TW201020498A - Method for manufacturing evaporator for looped heat pipe system - Google Patents

Method for manufacturing evaporator for looped heat pipe system Download PDF

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Publication number
TW201020498A
TW201020498A TW098131989A TW98131989A TW201020498A TW 201020498 A TW201020498 A TW 201020498A TW 098131989 A TW098131989 A TW 098131989A TW 98131989 A TW98131989 A TW 98131989A TW 201020498 A TW201020498 A TW 201020498A
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Taiwan
Prior art keywords
heat transfer
core
heat
component
core structure
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TW098131989A
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Chinese (zh)
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TWI382146B (en
Inventor
Chul-Ju Kim
Min-Whan Seo
Byung-Ho Sung
Jung-Hyun Yoo
Jee-Hoon Choi
Jung-Rae Jo
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Zalman Tech Co Ltd
Univ Sungkyunkwan Found
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Publication of TW201020498A publication Critical patent/TW201020498A/en
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Publication of TWI382146B publication Critical patent/TWI382146B/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0266Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/22Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
    • B22F3/225Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/04Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
    • F28D15/046Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure characterised by the material or the construction of the capillary structure
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/04Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer
    • H01L21/48Manufacture or treatment of parts, e.g. containers, prior to assembly of the devices, using processes not provided for in a single one of the subgroups H01L21/06 - H01L21/326
    • H01L21/4814Conductive parts
    • H01L21/4871Bases, plates or heatsinks
    • H01L21/4882Assembly of heatsink parts
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00Details of semiconductor or other solid state devices
    • H01L23/34Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/42Fillings or auxiliary members in containers or encapsulations selected or arranged to facilitate heating or cooling
    • H01L23/427Cooling by change of state, e.g. use of heat pipes
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2029Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
    • H05K7/20336Heat pipes, e.g. wicks or capillary pumps
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001Technical content checked by a classifier
    • H01L2924/0002Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Sustainable Development (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Power Engineering (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

Provided is a method of manufacturing an evaporator for a looped heat pipe (LHP) system, the method including the operations of forming a plurality of wicks having pores; forming a plurality of heat transferring fins respectively having a wick coupler to be coupled to one of the plurality of wicks; inserting each of the wicks into the wick coupler of each of the heat transferring fin, thereby forming a plurality of unit assemblies; applying at least one of heat and pressure to the unit assemblies, and cross-coupling a contact surface of the wick and a contact surface of the heat transferring fin; horizontally disposing the unit assemblies to enable a bottom surface of each of the unit assemblies to be located on a planar surface, and forming an assembly structure; applying at least one of heat and pressure to the assembly structure, and cross-coupling the unit assemblies; and disposing the assembly structure on a top surface of a heat transferring plate having a planar plate shape.

Description

201020498 六、發明說明: 【發明所屬之技術領域】 本發明是有關一種迴路式熱管系統的蒸發器的製造 方法,其包含一冷凝器、一氣體傳輸線、一液體傳輸線, 且特別是有關一種用於一迴路式熱管系統的蒸發器的製造 方法’其中一蕊狀結構物與一傳熱鰭片互相(cross)連結以 形成一組件單元’且多個組件單元經排列配置後連結至一 傳熱板而形成一蒸發器,藉此將蕊狀結構物與傳熱鰭片製 造成各種形狀和尺寸,而最小化了蕊狀結構物與傳熱鰭片 間的熱接觸阻抗。 【先前技術】 用來作為各種像是電腦之類的電子裝置的電子零件例 如中央處理器或半導體晶片,在運作時會產生大量的埶 能。因這些電子裝置通常設計在室溫下使用,故這些電 裝置需要降低在運作時所產生的熱能。 ^千裝置$派的夕禋枝術之一為使用相變熱傳輸系 統’種這裡介紹崎技術為迴路式熱管(LHp)系統。 圖一為一常用的迴路式熱管系統110的示意圖。 迴路:熱管系、统110包含—冷凝器112 Z ns 118 5 ^ 體線118的兩端分別連接冷凝器u 流體注入迴路式埶管系絲 …發114工作 不同,多個具與一般具有圓柱狀的熱管 統110的蒸發器m中。、配置在迴路式熱管系 201020498 迴路式熱管系統110以下述的方式運作: 首先,蒸發器114與一加熱中的電子元件(未畫於圖) 即熱源接觸。當蒸發器被熱源加熱,處於液態的工作流體 滲透並通過蕊狀結構物而變相為氣態。 此產生的氣體經由連接於蒸發器114 一端的氣體線 116而流向冷凝器112。當此氣體通過冷凝器112時,所夾 帶的熱能向外散失而液化。此液化的工作流體再經由連接201020498 VI. Description of the Invention: [Technical Field] The present invention relates to a method for manufacturing an evaporator of a loop type heat pipe system, comprising a condenser, a gas transmission line, a liquid transmission line, and particularly related to A method for manufacturing an evaporator of a one-loop heat pipe system in which a core structure and a heat transfer fin are cross-coupled to form a component unit and a plurality of component units are arranged and connected to a heat transfer plate An evaporator is formed whereby the core structure and the heat transfer fins are fabricated into various shapes and sizes while minimizing the thermal contact resistance between the core structure and the heat transfer fins. [Prior Art] Electronic components such as a central processing unit or a semiconductor chip used as an electronic device such as a computer generate a large amount of power during operation. Since these electronic devices are usually designed to be used at room temperature, these devices need to reduce the amount of heat generated during operation. One of the thousands of devices used to send the 禋 术 为 is to use the phase change heat transfer system. Here, the Saki technology is a loop heat pipe (LHp) system. FIG. 1 is a schematic diagram of a conventional loop heat pipe system 110. Circuit: heat pipe system, system 110 includes - condenser 112 Z ns 118 5 ^ The two ends of the body line 118 are respectively connected to the condenser u. The fluid is injected into the loop type manifold wire. The hair 114 is different in operation, and the plurality of members have a cylindrical shape. The heat pipe system 110 is in the evaporator m. Configuring the loop heat pipe system 201020498 The loop heat pipe system 110 operates in the following manner: First, the evaporator 114 is in contact with a heating electronic component (not shown), that is, a heat source. When the evaporator is heated by the heat source, the working fluid in the liquid phase penetrates and is phase-shifted into a gaseous state by the core structure. This generated gas flows to the condenser 112 via a gas line 116 connected to one end of the evaporator 114. When this gas passes through the condenser 112, the entrained thermal energy is dissipated outward and liquefied. The liquefied working fluid is connected again

