TW200301815A - Heat exchanger for providing supercritical cooling of a working fluid in a transcritical cooling cycle - Google Patents
Heat exchanger for providing supercritical cooling of a working fluid in a transcritical cooling cycle Download PDFInfo
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- TW200301815A TW200301815A TW091133260A TW91133260A TW200301815A TW 200301815 A TW200301815 A TW 200301815A TW 091133260 A TW091133260 A TW 091133260A TW 91133260 A TW91133260 A TW 91133260A TW 200301815 A TW200301815 A TW 200301815A
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- 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
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/02—Tubular elements of cross-section which is non-circular
- F28F1/022—Tubular elements of cross-section which is non-circular with multiple channels
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- 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
- F28D1/0477—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 the conduits being bent in a serpentine or zig-zag
- F28D1/0478—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 the conduits being bent in a serpentine or zig-zag the conduits having a non-circular cross-section
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/02—Tubular elements of cross-section which is non-circular
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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
- 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
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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
- 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
- F28F1/126—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 consisting of zig-zag shaped fins
- F28F1/128—Fins with openings, e.g. louvered fins
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- 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
- F25B2309/00—Gas cycle refrigeration machines
- F25B2309/06—Compression machines, plants or systems characterised by the refrigerant being carbon dioxide
- F25B2309/061—Compression machines, plants or systems characterised by the refrigerant being carbon dioxide with cycle highest pressure above the supercritical pressure
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- 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
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/002—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
- F25B9/008—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being carbon dioxide
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- 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
- F28D2021/0073—Gas coolers
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- 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)
Abstract
Description
200301815 ⑴ 玖、發明說明 月應敘月.發明所屬之技術領域、先前技術、内容、實施方式及圖式簡單說 發明範圍 >本I月係有關於一種熱交換器’且更明確地係一種在跨 臨界冷心;!壞巾提供玉作流體超臨界冷卻之教交換哭。 發明背景 ' 一種常見型式之熱交換器包括由複數個管件及複數個互 連二熱片組成之一所謂「核心部」。一流體係通過該核心部 之官件,而一第二流體則在該等散熱片與該等管件之間的 空間中通過該核心部本身。典型地,該等管件之相對末端 係❹至-平行歧管或「槽體」,且其中—該等歧管係一輸 入歧管,而另一歧管則為一輸出歧管,以分別將其中一該 等流體導引入與導引出該等管件。 該-般型熱交換器可用於譬如散熱器、凝結器、蒸發器 、充氣冷卻器(charge air cooler)、冷油器等多種用途,且 該等者皆可在車輛中使用。該型熱交換器之一共同型式係 已知的一平行流熱交換器,其中複數個扁平、多孔式管件 係將-冷媒導引通過該熱交換器。典型地,該等扁平管件 係呈筆直’且該等歧管係在該熱交換器之相對側端上互相 間隔,以接收該等管件之相對末端。然而,已知將該等扁 平管件弯曲,使得每-該等管件皆成型為具有兩平行腿的 -所謂「髮失型」管件,且其中該輪入與輸出歧管係定位 成互相鄰近,以接收該等管件之末端。發證予H〇shin〇等之 美國專利案第5,531,268號中已顯示出這種結構。儘管第 5,53 1,268號專利案中所示之結構可適用於其目的,但仍有 (2) (2)200301815 改良空間。更,該結構並不適用於或最適宜使用於依靠_ 較高操作壓力之某些空調系統中,該等系統係譬如為需要 用於提供超臨界冷卻二氧化碳(c〇2)等冷媒之一氣體冷卻 器的一跨臨界冷卻循環。 由於使用譬如CFC12及影響程度較小之HFC134a等許多 白知冷媒所造成的環境問題不斷增加,已導致需考慮跨臨 界二氧化碳系統,且特別在車輛應用中尤然。首先,在這 種糸統中作為一冷媒使用之二氧化碳係在初始時自大氣中 取待因此备其自該系統洩漏回大氣時,將不致使大氣中 一氧化奴含I淨增加。此外,儘管由溫室效應的觀念而言 ’亚不歡迎二氧化碳,由於不致因洩漏而使大氣中二氧 化碳含量淨增加,因此將不會影響臭氧層且不致增強溫室 效應。 發明概要 本毛月之主要目的係提供一種新穎且改良的熱交換器。 本發明之另-目的係提供一種改良交換器,其適用於在 一跨臨界冷卻循環中,超臨界冷卻-工作流體。 7 ,發^之一說明用具體實施例可藉一種在一跨臨界冷卻 循%中提供一工作流體超臨界冷卻的熱交換器,來達成至 ^某些别述目的。該熱交換器包括一對細長型管集箱,其 具有大體上互相平行設置之縱向軸,複數個細 , 沿著該箄營隹f —^目之縱向軸而以側邊對側邊之關係互相間隔 ,其中母一該等管件本身皆向上彎摺以界定該管件之至少 兩平行腿’使得該工作流體自其中一該等管集箱至另一個 (3) 200301815200301815 ⑴ 玖, the description of the invention shall be described in the month. The technical field to which the invention belongs, the prior art, the content, the embodiments and the drawings briefly describe the scope of the invention > This month is about a heat exchanger 'and more specifically a In transcritical cold heart ;! Bad towels provide a cry for teaching exchange of supercritical cooling of jade fluid. BACKGROUND OF THE INVENTION '' A common type of heat exchanger includes a so-called "core portion" consisting of a plurality of tubes and a plurality of interconnected two heat fins. The first-class system passes through the core parts, and a second fluid passes through the core itself in the space between the fins and the pipes. Typically, the opposite ends of these fittings are ❹-parallel manifolds or "slots", and where-the manifolds are an input manifold and the other manifold is an output manifold to separate the One of these fluid guides leads in and out of the pipes. The general heat exchanger can be used for various purposes such as radiators, condensers, evaporators, charge