 104729329 B CN104729329 B CN 104729329B CN 201510178536 A CN201510178536 A CN 201510178536A CN 104729329 B CN104729329 B CN 104729329B
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radiator
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cooling system
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CN104729329A (en
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孙奉仲
李岩
赵元宾
高明
魏伟
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Shandong University
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Abstract

本发明公开了一种用于海勒式间接空冷系统的非均匀翅片散热器,所述非均匀翅片散热器沿高度方向分为顶部、中部和底部,这三个区域的高度分别为h1、h2和h3,顶部、中部和底部的散热翅片分布间距分布为d1、d2和d3;当0.02H≤h1≤0.25H,0.5H≤h2≤0.96H,0.02H≤h3≤0.25H时,1.1d≤d1≤3.5d,d2=d,1.1d≤d3≤3.5d,其中H为包含散热翅片的散热器长度,d为散热翅片均匀布置时的翅片间距。本发明优化了翅片的分布,减小了散热器底部及顶部的通风阻力,消弱了散热器背部区域的漩涡,增强了散热器的整体换热性能,同时由于翅片数目的减少,也节约了少量铝资源。

The invention discloses a non-uniform finned radiator for Heller type indirect air cooling system, said non-uniform finned radiator is divided into top, middle and bottom along the height direction, and the heights of these three regions are h1 respectively , h 2 and h 3 , the top, middle and bottom cooling fin distribution pitch distribution is d 1 , d 2 and d 3 ; when 0.02H≤h 1 ≤0.25H, 0.5H≤h 2 ≤0.96H, 0.02H ≤h 3 ≤0.25H, 1.1d≤d 1 ≤3.5d, d 2 =d, 1.1d≤d 3 ≤3.5d, where H is the length of the radiator including the cooling fins, and d is the uniform arrangement of the cooling fins fin spacing. The invention optimizes the distribution of fins, reduces the ventilation resistance at the bottom and top of the radiator, weakens the vortex in the back area of the radiator, and enhances the overall heat exchange performance of the radiator. Save a small amount of aluminum resources.

Description

一种用于海勒式间接空冷系统的非均匀翅片散热器A Non-Uniform Fin Radiator for Heller Type Indirect Air Cooling System

技术领域technical field

本发明涉及一种用于海勒式间接空冷系统的非均匀翅片散热器。The invention relates to a non-uniform fin radiator for Heller type indirect air cooling system.

背景技术Background technique

干式冷却塔或直接空冷系统与采用湿式冷却塔的火电机组相比,可节水65%-90%,这对于富煤缺水地区电力工业的可持续性发展具有重要的意义。干式冷却系统可以分为直接空冷系统和间接空冷系统(下称间冷系统),根据凝汽器的型式及散热器布置位置的不同,间冷系统又可分为海勒式、哈蒙式、SCAL型。间冷系统由于气水两相间传热为非接触式传热,故冷却极限为环境空气的干球温度,使得平均煤耗较湿冷机组煤耗高3.3%-6.2%。另外间冷系统工作性能的好坏直接影响到凝汽器的真空以及供电煤耗。数据表明:冷却塔出口水温每降低1℃,凝汽器真空变化0.4KPa,影响供电煤耗1g/kwh左右。Compared with thermal power units using wet cooling towers, dry cooling towers or direct air cooling systems can save 65%-90% of water, which is of great significance for the sustainable development of the power industry in areas rich in coal and short of water. Dry cooling system can be divided into direct air cooling system and indirect air cooling system (hereinafter referred to as intercooling system). According to the type of condenser and the arrangement position of radiator, intercooling system can be divided into Heller type and Harmon type. , SCAL type. In the intercooling system, since the heat transfer between the gas and water phases is non-contact heat transfer, the cooling limit is the dry bulb temperature of the ambient air, making the average coal consumption 3.3%-6.2% higher than that of the wet cooling unit. In addition, the working performance of the intercooling system directly affects the vacuum of the condenser and the coal consumption of power supply. The data shows that every time the water temperature at the outlet of the cooling tower decreases by 1°C, the vacuum of the condenser changes by 0.4KPa, which affects the coal consumption of power supply by about 1g/kwh.