於冷凝器112 —端的液體線118而流回蒸發器114。經由 上述的過程重複運作,使得電子零件即熱源降溫。 同時,為了迴路式熱管系統11()的緊密性與高效能, 總熱電阻應降低。當總電熱阻降低,熱源即此電子元 可在低溫下運作。 必須考慮各種因素以降低迴路式熱管系統! i 〇的總熱 電阻。其巾最重要的因素為蕊狀結構物的接觸面與蒸發器 U4基底鋪面間的熱接觸阻抗。此熱接娜抗不止受表 ^上熱傳遞在二物體接觸面的面積影響。換言之,即使表 t接觸面平坦’二物體實際上的接觸介面的尺寸會隨著 瞭解所以我們必須藉著接觸面的狀態來 哭=接觸”面的尺寸。在餘結構物的接觸面與蒸發 51 114^的接觸面間之熱傳導發生於蕊狀結構物與蒸發 ^路哭二的實際接觸介面的熱傳導,以及綠結構物與 ^接觸且^底接觸面間的真空區域的熱傳導 。大部分的 Γ、a几疋由焱狀結構物與蒸發器114基底間的真空 V〇1 & _所產生°所以藉著增加蕊狀結構物與蒸發器114 5 201020498 基底間的接觸面積,可降低熱接觸阻抗。換言之,熱接觸 阻抗與二個金屬表面接觸時所產生的熱阻抗有關,且依據 接觸表面的面積而有可觀的不同。 一般而言,藉著將二物體接觸面拋光後互相接觸,或 在接觸面加上具有高熱導的潤滑油,來擴大二物體 際接觸面積。 迴路式熱管系統110的熱接觸阻抗與蒸發器114加埶 中,介面狀態及燒結的蕊狀結構物與蒸發器114的接觸'面 狀態都具有高度相關。同樣地,熱接觸阻抗是工作流體自 液態變相為汽態時對熱起反應的極為重要的因素。” 即使燒結的蕊狀結構物與功用類似於熱板的基底明顯 地形成一大的互相接觸面,但當燒結的蕊狀結構物與基底 的實際接觸介面狀態不合宜時,傳向燒結的蕊狀結構物的 熱傳導便不平穩。若如此’功用類似於蒸發器U4的熱板 的基底的溫度升高,使氣體溫度增加至迴路式熱管系統 110的工作水平(level)。目氣體的功用為傳輸熱能至冷凝器 112 ’則當迴路式熱管系、統i 10 α高溫氣體運作_,迴路式 熱管系統110的總熱阻抗即增加。 因此,關於蒸發器114的關鍵在於加大排置於蒸發器 114中的燒結的蕊狀結構物及蒸發器内部結構的際^ 面積’而降低熱漏隨值’叹電子零件可料至低温。 關於蒸發^ 114,韓國專利申親:1()細請2侧 揭露-種使-綠結構物與—蒸發器中之結構之間的接觸 面積增大馳術。參考自此申請書,這樣—習知技術揭露 201020498 内部結構的突起物12〇之 处槿二3 構考4 °然而’此方法限制了内部 :構=所需要的形狀,且在此例中,接觸面的狀態不合 且夺導致熱傳導進行時的效率不佳。 之’在此習知技術中,參考該中請案的圖^、 〇刀別對應到本發明的圖2、3 4) =r;r突—較先前 ^ 實上成'狀結構物410只是簡單嵌入並連 、,於各犬起物120之間,是以蕊狀結構物4H)與突起物120 =間的實際接觸面的狀態並不是所期望者。換言之,產生了點 效轉觸使得自突起物12G至蕊狀結獅410的熱傳遞 圖5說明蕊狀結構物及突起物12〇間的一接觸 ==狀結漏41G與突起物12㈣溫度梯度㈣㈣ ^意,。此圖是由電子顯微鏡放大了接觸面而得。參考 ,5 ’ ^狀結構物41G與突起物m主要經由點接觸而做 互相連接’因此’可以看到在接觸介面上溫度降低。 =此’此例中洛發II雖然在—值定熱負載下運作,但 t表面的溫度卻會隨著蒸發_熱_阻抗值而改變, 备接觸阻抗大,則加熱介面的溫度即 ^ 接觸阻抗小,加熱介面的溫度即下降 , 田”、、 限制了突起物120的形狀或表面粗輪的調整。同樣地,蕊 7 201020498 狀結構物410依據突起物12〇的形狀而嵌入至突起物12〇 中,如此,限制了蕊狀結構物的材料及形狀的選擇。這些限制 為造成接觸面狀態的改良困難的主要因素。 換言之,根據習知技術,突起物丨2〇及熱源接觸單元n〇 皆整體形成於蒸發龍4巾,减人至狄物12G巾的蕊狀結 構物410的形狀對應於突起物120的形狀。於是,限制了蕊 狀結構物的各種形狀的獲得。以上,由於突起物120與蕊狀結 構物410之間的接觸面之不適宜的狀態而造成高的熱接觸阻 抗’使電子零件不能有效地冷卻。 【發明内容】 『發明的技術目標』 ^本發明提供一種用於迴路式熱管系統的蒸發器的製 造方法二其中蒸發器的傳熱鰭片可以各種形狀形成且蒸 發器的蕊狀結構物可以各種形狀及材料形成,藉以改善傳 熱鰭片及蕊狀結構物之間的接觸狀態。 『達到技術目標的手段』The liquid line 118 at the end of the condenser 112 flows back to the evaporator 114. Repeated operation through the above process causes the electronic component, that is, the heat source to cool down. At the same time, for the tightness and high performance of the loop heat pipe system 11 (), the total thermal resistance should be reduced. When the total electric resistance is lowered, the heat source, that is, the electron element can operate at a low temperature. Various factors must be considered to reduce the loop heat pipe system! i 〇 total thermal resistance. The most important factor of the towel is the thermal contact resistance between the contact surface of the core structure and the base surface of the evaporator U4. This heat contact is not only affected by the surface heat transfer on the contact surface of the two objects. In other words, even if the contact surface of the table t is flat, the size of the actual contact interface of the two objects will be known. Therefore, we must cry the state of the contact surface by the state of the contact surface. The contact surface of the remaining structure and evaporation 51 The heat conduction between the contact surfaces of 114^ occurs from the thermal conduction of the actual contact interface between the core structure and the evaporation system, and the heat conduction between the green structure and the vacuum region between the contact surface and the bottom contact surface. , a several 疋 by the vacuum V 〇 1 & _ between the 焱 structure and the base of the evaporator 114, so by increasing the contact area between the core structure and the evaporator 114 5 201020498 substrate, can reduce thermal contact Impedance. In other words, the thermal contact resistance is related to the thermal impedance generated when the two metal surfaces are in contact, and there is a considerable difference depending on the area of the contact surface. Generally, the two contact surfaces are polished to each other, or A lubricating oil having a high thermal conductivity is added to the contact surface to expand the contact area between the two objects. The thermal contact resistance of the loop heat pipe system 110 and the evaporator 114 are twisted, and the interface is Both the sintered core structure and the contact 'surface state of the evaporator 114 are highly correlated. Similarly, the thermal contact resistance is an extremely important factor for the reaction of the working fluid from the liquid phase to the vapor state. The core structure and the substrate similar in function to the hot plate form a large mutual contact surface, but when the sintered core structure is not suitable for the actual contact interface state of the substrate, the sintered core structure is transferred to the sintered core structure. The heat transfer is not smooth. If so, the temperature of the substrate of the hot plate of the evaporator U4 is increased, and the temperature of the gas is increased to the level of the loop heat pipe system 110. The function of the gas is to transfer thermal energy to the condenser 112'. When the loop heat pipe system, the total heat resistance of the loop heat pipe system 110 increases. Therefore, the key to the evaporator 114 is to increase the area of the sintered core structure and the internal structure of the evaporator disposed in the evaporator 114 to reduce the heat leak value. Regarding the evaporation ^ 114, the Korean patent application: 1 () fine 2 side reveals - the contact area between the seed-green structure and the structure in the evaporator is increased. Reference is made to this application, such that the prior art discloses that the protrusions of the internal structure of 201020498 are 12 槿 2 3 构 4 ° However, this method limits the internal: structure = the required shape, and in this case, The state of the contact faces is not uniform and the efficiency of the heat conduction is poor. In the prior art, reference is made to the figure of the present application, and the file corresponds to the figure 2, 3 4 of the present invention. = r; r protrusion - compared to the previous ^ is actually a 'structure 410 It is not desirable to simply embed and join, and between the respective canines 120, the actual contact surface between the core structure 4H) and the protrusion 120 =. In other words, a point-effect turn is made to cause heat transfer from the protrusion 12G to the core lion 410. FIG. 5 illustrates a contact between the core structure and the protrusion 12〇== junction leakage 41G and protrusion 12 (four) temperature gradient (4) (4) ^ Italian,. This figure is obtained by magnifying the contact surface with an electron microscope. Referring to the reference, the 5'-like structure 41G and the protrusion m are mainly connected to each other via point contact. Therefore, it can be seen that the temperature is lowered at the contact interface. ==In this case, although Luofa II operates under a constant heat load, the temperature of the t surface changes with the evaporation_heat_impedance value. When the contact impedance is large, the temperature of the heating interface is ^ contact. The impedance is small, the temperature of the heating interface is lowered, and the shape of the protrusion 120 or the adjustment of the surface rough wheel is limited. Similarly, the core 7 201020498 structure 410 is embedded in the protrusion according to the shape of the protrusion 12〇. In this case, the choice of the material and shape of the core structure is limited. These limitations are the main factors that cause improvement in the state of the contact surface. In other words, according to the prior art, the protrusion 丨2〇 and the heat source contact unit n The crucibles are all formed integrally in the evaporating dragon 4 towel, and the shape of the core structure 410 reduced to the wafer 12G towel corresponds to the shape of the protrusion 120. Thus, the various shapes of the core structure are limited. The unfavorable state of the contact surface between the protrusion 120 and the core structure 410 causes a high thermal contact resistance to prevent the electronic component from being effectively cooled. [Summary of the Invention] The present invention provides a method for manufacturing an evaporator for a loop type heat pipe system. The heat transfer fin of the evaporator can be formed in various shapes and the core structure of the evaporator can be formed in various shapes and materials to improve heat transfer. Contact state between fins and core structures. "Means to achieve technical goals"