air coolers, oil coolers, etc., and these can be used in vehicles. One common type of this type of heat exchanger is a known parallel flow heat exchanger, in which a plurality of flat, porous tubes guide the refrigerant through the heat exchanger. Typically, the flat tubes are straight 'and the manifolds are spaced from each other on opposite side ends of the heat exchanger to receive the opposite ends of the tubes. However, it is known to bend these flat fittings such that each of these fittings is formed into a so-called "lost-type" fitting with two parallel legs, and wherein the wheel-in and output manifolds are positioned adjacent to each other to Receive the ends of these fittings. This structure is shown in U.S. Patent No. 5,531,268 issued to Hoshin, et al. Although the structure shown in Patent No. 5,53 1,268 is applicable to its purpose, there is still room for improvement (2) (2) 200301815. In addition, this structure is not suitable or most suitable for use in certain air-conditioning systems that rely on high operating pressures. These systems are, for example, one of the refrigerants required to provide supercritical cooling carbon dioxide (CO2). A transcritical cooling cycle of the cooler. The increasing environmental problems caused by the use of many white refrigerants such as CFC12 and HFC134a, which has a lesser impact, have led to the need to consider transboundary carbon dioxide systems, especially in vehicle applications. First of all, the carbon dioxide used as a refrigerant in this system is initially taken from the atmosphere, so when it is leaked back to the atmosphere from the system, it will not cause a net increase in nitric oxide in the atmosphere. In addition, although carbon dioxide is unwelcome from the perspective of the greenhouse effect, it will not affect the ozone layer and will not enhance the greenhouse effect because it does not cause a net increase in the carbon dioxide content in the atmosphere due to leakage. SUMMARY OF THE INVENTION The main object of the present invention is to provide a novel and improved heat exchanger. Another object of the present invention is to provide an improved exchanger suitable for supercritical cooling-working fluid in a transcritical cooling cycle. 7. One of the instructions indicates that a specific embodiment can be used to achieve some of the other objectives by using a heat exchanger that provides supercritical cooling of the working fluid in a transcritical cooling cycle%. The heat exchanger includes a pair of elongated tube headers having longitudinal axes arranged substantially parallel to each other, and a plurality of thin, along side-to-side relationships along the longitudinal axis of the 箄 f 箄 ^^ mesh. Spaced from each other, where the mother-of-pipe fittings are bent upwards to define at least two parallel legs of the pipe-fitting, such that the working fluid flows from one of the pipe headers to the other (3) 200301815
七績地流通過至少兩平扞s β4 及歿數個蛇紋式彎曲散熱 月’在相鄒之成對該等管侔 Η比日士 τ — 件之間延伸,其中每一該等散熱 …I::、”τ於該等相鄰管件平行腿延伸的-身長。每一 该等管件皆具有一扁立,丨& “有料剖面’且該剖面具有一長尺寸及一 :二母-該"件平行腿之長尺寸係位於與該等管集 σ / A a i k ^又的—共同平面中。每-該等管件 白具有連接至其中一該等 H 木相之弟一末端,及連接至Qichi Earthly Flow passes through at least two levels of protection s β4 and several snake-shaped curved heat dissipation months' extending between Xiang Zou Zhicheng and these pipes, Bi Ri Shi τ — each of these heat dissipation ... I :: "" Τ extends parallel to the legs of these adjacent fittings-the length. Each of these fittings has a flat, "&" material section "and the section has a long dimension and one: two female-the" The lengths of the parallel legs of the pieces are located in a common plane with the tube sets σ / A aik ^ and. Each-the fittings have one end connected to one of the H wood phases, and connected to
s -相之-第二末端,以使該工作流體在該 之間轉移。 -型式t ’每—料蛇紋式彎曲散熱片皆具有橫跨該 相鄰官件平行腿延伸的一橫向寬度。每一該等散埶片皆 括平行於該等平行腿延伸的複數個交錯翼片及細長型分1 牛且^等翼片及分離件係設於該等相鄰管件平行腿之j 以將母一該等散熱片寬度分割成藉由該等翼片而互相〗 接之複數個離散的散熱片元件。每_該等散熱片元件皆js-phase-second end to transfer the working fluid between the two. The pattern t 'each has a serpentine curved heat sink having a lateral width extending across the parallel legs of the adjacent member. Each of these scattered pieces includes a plurality of staggered fins and elongated points extending parallel to the parallel legs, and the fins and separators are provided on the parallel legs of the adjacent pipe pieces to The width of the female heat sink is divided into a plurality of discrete heat sink elements connected to each other by the wings. Each of these heat sink components is j
母一該等相鄰管件之其中—該等平行腿相對應且沿著❸ 伸0 型式中,每一該等管件之平行腿係互相間隔。 一里式中,每一該等管件本身皆向上彎摺至少兩次,丄 疋義4 g件之至少二個平行腿,使得該工作流體連續地支 k自某、名等官集粕至另一個的三平行流體通道。 型式中,每一該等管件皆為一多孔式管件,且該管4 具有範圍介於〇·〇15英吁至G._英对内的—液壓直後。 ^式中,每一該等管件之長尺寸係不超過0.500英吋 -10- (4) 200301815One of the two adjacent pipe fittings-the parallel legs corresponding to and extending along the 00 type, the parallel legs of each of these pipe fittings are spaced from each other. In one mile type, each of these pipe fittings is bent upwards at least twice, meaning at least two parallel legs of a 4 g piece, so that the working fluid continuously supports k from a certain official name to another Three parallel fluid channels. In the type, each of these pipe fittings is a porous pipe fitting, and the pipe 4 has a hydraulic pressure ranging from 0.015 to G._English pair. ^ In the formula, the length of each such fitting is not more than 0.500 inches -10- (4) 200301815