海勒式间冷系统的核心部件为喷射式凝汽器、间冷塔及塔外垂直布置的福哥型铝管铝翅片散热器,该类型散热器也称为匈牙利福哥(Forgo)型散热器,由管片式翅片管束组成,结构为全铝制的圆形管外套大翅片,水侧流程为双流程,目前应用于工程实际的主要型式有第五代海勒-福哥(Heller-Forgo)T60型6排管和第六代福哥型4排管。The core components of the Heller-type intercooling system are jet condensers, intercooling towers, and Fogo-type aluminum tube and aluminum-fin radiators arranged vertically outside the tower. This type of radiator is also known as the Hungarian Forgo type. The radiator is composed of tube-finned tube bundles. The structure is an all-aluminum circular tube with large fins. The water side flow is a double flow. The main type currently used in engineering practice is the fifth-generation Heller-Fogger (Heller-Forgo) T60 type 6-row pipe and the sixth generation Fogo type 4-row pipe.

空气流经散热器区域是一个吸热升温的过程,这种翅片均匀布置的福哥型散热器在实际运行过程中,对于散热器底部及顶部区域,局部换热面积与中部区域相同,然而由于地面及顶部封板的影响,使得空气流速较低,势必造成该区域局部换热能力低于散热器中部区域,基于冷却塔最优空气动力场理论,各处空气动力场、温度场及气水两相间的传热驱动力越均衡,整体换热能力越强,因此翅片均匀布置的散热器空气动力场与局部换热面积并不是最佳的匹配关系;同时由于沿高度方向空气流速的不同,在散热器背面容易出现纵向漩涡,产生局部阻力,不利于空气的流通,整体上并不利于散热器的散热,导致空冷塔的冷却效率降低。Air flowing through the radiator area is a heat-absorbing and heating-up process. During the actual operation of the Fogo radiator with evenly arranged fins, the local heat exchange area is the same as that in the middle area for the bottom and top areas of the radiator. However, Due to the influence of the ground and top sealing plates, the air flow rate is low, which will inevitably cause the local heat transfer capacity in this area to be lower than that in the middle of the radiator. Based on the optimal aerodynamic field theory of cooling towers, the aerodynamic field, temperature field and gas The more balanced the heat transfer driving force between the two phases of water, the stronger the overall heat transfer capacity. Therefore, the aerodynamic field of the radiator with evenly arranged fins is not the best matching relationship with the local heat transfer area; Different, vertical vortexes are prone to appear on the back of the radiator, resulting in local resistance, which is not conducive to the circulation of air, and is not conducive to the heat dissipation of the radiator as a whole, resulting in a decrease in the cooling efficiency of the air cooling tower.

发明内容Contents of the invention

为了解决现有技术的缺点,本发明提供一种用于海勒式间接空冷系统的非均匀翅片散热器。In order to solve the disadvantages of the prior art, the present invention provides a non-uniform fin radiator for Heller type indirect air cooling system.

本发明采用以下技术方案:The present invention adopts following technical scheme:

一种用于海勒式间接空冷系统的非均匀翅片散热器,包括若干冷却元件,所述冷却元件包括四个并联的冷却管束,并联的冷却管束两端设有管板,所述管板固定在连接板上;所述冷却管束,包括圆管、散热翅片及加强板,所述散热翅片和加强板上均设有预留孔,所述圆管穿过散热翅片及加强板的预留孔;若干所述冷却元件串联在一起固定在连接板上构成冷却柱;所述冷却柱的顶部设有顶部水室,冷却柱的底部设有底部水室;所述管板用螺栓与连接板固定。所述散热翅片为铝质散热翅片,散热翅片由冲压法成型。所述圆管与散热翅片及加强板采用胀接方法固定。所述圆管为包括铝管。所述加强板的材质为铝合金。所述加强板的外形似工字钢。A non-uniform fin radiator for Heller-type indirect air-cooling systems, including several cooling elements, the cooling elements include four parallel cooling tube bundles, tube sheets are arranged at both ends of the parallel cooling tube bundles, and the tube sheets are fixed On the connecting plate; the cooling tube bundle includes circular tubes, heat dissipation fins and reinforcement plates, and the heat dissipation fins and reinforcement plates are provided with reserved holes, and the circular tubes pass through the heat dissipation fins and reinforcement plates reserved holes; several cooling elements are connected in series and fixed on the connection plate to form a cooling column; the top of the cooling column is provided with a top water chamber, and the bottom of the cooling column is provided with a bottom water chamber; the tube plate is connected with bolts The connecting plate is fixed. The heat dissipation fins are aluminum heat dissipation fins, and the heat dissipation fins are formed by stamping. The circular tube, the cooling fins and the reinforcing plate are fixed by means of expansion joints. The round tube includes an aluminum tube. The material of the reinforcing plate is aluminum alloy. The shape of the reinforcing plate is like an I-beam.