^本發明提出一種用於迴路式熱管系統的蒸發器的製 造^法’其包括形成多個具有細孔的蕊狀結構物;形成多 :二別具有-連結至多個蕊狀結構物之—的蕊狀結構物連 …器的傳熱鰭片;將每一個蕊狀結構物分別嵌入至每一個 ,熱韓片的蕊狀結構物連結器,從而形成多個組件單元; 施加至少熱及壓力之一至組件單元,且將蕊狀結構物之一 接觸Ϊ與傳熱韓片之一接觸面做互相連接;水平配置這些 組件单元,使得每-組件單元的底面可配置於一平面,I ❹The present invention provides a method for fabricating an evaporator for a loop-type heat pipe system, which comprises forming a plurality of core structures having pores; forming a plurality: two having - bonded to a plurality of core structures - a heat transfer fin of a core structure; each of the core structures is embedded in each of the core structure connectors of the hot Korean sheet to form a plurality of component units; applying at least heat and pressure a component unit, and one of the core structures is contacted with one of the contact faces of the heat transfer film to be interconnected; the component units are horizontally arranged such that the bottom surface of each of the component units can be disposed on a plane, I ❹

G 201020498 形成-組件結構;彻至少缺 =件單元做互相連接;叹 右並 平板形狀的傳熱板之頂面上 "、、且件、、、口構至一具有一 面上的組件結構,並將 ==力至頂 接觸面做連結。 < 接觸面及傳熱板之一 粉末成可包含使用-種自金屬 集合中選定的材料,至;組成的 的材!过=多個具有希望的形狀的蕊細】:選定 熱及廢力之一至混4 混和,然後施加 蕊狀結構物。 從而形成多個具有希望的形狀的 在形成多個具有希望的形狀的蕊狀結構物之後,多個 ^結構物的形成更包含使用溶劑抽取法和熱解法之一來 移除已混合賴雜聚合物或已齡的有機溶劑。 二在蕊狀結構物嵌入至傳熱鰭片的蕊狀結構物連結器 之别,組件單7〇的形成更包括嵌入選用自金屬粉末與連結 ^料的連結催化劑(c〇upUngpr〇m〇ter),以使該連結催化劑 可以置於該蕊狀結構物與傳熱鰭片間的接觸面的至少一部 份上。 上述組件結構的形成更包含:在相鄰的組件單元之間 配置至少一中間蕊狀結構物及一隔離物(spacer)之一。 上述組件結構的形成更包含:在組件結構上水平地施 9 201020498 加壓力,從而使蕊狀結構物中細孔的孔徑縮小。G 201020498 Forming-component structure; at least the missing parts are connected to each other; the top surface of the heat transfer plate slanting right and flat shape has a component structure on one side, And == force to the top contact surface to make a connection. < One of the contact surface and the heat transfer plate powder may comprise a material selected from the group of metals, to a material composed of: a plurality of cores having a desired shape: selected heat and waste force One of them is mixed with the mixture 4, and then the core structure is applied. Thus, after forming a plurality of core structures having a desired shape and forming a plurality of core structures having a desired shape, the formation of the plurality of structures further includes using one of a solvent extraction method and a pyrolysis method to remove the mixed conjugate polymerization. Or aged organic solvent. 2. In the case of a core structure connector in which the core structure is embedded in the heat transfer fin, the formation of the component 7 更 includes the bonding catalyst selected from the metal powder and the binder (c〇upUngpr〇m〇ter) And so that the bonding catalyst can be placed on at least a portion of the contact surface between the core structure and the heat transfer fins. The forming of the above component structure further comprises: arranging at least one intermediate core structure and one spacer between adjacent component units. The formation of the above-mentioned component structure further comprises: applying a pressure on the component structure horizontally, 201020498, so that the pore size of the pores in the core structure is reduced.

