CN103857974B - Fin-tube heat exchanger and its manufacture method - Google Patents
Fin-tube heat exchanger and its manufacture method Download PDFInfo
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- CN103857974B CN103857974B CN201380003502.3A CN201380003502A CN103857974B CN 103857974 B CN103857974 B CN 103857974B CN 201380003502 A CN201380003502 A CN 201380003502A CN 103857974 B CN103857974 B CN 103857974B
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- 238000004519 manufacturing process Methods 0.000 title claims description 12
- 238000000034 method Methods 0.000 title claims description 12
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- 239000012530 fluid Substances 0.000 claims abstract description 5
- 238000000576 coating method Methods 0.000 claims description 22
- 239000011248 coating agent Substances 0.000 claims description 21
- 239000000463 material Substances 0.000 claims description 19
- 239000011247 coating layer Substances 0.000 claims description 10
- 239000010410 layer Substances 0.000 claims description 7
- 239000000758 substrate Substances 0.000 claims description 4
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 230000010148 water-pollination Effects 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 60
- 238000012546 transfer Methods 0.000 abstract description 16
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- 238000005516 engineering process Methods 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 230000001050 lubricating effect Effects 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- 238000009423 ventilation Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
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- 229920005989 resin Polymers 0.000 description 2
- 238000004381 surface treatment Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001593 boehmite Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- WMYWOWFOOVUPFY-UHFFFAOYSA-L dihydroxy(dioxo)chromium;phosphoric acid Chemical compound OP(O)(O)=O.O[Cr](O)(=O)=O WMYWOWFOOVUPFY-UHFFFAOYSA-L 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- FAHBNUUHRFUEAI-UHFFFAOYSA-M hydroxidooxidoaluminium Chemical compound O[Al]=O FAHBNUUHRFUEAI-UHFFFAOYSA-M 0.000 description 1
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- 235000019353 potassium silicate Nutrition 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F17/00—Removing ice or water from heat-exchange apparatus
- F28F17/005—Means for draining condensates from heat exchangers, e.g. from evaporators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/047—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B39/00—Evaporators; Condensers
- F25B39/02—Evaporators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0068—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for refrigerant cycles
- F28D2021/0071—Evaporators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2240/00—Spacing means
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Geometry (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Details Of Fluid Heaters (AREA)
Abstract
本发明提供一种翅片管热交换器,其具有:形成气体流路的多个翅片(1);和贯通多个翅片且内部流通与气体进行热交换的流体的导热管(21),翅片具有:第一倾斜部(6),其相对于气体的流动方向倾斜以使得至少形成一个峰部(3);管周围部(5),其分别形成于在沿重力方向相互分开的第一位置和第二位置贯通翅片的导热管周围;和第二倾斜部(7),其将管周围部和第一倾斜部相互连接,连接第一位置和第二位置中的各自的第二倾斜部的槽部(8)形成于第一倾斜部的表面,由此冷凝水顺着槽部流动,向重力方向下方顺畅地被引导,排水性能提高。
The present invention provides a finned tube heat exchanger, which has: a plurality of fins (1) forming a gas flow path; and a heat conduction tube (21) passing through the plurality of fins and circulating fluid for heat exchange with gas , the fins have: a first inclined portion (6), which is inclined relative to the flow direction of the gas so that at least one peak portion (3) is formed; tube peripheral portions (5), which are respectively formed at The first position and the second position pass through the periphery of the heat transfer tube of the fin; and the second inclined part (7), which connects the surrounding part of the tube and the first inclined part to each other, and connects the respective first positions in the first position and the second position The groove portion (8) of the second inclined portion is formed on the surface of the first inclined portion, whereby the condensed water flows along the groove portion and is smoothly guided downward in the direction of gravity, thereby improving drainage performance.
Description
技术领域technical field
本发明涉及与气体进行热交换的翅片管热交换器和其制造方法。The present invention relates to a finned tube heat exchanger for exchanging heat with gas and its manufacturing method.
背景技术Background technique
目前,这种翅片管热交换器由以规定间隔排列的多个翅片和贯通多个翅片的导热管构成。空气(气体)在翅片与翅片之间流动来与导热管中的流体进行热交换。Conventionally, such a finned tube heat exchanger is composed of a plurality of fins arranged at predetermined intervals and a heat transfer tube passing through the plurality of fins. Air (gas) flows between the fins to exchange heat with the fluid in the heat pipe.
在此,在使用翅片管热交换器作为蒸发器的情况下,当翅片的表面温度比进行热交换的空气的露点低时,空气中的水分凝结,水滴(冷凝水)附着于翅片表面。当这样在翅片表面上附着冷凝水时,在相邻的翅片间等产生水分架桥(交联),翅片间的空气流路被该冷凝水堵塞,而导致通风阻力的增大。Here, in the case of using a finned tube heat exchanger as an evaporator, when the surface temperature of the fin is lower than the dew point of the air for heat exchange, moisture in the air condenses and water droplets (condensed water) adhere to the fin surface. When condensed water adheres to the surface of the fins in this way, moisture bridging (crosslinking) occurs between adjacent fins, and the air flow path between the fins is blocked by the condensed water, resulting in an increase in ventilation resistance.
其结果是,在使用这种翅片管热交换器的空气调节机或供热水器等设备中存在消耗电力增加且能量效率降低的课题。因此,优选从翅片表面迅速地除去冷凝水。As a result, in equipment such as an air conditioner and a water heater using such a finned tube heat exchanger, there are problems of increased power consumption and decreased energy efficiency. Therefore, it is preferable to quickly remove condensed water from the fin surface.
因此,通过在翅片表面形成亲水性覆膜层,且缩小相对于在翅片表面附着的水的接触角,来提高排水性并进行防止生成的冷凝水引起的翅片间的空气流路的堵塞(例如,参照文献1)。Therefore, by forming a hydrophilic coating layer on the surface of the fins and reducing the contact angle with respect to the water adhering to the surface of the fins, the drainage performance is improved and the air flow path between the fins caused by the generated condensed water is prevented. of clogging (for example, see reference 1).