且其短尺寸係不超過0.100英时。 片 一型式中’每-該等散熱片皆具有自某 一相鄰該等管件、且平行於該等管集箱縱向:延二至 =高度’並且該等管件之長尺寸係不超過該 一型式中,每一該等管件之具 長尺寸ίτ、在該管件末端 至該管集箱處、與該等管集箱之縱向軸平行地延伸。 由以下結合了隨附圖式之說明書,將可明白其他目的 優點。 圖式之簡單說明 冷卻糸 圖1係包括有具體實施本發明之一熱交換器的 統概略正視圖; 圖2係圖1所示之熱交換器的正視圖; 圖3係圖2所示之熱交換器的側視圖; 圖4係圖2所示之熱交換器的上視圖; 圖5係沿圖3中線5-5截取之放大、局部剖面; 圖6係應用於圖丨至圖5所示熱交換器之一管件的放大、局 交換器中所利用的 圖7係顯示在具體實施本發明之一熱 一管件及一散熱片透視圖。 較佳具體實施例說明 、參考圖1 ’其顯示出關於產生一跨臨界冷卻循環之一基本 冷卻系統12、且具體實施本發明的一熱交換器1〇。圖=之 熱交換器1〇係呈一氣體冷卻器13型式,其可藉由在熱交換 200301815And its short size is not more than 0.100 inches. In the type of sheet one, 'each-the fins have from one of the adjacent pipe fittings and are parallel to the longitudinal direction of the headers: two to = height' and the length of the pipe fittings does not exceed that one. In the type, each of these pipe fittings has a long dimension τ, extending from the end of the pipe fitting to the pipe header, parallel to the longitudinal axis of the pipe header. Other purposes and advantages will become apparent from the following description combined with the accompanying drawings. Brief Description of Drawings Cooling: Figure 1 is a schematic front view of a heat exchanger embodying the present invention; Figure 2 is a front view of the heat exchanger shown in Figure 1; Figure 3 is a view of Figure 2 Side view of the heat exchanger; Figure 4 is a top view of the heat exchanger shown in Figure 2; Figure 5 is an enlarged, partial section taken along the line 5-5 in Figure 3; Figure 6 is applied to Figures 丨 to 5 FIG. 7 is an enlarged view of a tube of a heat exchanger shown and used in a local exchanger. FIG. 7 shows a perspective view of a tube and a heat sink in the embodiment of the present invention. Description of the preferred embodiment, with reference to Fig. 1 ', which shows a basic cooling system 12 for generating a transcritical cooling cycle and a heat exchanger 10 embodying the present invention. Figure = The heat exchanger 10 is a gas cooler type 13, which can be used in heat exchange 200301815
(5) 器Η)散熱片側上,將熱排放至譬如一空氣流A等一介質中, 而提供冷卻系統12之譬如二氧化碳等工作流體或冷媒超臨 界冷卻。冷卻系統12包括熱交換器1〇,將氣態冷媒壓縮至 超臨界£力以運送至熱父換态i 〇的一壓縮機Μ,將接收 自熱交換器10之冷媒的壓力降低而使得至少某些冷媒進入 液態的-膨脹裝置16,將熱自某一介質轉移至冷媒中以使 該冷媒自液態轉變成氣態的一蒸發器17,一積f器18(選擇 性地),以及將熱自排出熱交換器10之冷媒中轉移至排出蒸 發益1 7之冷媒中、或倘若有使用積蓄器丨8時亦轉移至其中 的一吸引管路熱交換器19。應了解到,熱交換請可在其 他型式之冷卻系統中、及實施一跨臨界冷卻循環之其他冷 部系統配置中發現用途,且並非以結合圖丨所示之特定冷卻 糸統使用為限,除非申請專利範圍中有特別提及以外。更 ,儘管揭露之熱交換器10作為一氣體冷卻器13用時可提供 顯著優點,然當用作譬如一凝結器或一蒸發器等其他用途 時亦可展現其優點,而不論其是否關於一跨臨界冷卻循環 使用。 參考圖2至圖4,熱交換器1〇包括一對細長型管狀之管集 箱-0及22,其分別具有縱向軸24與26且大體上互相平行地 0又豆,複數個細長型管件28 ,以側邊對側邊之關係沿著管 市相20、22之縱向軸24、26互相間隔;以及複數個蛇紋式 ’考曲散熱片30,在相鄰之成對管件28之間延伸。應了解到 在圖式顯示之具體實施例中,每一散熱片3 〇皆延伸管件 28之一身長L,但圖2中為了方便解說而並未顯示出該等身 200301815(5) Device ii) On the side of the heat sink, the heat is discharged to a medium such as an air flow A, and the working system 12 such as carbon dioxide or a cooling medium of the cooling system 12 is provided with ultra-critical cooling. The cooling system 12 includes a heat exchanger 10, which compresses a gaseous refrigerant to a supercritical pressure to be transported to a compressor M of the thermal parent state i 0, and reduces the pressure of the refrigerant received from the heat exchanger 10 such that at least some These refrigerants enter the liquid-expansion device 16, an evaporator 17, an evaporator 18 (optionally) that transfers heat from a medium to the refrigerant to change the refrigerant from a liquid state to a gaseous state, and The refrigerant discharged from the heat exchanger 10 is transferred to the refrigerant discharged from the evaporation evaporator 17 or, if an accumulator 8 is used, it is also transferred to one of the suction pipe heat exchangers 19. It should be understood that the use of heat exchange can be found in other types of cooling systems and other cold section system configurations that implement a transcritical cooling cycle, and is not limited to the use of the specific cooling system shown in Figure 丨. Unless specifically mentioned in the scope of the patent application. Moreover, although the disclosed heat exchanger 10 can provide significant advantages when used as a gas cooler 13, its advantages can also be exhibited when used as other uses such as a condenser or an evaporator, regardless of whether it is related to a Transcritical cooling cycle. Referring to FIGS. 2 to 4, the heat exchanger 10 includes a pair of elongated tube headers-0 and 22, respectively having longitudinal axes 24 and 26 and substantially parallel to each other, and a plurality of elongated tube pieces. 28, spaced side-to-side along the longitudinal axis 24, 26 of the tube city phase 20, 22; and a plurality of serpentine 'coqu heat sinks 30, extending between adjacent pairs of pipe pieces 28 . It should be understood that in the specific embodiment shown in the figure, each heat sink 30 extends one of the length L of the tube member 28, but the body is not shown in FIG. 2 for convenience of explanation.