At上述組件結構的形成更包含配置壓力元件,該壓力元 2此在該組件結構之侧的方向中將壓力施加在該組件 、、Ό構且可使凝狀結構物中細孔的孔徑縮小。 在上述多個蕊狀結構物的形成,多個傳熱鰭片的形 成’組件單元的形成,以及組件結構的形成之後,蕊狀結 構物及傳熱韓片之接觸面的互相連結,組件單元的互相連 、、Ό以及組件結構與傳熱板的接觸面的連結皆同時以同一 程序;成,焱狀結構物及傳熱鰭片之接觸面的互相連結, 與組件單元的互相連結同時完成,然後進行組件結構與傳 熱板之接觸面的連結,或是,進行蕊狀結構物及傳熱鰭片 之接觸面的互相連結,然後進行各組件單元的互相連結, 以及組件結構與傳熱板之接觸面的連結。 『發明的效果』 根據本發明之一個或多個實施例之用於迴路式熱管 系統的蒸發器的製造方法,首先製造蕊狀結構物及傳熱^ 片,並排列配置多個蕊狀結構物及傳熱鰭片,然後連結至 一傳熱板即一金屬平板,如此製造出蒸發器。以此方=, 可很容易形成一複雜形狀或所需形狀的傳熱鰭片,可改良 蕊狀結構物及傳熱鰭片的接觸狀態,如此一來,可擴大2 熱面積及氣體產生面積,並使蕊狀結構物及傳熱鰭片間的 熱接觸阻抗最小化。 … Β 為讓本發明之上述特徵和優點能更明顯易懂,下文特 舉實施例,並配合所附圖示作詳細說明如下。 201020498 【實施方式】 製造明ί關於—種用於迴路式熱管系統的蒸發器的 傳輸線。迴路器、一氣體傳輸線、以及一液體 的描述。(、、、s系統的運作符合上述相關於先前技術 1依Γ構可參相6來描述,蒸發器 造方法所製造圖路式熱管系統的蒸發器的製 墓路盟16為蒸發器1的分解透視圖。 一僂1包含多個蕊狀結構物1〇,多個傳熱鰭片20, 傅熱板50,以及-遮蓋件60。 -薄多個蕊狀結構物1G具有細孔,且個別具有 H 22 個傳熱韓片2G各別具有一蕊狀結構物連結 愁狀姓構# H以此連結器可連結減狀結構物1〇。 縛片2〇互相連結形成-組件單元3。 Φ 圖^平配置多個組件單元3()形成—組件結構4〇 (參考 傳熱板5G連結至组件結構的底部4〇。 自教ί金屬顧’且料面接雜源並接收來 零件例如-電腦的中央處理器:、-顯示t ίίο::連結至傳熱板50之頂面。此遮蓋件60與 板5〇形成—内部空間’使組件結構40放置其中。遮 11 201020498 蓋件60的侧表面上形成一用於連接至氣體傳輸線之氣體 線連接孔62,且在遮蓋件6〇的頂面上形成一用於連接至 液體傳輸線之液體線連接孔64。 同時,在組件結構40中,蕊狀結構物10及傳熱鰭片 20互相連結而形成一介於蕊狀結構物1〇及傳熱鰭片加之 犬起物26及28之間的氣體通道,因此,由蕊狀結構物川 中產生之氣體可經由遮蓋件60之氣體線連接孔62而排出。 具有上述結構之蒸發器1之運作將描述於下。 ❹ 一液態之工作流體經由液體線連接孔64而注入至蒸 發器1巾,且渗入至許多形成於蕊狀結構物1〇内部中的: 孔中。由熱源經過傳熱板50而傳送至傳麟片2〇的熱於 :傳輸至蕊狀結構物1〇而使工作流體由液態相變: 逆葙孔62而由瘵發器1排出至外部。 1發明之實_之具有上述結構之迴路式 製造方法將參考圖7至圖12做以下描述 本實關之用於迴路式齡系朗 法包含形衫個級結獅之操作 \ k方 傳熱轉片之操作(操作S2),形形成多個 作幻),連結多個組件單元之操作(‘ 操作(操 組件結構之齡(操作S5) 料),形成- S6),以及遠社種〜且件結構之操作(择作 以及連結-傳熱板之操作(操作⑺。、裸作 12 201020498 有大量内部細孔的多孔結構。工作流體渗入 熱鰭片^來的熱能而工使作流體相 的說明,本實施例之蕊狀結構物1〇的七如,8 板,但此形狀可視需要而改變。 為一溥四角平 此蕊狀結構物10可使用至少一選定自金 金屬粉末,金屬纖維,以及非金 刀末 好料,心·^ ㈣屬纖維所組成之集合中的 材料絲成財料雜,紐絲 ❹ 至已選定的材料。換言之,施加熱或壓:2= 材料以獲得所希望的形狀。 一者至選疋的 成步=成細構物1G彻⑽作S1)可稱為前置形 蕊狀結構物10藉由使用金屬粉末及 在形成蕊狀結構物10的操作 及包含銅、龙:構件’使用像是金屬導線或金屬纖維,以 末來製作。兴、青銅、錄、欽、銘、不銹鋼等的金属粉 要,此材料選自金屬粉末及金屬纖維,但若必 可包含tit兩種或是更多種金屬粉末的選用,或亦 左盒屬粉末及金屬纖維的混和物。 的形熱及壓力之一至選定的材料以獲得所希望 或-模且r、 將金屬或金屬纖維填入至一治具(jig) 治且’然後施加熱及壓力任—者或兩者至此 加ί至燒結、:Ϊ具(In〇ld)以形成希望的形狀。加熱時, ,農又可用以燒結金屬,或加熱至低於燒結溫度 13 201020498 之預燒結溫度以燒結金屬。 在燒結溫度時金屬已燒結,預燒結溫度為約8〇%至約 90%的金屬已繞結的燒結溫度。 同樣地,加壓至金屬以得到所需要_狀時,可使用 射出成型法’錢用鑄模麵法(a method of fiUing a jig or a mold)並施加壓力至模具或治具中。 此時,金屬粉末或金屬纖維形成的蕊狀結構物1〇由 於燒結的程相為-纽燒結體。㈣,紐結構物1〇 =、?程序可在操作S1中進行,抑或在-隨後的操作程 疋連結組件單元的操作(操作⑷,連結組件結構的 操作(操作S6),以及連結傳熱板之步驟(S7)中在燒結 程序時將蕊狀結構物1G加熱至燒結溫度。 換《之,在形成蕊狀結構物之操作(S1)中就已完成 、、’。程序的情況下’將在隨後賴作巾施加低於燒結溫度 ,溫度以達到-優質的接_狀態。然而,在燒結程序不 =在形成蕊狀結構物之操作(S1)巾完成時,則在隨後的 操作程序巾驗㈣齡程序,錄結溫度_熱施加至 :隨後的操作程序’此時即可達到—接觸面的優良連結狀 態。 同時,藉由選用非金屬粉末及非金屬纖維中的至少一 材料以形成所要形狀的蕊狀結構物1G,然後再施加至少执 及壓力之一至此選定的材料。 上述的非金屬粉末實例可包含一種以陶瓷為主之氧 匕鋁(Al2〇3)粉末,—種碳質的活性碳粉末以及一種碳質 201020498 =石墨粉末。由此非金屬粉末及非金屬纖維來填滿-治 形==後施加熱或壓力或兩者至此治具或模具以 m 鲁 然而’在選用此非金屬材料來形成蕊狀結構物的 ^下’由非金屬材料形成的蕊狀結構物1G及由金屬材料 =成的傳熱鰭片可能無法在隨後的蕊狀結構物⑴及傳敎 ,片之互域接形絲件單福連結組件單元的操作 =)b鏡咖_連結,因此,蕊狀結構物ι〇及 傳熱韓片需經由壓力以擴大此二者的接觸面積。 在本實施例之形成蕊狀結構物10的操作(S1)中, =塑性聚合物及有機賴之—來與敎的材料混合以形 -具有所希望的靴的級結獅1G,錢再施加熱及 人力之-至此混和物。此熱雜聚合物類似於—黏著性聚 二物材料’包含聚乙婦、聚丙婦、丙烯樹脂、以及苯乙烯 此熱雜聚合物的崎為在實施燒轉作之前增加 粕末的黏滯性,以及在進行燒結操作時使發生 及體積變化最小化。 趨狀結構物10為以熱塑性聚合物及昇華性材料的有 =溶劑之—來與選自非金屬粉末及非金職_材料相混 合,然後進行注入或加壓而形成。 6有機溶劑為-昇華性物質,在室溫下呈固態,且在預 疋溫度加熱_從_變相為汽態。昇雜材料像是萘、 以太或酒精、或兩者皆可用作有機溶劑。 有機溶劑常用來製造一般難以形成的複雜形狀。因 201020498 此’有機溶劑是在成形的操作之前加入,而有機溶劑加入 後所形成的形狀的部份會在燒結過程中再華而製造出所需 的形狀。 同樣地’在金屬是以熱塑性聚合物及有機溶劑之一混 2的形成蕊狀結構物的操作(S1)中,當所需的蕊狀結構 ^形狀的成形完成時,此混和的熱塑性聚合物或混合的 有機溶劑可_溶解取法及祕法之—來移除。 七士Ϊ後在迴路式熱管系統運作時,剩餘的熱塑性聚合物 ^機溶劑可能會與工作流體反應,造成舰、污染、或 、體不凝結的情形。所以此剩餘物必須清除。 ―姑#的操作(S2 )中’形成多個分別具有 可器22的傳熱韓片2〇 ’且蕊狀結構物10 20是以 1工、;Γ7連結器22連結(參考圖9)。傳熱‘辖片 熱係數之金屬而^18 machine)等來加工具有相對較高導 金屬加工枝村被使用。 物10。 …、板50接收的熱能’傳送至蕊狀結構 ❹ 冰此及多個突起物%及 底部構件24的一末端向上突出。突起物26及此 16 201020498 -----I-- 間形成一空間。此空間用來作為蕊狀結構物10中所 產生的氧體的通道。形成傳熱則2G之材料與傳執板50 2之此’突起物26及28與蕊狀結構物連結器 β谷易製ia為一較複雜的形狀,並可調整製 粗链度至-所需的程度。 &的表面的 ^ ’形成蕊狀賴狀操作(Sl)及形成傳熱 之#作(S2)的順序可顛倒。At least the formation of the above-described component structure further includes arranging a pressure element which applies pressure to the assembly, the Ό structure in the direction of the side of the assembly structure, and which reduces the aperture of the pores in the condensed structure. After the formation of the plurality of core structures, the formation of the plurality of heat transfer fins, and the formation of the component structure, the interconnection of the contact surfaces of the core structure and the heat transfer film, the component unit The interconnection, the enthalpy, and the connection between the component structure and the contact surface of the heat transfer plate are simultaneously performed by the same procedure; the interconnection of the contact surfaces of the ridge structure and the heat transfer fin, and the interconnection of the component units are completed simultaneously. Then, the connection between the component structure and the contact surface of the heat transfer plate is performed, or the contact faces of the core structure and the heat transfer fin are connected to each other, and then the mutual connection of the component units, and the component structure and heat transfer are performed. The connection of the contact faces of the plates. 『Effect of the Invention>> According to one or more embodiments of the present invention, a method for manufacturing an evaporator for a loop type heat pipe system first manufactures a core structure and a heat transfer sheet, and arranges a plurality of core structures And the heat transfer fins are then joined to a heat transfer plate, that is, a metal plate, to thereby manufacture an evaporator. With this side =, a heat transfer fin of a complicated shape or a desired shape can be easily formed, and the contact state of the core structure and the heat transfer fin can be improved, thereby expanding the 2 thermal area and the gas generation area. And minimize the thermal contact resistance between the core structure and the heat transfer fins. The above-described features and advantages of the present invention will become more apparent from the following description. 201020498 [Embodiment] A transmission line for an evaporator for a loop type heat pipe system is manufactured. A description of the circuit breaker, a gas transmission line, and a liquid. The operation of the (,,, s system is in accordance with the above-mentioned prior art 1, and the structure of the system is described in detail. The evaporator of the evaporator-made heat pipe system is the evaporator 1 of the evaporator 1 An exploded perspective view. The stack 1 includes a plurality of core structures, a plurality of heat transfer fins 20, a heat plate 50, and a cover member 60. - a thin plurality of core structures 1G having fine pores, and Each of the H 22 heat transfer pieces 2G each has a core structure connecting the shape of the structure #H, and the connector can be connected to the reduced structure 1〇. The pieces 2〇 are connected to each other to form the component unit 3. Φ Figure 2 is a flat configuration of a plurality of component units 3 () forming - assembly structure 4 〇 (refer to the heat transfer plate 5G is connected to the bottom of the assembly structure 4 〇. Self-teaching 金属 顾 且 and the material is connected to the source and received parts such as - The central processing unit of the computer: - display t ίίο:: is attached to the top surface of the heat transfer plate 50. The cover member 60 forms an internal space with the plate 5' to place the component structure 40 therein. Cover 11 201020498 Cover member 60 A gas line connection hole 62 for connecting to the gas transmission line is formed on the side surface, and the cover member 6〇 A liquid line connection hole 64 for connecting to the liquid transmission line is formed on the top surface. Meanwhile, in the module structure 40, the core structure 10 and the heat transfer fins 20 are connected to each other to form a core structure 1 and The heat transfer fins and the gas passage between the canines 26 and 28, therefore, the gas generated by the core structure can be discharged through the gas line connection hole 62 of the cover member 60. The evaporator 1 having the above structure The operation will be described below. ❹ A liquid working fluid is injected into the evaporator through the liquid wire connection hole 64, and penetrates into a plurality of holes formed in the interior of the core structure. The plate 50 is transferred to the heat of the cymbal sheet 2 to be transferred to the core structure 1 〇 to change the working fluid from the liquid phase: the counter bore 62 is discharged to the outside by the hair splicer 1 The loop type manufacturing method having the above structure will be described below with reference to FIGS. 7 to 12. The operation of the circuit type ageing system includes the operation of the k-party heat transfer rotor ( Operation S2), forming multiple illusions, linking multiple The operation of the unit ('operation (operating the age of the assembly structure (operation S5)), forming -S6), and the operation of the remote structure and the structure of the structure (option and connection-heat transfer plate operation (operation (7). Naked work 12 201020498 A porous structure with a large number of internal pores. The working fluid penetrates into the heat energy of the heat fins to make a description of the fluid phase, and the core structure of the present embodiment is a seven-piece, eight-plate, However, the shape may be changed as needed. For the four-corner flat structure, the core structure 10 may use at least one selected from the group consisting of gold metal powder, metal fiber, and non-gold knife fine material, and heart (^) genus fibers. The material in the wire is miscellaneous, and the wire is added to the selected material. In other words, heat or pressure is applied: 2 = material to obtain the desired shape. One step to the selection of the = = fine structure 1G (10) for S1) can be referred to as the pre-formed structure 10 by using metal powder and in the operation of forming the core structure 10 and containing copper, dragon : The component 'is made like a metal wire or a metal fiber, and is made at the end. Metal powders such as Xing, Bronze, Record, Chin, Ming, and Stainless Steel, which are selected from metal powders and metal fibers, but must contain two or more types of metal powders, or A mixture of powder and metal fibers. One of the heat and pressure to the selected material to obtain the desired or mold and r, the metal or metal fiber is filled into a jig and then 'heat and pressure is applied either or both.烧结 to sintering,: InΪld to form the desired shape. When heated, the farmer can then use a sintered metal or heat to a pre-sintering temperature below the sintering temperature of 13 201020498 to sinter the metal. The metal is sintered at the sintering temperature, and the pre-sintering temperature is from about 8% to about 90% of the sintering temperature at which the metal has been entangled. Similarly, when pressurizing to the metal to obtain the desired shape, a method of fiUing a jig or a mold can be used and pressure is applied to the mold or jig. At this time, the core structure formed of the metal powder or the metal fiber is a sintered body of the sintered body. (4) The New Structure 1〇=, ? program can be performed in operation S1, or in the subsequent operation of the operation of the component unit (operation (4), operation of the joint assembly structure (operation S6), and the connection heat transfer plate In the step (S7), the core structure 1G is heated to the sintering temperature during the sintering process. In other words, in the operation (S1) for forming the core structure, ", in the case of the program" The subsequent application of the towel is lower than the sintering temperature, and the temperature is reached to a high quality state. However, in the sintering process, the operation is not performed in the operation of forming the core structure (S1), and then in the subsequent operation procedure. Test (four) age program, recording temperature _ heat applied to: the subsequent operating procedure 'this can be achieved at this time - the excellent joint state of the contact surface. At the same time, by selecting at least one of non-metallic powder and non-metal fiber to form The core structure of the desired shape is 1G, and then at least one of the pressures is applied to the selected material. The above non-metallic powder example may comprise a ceramic-based bismuth aluminum oxide (Al2〇3) powder, a carbon Quality life Carbon powder and a carbonaceous 201020498 = graphite powder. This is filled with non-metallic powders and non-metallic fibers - the shape == after applying heat or pressure or both to the fixture or mold to m The non-metallic material to form the core structure of the core structure 1G formed of a non-metallic material and the heat transfer fins formed by the metal material may not be able to pass through the subsequent core structure (1). The operation of the inter-domain wire-connecting unit of the sheet is the connection of the unit, so that the core structure and the heat transfer sheet are subjected to pressure to expand the contact area of the two. In the operation (S1) of forming the core structure 10 of the present embodiment, the = plastic polymer and the organic material are mixed with the material of the crucible to form a grade 1 lion with the desired boot, and the money is re-applied. Heating and manpower - to this mixture. This thermal hybrid polymer is similar to the adhesive polyimide material, which contains polyethylene, polypropylene, propylene, and styrene. This pyropolymer increases the viscosity of the haze before the conversion. And minimize the occurrence and volume change during the sintering operation. The conformation structure 10 is formed by mixing a thermoplastic polymer and a sublimation material with a solvent and a material selected from the group consisting of a non-metal powder and a non-metal material, followed by injection or pressurization. 6 The organic solvent is a sublimation substance, which is solid at room temperature and is heated at a pre-twist temperature _ from _ to a vapor state. The dopant material can be used as an organic solvent such as naphthalene, ether or alcohol, or both. Organic solvents are commonly used to make complex shapes that are generally difficult to form. Since 201020498, the organic solvent is added before the forming operation, and the shape of the formed body after the organic solvent is added is regenerated during the sintering process to produce the desired shape. Similarly, in the operation (S1) of forming a core structure in which the metal is a mixture of a thermoplastic polymer and an organic solvent, the mixed thermoplastic polymer is completed when the formation of the desired core structure is completed. Or the mixed organic solvent can be removed by the method of dissolution and the secret method. After the operation of the loop heat pipe system, the remaining thermoplastic polymer solvent may react with the working fluid, causing ship, pollution, or non-condensation. Therefore, this residue must be removed. In the operation (S2) of "Gu" #, a plurality of heat transfer sheets 2'' each having a heater 22 are formed, and the core structure 1020 is connected by a 工7 connector 22 (refer to Fig. 9). The heat transfer 'the ruling piece of the heat coefficient of the metal and ^18 machine), etc. to process the relatively high-conductivity metal processing branch is used. Matter 10. The heat energy received by the plate 50 is transmitted to the core structure. The ice and the plurality of protrusions % and one end of the bottom member 24 protrude upward. The protrusion 26 and the 16 201020498 -----I-- form a space. This space is used as a passage for the oxygen body generated in the core structure 10. The formation of heat transfer 2G material and the transfer plate 50 2 of the 'protrusions 26 and 28 and the core structure connector β Valley easy to make ia a more complex shape, and can adjust the thickness of the chain to - The degree of need. The order in which the surface of the &<>> forms a core-like operation (S1) and the formation of heat transfer (S2) can be reversed.