另外,还具有一种装置,其通过对翅片表面的亲水性覆膜层进行等离子照射,形成微细凹凸,来提高亲水性(例如,参照文献2)。In addition, there is also a device for improving hydrophilicity by irradiating a hydrophilic coating layer on the surface of a fin with plasma to form fine unevenness (for example, refer to Document 2).
另外,还具有通过在翅片上形成排水槽来提高冷凝水的排出性的装置(例如,参照文献3)。图10表示该文献3的翅片管热交换器的结构。如图10所示,在翅片131上设有排水槽116,该排水槽116从导热管121下方的排水(冷凝水113)滞留区域沿着翅片131的表面向斜下方延伸。通过设置该排水槽116,迅速地排出滞留在导热管121下方的排水滞留区域的冷凝水113。In addition, there is also a device that improves drainage of condensed water by forming drain grooves on fins (for example, refer to Document 3). FIG. 10 shows the structure of the finned tube heat exchanger of the document 3. As shown in FIG. As shown in FIG. 10 , a drain groove 116 is provided on the fin 131 , and the drain groove 116 extends obliquely downward along the surface of the fin 131 from the stagnant area of drain water (condensed water 113 ) under the heat pipe 121 . By providing the drain groove 116 , the condensed water 113 stagnant in the drain stagnation area below the heat transfer pipe 121 is quickly drained.
现有技术文献prior art literature
非专利文献non-patent literature
文献1:平泽秀公“预涂敷铝翅片材料的表面处理技术”,表面技术,Vol.57(2006),No.2,p.127Document 1: Hideko Hirasawa "Surface Treatment Technology of Pre-coated Aluminum Fin Material", Surface Technology, Vol.57 (2006), No.2, p.127
专利文献patent documents
文献2:(日本)特开2010-175131号公报Document 2: (Japanese) Unexamined Patent Publication No. 2010-175131
文献3:(日本)实开昭64-22186号公报Document 3: (Japan) Publication No. 64-22186
发明内容Contents of the invention
发明所要解决的课题The problem to be solved by the invention
但是,在文献1所记载的技术中,特别是在隔开规定间隔地层叠的翅片间产生冷凝水的交联的情况下,具有冷凝水的排水性不充分的课题。However, the technique described in Document 1 has a problem of insufficient drainage of condensed water, particularly when cross-linking of condensed water occurs between fins stacked at predetermined intervals.
另外,在文献2所记载的技术中,在翅片表面形成微细凹凸的情况下,具有需要等离子照射等高价的加工工艺且制造成本非常高的课题。In addition, in the technique described in Document 2, when fine unevenness is formed on the surface of the fin, an expensive processing process such as plasma irradiation is required, and there is a problem that the production cost is very high.
另外,文献3所记载的技术是在平翅片上设置排出槽的技术,也如文献3的图2和图5所示,具有在相邻的翅片间难以避免交联的产生且不能充分地将冷凝水顺畅地向翅片下方引导的课题。In addition, the technology described in Document 3 is a technology in which discharge grooves are provided on flat fins. As shown in FIGS. 2 and 5 of Document 3, it is difficult to avoid crosslinking between adjacent fins and cannot sufficiently The problem of smoothly guiding condensed water to the bottom of the fins.
本发明是鉴于上述情况而研发的,其目的在于,提供一种通过廉价的加工工艺提高附着于翅片表面的冷凝水的排水性能并且能量效率优异的翅片管热交换器和其制造方法。The present invention was developed in view of the above circumstances, and an object of the present invention is to provide a finned tube heat exchanger and a manufacturing method thereof that improve drainage performance of condensed water adhering to the fin surface through an inexpensive process and that are excellent in energy efficiency.
用于解决课题的技术方案Technical solutions for solving problems
为了解决所述现有的课题,本发明提供一种翅片管热交换器,其特征在于,具有:为了在彼此之间形成气体流路而平行地排列的多个翅片;和贯通所述多个翅片且在内部流通与所述气体进行热交换的流体的导热管,所述翅片具有:第一倾斜部,其相对于气体的流动方向倾斜以使得至少形成一个峰部;管周围部,其分别形成于在重力方向相互分开的第一位置和第二位置贯通所述翅片的所述导热管的周围;和第二倾斜部,其以将所述管周围部和所述第一倾斜部相互连接的方式相对于气体的流动方向倾斜,连接所述第一位置的所述第二倾斜部和第二位置的所述第二倾斜部的槽部形成于所述第一倾斜部的表面。In order to solve the above-mentioned conventional problems, the present invention provides a finned tube heat exchanger characterized in that it has: a plurality of fins arranged in parallel to form gas flow paths therebetween; A heat transfer pipe having a plurality of fins and passing a fluid for heat exchange with the gas inside, the fins having: a first inclined portion inclined with respect to the flow direction of the gas so as to form at least one peak; the circumference of the pipe parts, which are respectively formed at the circumference of the heat transfer tube penetrating the fin at first and second positions separated from each other in the direction of gravity; A manner in which an inclined portion is connected to each other is inclined relative to the gas flow direction, and a groove portion connecting the second inclined portion at the first position and the second inclined portion at the second position is formed in the first inclined portion s surface.
发明效果Invention effect
根据本发明,能够提供一种通过廉价的加工工艺提高附着于翅片表面的冷凝水的排水性能的能量效率优异的翅片管热交换器。According to the present invention, it is possible to provide a finned tube heat exchanger excellent in energy efficiency in which drainage performance of condensed water adhering to the surface of the fins is improved by an inexpensive process.
附图说明Description of drawings
图1是本发明实施方式1的翅片管热交换器的立体图。Fig. 1 is a perspective view of a finned tube heat exchanger according to Embodiment 1 of the present invention.