本发明的非均匀翅片散热器沿高度方向分为顶部、中部和底部三个区域,所述顶部、中部和底部的高度分别为h1、h2和h3,所述顶部、中部和底部三个区域的散热翅片分布间距分布为d1、d2和d3;当0.02H≤h1≤0.25H,0.5H≤h2≤0.96H,0.02H≤h3≤0.25H时,1.1d≤d1≤3.5d,d2=d,1.1d≤d3≤3.5d,其中,H为包含散热翅片的散热器长度,d为散热翅片均匀布置时的翅片间距。The non-uniform fin radiator of the present invention is divided into three regions along the height direction: top, middle and bottom, the heights of the top, middle and bottom are h 1 , h 2 and h 3 respectively, and the top, middle and bottom The distribution spacing of the heat dissipation fins in the three areas is d 1 , d 2 and d 3 ; when 0.02H≤h 1 ≤0.25H, 0.5H≤h 2 ≤0.96H, 0.02H≤h 3 ≤0.25H, 1.1 d≤d 1 ≤3.5d, d 2 =d, 1.1d≤d 3 ≤3.5d, wherein, H is the length of the radiator including the cooling fins, and d is the fin spacing when the cooling fins are evenly arranged.

当非均匀翅片散热器的顶部、中部和底部的高度满足:0.02H≤h1=h3≤0.25H,且0.5H≤h2≤0.96H时,1.1d≤d1=d3≤3.5d,d2=d。When the heights of the top, middle and bottom of the non-uniform fin radiator meet: 0.02H≤h 1 =h 3 ≤0.25H, and 0.5H≤h 2 ≤0.96H, 1.1d≤d 1 =d 3 ≤3.5 d,d 2 =d.

所述非均匀翅片散热器沿高度方向分为顶部、中部和底部,所述顶部、中部和底部占非均匀翅片散热器总高度的比例分别为5%、85%及10%时,d1=2d,d2=d,d3=1.8d。The non-uniform fin radiator is divided into top, middle and bottom along the height direction, and when the ratios of the top, middle and bottom to the total height of the non-uniform fin radiator are 5%, 85% and 10% respectively, d 1 = 2d, d 2 =d, d 3 =1.8d.

所述非均匀翅片散热器沿高度方向分为顶部、中部和底部,所述顶部、中部和底部占非均匀翅片散热器总高度的比例分别为10%、80%及10%时,d1=d3=1.8d,d2=d。The non-uniform fin radiator is divided into top, middle and bottom along the height direction, and when the ratios of the top, middle and bottom to the total height of the non-uniform fin radiator are 10%, 80% and 10% respectively, d 1 =d 3 =1.8d, d 2 =d.

所述非均匀翅片散热器沿高度方向分为顶部、中部和底部,所述顶部、中部和底部占非均匀翅片散热器总高度的比例分别为15%、70%及15%时,d1=d3=1.6d,d2=d。The non-uniform fin radiator is divided into top, middle and bottom along the height direction, and when the ratios of the top, middle and bottom to the total height of the non-uniform fin radiator are 15%, 70% and 15%, d 1 =d 3 =1.6d, d 2 =d.

所述非均匀翅片散热器沿高度方向分为顶部、中部和底部,所述顶部、中部和底部占非均匀翅片散热器总高度的比例分别为20%、60%及20%时,d1=d3=1.6d,d2=d。The non-uniform fin radiator is divided into top, middle and bottom along the height direction, and when the ratios of the top, middle and bottom to the total height of the non-uniform fin radiator are 20%, 60% and 20% respectively, d 1 =d 3 =1.6d, d 2 =d.