其次,進行形成該組件單元之操作(S3)。 在=成該組件單元之操作(S3)、中,將蕊狀結構物1〇 入至傳論片2G之蕊狀結構物連結器22以形成組 元30 ’如圖10所示。 同時’在本實施例中,形成該組件單元之操作(S3) 更包括.在蕊狀結構物1〇嵌入至傳熱韓片2 物連結器22之前,先嵌入一連結催化劑以置於; 10及傳熱縛片20之間的接觸介面的至少一部份上。在嵌 入該連結催化劑的操作中,該連結催化劑被置於 20與蕊狀結構物1〇相互接觸的接觸介面上。由於此連结 催化劑,蕊狀結構物10及傳熱鰭片2〇之間的接觸介面^ 成金屬鍵結。 選用金屬粉末與連結材料之一作為連結催化劑。在使 用連結催化劑的情形下,在施加熱及壓力之一至組件單元 時的連結該組件單元之操作(操作S4)中將熱施加至組件 單元。 以下述的方法將金屬粉末做為連結催化劑。 17 201020498 f嵌人至傳_^^之餘結構物連 :器22之刚,將金屬粉末嘴讓於突起物26及28之間、盘 面上。之後’再將蕊狀結構物ι〇叙入; ^當丨猫私及28之間。由於金屬粉末為具有微米級直徑的 屬粉末噴麗於相應的傳熱簿片2〇的表 構物i〇m蕊狀結構物10時’金屬粉末可置於蕊狀結 插相應1 傳熱則2G的表面,且隨後可將該 構物10插入至傳熱鰭片20中。 相互粉末置於蕊狀結構物10及傳_片20 相互接觸的接觸細上的放大剖面圖。 作時金屬粉末的金屬可以相同或不同於形成操 的材=連結材料可料連結催㈣。其中包含 一焊料為主 嵌入材料或其他材料被嵌入於蕊狀結構物ι〇 二時形成的空間中。換言之,-材料依據 入至上2G之基材的熔點而被選用並叙 及傳熱。舉^子,#‘餘結構物10 傳熱ϋ 20 A麵:形成或當蕊狀結構物10由鎳形成且 ψ, ΖΙ u 形成’此連結材料可包含的焊料為主的材 且傳^韓片^二或斜。當蕊狀結構物1G由不銹鋼形成 料、金谭料、銘炫粗形成,此連結材料可包含銀焊料、錄焊 抖鉑烊料、鋁焊料、鐵焊料等。 201020498 同時’一聚合黏著劑或一黏著聚合材料,也就是包括 聚乙稀、聚丙烯、丙烯樹脂、以及苯乙烯樹脂的熱塑性聚 合物’可作為連結催化劑使用。 構物10雜觸面及傳熱鰭片20的接觸面互相連結。此時, 該組件單元的操作(S3)包含技入該連結催化劑 的知作,則接觸面的連結可變成高硬度的狀態。 在連結該組件單元的操作(S4)中,至少施加熱及壓 力之至組件單元以使蕊狀結構物1〇的接觸面及傳熱鰭 片20的接觸面互相連結。換言之,可施加熱至組件單元 3一0’或在組件單元3〇的上下左右方向中施加壓力至組件單 ❹ 1 30,或施加熱及壓力此二者至組件單元30,以使蕊狀結 構物10的接細而》屈益蚀U— jli. -la 加熱時的溫度依據形成該蕊狀結構物 1〇的材料來做Next, an operation of forming the component unit is performed (S3). In the operation (S3) of the component unit, the core structure 1 is inserted into the core structure connector 22 of the argument sheet 2G to form the unit 30' as shown in Fig. 10. Meanwhile, in the present embodiment, the operation (S3) of forming the component unit further includes: embedding a bonding catalyst to be placed before the core structure 1 is embedded in the heat transfer film connector 22; And at least a portion of the contact interface between the heat transfer tabs 20. In the operation of embedding the linked catalyst, the bonded catalyst is placed on a contact interface where 20 and the core structure 1 are in contact with each other. Due to this bonding catalyst, the contact interface between the core structure 10 and the heat transfer fins 2 is metal-bonded. One of the metal powder and the joining material is selected as the linking catalyst. In the case of using a bonding catalyst, heat is applied to the module unit in the operation of joining the module unit (operation S4) when one of heat and pressure is applied to the module unit. The metal powder was used as a linking catalyst in the following manner. 17 201020498 f embedded in the _ ^ ^ after the structure of the structure: the device 22, the metal powder mouth between the protrusions 26 and 28, on the disk. After that, the rhythm structure is re-introduced; ^ when the cat is between the private and 28. Since the metal powder is a micron-sized genus powder sprayed on the corresponding heat transfer sheet 2〇's surface structure i〇m core structure 10' metal powder can be placed in the core-like knot corresponding to 1 heat transfer The surface of 2G, and then the structure 10 can be inserted into the heat transfer fins 20. An enlarged cross-sectional view of the mutual powder placed on the contact fines of the core structure 10 and the sheet 20 in contact with each other. The metal of the metal powder may be the same or different from the material forming the operation = the joining material may be linked (4). It contains a solder-based embedded material or other material that is embedded in the space formed by the core structure. In other words, the material is selected and heat transfer based on the melting point of the substrate into the upper 2G. ^^,#'余结构10 Heat transfer ϋ 20 A face: formed or when the core structure 10 is formed of nickel and ψ, ΖΙ u forms 'the solder which can be contained in this joint material and is transmitted to Han Pieces ^ two or oblique. When the core structure 1G is formed of a stainless steel forming material, a gold tantalum material, and a magenta thick, the joining material may include silver solder, a recording solder vibrating platinum material, aluminum solder, iron solder, and the like. 201020498 Meanwhile, a polymeric adhesive or an adhesive polymeric material, that is, a thermoplastic polymer comprising polyethylene, polypropylene, propylene resin, and styrene resin can be used as a linking catalyst. The contact faces of the structure 10 hetero-contact surface and the heat transfer fins 20 are connected to each other. At this time, the operation (S3) of the module unit includes a known technique of incorporating the catalyst, and the connection of the contact faces can be made into a state of high hardness. In the operation (S4) of joining the unit units, at least heat and pressure are applied to the unit unit to connect the contact faces of the core structure 1 and the contact faces of the heat transfer fins 20 to each other. In other words, heat can be applied to the module unit 3 - 0' or pressure can be applied to the assembly unit 1 30 in the up, down, left and right directions of the unit unit 3, or both heat and pressure can be applied to the unit unit 30 to make the core structure The temperature of the object 10 is the same as that of the material forming the core structure.