图2A是实施方式1的翅片管热交换器的波纹翅片的平面图。2A is a plan view of corrugated fins of the finned tube heat exchanger according to Embodiment 1. FIG.
图2B是图2A的波纹翅片的A-A剖面图。Fig. 2B is an AA sectional view of the corrugated fin of Fig. 2A.
图2C是图2A的波纹翅片的B-B剖面图。Fig. 2C is a BB sectional view of the corrugated fin in Fig. 2A.
图3是表示实施方式1的翅片管热交换器的翅片材料结构的剖面图。3 is a cross-sectional view showing a fin material structure of the fin-tube heat exchanger according to Embodiment 1. FIG.
图4是本实施方式1的比较例的在翅片管热交换器的波纹翅片滞留有冷凝水的状态的说明图。FIG. 4 is an explanatory view of a state in which condensed water stagnates in the corrugated fins of the finned tube heat exchanger according to the comparative example of the first embodiment.
图5是实施方式1的翅片管热交换器的波纹翅片的冷凝水排水作用的说明图。Fig. 5 is an explanatory diagram of the condensed water drainage function of the corrugated fins of the finned tube heat exchanger according to the first embodiment.
图6是表示实施方式1的翅片管热交换器的槽部的详细形状的剖面图。6 is a cross-sectional view showing a detailed shape of a groove portion of the fin-tube heat exchanger according to Embodiment 1. FIG.
图7是表示实施方式1的翅片管热交换器的槽部的其它详细形状的剖面图。7 is a cross-sectional view showing another detailed shape of the groove portion of the fin-tube heat exchanger according to Embodiment 1. FIG.
图8是本发明实施方式2的翅片管热交换器的波纹翅片的平面图。Fig. 8 is a plan view of corrugated fins of a finned tube heat exchanger according to Embodiment 2 of the present invention.
图9A是实施方式3的翅片管热交换器的波纹翅片的平面图。9A is a plan view of corrugated fins of the finned tube heat exchanger according to Embodiment 3. FIG.
图9B是图9A的波纹翅片的A-A剖面图。Fig. 9B is an AA sectional view of the corrugated fin of Fig. 9A.
图9C是图9A的波纹翅片的B-B剖面图。Fig. 9C is a BB sectional view of the corrugated fin in Fig. 9A.
图10是现有的翅片管热交换器的翅片的平面图。Fig. 10 is a plan view of a fin of a conventional finned tube heat exchanger.
具体实施方式Detailed ways
第一发明提供一种翅片管热交换器,其具有:为了在彼此之间形成气体流路而平行地排列的多个翅片;和贯通上述多个翅片且在内部流通与上述气体进行热交换的流体的导热管,上述翅片具有:第一倾斜部,其相对于气体的流动方向倾斜以使得至少形成一个峰部;管周围部,其分别形成于在重力方向相互分开的第一位置和第二位置贯通上述翅片的上述导热管的周围;和第二倾斜部,其以将上述管周围部和上述第一倾斜部相互连接的方式相对于气体的流动方向倾斜,连接上述第一位置的上述第二倾斜部和第二位置的上述第二倾斜部的槽部形成于上述第一倾斜部的表面。The first invention provides a finned tube heat exchanger comprising: a plurality of fins arranged in parallel to form a gas flow path therebetween; A heat pipe for heat exchange fluid, the above-mentioned fins have: a first inclined portion, which is inclined with respect to the direction of gas flow so as to form at least one peak portion; The position and the second position pass through the periphery of the heat transfer tube of the above-mentioned fin; and the second inclined part, which is inclined with respect to the flow direction of the gas in such a manner as to connect the above-mentioned tube peripheral part and the above-mentioned first inclined part to each other, connects the above-mentioned first inclined part. The first inclined portion and the groove portion of the second inclined portion at the second position are formed on the surface of the first inclined portion.
由此,能够将冷凝水从成为冷凝水主要的滞留区域的第二倾斜部(或经由第二倾斜部从管周围部)通过槽部有效地向重力方向下方引导。即,能够将滞留在第一位置的第二倾斜部的冷凝水通过槽部有效地向位于比第一位置更靠重力方向下方的第二位置的第二倾斜部引导。由此,能够提高附着于翅片表面的冷凝水的排水性能,能够抑制在相邻的翅片间等产生交联,能够提供能量效率优异的翅片管热交换器。另外,这种槽部能够通过比较简单的加工工艺形成,能够抑制伴随槽部的形成的制造成本的上升。Thereby, condensed water can be efficiently guided downward in the direction of gravity from the second inclined portion (or from the pipe peripheral portion via the second inclined portion) which is the main stagnation area of the condensed water through the groove portion. That is, the condensed water stagnant at the second slope at the first position can be efficiently guided to the second slope at the second position below the first position in the direction of gravity through the groove. Thereby, the drainage performance of condensed water adhering to the fin surface can be improved, crosslinking between adjacent fins and the like can be suppressed, and a fin-tube heat exchanger excellent in energy efficiency can be provided. In addition, such a groove portion can be formed by a relatively simple process, and an increase in manufacturing cost accompanying the formation of the groove portion can be suppressed.
第二发明如第一发明的翅片管热交换器,其中,上述槽部的开口宽度尺寸为2mm以下。A second invention is the finned tube heat exchanger according to the first invention, wherein the opening width of the groove is 2 mm or less.
由此,因为在槽部和冷凝水之间产生毛细管效应,所以能够更有效地进行冷凝水的排水。Accordingly, since a capillary effect is generated between the groove portion and the condensed water, the condensed water can be drained more efficiently.
第三发明如第一或第二发明的翅片管热交换器,其中,在上述翅片中,由上述第一倾斜部形成的上述峰部的棱线沿重力方向配置,上述槽部在重力方向延伸。The third invention is the finned tube heat exchanger according to the first or second invention, wherein in the fins, the ridges of the peaks formed by the first slope are arranged along the direction of gravity, and the grooves are arranged in the direction of gravity. direction extension.