(6) 長之中間部份。較佳地,散熱片3〇係具有放氣孔。如圖3 中所示,每一管件28皆具有連接至管集箱20的一第一末端 31,以及連接至管集箱22的一第二末端32,以在管集箱2〇 與22之間轉移冷媒。 每一官件28皆具有一扁平剖面,且該剖面具有一長尺寸〇 及一短尺寸d,如圖5最清楚地顯示。每一管件28較佳地皆 為一多孔式官件,且在極佳具體實施例中為具有範圍介於 〇.〇 15英吋至0.045英吋之一液壓直徑的一多孔式管件。就此 而淪’應了解到,儘管圖5中係顯示六個孔口 34,但在某些 應用中,每一多孔式管件28皆包括超過、或少於六個孔口 34者可能較為有利。譬如,在一較佳具體實施例中,每一 該等管件皆具有四個孔口 34。在一較佳具體實施例中,該 等官件係配置成,可在環境7〇卞時抵抗至少65〇〇英磅/平方 英吋(ps〇的爆裂壓力,此即作為一跨臨界二氧化碳冷卻系 統中之一氣體冷卻器時所需者。 較佳地,每一管件28之長尺寸〇一般不超過〇5〇〇英吋, 且短尺寸d—般不超過〇」00英吋,而在某些極佳具體實施 例中,短尺寸d—般係不超過〇.〇6〇英吋,且長尺寸D一般係 不超過0^20英吋。就此而論,減少長尺寸D可提供眾多優 點。譬如,由於每一管件28皆包括至少兩平行腿36,因此 熱父換為10之深度將高度地依據長尺寸D之大小並且將隨 著長尺寸D之減少而縮小。更,管集箱2〇、22之直徑可在管 件末纟而3 1、j2長尺寸D係與管集箱2〇、22縱向軸24、26橫向 父叉地延伸的一結構、而非圖丨至圖4所示之平行結構中減 -13- 200301815 少’且其中該長尺寸與該等縱向軸係在末端31、32連接至 官集箱20、22處橫向交又。此外,管集箱2〇、”之身長可 在譬如圖1至圖4中所示之管件末端3卜32長尺寸D平行管 集箱20、22縱向軸24、26延伸的一結構中減小。最後,在 某些較佳具體實施财,長尺寸_小可允許散熱#高度縮 小。然而應了解到’較大之散熱片高度可提供關於空氣側 效率之優點。 如圖3、圖4、及圖6中最清楚地顯示,每一管件2δ本身皆 向上彎摺,以界定至少兩個管件28平行腿%,使得冷媒自 管集箱20經由至少兩個平行流體通道38連續地流動至管集 箱22。就此而論,最好選擇輸入及輸出管集箱“、22,使 得當熱交換器10作為一氣體冷卻器時,其將以相對於熱交 換器10散熱片側上流體流動之一交又_逆流配置操作。每一 對平行腿皆藉由在一彎摺點39處相對於腿部36扭轉9〇。之 泫考摺點39而接合,使得長尺寸D在彎摺點39處與軸%、 平行而非橫向交叉地延伸。較佳地,彎摺點39係藉由先在 彎摺點39處相對於管件28部扭轉腿部36 9〇。、接著再於彎摺 點39處彎曲該管件大約ι8〇。形成彎摺點%,而得形成。就 此而論,應了解到,每一腿36相對於彎摺點39之9〇。扭轉係 依據何種配置可提供熱交換器1〇特殊應用最多優點,而為 圖3及圖6中之相同方向或相反方向。如圖6中最清楚地顯示 ,每一管件28之平行腿36較佳地係互相間隔一距離χ,且該 距離係與每一平行腿%之長尺寸D位於一共同平面中,其中 該共同平面係在圖2及圖5中以虛線Ρ表示且與管集箱2〇、22 -14- 200301815 ⑻ 之縱向軸24、26大體上橫向交又。如此將允許長尺寸β盘介 質通過散熱片30之流動方向平行地延伸。由於冷媒之溫度 可隨著其自管集箱20經由管件28流動至另_管集箱22 = 體上改變,因此當熱交換器1〇正在提供超臨界冷卻時,藉 由間隔X來減少由某一腿36至另—個之熱傳導將屬較㈣ k佳地,可藉由銅焊材料,使距離χ在銅焊埶交換哭1 〇 期間足以防止相鄰平行腿%之間的空間閉合或㈣^最 小化’但不致於太大而過度地增加熱交換器Μ之深度。作 管每:管件28之相鄰平行腿36最好互相間隔,但在某些: 用中並不需要及/或不希望有該間隔。 如圖1至圖5所示’每一散熱片3〇皆具有相同於相鄰管件 28之間間隔的-散熱片高度H,亦即_散熱片高度η係自其 中-管件28平行於管集箱2〇、22縱向軸24、观延伸至— 相鄰管件28。較佳地,管件28之長尺寸〇不可超過散執片高 度Η。這將允許每-管件末端3卜32可相對於平行㈣扭轉 90。且該等管件末端將由此開始延伸的—結構,使得末端Η 、32之長尺寸Dm巾所示者,在管件末端Μ及η與管 集箱20及22相連接之處、平行於管集箱2()、22縱向韩^、 26延伸。這在譬如用於跨臨界冷媒系統中之氣體冷卻器等 高壓力應用中非常重要,其中係希望管集箱2〇、22之直徑 儘可π地小。&種結構中之長尺寸〇係'可預期地、甚至恰好 地大於任-管集箱20、24之内徑。藉由允許長尺寸D在管件 末端3 1、32與管集箱2G、22相連接處平行於管集箱2〇、22 縱向軸24、26延伸,每一管件28之長尺寸!)將可大於任一管 (9) (9)200301815(6) The middle part of the length. Preferably, the heat sink 30 has a vent hole. As shown in FIG. 3, each of the tube pieces 28 has a first end 31 connected to the tube header 20 and a second end 32 connected to the tube header 22 so as to be between the tube headers 20 and 22. Transfer refrigerant from time to time. Each member 28 has a flat cross section, and the cross section has a long dimension 0 and a short dimension d, as shown most clearly in FIG. 5. Each tube member 28 is preferably a perforated official member, and in a preferred embodiment is a perforated tube member having a hydraulic diameter ranging from 0.015 inch to 0.045 inch. It should be understood that although six orifices 34 are shown in FIG. 5, in some applications, it may be advantageous for each porous tube 28 to include more than or less than six orifices 34. . For example, in a preferred embodiment, each of these fittings has four orifices 34. In a preferred embodiment, the parts are configured to withstand a burst pressure of at least 6500 pounds per square inch (ps0) at an ambient temperature of 70 °, which is referred to as a transcritical carbon dioxide cooling. Required for one of the gas coolers in the system. Preferably, the length of each tube 28 is generally not more than 0500 inches, and the short dimension d is generally not more than 0 "00 inches. In some excellent embodiments, the short dimension d is generally not more than 0.060 inches, and the long dimension D is generally not more than 0 ^ 20 inches. In this regard, reducing the long dimension D may provide a large number of Advantages. For example, since each tube 28 includes at least two parallel legs 36, changing the depth of the hot parent to 10 will highly depend on the size of the long dimension D and will decrease as the long dimension D decreases. Furthermore, the tube set The diameter of the boxes 20 and 22 can be at the end of the pipe, and the length of the long dimension D1 and j2 is a structure that extends longitudinally from the longitudinal axis 24 and 26 of the pipe header 20, 22, instead of the figure 丨 to FIG. 4 -13-200301815 less in the parallel structure shown, and wherein the long dimension is at the ends 31, 32 with the longitudinal axes It connects to the official header box 20 and 22 at the intersection. In addition, the length of the tube header box 20, "can be at the end of the pipe as shown in Fig. 1 to Fig. 4 32 long D parallel tube header box 20, 22 The length of the longitudinal axis 24, 26 is reduced in a structure. Finally, in some preferred implementations, the long size_small may allow heat dissipation # the height is reduced. However it should be understood that 'larger heat sink heights can provide information about Advantages of air-side efficiency. As shown most clearly in Figs. 3, 4, and 6, each tube 2δ itself is bent upwards to define at least two tube pieces 28 parallel legs%, so that the refrigerant from the tube header 20 Continuously flows to the header manifold 22 via at least two parallel fluid channels 38. In this connection, it is better to select the input and output header headers ", 22", so that when