操作下進行來適當地設定。 10的材料為金屬,加熱 前操作下進行或稍後的 开>成該組件結構的操作(s5)中Perform the operation and set it appropriately. The material of 10 is metal, which is carried out under the pre-heating operation or later (in the operation of the assembly structure (s5))

說'狀結構物12被配置於相鄰的 ❹ 形成該組件結構的操作(S5) =30間配”間蕊狀結構物 :40的示意圖,其中該中間 '的紐件單元之間。藉著加 201020498 w)pu 入該中間蕊狀結構物12,可擴大傳熱區域及氣體產生區 域。 同樣地’也可利用隔離物(spacers)來代替中間蕊狀結 構物12。圖13至圖16為二個組件結構40a及40b的示意 圖,其中多個隔離物配置於組件單元之間。組件單元間的 隔離物所形成的空間作為氣體通道’由此可允許蕊狀結構 物10中所產生的氣體平穩地排出至外部。It is said that the 'structure 12 is disposed adjacent to the ❹ to form the structure of the assembly (S5) = 30 between the "rock" structure: 40, wherein the middle ' between the unit units. Adding 201020498 w)pu into the middle core structure 12, the heat transfer area and the gas generating area can be enlarged. Similarly, spacers can be used instead of the middle core structure 12. Fig. 13 to Fig. 16 A schematic view of two component structures 40a and 40b, wherein a plurality of spacers are disposed between the component units. The space formed by the spacers between the component units serves as a gas passage 'which thereby allows gas generated in the core structure 10 Smoothly discharged to the outside.