由此,能够将进入到槽部内的冷凝水有效地向重力方向下方排水。Thereby, the condensed water which has entered into the groove part can be efficiently drained downward in the direction of gravity.
第四发明如第一~第三发明中任一项的翅片管热交换器,其中,上述翅片具有基材和形成于上述基材的表面的覆膜层,构成上述覆膜层的层的一部分为亲水性覆膜。A fourth invention is the finned tube heat exchanger according to any one of the first to third inventions, wherein the fin has a base material and a coating layer formed on the surface of the base material, and the layers constituting the coating layer are Part of it is a hydrophilic coating.
由此,通过亲水性覆膜,滞留在管周围部或第二倾斜部的冷凝水沿着翅片表面平坦地蔓延(扩展),能够进一步抑制交联的产生,并且容易向槽部引导冷凝水。As a result, the condensed water stagnant at the tube periphery or the second inclined portion spreads (spreads) flatly along the fin surface due to the hydrophilic coating, further suppressing the occurrence of crosslinking, and making it easier to guide the condensed water to the groove. water.
第五发明提供一种第四发明中的翅片管热交换器的制造方法,在上述基材上形成上述亲水性覆膜后,使用上述基材同时成形上述第一倾斜部、上述第二倾斜部、上述槽部来成形上述翅片。The fifth invention provides the method for manufacturing the finned tube heat exchanger according to the fourth invention, comprising forming the first inclined portion, the second inclined portion, and the second slope simultaneously by using the base material after forming the hydrophilic coating on the base material. The fins are formed by forming the inclined portion and the groove portion.
由此,同时成形翅片的第一、第二倾斜部和槽部,因此不增加加工工艺,就能够提供抑制制造成本且能量效率优异的翅片管热交换器。Accordingly, since the first and second inclined portions and the groove portions of the fins are formed at the same time, it is possible to provide a finned tube heat exchanger with reduced manufacturing costs and excellent energy efficiency without increasing the manufacturing process.
以下,参照附图对本发明的实施方式进行说明。此外,本发明不被该实施方式限定。Hereinafter, embodiments of the present invention will be described with reference to the drawings. In addition, this invention is not limited by this embodiment.
(实施方式1)(implementation mode 1)
图1表示本发明的实施方式1的翅片管热交换器的立体图。如图1所示,本实施方式1的翅片管热交换器100具有为了形成空气A(气体)的流路而隔开规定间隔平行地排列的多个翅片1和贯通这些翅片1的导热管21。翅片管热交换器100使在导热管21内部流通的介质B与沿着翅片1的表面流动的空气A进行热交换。FIG. 1 shows a perspective view of a finned tube heat exchanger according to Embodiment 1 of the present invention. As shown in FIG. 1 , the finned tube heat exchanger 100 according to Embodiment 1 has a plurality of fins 1 arranged in parallel at predetermined intervals in order to form a flow path of air A (gas), and a fin penetrating through these fins 1 . Heat pipe 21. The finned tube heat exchanger 100 exchanges heat between the medium B flowing inside the heat transfer tube 21 and the air A flowing along the surface of the fin 1 .
作为介质B例如能够使用二氧化碳、氢氟烃等制冷剂。导热管21可以连成1个,也可以分成多个。As the medium B, for example, a refrigerant such as carbon dioxide or hydrofluorocarbon can be used. The heat transfer pipe 21 may be connected into one, or may be divided into a plurality.
图2A、图2B、图2C表示本实施方式1的翅片1的详细构造。如图2A所示,翅片1形成为相对于空气的流动方向S至少出现一个峰部3。具体而言,翅片1相对于空气的流动方向S具有两个峰部3,如图2B的剖面图所示,形成为具有大致M字形的截面形状的波纹翅片。2A, 2B, and 2C show the detailed structure of the fin 1 according to the first embodiment. As shown in FIG. 2A , the fin 1 is formed so that at least one peak 3 appears with respect to the flow direction S of the air. Specifically, the fin 1 has two crests 3 with respect to the air flow direction S, and is formed as a corrugated fin having a substantially M-shaped cross-sectional shape as shown in the cross-sectional view of FIG. 2B .
另外,如图2B和图2C所示,翅片1具有:形成于贯通翅片1的导热管21的周围的管周围部5、相对于空气的流动方向S倾斜以形成峰部3的第一倾斜部6、和将管周围部5与第一倾斜部6相互连接的第二倾斜部7。In addition, as shown in FIG. 2B and FIG. 2C , the fin 1 has a tube peripheral portion 5 formed around the heat transfer tube 21 passing through the fin 1 , and a first peak portion 3 that is inclined with respect to the flow direction S of the air to form a peak portion 3 . The inclined portion 6 and the second inclined portion 7 connecting the pipe peripheral portion 5 and the first inclined portion 6 to each other.
如图2B所示,通过交替连接相对于空气的流动方向S的倾斜角不同的第一倾斜部6,形成两个峰部3和配置于该峰部3之间的谷部4。本实施方式1的翅片1中,峰部3的棱线和谷部4分别沿着重力方向形成。As shown in FIG. 2B , two peaks 3 and valleys 4 disposed between the peaks 3 are formed by alternately connecting first inclined portions 6 having different inclination angles with respect to the air flow direction S. In the fin 1 according to Embodiment 1, the ridges of the peaks 3 and the valleys 4 are formed along the direction of gravity, respectively.
管周围部5是在导热管21向翅片1贯通的贯通位置以包围导热管21的周围的方式配置的环状部分。如图2C所示,本实施方式1中,管周围部5形成为沿着空气的流动方向的平面即平坦的面。另外,如图2A所示,导热管21在沿着重力方向分开的多个位置贯通翅片1,在各个贯通位置设有管周围部5。The tube peripheral portion 5 is an annular portion disposed so as to surround the periphery of the heat transfer tube 21 at the penetration position where the heat transfer tube 21 penetrates into the fin 1 . As shown in FIG. 2C , in Embodiment 1, the tube peripheral portion 5 is formed as a flat surface that is a plane along the air flow direction. In addition, as shown in FIG. 2A , the heat transfer tubes 21 penetrate the fin 1 at a plurality of positions separated along the gravity direction, and the tube peripheral portions 5 are provided at the respective penetration positions.