the heat exchanger 10 is used as a gas cooler, it will The fluid flow on the fin side of the heat exchanger 10 is intersected _ countercurrent configuration operation. Each pair of parallel legs is twisted 90 relative to the leg 36 at a bend point 39. The test point 39 And the joint is made, so that the long dimension D is parallel to the axis at the bending point 39, and is not horizontal. Extending crosswise. Preferably, the bending point 39 is obtained by first twisting the leg portion 36 9 at the bending point 39 relative to the tube 28, and then bending the tube at the bending point 39 by about 80. The bending point% is formed, and it must be formed. In this connection, it should be understood that each leg 36 is 90% of the bending point 39. According to what configuration the torsion system can provide the heat exchanger 10 with the most advantages for special applications, 3 and FIG. 6 are the same or opposite directions. As shown most clearly in FIG. 6, the parallel legs 36 of each tube 28 are preferably spaced a distance χ from each other, and the distance is parallel to each The length D of the leg% is located in a common plane, which is indicated by the dashed line P in FIG. 2 and FIG. 5 and is substantially the same as the longitudinal axis 24, 26 of the header box 20, 22 -14- 200301815 ⑻. Crosswise again. This will allow the long beta disk medium to extend in parallel through the flow direction of the heat sink 30. Since the temperature of the refrigerant can be changed as it flows from the header 20 to the header 22 through the tube 28, when the heat exchanger 10 is providing supercritical cooling, the distance X is reduced by The heat conduction from one leg to the other will be better. The brazing material can be used to make the distance χ during the brazing welding exchange for 10, which is sufficient to prevent the space between the adjacent parallel legs% from closing or ㈣ ^ Minimize 'but not too large and excessively increase the depth of the heat exchanger M. The adjacent parallel legs 36 of the tube members 28 are preferably spaced apart from each other, but in some applications this spacing is not required and / or undesirable. As shown in Figures 1 to 5, 'Each fin 30 has the same distance between the adjacent fins 28-the fin height H, that is, the fin height η is from it-the fins 28 are parallel to the tube set. Boxes 20, 22 longitudinal axes 24, 28 extend to-adjacent pipe 28. Preferably, the length 0 of the tube member 28 should not exceed the height of the loose piece Η. This will allow each end of the tube 3 to 32 to be twisted 90 relative to the parallel cymbal. And the ends of these pipe fittings will begin to extend from this-the structure, so that the ends Η, 32 of the long size Dm towels, shown at the ends of the pipe fittings M and η and the pipe headers 20 and 22 are parallel to the pipe header 2 (), 22 vertical Han ^, 26 extended. This is very important in high pressure applications such as gas coolers used in transcritical refrigerant systems, where it is desirable that the headers 20, 22 have a diameter as small as possible. & The long dimension 0 in the structure is' expectedly, even just larger than the inner diameter of the Ren-tube header 20,24. By allowing the long dimension D to extend parallel to the longitudinal headers 24, 26 of the headers 20, 22 at the ends of the headers 3 1, 32 and the headers 2G, 22, the length of each header 28! ) Will be larger than any tube (9) (9) 200301815
集相20、22之内徑。儘管管件末端31、32之長尺寸〇最好在 管件末端3i、32與管集箱20、22相連接處平行於管集箱2〇 、22縱向軸24、26延伸,但在某些應用中,長尺+ D在該等 位置處具有其他方位者可能較優。譬如,在某些應用中, &件末端31、32之長尺寸D在管件末端31、32與管集箱⑼ 、22相連接處,最好與縱向軸以、%橫向交叉地延伸。 如上述之討論,每一蛇紋式彎曲散熱片3〇皆具有平行於 相鄰管件28平行腿36延伸的_身長L,以及如圖钟最清楚 顯示出之橫跨相鄰管件28平行腿36延伸的一橫向寬度w。 為I方便解說,圖5係顯示出管件28之三個腿部%且圖玲 顯不出結合一熱交換器結構1〇使用的一散熱片3〇,豆中每 一管件28僅具有兩平行腿36。請參考圖7,每一散熱片3〇 皆包括平行於平行腿36延伸且位於㈣管㈣平行腿此 間的複數個交錯翼片懈細長型分離件42,以將每一散熱 片30之見度W刀割成藉由翼片4〇而互相連接的兩個或更多 離散的散熱片細長條或元件44。每一散熱片元件料係盘每 :相鄰管件28之其中—平行腿36相對應且沿著其延伸。分 離件42係呈大致筆直線且具有互相面對之相對邊緣心,並 且與介質流動通過散熱片說方向大致橫向交叉。儘管圖7 中係顯不出’具有兩平行腿36之管件28所使用之散熱片3〇 ’然而應了解到,上述中包括翼片40、分離件42、及散熱 ^元件44之結構可運用於譬如圖2至圖5所示之結構等每二 :件28皆具有超過兩個平行腿36的熱交換器10結構中。在 這種結構中,每—散熱片30較佳地係橫跨所有平行腿36延 -16- (10) (10)200301815Collector inner diameter of 20,22. Although the long dimensions of the end 31, 32 of the fitting 〇 preferably extend parallel to the longitudinal axis 24, 26 of the header 20, 22 where the end 3i, 32 of the fitting is connected to the header 20, 22, but in some applications , Long ruler + D with other orientations at these positions may be better. For example, in some applications, the long dimension D of the end pieces 31, 32 is at the junction of the end pieces 31, 32 and the headers ⑼, 22, and preferably extends transversely to the longitudinal axis by%. As discussed above, each serpentine curved heat sink 30 has a length L that extends parallel to the parallel legs 36 of the adjacent tube 28, and extends across the parallel legs 36 of the adjacent tube 28 as best shown in the clock A lateral width w. For the convenience of explanation, FIG. 5 shows three leg portions of the tube 28 and Tu Ling does not show a heat sink 30 used in combination with a heat exchanger structure 