在圖13及圖14中的組件結構40a中,梳狀隔離物14 配置於多個組件單元3〇a之間。這裡,分別連結於多個蕊 狀結構物10的多個傳熱鰭片20a形成為具有與先前實施例 比較下,相對極薄的厚度。因為傳熱鰭片2〇a為獨立製造, 故多個底部構件24a及多個突起物26a及28a可製造成為 具有極薄的厚度。組件單元30a間的多個氣體通 隐 離物14而形成。 固〇及圖16為包含多個隔離物16的組件結構示^ 圖,不同於圖13及圖14之實施例。在此組件結構°14/中‘!In the assembly structure 40a of Figures 13 and 14, the comb spacers 14 are disposed between the plurality of component units 3a. Here, the plurality of heat transfer fins 20a respectively joined to the plurality of core structures 10 are formed to have a relatively extremely thin thickness as compared with the prior embodiment. Since the heat transfer fins 2a are independently manufactured, the plurality of bottom members 24a and the plurality of protrusions 26a and 28a can be manufactured to have an extremely thin thickness. A plurality of gases between the module units 30a are formed by the concealment 14. The solid structure and FIG. 16 are assembly structural diagrams including a plurality of spacers 16, which are different from the embodiments of FIGS. 13 and 14. In this component structure °14/zhong ‘!

=鱗片2%包括-底部構件24b*多個具有極薄的厚/ 26b及28b。多個組件單元4Gb間的氣體通道1 因隔離物16而形成。 齡^時’為了形成氣體通道15及17,可使用具有鱼R Z i16相似形狀的治具(未圖示)以作為隔離物1 結構連結至傳熱板則,料可由組件結H中Γ、㈣ 同樣地’形成組件結構之操作(S5)更包括施加々 20 201020498 方向的壓力至組件結構40之操作,也就是組件單元可在此 方向上配置為一列,因此使蕊狀結構物10中的孔徑縮小。 圖17為以箭頭標明加壓方向的示意圖。 圖18為以箭頭指示的方向中加壓一非加壓的細孔以 而使蕊狀結構物10中之細孔18之直徑的長度由D〇縮小 至D1的情形。此縮小的細孔18即使在壓力移除後仍維持 在壓縮的狀態’原因為根據蕊狀結構物1〇的材料而發生的 塑膠形變。 凝狀結構物10作為藉由毛細壓力而輸送工作流體至 蒸發器介面的功能。此時,當細孔18之直徑收縮,換言之, 當直徑減小,毛細壓力可增加,因而加速傳輸工作流體至 發生蒸發之蒸發介面。因此,可增加冷卻效率。 再者,依據其他實施例,形成該組件結構之操作(S5) 更包括配置壓力元件,可用來施加壓力於組件結構4〇的任 =侧面方向中《«此壓力元件可在組件結構4〇之任一測的水 平方向中加壓,且可使蕊狀結構物10中細孔的孔徑縮小。 如圖19說明,此壓力元件可為一四方形框架,或 y為銜接於組件結構4〇之任一侧面方向中的夹緊件(未 示於圖)且可經由螺絲等來拉緊該組件結構40。 同樣地’可形成一水平穿透此組件結構之穿透孔, 件置在穿透孔之中以在水平方向中加壓至此組 在連結該Μ件結構之操作(S6)巾至少施加熱及屋 力之一至崎結構4㈣使各組件單元3G互相連接。 21 201020498 4。二::藉壓著===著在組件结構 將組件單元30 力^崎結構仙, ^ ^所示,在連結該傳熱板之操作中(S7),组杜 二 =雜加熱、-熱: 面。 先,。構4G之接觸表面及傳熱板50的接觸表 此時’根據傳熱板50的材料的性質, ❹ 40 ^ 至傳=^:=)後,-遮一 統的=的3?5^7實==,迴路式熱管系 至S7的操作順序並非必須遵守。換古之操;先J而’ S1 =;Ϊ?物之操作(S1),形成傳_片之操作(J), ❹ 二:及在連結傳熱板之操作(===:: 或熱及=】4。,、及87操作中使用熱及勤之-, (S1) ^ 形成組件結構之操作(S5),隨後二:=)之二及 22= Scale 2% includes - bottom member 24b * multiple with very thin thickness / 26b and 28b. The gas passage 1 between the plurality of component units 4Gb is formed by the separator 16. At the age of 'in order to form the gas passages 15 and 17, a jig (not shown) having a similar shape of the fish RZ i16 can be used as the spacer 1 structure to be bonded to the heat transfer plate, and the material can be assembled from the assembly H, (4) Similarly, the operation of forming the component structure (S5) further includes applying the pressure in the direction of 々20 201020498 to the operation of the component structure 40, that is, the component units can be arranged in a row in this direction, thus making the aperture in the core structure 10 Zoom out. Fig. 17 is a schematic view showing the direction of pressurization by arrows. Fig. 18 is a view showing a case where a non-pressurized fine hole is pressed in a direction indicated by an arrow to reduce the length of the diameter of the fine hole 18 in the core structure 10 from D 至 to D1. This reduced pore 18 is maintained in a compressed state even after the pressure is removed. The reason is that the plastic deformation occurs according to the material of the core structure. The condensed structure 10 functions as a working fluid to be delivered to the evaporator interface by capillary pressure. At this time, when the diameter of the pores 18 is contracted, in other words, as the diameter is decreased, the capillary pressure can be increased, thereby accelerating the transfer of the working fluid to the evaporation interface where evaporation occurs. Therefore, the cooling efficiency can be increased. Furthermore, according to other embodiments, the operation of forming the assembly structure (S5) further comprises configuring a pressure element for applying pressure in any of the side directions of the assembly structure 4" "This pressure element can be in the assembly structure 4" The pressure is applied in any of the measured horizontal directions, and the pore diameter of the pores in the core structure 10 can be reduced. As illustrated in Figure 19, the pressure element can be a square frame, or y is a clamping member (not shown) that engages in either side of the assembly structure 4〇 and can be tensioned via screws or the like. Structure 40. Similarly, a through hole penetrating through the structure of the module can be formed, and the member is placed in the through hole to be pressed in the horizontal direction to the group. At least the heat is applied to the operation of joining the member structure (S6). One of the house forces to the Kakisaki structure 4 (4) connects the component units 3G to each other. 21 201020498 4. Two:: By pressing === in the component structure, the component unit 30 is shown in the structure of the force unit, ^ ^, in the operation of joining the heat transfer plates (S7), group Du 2 = miscellaneous heating, - heat : Face. first,. The contact surface of the 4G contact surface and the heat transfer plate 50 is at this time 'according to the nature of the material of the heat transfer plate 50, ❹ 40 ^ to pass = ^:=), after the cover of the unified = 3? 5 ^ 7 ==, the order of operation of the loop heat pipe to S7 is not mandatory. For the ancient operation; first J and 'S1 =; Ϊ? the operation of the object (S1), the formation of the transmission _ film operation (J), ❹ 2: and the operation of the connection heat transfer plate (===:: or heat And ==4,,, and 87 use heat and diligence -, (S1) ^ to form the operation of the component structure (S5), then two: =) two and 22