第二倾斜部7是配置于管周围部5的周围的部分。如图2C所示,作为平坦面的管周围部5和作为倾斜面的第一倾斜部6由作为倾斜面的第二倾斜部7连接。因此,如图2C所示,在导热管21的贯通位置的周围形成由第二倾斜部7的倾斜面包围的凹状区域。该凹状区域成为易于冷凝水滞留的区域。The second inclined portion 7 is a portion disposed around the pipe peripheral portion 5 . As shown in FIG. 2C , the pipe peripheral portion 5 which is a flat surface and the first inclined portion 6 which is an inclined surface are connected by a second inclined portion 7 which is an inclined surface. Therefore, as shown in FIG. 2C , a concave region surrounded by the inclined surface of the second inclined portion 7 is formed around the penetration position of the heat transfer pipe 21 . This concave area becomes an area where condensed water tends to stagnate.
本实施方式1的翅片1中,形成有将滞留在第二倾斜部7的冷凝水排水的多个凹状的槽部8。具体而言,凹状的槽部8形成为在形成谷部4的一对第一倾斜部6的表面沿着重力方向延伸。各个槽部8沿着峰部3和谷部4形成,形成于谷部4的附近。In the fin 1 according to Embodiment 1, a plurality of concave grooves 8 for draining the condensed water accumulated in the second slope 7 are formed. Specifically, the concave groove portion 8 is formed so as to extend in the gravitational direction on the surface of the pair of first inclined portions 6 forming the valley portion 4 . Each groove portion 8 is formed along the peak portion 3 and the valley portion 4 , and is formed in the vicinity of the valley portion 4 .
另外,如图2A所示,翅片1中,分别配置于在重力方向上相互分开的第一位置P1和第二位置P2贯通翅片1的导热管21的周围的凹状的区域(第二倾斜部7),通过多个槽部8相互连接。即,各个槽部8沿重力方向延伸以将由重力方向上相邻的第二倾斜部7包围的凹状区域相互连接。此外,槽部8优选在与第二倾斜部7的连接部分,使凹状截面的至少一部分在第二倾斜部7侧开口。In addition, as shown in FIG. 2A , in the fin 1 , the first position P1 and the second position P2 that are separated from each other in the direction of gravity are respectively disposed in the concave region around the heat transfer pipe 21 of the fin 1 (the second inclination part 7) are connected to each other by a plurality of groove parts 8. That is, each groove portion 8 extends in the gravitational direction to connect concave regions surrounded by the gravitational adjacent second inclined portions 7 to each other. In addition, it is preferable that at least a part of the concave cross section of the groove portion 8 is opened on the second slope portion 7 side at the connection portion with the second slope portion 7 .
关于翅片1的表面的材质,优选使用与水的接触角成为30度以下的金属。另外,当金属暴露于空气或水分中时,形成氧化覆膜或腐蚀生成物,因此也可以使用作为构成翅片1的基材的表面处理形成有亲水性覆膜的基材。As for the material of the surface of the fin 1, it is preferable to use a metal whose contact angle with water is 30 degrees or less. In addition, when the metal is exposed to air or moisture, an oxide film or a corrosion product is formed, so a substrate having a hydrophilic coating formed by surface treatment as a substrate constituting the fin 1 can also be used.
在该情况下,作为翅片材料如图3所示使用在基材9的表面上形成有覆膜层10的材料。覆膜层10是重叠有耐腐蚀性覆膜10a,并且在其上重叠有亲水性覆膜10b和润滑性覆膜10c的层。关于基材9能够应用钢铁材、铜材、铝材。In this case, as the fin material, as shown in FIG. 3 , a material in which the coating layer 10 is formed on the surface of the base material 9 is used. The coating layer 10 is a layer in which a corrosion-resistant coating 10a is superimposed, and a hydrophilic coating 10b and a lubricating coating 10c are superimposed thereon. As for the base material 9, a steel material, a copper material, or an aluminum material can be applied.
耐腐蚀性覆膜10a通过磷酸铬酸盐处理而形成,作为亲水性覆膜10b能够使用无机类(水玻璃类、勃姆石类)、有机树脂类和有机·无机复合类的覆膜。本实施方式1中,作为亲水性覆膜10b使用通过化成处理形成作为有机·无机复合类的二氧化硅/树脂的复合类的覆膜的覆膜。The corrosion-resistant coating 10 a is formed by phosphoric acid chromate treatment, and the hydrophilic coating 10 b can use inorganic (water glass-based, boehmite-based), organic resin-based, and organic-inorganic composite-based coatings. In Embodiment 1, as the hydrophilic coating 10b, a coating formed of a composite coating of silica/resin, which is an organic-inorganic composite, is used by chemical conversion treatment.
另外,润滑性覆膜10c用于提高将翅片材料冲压加工成翅片1时的润滑性,在使用水溶性的覆膜时,由于在翅片1上产生的冷凝水而容易消失。因此,不会由于在上层形成的该润滑性覆膜10c而使亲水性覆膜10b的亲水性降低。In addition, the lubricating coating 10 c is used to improve the lubricity when the fin material is press-worked into the fin 1 , and when a water-soluble coating is used, it tends to disappear due to condensed water generated on the fin 1 . Therefore, the hydrophilicity of the hydrophilic coating 10b is not lowered by the lubricating coating 10c formed on the upper layer.