10. Each tube 28 in the bean has only two parallel Legs 36. Please refer to FIG. 7, each heat sink 30 includes a plurality of staggered fins 42 extending parallel to the parallel legs 36 and located between the parallel legs of the stern tube, so as to provide visibility of each heat sink 30. The W-blade is cut into two or more discrete fin strips or elements 44 interconnected by the fins 40. Each of the heat sink element materials is arranged in parallel to each of the adjacent tube pieces 28-parallel legs 36 and extends along it. The separating member 42 is substantially straight and has opposite edge centers facing each other, and substantially crosses the direction in which the medium flows through the heat sink. Although FIG. 7 does not show 'the heat sink 30 used for the pipe member 28 having two parallel legs 36', it should be understood that the structure including the fin 40, the separation member 42, and the heat dissipation element 44 in the above can be used. For example, in the structure shown in FIG. 2 to FIG. 5, every two: two pieces 28 each have a structure of the heat exchanger 10 having more than two parallel legs 36. In this structure, each fin 30 is preferably extended across all parallel legs 36 -16- (10) (10) 200301815
伸,而一散熱片元件44係對應於每一相鄰管件28之每一平 行腿36且沿著其延伸,並且翼㈣及分離料係設於每一 散熱片元件44之間。 每-散熱片30中之交錯翼片4〇係用於限制散熱片元件料 互相相對運動,使得在組立熱交換器1〇期間,每一散熱片 元件30仍保持為-單體式組件,且更加地係將散熱片元件 44保持互相對正,以減少該熱交換器散熱片側上之壓力降 。使用細長型分離件42之目的係藉由中斷而使每一管件28 之每一平行腿36至任一相鄰平行腿36的熱傳導最小化,且 因此可將關聯於每一平行腿36之散熱片元件料之間的熱傳 :最小化。這在譬如圖2至圖4之氣體冷卻器13等應用中非 “要’其中進入熱父換器1 〇之工作流體溫度係與離開熱 交換器10之工作流體需求溫度顯著不同。已針對僅有 高度不具有放氣孔之一散熱片30(典型的一具有放氣孔之 散熱片)計算’平行腿36之間多達4〇0/〇的總熱傳將經由該等 散熱片傳導,且因此不致排放入空氣中。在某些情況下, 對接收自熱交換器10熱側上散熱片3〇的熱作傳導,實際上 將使熱交換器10冷側上之散熱片30較流動通過冷側1 =件 28之工作流體更熱,而導致在工作流體離開熱交換器1〇之 前將熱傳回工作流體中的不佳情況。是以,並不希望每一 細長型分離件42皆沿著散熱片30身長作儘可能遠地連鋒延 伸,且不希望將翼片40之數量與尺寸最小化至需要防:每 —散熱片元件44在組立期間分離、以及需要使散熱片元件 44與每一散熱片30在組立期間皆保持一可接受對正程=的 00 200301815A heat sink element 44 extends along and extends along each parallel leg 36 of each adjacent pipe member 28, and a wing fin and a separator are provided between each heat sink element 44. The staggered fins 40 in each of the fins 30 are used to restrict the relative movement of the fin element materials to each other, so that during the assembly of the heat exchanger 10, each of the fin elements 30 remains as a single unit, and The fin elements 44 are kept aligned with each other to reduce the pressure drop on the fin side of the heat exchanger. The purpose of using the elongated separators 42 is to minimize the heat transfer from each parallel leg 36 of each tube 28 to any adjacent parallel leg 36 by interruption, and therefore the heat dissipation associated with each parallel leg 36 Heat transfer between chip components: minimized. In applications such as the gas cooler 13 shown in FIGS. 2 to 4, the temperature of the working fluid that does not “need” to enter the heat exchanger 10 is significantly different from the required temperature of the working fluid leaving the heat exchanger 10. There is a heat sink 30 (typically a heat sink with air vents) that does not have air vents. The total heat transfer of up to 400 / 〇 between parallel legs 36 will be conducted via these heat sinks, and therefore It will not be discharged into the air. In some cases, conducting heat received from the heat sink 30 on the hot side of the heat exchanger 10 will actually make the heat sink 30 on the cold side of the heat exchanger 10 pass through the cold Side 1 = The working fluid of element 28 is hotter, resulting in a poor condition in which heat is transferred back to the working fluid before it leaves the heat exchanger 10. Therefore, it is not desirable that each of the elongated separation elements 42 be along The heat sink 30 is extended as far as possible, and it is not desirable to minimize the number and size of the fins 40 to prevent: each-the heat sink element 44 is separated during assembly, and the heat sink element 44 needs to be separated from each other. A heat sink 30 is maintained during assembly An acceptable pair of forwards = 00 200301815
狀態。 種配置了’翼片40與細長型分離件42可能為i 3 ,在—散熱片30係由鋁製成且該散教片3();ΐstatus. This configuration is provided with the 'wing piece 40 and the elongated separating member 42 which may be i 3. In the-the heat sink 30 is made of aluminum and the diffuser piece 3 (); ΐ
放.、片30身長延伸大约0 020英对且由銘製成之一气 30的每—細長型分離件42皆係沿著該未㈣散教2身、 =大約8.G英心在該散熱㈣之—較佳具體實、 分離件42具有平行於未彎擅狀態散熱片3。身長延 、1分離件42身長對翼片爾長之比率係介於細 =的範圍内。在譬如圖7所示之另—具體 ' —細長型分離件42皆係自某_翼片概次 :: 延伸_ 14個彎㈣46,而散 j 4G連績地 叩狀…片30則係處於彎摺狀Put., Each of the elongated separation pieces 42 of the length 30 of the sheet 30 extending about 0 020 pairs of pairs and made of a gas 30 are along the non-traditional Sanjiao 2 body, = about 8. G Yingxin in the heat dissipation In other words, preferably, the separating member 42 has the heat sink 3 parallel to the unbent state. The body length extension, the length of one separator 42 to the length of the flaps are in the range of fine =. For example, as shown in Fig. 7, another-specific "-the slender separators 42 are all from a certain _ wing profile: :: extension _ 14 bends 46, and scattered j 4G continuous 叩 shape ... The piece 30 is at Bent