本发明的有益效果为:The beneficial effects of the present invention are:

(1)本发明的翅片根据海勒式空冷塔散热器外实际风速分布规律,基于冷却塔最优空气动力场理论,优化了翅片的分布,减小了散热器底部及顶部的通风阻力,消弱了散热器背部区域的漩涡,强化了散热器底部及顶部的换热,散热器沿高度方向换热更加均衡,从而增强了散热器的整体换热性能,同时由于翅片数目的减少,也节约了少量铝资源;(1) The fins of the present invention optimize the distribution of the fins according to the actual wind speed distribution law outside the radiator of the Heller type air cooling tower, based on the theory of the optimal aerodynamic field of the cooling tower, and reduce the ventilation resistance at the bottom and top of the radiator , which weakens the vortex in the back area of the radiator, strengthens the heat transfer at the bottom and top of the radiator, and makes the heat transfer of the radiator more balanced along the height direction, thus enhancing the overall heat transfer performance of the radiator. At the same time, due to the reduction in the number of fins , and also save a small amount of aluminum resources;

(2)本发明不仅可用于第五代海勒-福哥(Heller-Forgo)T60型6排管,也可用于第六代福哥型4排管。(2) The present invention can be used not only for the fifth generation Heller-Forgo T60 type 6-row pipe, but also for the sixth generation Fogo type 4-row pipe.

附图说明Description of drawings

图1(a)为Heller-Forgo T60型铝圆管结构示意图;Fig. 1 (a) is the structural schematic diagram of Heller-Forgo T60 type aluminum round tube;

图1(b)为Heller-Forgo T60型铝翅片结构示意图;Figure 1(b) is a schematic diagram of the Heller-Forgo T60 aluminum fin structure;

图2为冷却管束结构示意图;Figure 2 is a schematic diagram of the structure of the cooling tube bundle;

图3为冷却元件结构示意图;Fig. 3 is a structural schematic diagram of a cooling element;

图4为实施例一、二、三、四的散热器结构示意图;Fig. 4 is the structural representation of radiator of embodiment one, two, three, four;

其中,1、铝圆管;2、散热翅片;3、铝圆孔;4、湍流强化结构;5、加强板;6、管板;7、连接板;8、顶部水室;9、底部水室。Among them, 1. Aluminum round tube; 2. Radiating fins; 3. Aluminum round hole; 4. Turbulent flow strengthening structure; 5. Strengthening plate; 6. Tube plate; 7. Connecting plate; 8. Top water chamber; water room.

具体实施方式detailed description

下面结合附图与实施例对本发明做进一步说明:Below in conjunction with accompanying drawing and embodiment the present invention will be further described:

基于以上对翅片均匀布置的福哥型散热器在实际运行过程中缺点的分析,对福哥型散热器的翅片做如下优化:以第五代海勒-福哥(Heller-Forgo)T60型6排管为例,说明非均匀翅片散热器的结构组成,本发明并不改变原来翅片散热器的尺寸、材质、制造工艺及连接方式,仅对散热翅片的分布方式做适当调整。Based on the above analysis of the shortcomings of the Fogo radiator with evenly arranged fins in the actual operation process, the fins of the Fogo radiator are optimized as follows: the fifth generation Heller-Forgo (Heller-Forgo) T60 Type 6 row of tubes is taken as an example to illustrate the structural composition of the non-uniform finned radiator. The present invention does not change the size, material, manufacturing process and connection method of the original finned radiator, but only makes appropriate adjustments to the distribution of the radiating fins .

本发明的非均匀翅片散热器沿高度方向分为顶部、中部和底部三个区域,所述顶部、中部和底部的高度分别为h1、h2和h3,所述顶部、中部和底部三个区域的散热翅片分布间距分布为d1、d2和d3;当0.02H≤h1≤0.25H,0.5H≤h2≤0.96H,0.02H≤h3≤0.25H时,1.1d≤d1≤3.5d,d2=d,1.1d≤d3≤3.5d,其中,H为包含散热翅片的散热器长度,d为散热翅片均匀布置时的翅片间距。The non-uniform fin radiator of the present invention is divided into three regions along the height direction: top, middle and bottom, the heights of the top, middle and bottom are h 1 , h 2 and h 3 respectively, and the top, middle and bottom The distribution spacing of the heat dissipation fins in the three areas is d 1 , d 2 and d 3 ; when 0.02H≤h 1 ≤0.25H, 0.5H≤h 2 ≤0.96H, 0.02H≤h 3 ≤0.25H, 1.1 d≤d 1 ≤3.5d, d 2 =d, 1.1d≤d 3 ≤3.5d, wherein, H is the length of the radiator including the cooling fins, and d is the fin spacing when the cooling fins are evenly arranged.