这样,如果以亲水性覆膜10b构成由多个层构成的覆膜层10的至少一层,则冷凝水沿着翅片表面平坦地蔓延。因此,能够抑制在相邻的翅片1之间等产生交联,并且如后述那样易于向槽部8引导冷凝水。In this way, if at least one layer of the coating layer 10 composed of a plurality of layers is constituted by the hydrophilic coating 10b, condensed water spreads flatly along the surface of the fin. Therefore, generation of cross-linking between adjacent fins 1 and the like can be suppressed, and condensed water can be easily guided to the groove portion 8 as will be described later.
接着,关于具有这种结构的本实施方式1的翅片管热交换器100,对排出附着于翅片1的冷凝水的动作、作用进行说明。Next, with regard to the fin-tube heat exchanger 100 of the first embodiment having such a structure, the operation and effect of discharging the condensed water adhering to the fins 1 will be described.
在此,图4表示作为本实施方式1的比较例的翅片管热交换器,没有形成槽部8的翅片1的平面图。此外,对槽部8以外的结构标注与本实施方式1的翅片1的各构成部件相同的参照符号并省略其说明。Here, FIG. 4 shows a plan view of the fin 1 in which the groove portion 8 is not formed in the fin-tube heat exchanger as a comparative example of the first embodiment. In addition, the structure other than the groove part 8 is attached|subjected with the same reference number as each component of the fin 1 of this Embodiment 1, and the description is abbreviate|omitted.
如图4所示,在没有形成槽部8的比较例的翅片管热交换器中,在翅片1中,特别是在导热管21的周围产生的冷凝水13沿着翅片1表面逐渐向重力方向下方流动。该冷凝水13在管周围部5和第二倾斜部7,不能越过与第一倾斜部6的边界部分的峰部3,而逐渐滞留。As shown in FIG. 4 , in the finned tube heat exchanger of the comparative example in which the groove portion 8 is not formed, the condensed water 13 generated in the fin 1 , especially around the heat transfer tube 21 gradually flows along the surface of the fin 1 . flow downward in the direction of gravity. The condensed water 13 gradually stagnates in the pipe peripheral portion 5 and the second slope portion 7 without passing over the peak portion 3 at the boundary portion with the first slope portion 6 .
当进一步产生冷凝水13时,滞留的冷凝水量增加,在相邻的翅片1之间产生交联,将翅片1之间堵塞。其结果是,通风阻力增大,并且用于与空气进行热交换的翅片的导热面积减少,导致能量效率的降低。When the condensed water 13 is further generated, the amount of retained condensed water increases, crosslinking occurs between adjacent fins 1 , and the space between the fins 1 is blocked. As a result, the ventilation resistance increases, and the heat transfer area of the fins for heat exchange with air decreases, resulting in a decrease in energy efficiency.
接着,使用图5说明本实施方式1的翅片1的冷凝水的排水作用。图5从左边起依次时序性地排列有(a)、(b)、(c)、(d)。首先,如图5(a)所示,在第一位置P1,当在第二倾斜部7开始滞留冷凝水13时,如图5(b)所示滞留的冷凝水被引导到与第二倾斜部7的重力方向下部连接的槽部8内,通过槽部8冷凝水被引导向与重力方向下方相邻的第二位置P2的第二倾斜部7。通过该槽部8产生的冷凝水的引导作用,冷凝水13从重力方向上方(第一位置P1)的管周围部5和第二倾斜部7向重力方向下方(第二位置P2)的管周围部5和第二倾斜部7输送(图5(c))。通过反复进行该槽部8产生的冷凝水的引导作用,将冷凝水13进一步向下方输送(图5(d))。Next, the drainage action of the condensed water in the fin 1 of the first embodiment will be described using FIG. 5 . 5 , (a), (b), (c), and (d) are sequentially arranged sequentially from the left. First, as shown in FIG. 5( a ), at the first position P1 , when the condensed water 13 starts to stagnate in the second inclined portion 7 , the stagnant condensed water is guided to the second inclined portion 7 as shown in FIG. 5( b ). In the groove part 8 connected to the lower part of the part 7 in the direction of gravity, the condensed water is guided by the groove part 8 to the second inclined part 7 at the second position P2 adjacent to the lower part in the direction of gravity. Condensed water 13 is guided from the tube peripheral part 5 and the second inclined part 7 above the gravity direction (first position P1) to the tube circumference below the gravity direction (second position P2) by the guide action of the condensed water generated by the groove part 8. Section 5 and the second inclined section 7 are conveyed (Fig. 5(c)). By repeating the guide action of the condensed water generated in the groove portion 8 , the condensed water 13 is further conveyed downward ( FIG. 5( d )).
这样,通过槽部8产生的冷凝水的引导作用,能够迅速地排出滞留于管周围部5和第二倾斜部7的冷凝水13,因此能够显著提高翅片1的排水性能。In this way, the condensed water 13 accumulated in the tube peripheral portion 5 and the second inclined portion 7 can be quickly discharged by the guiding function of the condensed water generated by the groove portion 8 , so that the drainage performance of the fin 1 can be remarkably improved.
此外,在本实施方式1中,以将在重力方向上相邻的第二倾斜部7之间相互连接的方式形成有槽部8,但是只要槽部8至少与形成于比导热管21更靠重力方向下部位置的第二倾斜部7相接,就能够向重力方向下方引导滞留在第二倾斜部7的冷凝水。Furthermore, in Embodiment 1, the grooves 8 are formed so as to connect the second inclined portions 7 adjacent in the direction of gravity to each other. When the second inclined portion 7 at the lower position in the direction of gravity is in contact with each other, the condensed water remaining on the second inclined portion 7 can be guided downward in the direction of gravity.