=可精多種以來形成翼片似分離件42,但分離件 熱片=為散熱片材料中之切口或狹縫而無需在形成於散 :、的方式之:二:除散熱片材料。一種達成這類狹縫或切 散熱片;…二材料形成散—,在 片3。切成! ^圓盤㈣ht,,以在散熱 般辟 口。可在每次旋轉中消除—小背圓 ,裂以形成翼片40,而確保散熱片3〇之每一散敎: 二與相鄰散熱片元件44連接。這將在散熱片30中二 結二二而無需減損散熱片表面。在某-這種 熱片元件::可ί:45'幾乎、但並非完全地互相鄰接。散 %在銅焊製程期間互相銅焊係-問題。一種 題最小化的方法係使鋼焊材料設於鄰接散熱片3〇的 -18- (12) 200301815 官件腿部36側壁上,而非使銅焊材料被覆於散熱片上, 另-種將該問題最小化之方法,係使散熱片3Q之相鄰散熱 片元件44偏置於遠離翼片4〇之位置處,如此可允許被覆散 熱片。另一種方法係使藉由狹縫略微分開而形成之邊緣化 弓曲來形成一極小放氣孔,如此亦允許被覆散熱片。又一= Various types of fins can be formed since the separation piece 42, but the separation piece. The heat piece = is a cut or slit in the heat sink material without the need to be formed in the form of the two :, except for the heat sink material. One achieves this kind of slit or cuts the heat sink; ... two materials form a scatter-in the sheet 3. Cut into! ^ Disc ㈣ht, in order to dissipate heat. It can be eliminated in each rotation-small back circle, split to form the fins 40, and ensure that each of the heat sinks 30 is scattered: Two are connected to adjacent heat sink elements 44. This will be done in the heat sink 30 without damaging the surface of the heat sink.在 一个-Such thermal film elements :: 可 ί: 45 'are almost, but not completely, adjacent to each other. Scatter% brazing to each other during the brazing process-problem. One method of minimizing the problem is to set the steel welding material on the -18- (12) 200301815 side wall of the leg 36 adjacent to the heat sink 30, instead of coating the brazing material on the heat sink, and another way The method for minimizing the problem is to bias the adjacent heat sink element 44 of the heat sink 3Q away from the wing 40, so that the heat sink can be covered. Another method is to make the marginal bow formed by the slits slightly separated to form a very small air vent, which also allows the heat sink to be covered. Another
種方法係壓印每一翼片部4〇,以更進一步地互相分離散熱 片兀件44。又,該最後一方法可允許被覆散熱片。儘管狹 縫係屬較佳者,但在某些應用中,使分離件42形成為必須 在幵7成政熱片3 0時移除散熱片材料的溝槽可能較優。就此 而論,使該等溝槽具有平行於散熱片3〇寬度w之數千分之 一英σ寸的一寬度即已足夠。 儘官散熱片30最好包括翼片40及分離件44,但在某政應 用中並不希望有及/或需要翼片4〇及分離件42。 散熱片30最好具有放氣孔,且其多種型式係屬已知。放 氣孔之確切配置係高度地依據譬如熱交換器丨〇散熱片側上 之流體、熱交換器1 〇散熱片側上之可用壓力降、每一管件 28中之平行腿36數量、以及每一管件28中具有奇數或偶數 個平行腿36等特定應用之參數而定。 應了解到,當作為系統12中之一氣體冷卻器丨3時,熱交 換器1 0典型地將提供超臨界冷卻冷媒;然而,仍具有環境 溫度低於臨界溫度之操作狀態,熱交換器丨〇在這種情況下 將作為提供次臨界冷卻冷媒的一凝結器。 如圖3中最清楚地顯示,圖式中之熱交換器1〇包括每一管 件28所具有的12個平行腿36。然而應了解到,每一熱交換 -19- (13) 200301815One method is to emboss each of the fin portions 40 to further separate the heat sink element 44 from each other. In addition, this last method allows covering the heat sink. Although the slit system is preferred, in some applications, it may be advantageous to form the separating member 42 as a groove that must be removed from the heat sink material 30%. In this connection, it is sufficient to make the grooves have a width parallel to the heat sink 30 width of one thousandth of an inch σ. The good heat sink 30 preferably includes the fins 40 and the separation members 44, but it is not desirable and / or required for the fins 40 and the separation members 42 in a certain application. The heat sink 30 preferably has a vent hole, and various types thereof are known. The exact arrangement of the vent holes is highly dependent on, for example, the fluid on the heat sink, the heat sink side, the available pressure drop on the heat sink side, the number of parallel legs 36 in each tube 28, and the number of each tube 28. There are odd or even parallel legs 36 depending on the particular application parameters. It should be understood that when used as one of the gas coolers in the system 12, the heat exchanger 10 will typically provide supercritical cooling refrigerant; however, there is still an operating state where the ambient temperature is below the critical temperature, the heat exchanger. 〇In this case, it will be used as a condenser to provide subcritical cooling refrigerant. As best shown in Figure 3, the heat exchanger 10 in the figure includes twelve parallel legs 36 of each tube 28. It should be understood, however, that each heat exchange -19- (13) 200301815
高度地依據譬如系統12之 入之外殼及環境、以及該 空調(AC)或熱泵系統中之 器等特定應用之特殊參數 能希望每一管件28僅具有 器10應用中之平行腿最佳數量係 工作流體、熱交換器10必須封裝 熱交換器之功用、亦即其用作為 一氣體冷卻器、凝結器、或蒸發 而定。譬如,在某些應用中,可 兩或三個平行腿36。 另一選擇為,可在箪__H ^ ^Depending on the particular parameters of the particular application, such as the enclosure and environment of the system 12, and the equipment in the air conditioning (AC) or heat pump system, it is desirable that each tube 28 has only the optimal number of parallel legs in the device 10 application. The working fluid, the heat exchanger 10 must encapsulate the function of the heat exchanger, that is, its use as a gas cooler, condenser, or evaporation. For example, in some applications, two or three parallel legs 36 may be used. Another option is to use 箪 __H ^ ^