当非均匀翅片散热器的顶部、中部和底部的高度满足:0.02H≤h1=h3≤0.25H,且0.5H≤h2≤0.96H时,1.1d≤d1=d3≤3.5d,d2=d。When the heights of the top, middle and bottom of the non-uniform fin radiator meet: 0.02H≤h 1 =h 3 ≤0.25H, and 0.5H≤h 2 ≤0.96H, 1.1d≤d 1 =d 3 ≤3.5 d,d 2 =d.

如图1(a)所示,为Heller-Forgo T60型铝圆管的结构示意图,铝圆管1的外径为17.75mm,厚度为0.75mm;散热翅片2,选用铝大板翅片,翅片厚度为0.33mm,原翅片间距为2.88mm。As shown in Figure 1(a), it is a schematic structural diagram of the Heller-Forgo T60 aluminum round tube. The outer diameter of the aluminum round tube 1 is 17.75mm and the thickness is 0.75mm; the heat dissipation fin 2 is made of large aluminum plate fins. The fin thickness is 0.33mm, and the original fin spacing is 2.88mm.

如图1(b)所示,4为湍流强化结构,铝圆管1错位排列,纵向中心距为30mm,横向为气流方向,铝圆管1设置六排,中心距为25mm,散热翅片2由冲压法成型,铝圆管1穿过散热翅片2上预留的铝圆孔3,且与散热翅片2采用胀接方法固定。As shown in Figure 1(b), 4 is a turbulence-intensified structure. The aluminum round tubes 1 are misplaced, the longitudinal center distance is 30mm, and the horizontal direction is the airflow direction. Aluminum round tubes 1 are arranged in six rows with a center distance of 25mm. Formed by stamping, the aluminum round tube 1 passes through the aluminum round hole 3 reserved on the heat dissipation fin 2, and is fixed with the heat dissipation fin 2 by means of expansion joint.

图2为冷却管束结构示意图。图中,加强板5的材质为铝合金,外形似工字钢,高170mm,长599mm,厚6mm,中间留孔,铝圆管1在孔中穿过;每个管束由60根长4840mm的铝圆管1。Figure 2 is a schematic diagram of the structure of the cooling tube bundle. In the figure, the reinforcing plate 5 is made of aluminum alloy, looks like an I-beam, is 170mm high, 599mm long, and 6mm thick, with a hole in the middle through which the aluminum round tube 1 passes; each tube bundle consists of 60 tubes with a length of 4840mm Aluminum round tube 1.

图3为冷却元件结构示意图。图中,管板6的材质为铝合金,留有管孔及螺栓孔;四个冷却管束由管板6并联构成一个冷却元件,此元件为散热器的最基本单元,由它串联组成各种长度的冷却柱,即散热器。Fig. 3 is a schematic diagram of the structure of the cooling element. In the figure, the material of the tube plate 6 is aluminum alloy, and there are tube holes and bolt holes; four cooling tube bundles are connected in parallel by the tube plate 6 to form a cooling element, which is the most basic unit of the radiator, and it is connected in series to form various The length of the cooling column, that is, the radiator.

图4为散热器结构示意图,每个冷却柱由若干个冷却元件串联而成,两端管板用螺栓与连接板7固定,冷却柱顶部与顶部水室8相连,底部与底部水室9相连,水室与管板间用螺栓固定。Figure 4 is a schematic diagram of the structure of the radiator. Each cooling column is composed of several cooling elements connected in series. The tube plates at both ends are fixed to the connecting plate 7 with bolts. The top of the cooling column is connected to the top water chamber 8, and the bottom is connected to the bottom water chamber 9. , The water chamber and the tube sheet are fixed with bolts.