此外,在本实施方式1中,沿着由第一倾斜部6形成的峰部3的棱线平行地形成两个槽部8,但也可以是1个,还可以是3个以上。另外,本实施方式1中避开由第一倾斜部6形成的峰部3或谷部4的棱线地形成槽部8,但是也可以在这些棱线上使峰部3或谷部4进一步凹下而形成槽部。In addition, in the first embodiment, two grooves 8 are formed parallel to the ridgeline of the peak 3 formed by the first slope 6 , but there may be one groove 8 or three or more grooves. In addition, in the first embodiment, the grooves 8 are formed avoiding the ridgelines of the peaks 3 or valleys 4 formed by the first slope 6, but the peaks 3 or valleys 4 may be further formed on these ridgelines. Concave to form a groove.
此外,如图6所示,为了利用毛细管现象,槽部8的开口宽度尺寸L优选为2mm以下,为了进一步提高毛细管现象的效果,优选为0.5mm以下。通过采用这种开口宽度尺寸,能够大幅度提高槽部8产生的冷凝水13的引导作用。In addition, as shown in FIG. 6 , the opening width L of the groove portion 8 is preferably 2 mm or less in order to utilize the capillary phenomenon, and preferably 0.5 mm or less in order to further enhance the effect of the capillary phenomenon. By adopting such an opening width dimension, it is possible to significantly improve the guiding effect of the condensed water 13 generated in the groove portion 8 .
此外,图6所示的槽部8的形状,考虑到通过翅片1间的空气的通风阻力的降低,构成为侧面8a倾斜的形状,但如图7所示,侧面8a也可以垂直,另外也可以形成为相对的侧面8a在底部8b相接那样的尖形(V字形状)。In addition, the shape of the groove portion 8 shown in FIG. 6 is configured so that the side surface 8a is inclined in consideration of the reduction of the ventilation resistance of the air passing between the fins 1. However, as shown in FIG. 7, the side surface 8a may also be vertical. It may be formed in a pointed shape (V-shape) such that opposing side surfaces 8 a meet at bottom 8 b.
具有这种结构的本实施方式1的翅片1,通过对形成有覆膜层的基材进行冲压加工,可以同时成形第一倾斜部6、第二倾斜部7和槽部8。因此,不追加新的加工工艺,就可以制造廉价且排水性优异的翅片管热交换器。In the fin 1 of the first embodiment having such a structure, the first inclined portion 6 , the second inclined portion 7 , and the groove portion 8 can be simultaneously formed by pressing the base material on which the film layer is formed. Therefore, it is possible to manufacture an inexpensive fin-tube heat exchanger with excellent drainage without adding a new process.
(实施方式2)(Embodiment 2)
图8是本发明实施方式2的翅片管热交换器的翅片的平面图。此外,本实施方式2中,对与上述实施方式1相同的结构部分标注相同的参照符号,并省略其详细的说明。Fig. 8 is a plan view of the fins of the finned tube heat exchanger according to Embodiment 2 of the present invention. In addition, in this second embodiment, the same components as those in the above-mentioned first embodiment are given the same reference numerals, and their detailed descriptions are omitted.
本实施方式2与上述实施方式1的差异在于,在翅片1的峰部3附近设有槽部8。The second embodiment differs from the first embodiment described above in that grooves 8 are provided near the crests 3 of the fins 1 .
如图8所示,槽部8形成为沿着翅片1的峰部3将重力方向上相邻的第二倾斜部7之间连接。As shown in FIG. 8 , the groove portion 8 is formed to connect adjacent second inclined portions 7 in the gravity direction along the crest portion 3 of the fin 1 .
这种结构中,第二倾斜部7的重力方向的各个下端和槽部8的各个上端连接,因此能够将滞留在第二倾斜部7的冷凝水13顺畅地向下方引导。In such a structure, each lower end in the direction of gravity of the second inclined portion 7 is connected to each upper end of the groove portion 8, so that the condensed water 13 stagnant on the second inclined portion 7 can be smoothly guided downward.
(实施方式3)(Embodiment 3)
图9A是本发明实施方式3的翅片管热交换器的波纹翅片的平面图,图9B和图9C为剖面图。此外,本实施方式3中,对与上述实施方式1相同的结构部分标注相同的参照符号,并省略其详细的说明。9A is a plan view of corrugated fins of a finned tube heat exchanger according to Embodiment 3 of the present invention, and FIGS. 9B and 9C are cross-sectional views. In addition, in this Embodiment 3, the same reference numerals are assigned to the same components as in the above-mentioned Embodiment 1, and detailed description thereof will be omitted.
本实施方式3和上述实施方式1的差异在于,如图9B和图9C所示,翅片15形成为具有大致倒V字形的截面形状的波纹翅片这一点(即,翅片15中只形成一个峰部3)。The difference between this third embodiment and the above-mentioned first embodiment is that, as shown in FIG. 9B and FIG. 9C , the fins 15 are formed as corrugated fins having a substantially inverted V-shaped cross-sectional shape (that is, only one peak 3).
另外,如图9A所示,槽部8形成为沿着翅片15的峰部3将重力方向上相邻的第二倾斜部7之间连接。In addition, as shown in FIG. 9A , the groove portion 8 is formed to connect the adjacent second slope portions 7 in the direction of gravity along the crest portion 3 of the fin 15 .
通常,与M字形波纹翅片相比,V字形波纹翅片易于较大地形成表面积,且易于提高热交换性能。Generally, the V-shaped corrugated fin tends to have a larger surface area than the M-shaped corrugated fin, and tends to improve heat exchange performance.
另一方面,与M字形波纹翅片相比,V字形波纹翅片具有如下课题,即,由于平坦的管周围部5和第二倾斜部7的面积变大,冷凝水13的滞留区域变大,而易于冷凝水13滞留。On the other hand, compared with the M-shaped corrugated fin, the V-shaped corrugated fin has the problem that the stagnation area of the condensed water 13 becomes larger due to the larger area of the flat tube peripheral portion 5 and the second inclined portion 7 , and the condensed water 13 is easy to stay.