在某或兩個管集箱20、22内提供一布 或更多阻板,以將冷媒自營隹 千目&木相20導引通過管件28之某一 次組合而至管韋益9 9,η ^ /、相22且接者返回通過管件28之一不同$ 組合而至管集箱2〇,並且繼婷私,一 &丄 且、.fe、嚼執仃與自一管集箱至另一 | 集箱之通道數量相箄的+ # ^ , 的數’其中該通道數量係提供每- 特疋應用之指定性能所需者。 在一較佳具體實施财,管㈣20、22及管件28以及散 熱片30白由!g製成’且藉_適當的銅焊材料銅焊。然而應Provide one or more baffle plates in one or two tube headers 20, 22 to guide the refrigerant self-propelled Chime & wood phase 20 through a certain combination of tube pieces 28 to tube Wei Yi 9 9 , Η ^ /, phase 22 and the receiver returns to the header box 20 through a different $ combination of one of the tube pieces 28, and following Ting private, one & 丄 ,, .fe, chewing 仃 and from a tube header + # ^, The number of channels with the same number of channels to another | where the number of channels is required to provide the specified performance per-special applications. In a preferred embodiment, the pipes 20, 22, the pipe fittings 28, and the heat sink 30 are free! g is made and brazed with a suitable brazing material. However should
了解i纟某二應用中,由其他適當材料製成者亦可運用 至由特定應用之參數所指定的該等組件。 應了解到,儘官圖1至圖3中顯示出之熱交換器^ 〇係使管 集箱20、22之縱向抽24、26沿-水平方向延伸,且管件28 之平仃腿36沿一垂直方向延伸,但在某些應用中,希望一 熱交換器1〇具有-不同方位,譬如使軸24、26沿一垂直方 向延伸且平行腿36沿-水平方向延伸的-方位。更,儘管 圖1至圖3中顯示出之熱交換器1〇管集箱2〇、22係設於熱交 換器ίο之相同側上,但在某些應用中係希望管集箱2〇、22 設於熱交換器10之相對側上。管集箱2〇、22位於該熱交換 -20- 200301815Understand that in some applications, those made of other suitable materials can also be applied to those components specified by the parameters of the specific application. It should be understood that the heat exchangers ^ 〇 shown in Figures 1 to 3 are such that the longitudinal extractions 24, 26 of the headers 20, 22 extend in a horizontal direction, and the flat legs 36 of the tube 28 follow a It extends vertically, but in some applications, it is desirable for a heat exchanger 10 to have a different orientation, such as having the shafts 24 and 26 extend in a vertical direction and the parallel legs 36 extend in a horizontal direction. Furthermore, although the heat exchanger 10 tube headers 20 and 22 shown in Figs. 1 to 3 are provided on the same side of the heat exchanger ο, the tube header 20, 22 is provided on the opposite side of the heat exchanger 10. The headers 20 and 22 are located at this heat exchange -20- 200301815
(14) 器相同側上的一結構,典型地將造成每一管件28皆具有偶 數個平行腿36,而管集箱20、22位於熱交換器1〇相對側上 的一結構,典型地將造成每一管件28皆具有奇數個平行腿 用有需要’則亦可由配 管集箱20、22。 3 6的一結構。當然,倘若一特定應 合槽體之管集箱板件來取代管狀之 圖式代表符號說明 10 熱交換器(結構) 12 冷卻系統 13 氣體冷卻器 14 壓縮器 16 膨脹裝置 17 蒸發器 18 積蓄器 19 吸引管路熱交換器 20、22 管集箱 24、26 縱向轴 28 (細長型)管件 30 (蛇紋式彎曲)散熱片 31 第一末端 管件末端 32 第一末端 管件末端 34 孑L 口 36 平行腿腿部 參 t •21- 200301815 (15) 38 流體通道 39 流體通道 40 (交錯)翼片 42 (細長型)分離件 44 散熱片元件 45 邊緣 46 D 長尺寸 d 短尺寸 L 身長 H 散熱片高度 A 空氣流 W (橫向)寬度 X 距離間隔(14) A structure on the same side of the device will typically result in each tube 28 having an even number of parallel legs 36, and a structure where the headers 20, 22 are located on the opposite side of the heat exchanger 10, typically If each tube 28 has an odd number of parallel legs, it is necessary to use the piping headers 20 and 22. A structure of 3 6. Of course, if the tube header plate of a specific application tank is used instead of the tubular representation of the symbolic representation 10 heat exchanger (structure) 12 cooling system 13 gas cooler 14 compressor 16 expansion device 17 evaporator 18 accumulator 19 Suction line heat exchanger 20, 22 Tube header 24, 26 Longitudinal axis 28 (slim) tube fitting 30 (snake-shaped bend) heat sink 31 First end tube end 32 First end tube end 34 孑 L port 36 parallel Legs and legs t • 21- 200301815 (15) 38 fluid channel 39 fluid channel 40 (staggered) fins 42 (slim) separator 44 heat sink element 45 edge 46 D long size d short size L length H heat sink height A Air flow W (transverse) width X distance interval
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-
2001
- 2001-11-30 US US10/013,018 patent/US20030102113A1/en not_active Abandoned
-
2002
- 2002-10-30 AU AU2002365762A patent/AU2002365762B2/en not_active Expired - Fee Related
- 2002-10-30 CN CNB028236556A patent/CN100380081C/en not_active Expired - Fee Related
- 2002-10-30 MX MXPA04004660A patent/MXPA04004660A/en unknown
- 2002-10-30 CN CNA2007101049458A patent/CN101089533A/en active Pending
- 2002-10-30 WO PCT/US2002/034606 patent/WO2003048670A1/en active Application Filing
- 2002-10-30 KR KR1020047008270A patent/KR20050058253A/en not_active Application Discontinuation
- 2002-10-30 EP EP02804409A patent/EP1448945A1/en not_active Withdrawn
- 2002-10-30 BR BR0214479-4A patent/BR0214479A/en active Search and Examination
- 2002-10-30 JP JP2003549821A patent/JP2005512009A/en not_active Ceased
- 2002-10-30 CA CA002467137A patent/CA2467137A1/en not_active Abandoned
- 2002-10-30 RU RU2004117856/06A patent/RU2319094C2/en not_active IP Right Cessation
- 2002-11-13 TW TW091133260A patent/TW200301815A/en unknown
- 2002-11-25 AR ARP020104527A patent/AR037428A1/en not_active Application Discontinuation
Also Published As
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RU2004117856A (en) | 2005-04-27 |
CA2467137A1 (en) | 2003-06-12 |
AR037428A1 (en) | 2004-11-10 |
CN101089533A (en) | 2007-12-19 |
BR0214479A (en) | 2004-09-14 |
AU2002365762B2 (en) | 2008-02-21 |
CN100380081C (en) | 2008-04-09 |
CN1596360A (en) | 2005-03-16 |
EP1448945A1 (en) | 2004-08-25 |
JP2005512009A (en) | 2005-04-28 |
MXPA04004660A (en) | 2004-08-13 |
US20030102113A1 (en) | 2003-06-05 |
WO2003048670A1 (en) | 2003-06-12 |
AU2002365762A1 (en) | 2003-06-17 |
KR20050058253A (en) | 2005-06-16 |
RU2319094C2 (en) | 2008-03-10 |
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