实施例一:Embodiment one:

本实施例将散热器按照高度方向分为三部分,顶部、中部、底部,三部分占总高度的比例分别为5%、85%及10%,顶部翅片间距d1=2d=5.76mm,底部翅片间距为d3=1.8d=5.184mm,翅片的其他参数不变,其中d为散热翅片均匀布置时的翅片间距,2.88mm。In this embodiment, the heat sink is divided into three parts according to the height direction, the top, the middle, and the bottom. The proportions of the three parts to the total height are 5%, 85% and 10% respectively, and the top fin spacing d 1 =2d=5.76mm, The pitch of the bottom fins is d 3 =1.8d=5.184mm, and other parameters of the fins remain unchanged, where d is the fin pitch when the cooling fins are evenly arranged, 2.88mm.

实施例二:Embodiment two:

该实施例将散热器按照高度方向分为三部分,顶部、中部、底部,三部分占总高度的比例分别为10%、80%及10%,顶部及底部的翅片间距为d1=d3=1.8d=5.184mm,翅片的其他参数不变。In this embodiment, the heat sink is divided into three parts according to the height direction, the top, the middle, and the bottom. The proportions of the three parts to the total height are 10%, 80% and 10% respectively, and the fin pitch at the top and bottom is d 1 =d 3 = 1.8d = 5.184mm, other parameters of the fin remain unchanged.

实施例三:Embodiment three:

该实施例将散热器按照高度方向分为三部分,顶部、中部、底部,三部分占总高度的比例分别为15%、70%及15%,顶部及底部的翅片间距为d1=d3=1.6d=4.608mm,翅片的其他参数不变。In this embodiment, the radiator is divided into three parts according to the height direction, the top, the middle, and the bottom. The proportions of the three parts to the total height are 15%, 70% and 15% respectively, and the fin pitch at the top and bottom is d 1 =d 3 = 1.6d = 4.608mm, other parameters of the fin remain unchanged.

实施例四:Embodiment four:

该实施例将散热器按照高度方向分为三部分,顶部、中部、底部,三部分占总高度的比例分别为20%、60%及20%,顶部及底部的翅片间距为d1=d3=1.2d=4.032mm,翅片的其他参数不变。In this embodiment, the heat sink is divided into three parts according to the height direction, the top, the middle part and the bottom. The proportions of the three parts to the total height are 20%, 60% and 20% respectively, and the fin pitch at the top and bottom is d 1 =d 3 = 1.2d = 4.032mm, other parameters of the fin remain unchanged.

本发明的散热原理为:Heat dissipation principle of the present invention is:

(1)当散热器翅片沿高度方向均匀布置(1) When the radiator fins are evenly arranged along the height direction

散热器入口处空气流速沿高度方向的分布规律如下:由于受地面阻力影响,在较低位置处,风速较小,随着高度的增加,风速逐渐增大,大约在散热器的中间范围风速达到最大,散热器顶部区域,由于受散热器及塔沿之间顶部封板的影响,风速又变小,由于局部散热面积相同,故造成沿高度方向局部散热量不同,顶部及底部区域的散热器的散热能力并没有最大化;空气流经散热器之后进入空冷塔,沿散热器高度方向,空气流速不同,易产生纵向漩涡,形成局部阻力,不利于空气的流通,整体上不利于散热器的散热,导致空冷塔的冷却效率降低。The distribution law of the air flow velocity along the height direction at the entrance of the radiator is as follows: due to the influence of the ground resistance, the wind speed is small at the lower position, and gradually increases with the increase of the height, and the wind speed reaches about the middle range of the radiator. The largest, the top area of the radiator, due to the influence of the top sealing plate between the radiator and the tower edge, the wind speed becomes smaller, because the local heat dissipation area is the same, so the local heat dissipation is different along the height direction, the top and bottom areas of the radiator The heat dissipation capacity of the radiator is not maximized; the air flows through the radiator and then enters the air cooling tower. Along the height direction of the radiator, the air flow velocity is different, which is easy to generate longitudinal vortices, forming local resistance, which is not conducive to the circulation of air, and is not conducive to the cooling of the radiator as a whole. Heat dissipation, resulting in a reduction in the cooling efficiency of the air-cooling tower.