因此,如本实施方式3,通过设置槽部8,可以顺畅地向重力方向下方引导冷凝水13。因此,可以实现热交换性能高且排水性能也优异的V字形波纹翅片。Therefore, like the third embodiment, by providing the groove portion 8, the condensed water 13 can be smoothly guided downward in the direction of gravity. Therefore, a V-shaped corrugated fin having high heat exchange performance and excellent drainage performance can be realized.
上述说明中,以槽部8沿重力方向延伸的情况为例进行了说明,但槽部只要连续具有向重力方向下方的方向成分即可,例如也可以是相对于重力方向倾斜的情况或弯曲的情况。In the above description, the case where the groove portion 8 extends in the gravitational direction has been described as an example, but the groove portion only needs to continuously have a direction component downward in the gravitational direction, for example, it may be inclined or curved relative to the gravitational direction. Happening.
上述说明中,说明了通过在翅片表面设置槽部而能够提高附着于翅片表面的冷凝水的排水性的情况,但是除了冷凝水以外,还能够提高附着于翅片表面的液体的排出性。In the above description, the case where the drainability of the condensed water adhering to the fin surface can be improved by providing grooves on the fin surface has been described, but in addition to the condensed water, the drainability of liquid adhering to the fin surface can also be improved .
另外,上述说明中,以在与通过翅片管热交换器的空气之间进行热交换的情况为例进行了说明,但是也可以是空气以外的气体通过翅片管热交换器而在与该气体之间进行热交换那样的情况。In addition, in the above description, the case of exchanging heat with the air passing through the finned tube heat exchanger has been described as an example, but it is also possible that a gas other than air passes through the finned tube heat exchanger and is exchanged with the air. A case where heat is exchanged between gases.
此外,通过适当组合上述各种各样的实施方式中的任意实施方式,能够实现各自具有的效果。In addition, by appropriately combining any of the various embodiments described above, respective effects can be achieved.
本发明参照附图对优选的实施方式进行充分记载,但对该技术熟练的人而言,当然可以进行各种变形或修正。这种变形或修正只要不脱离添加的权利要求的本发明的范围,就应该理解为包含在本发明保护的范围之中。Preferred embodiments of the present invention have been fully described with reference to the accompanying drawings, but it is a matter of course for those skilled in the art that various modifications and corrections can be made. Such changes and corrections should be understood to be included in the scope of protection of the present invention as long as they do not depart from the scope of the present invention of the appended claims.
工业上的可利用性Industrial availability
如上述,本发明的翅片管热交换器能够通过设于翅片表面的槽部提高排水性,因此能够适用于空气调节装置、供热水装置、取暖装置等中使用的热交换器。As described above, the finned tube heat exchanger of the present invention can improve drainage by the grooves provided on the surface of the fins, so it can be applied to heat exchangers used in air conditioners, water heaters, heaters, and the like.
符号说明Symbol Description
1、15 翅片(波纹翅片)1, 15 fins (corrugated fins)
3 峰部3 peaks
4 谷部4 Tanibe
5 管周围部5 around the tube
6 第一倾斜部6 first slope
7 第二倾斜部7 Second inclined part
8 槽部8 slots
9 基材9 Substrate
10 覆膜层10 coating layer
10a 耐腐蚀性覆膜10a Corrosion Resistant Coating
10b 亲水性覆膜10b Hydrophilic coating
10c 润滑性覆膜10c Lubricious coating
13 冷凝水13 Condensate
21 导热管21 heat pipe
100 翅片管热交换器100 Fin Tube Heat Exchanger
P1 第一位置P1 first position
P2 第二位置P2 second position
S 空气的流动方向S Air flow direction
L 开口部的开口宽度尺寸L Opening width dimension of the opening
Claims (5)
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JP2012-097380 | 2012-04-23 | ||
PCT/JP2013/002710 WO2013161263A1 (en) | 2012-04-23 | 2013-04-22 | Fin tube heat exchanger and method for manufacturing same |
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CN103857974B true CN103857974B (en) | 2018-03-16 |
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JP (1) | JP6128492B2 (en) |
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JP6449032B2 (en) * | 2015-01-28 | 2019-01-09 | アクア株式会社 | COOLER, MANUFACTURING METHOD THEREOF, AND REFRIGERATOR HAVING THE COOLER |
CN106066133A (en) * | 2016-06-22 | 2016-11-02 | 上海和衡能源科技发展有限公司 | Single-tube fin type heat exchanger and assembling thereof |
DE102017120124A1 (en) * | 2017-09-01 | 2019-03-07 | Miele & Cie. Kg | Finned tube heat exchanger |
DE102017120123A1 (en) * | 2017-09-01 | 2019-03-07 | Miele & Cie. Kg | Finned tube heat exchanger |
CN108613232B (en) * | 2018-05-28 | 2024-08-30 | 广东美的厨房电器制造有限公司 | Heat exchanger for refrigerating cigarette machine and refrigerating cigarette machine with heat exchanger |
CN111981583B (en) * | 2020-08-14 | 2021-12-07 | 青岛海信日立空调系统有限公司 | Outdoor unit of air conditioner |
CN114526614B (en) * | 2022-02-28 | 2023-12-15 | 四川奥格莱能源科技有限公司 | High-temperature high-pressure multi-tube condensing type steam heat exchanger |
JP7436895B1 (en) | 2022-08-12 | 2024-02-22 | ダイキン工業株式会社 | Heat exchanger |
KR20240115602A (en) * | 2023-01-19 | 2024-07-26 | 엘지전자 주식회사 | Heat exchanger |
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- 2013-04-22 EP EP13781866.2A patent/EP2843346B1/en active Active
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WO2013161263A1 (en) | 2013-10-31 |
EP2843346A1 (en) | 2015-03-04 |
JP6128492B2 (en) | 2017-05-17 |
JPWO2013161263A1 (en) | 2015-12-21 |
CN103857974A (en) | 2014-06-11 |
EP2843346B1 (en) | 2018-12-26 |
EP2843346A4 (en) | 2015-06-03 |
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