(2)当散热器翅片沿高度方向不均匀布置(2) When the radiator fins are unevenly arranged along the height direction

(2.1)当散热器顶部和底部的散热翅片分布间距与中部不相等,由于增大了顶部及底部的翅片间距,减小了散热器的局部阻力,空气流速增大,该区域的通风量增大,使得该区域的局部散热面积与空气流速更加匹配,局部散热能力得到提高。基于冷却塔最优空气动力场理论分析可知,整体散热效果优于翅片均匀布置的散热器。(2.1) When the fin distribution spacing of the top and bottom of the radiator is not equal to that of the middle part, due to the increase of the fin spacing at the top and bottom, the local resistance of the radiator is reduced, the air flow rate increases, and the ventilation in this area The increase of the amount makes the local heat dissipation area in this area more matched with the air velocity, and the local heat dissipation capacity is improved. Based on the theoretical analysis of the optimal aerodynamic field of the cooling tower, it can be known that the overall heat dissipation effect is better than that of the radiator with evenly arranged fins.

(2.2)由于顶部及底部散热器区域的空气流速增大,使得沿高度方向,散热器背部区域的空气流速更加平衡,因此减弱了该区域纵向漩涡的生成能力及由漩涡所带来的局部阻力,更加有利于散热器的散热。(2.2) Due to the increased air velocity in the top and bottom radiator regions, the air velocity in the back region of the radiator is more balanced along the height direction, thus weakening the generation ability of the longitudinal vortex in this region and the local resistance brought by the vortex , which is more conducive to the heat dissipation of the radiator.

上述虽然结合附图对本发明的具体实施方式进行了描述,但并非对本发明保护范围的限制,所属领域技术人员应该明白,在本发明的技术方案的基础上,本领域技术人员不需要付出创造性劳动即可做出的各种修改或变形仍在本发明的保护范围以内。Although the specific implementation of the present invention has been described above in conjunction with the accompanying drawings, it does not limit the protection scope of the present invention. Those skilled in the art should understand that on the basis of the technical solution of the present invention, those skilled in the art do not need to pay creative work Various modifications or variations that can be made are still within the protection scope of the present invention.

Claims (6)

1. the non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that described non-homogeneous fin dissipates Hot device is divided into top, middle part and region, three, bottom along short transverse, and the height of described top, middle part and bottom is respectively h1、h2 And h3, the trizonal radiating fin in described top, middle part and bottom distribution spacing is distributed as d1、d2And d3;When 0.02H≤h1≤ 0.25H, 0.5H≤h2≤ 0.96H, 0.02H≤h3During≤0.25H, 1.1d≤d1≤ 3.5d, d2=d, 1.1d≤d3≤ 3.5d, Wherein, H is the radiator length comprising radiating fin, and d is radiating fin spacing of fin when being evenly arranged.
A kind of non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that When the height of top, middle part and the bottom of described non-homogeneous fin radiator meets: 0.02H≤h1=h3≤ 0.25H, and 0.5H≤h2During≤0.96H, 1.1d≤d1=d3≤ 3.5d, d2=d.
A kind of non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that Described non-homogeneous fin radiator is divided into top, middle part and bottom, described top, middle part and bottom to account for non-homogeneous wing along short transverse When the ratio of sheet heat radiator total height is respectively 5%, 85% and 10%, d1=2d, d2=d, d3=1.8d.
A kind of non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that Described non-homogeneous fin radiator is divided into top, middle part and bottom, described top, middle part and bottom to account for non-homogeneous wing along short transverse When the ratio of sheet heat radiator total height is respectively 10%, 80% and 10%, d1=d3=1.8d, d2=d.
A kind of non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that Described non-homogeneous fin radiator is divided into top, middle part and bottom, described top, middle part and bottom to account for non-homogeneous wing along short transverse When the ratio of sheet heat radiator total height is respectively 15%, 70% and 15%, d1=d3=1.6d, d2=d.
A kind of non-homogeneous fin radiator for Heller type indirect air cooling system, it is characterised in that Described non-homogeneous fin radiator is divided into top, middle part and bottom, described top, middle part and bottom to account for non-homogeneous wing along short transverse When the ratio of sheet heat radiator total height is respectively 20%, 60% and 20%, d1=d3=1.6d, d2=d.
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