傳熱板50與-電子零件(未示於圖熱源相連接, 以接收源自於電子零件的熱能。此接㈣熱能再傳輸至傳 熱鰭片20,而後傳輸至蕊狀結構# 1〇。由於此熱能傳輸至 具有細孔的蕊狀結獅,使得存在於細孔騎態工作流體 汽化,隨後經配置於蕊狀結構物1〇上的氣髏通路,再經氣 體線而至冷凝器。此卫作㈣在冷凝器巾向外散熱後液 化,而後再經由液態線供給至蕊狀結構物1〇。重複上述的 過程使電子零件冷卻。 201020498 (S4)及連結組件結構之操作(S6)可於同一過 進行,而後連結傳熱板之操作(S7)可分開實行。 、 或者,首先進行形成蕊狀結構物之^ 傳熱鰭片之操作(S2)’形成組件單元之操作( 形成組件結構之操作(S5),隨後,進行連結組件單元之 操作(S4)’轉連輪件結構之操作(s6)與連 板之操作(S7)可於同一過程中同時進行。 …、 以先前本實施例提到的方法所製造的用於迴路式熱 系統的蒸發器的操作,以下將做簡短描述。 … 先前提到用於迴路式熱管系統的蒸發器的製造方法的 效能將做以下描述。 ,根據本發明之實施例,傳熱鰭片連結於蕊狀結構物以 形成:獨立的構件’蕊狀結構物與傳熱板互相連結形成一 組件單元,多個組件單元水平配置以形成一組件結構而 後此組=結構再與傳熱板連結。因此,可製造各種形狀及 尺寸的蕊狀結構物及傳熱鰭片,以使蕊狀結構物及傳熱鳍 23 201020498 Wjpu 片間的熱接觸阻抗最小化。 換έ之,與習知技術比較,習知技術的所有的突起物 皆直接形成於傳熱板上,但在本實施例中,因為傳熱鰭片 以獨立構件製成,故可形成形狀較複雜的傳熱鰭片,且形 成具有極薄厚度的傳熱鰭片。 依據習知技術,蕊狀結構物與散熱鰭片之間的黏著性 只能以調整蕊狀結構物與傳熱鰭片間的容限(tolerance)或 類似的方式來增加,而限制了蕊狀結構物與傳熱鰭片之間 的黏著性的增加。然而,在本發明之實施例中,蕊狀結構 ® 物與傳熱鰭片之間的黏著性可增加,則可促使氣體的產生 而使蒸發器具有優良的功效。 同樣地,在本發明之實施例中,可很容易調整傳熱鰭 片的厚度,而可找到適用於氣體通道的尺寸來使用。再者, 可依據蕊狀結構的厚度來製造傳熱鰭片,如此,可使用一 薄蕊狀結構物以適當地調整氣體產生區域及傳熱區域而 得出一最佳的結構。 在本發明之實施例中,前述所提容易執行的最佳的結 ❹ 構可最大化加_域及氣體產生區域,並使蕊狀結構物^ 包括突起物之傳熱鰭片間的熱接觸阻抗最小化。如此,迴 路式熱管系統之總熱阻抗可降低。 如蕊狀結構物由金屬組成,則之蕊狀結構物與傳熱鰭 f之間的連結與傳熱鰭片及傳熱板之間的連結,不能=簡 單以實際接觸相對應的接觸面來達成,而應以熱及壓力之 一或二者所達到的金屬耦合來達成。如此,該接觸介面上 24 201020498 的熱接觸阻抗可降低。 根據習知的技術,在燒結的蕊狀結構物形成之後,此 燒結的蕊狀結構以物理方式嵌入至並連結於作為傳熱鰭片 的基底的突起物之間。由此,即使燒結的蕊狀結構物與基 底之間的接觸面的尺寸可增大,但此燒結的蕊狀結構物與 基底的突起物之間的接觸面中的連接是由點接觸而非面接 觸來達成,而使接觸面的狀態惡化,使得接觸面中的實際 熱阻抗相對地高,且難以平穩地將熱由熱源傳輸至燒結的 蕊狀結構物。 然而,在本實施例中,蕊狀結構物與傳熱鰭片之間的 接觸表面非以簡單的物理連結來達成,而改以金屬麵合來 達成,其中金屬略微熱熔化。如此,比較習知技術,在本 • 實施例中之熱接觸阻抗可大幅降低,使電子零件即熱源可 在低溫度下操作。 ^ '' 在此同時,在本實施例中,蕊狀結構物與傳熱鰭片無 直接接觸熱源’因此,能夠自由地調整傳熱韓片之結構, ® 蕊狀結構物之厚度與寬度等。換言之,在形成該傳熱鰭片 與蕊狀結構物方面,每一蕊狀結構物及傳熱韓片的厚度及 整個寬度可很容易地調整,以使傳熱區域與氣體產生區域 儘可能大。 當同時加熱及壓力以使蕊狀結構物及傳熱鰭片互相連 接時’此互相連結會變得非常堅硬而使接觸介面的熱阻抗 降低。 同樣地’因組件結構被水平加壓,蕊狀結構物中的細 25 201020498 孔之孔徑縮小,因此增加了毛細吸取力,結果使工作流體 可平穩地流動。 根據本發明之實施例,傳熱鰭片的形狀可改變且可配 置隔離物於組件單元之間。由於此構造,能夠將每一組件 的形狀自由地改變以使氣體可以平穩地排出至外部。 參 圖21至圖23為本發明之其他實施例,分別對應一修 改的傳熱鰭片2〇c、一組件單元3〇c及一組件結構4此之 不意圖。與圖9的傳熱鰭片比較,此實施例之傳熱鰭片2〇c 不包括置於傳熱鰭片2〇c 一側之突起物,只包括另一侧的 突起物28c,及一底部構件24c。 圖22至圖23分別為對應於連結一傳熱鰭片2〇c 狀結構物10 %得的組件單元30c,以及將組件單元3〇(:水 平配置而形成的組件結構4〇c的示意圖。 2本剌之實施例,之上賴㈣方法亦可以同樣 地用來製造該組件結構40c。 本發發明已以實施例揭露如上,然:其並非用以限定 本發明之精 視後附之申請專利範圍所界定者為準。 圖1為一般迴路式熱管系統的示意圖。 圖2至圖4為—種習知技術的示意圖。 關圖2至圖4中的介面及蕊狀結構物間的接觸 26 201020498 圖6為本實關之迴路·管线的蒸《的製造方法所 製造的蒸發器的透視分解圖。 圖7為本實_之迴路式熱管綠喊發器的製造方法的 流程圖。 圖8、圖9、® 10分別為對應的蕊狀結構物、傳熱 及組件單元的示意圖。 圖11為經由蕊狀結構物與傳熱鋒片間彼此 Ο e 粉末置於接觸介面時的橫剖面圖。 屬 圖12為組件結構的示意圖。 M林發抑—實施财組躲構料意圏及 為本發明另―實施财組件結構的示意圏及 =17及圖18為施加水平壓力至組件結構的示 19為本發㈣—實蝴巾& ^ 行框架的組件結構·意^ 力轉的-四邊 =20為-組件結構連結_傳熱板的示意圖。 片:二23分別為對應本發明另-實施例_ 片組件早疋、以及組件結構的示意圖。 得4 【主要元件符號說明】 1 ' 114 ·_蒸發器 1〇 · ‘游狀結構物 12 :中間蕊狀結構物 14、16 :隔離物 27 201020498 15、17 :氣體通道 18 :細孔 20、20a、20b、20c :傳熱鰭片 22 :蕊狀結構物連結器 24、24a、24b、24c :底部構件 26、28、26a、26b、28a、28b、28c、120 :突起物 29 :組件單元的底面 30、30a、30b、30c :組件單元 40、40a、40b、40c :組件結構 42 :四邊形框架 50 :傳熱板 60 :遮蓋件 62 :氣體線連接孔 64 :液體線連接孔 110 :迴路式熱管系統 112 :冷凝器 116 :氣體線 118 :液體線 410 :蕊狀結構物 D0 :未壓縮細孔的孔徑 D1 :壓縮後細孔的孔徑The heat transfer plate 50 is connected to an electronic component (not shown in the figure to receive thermal energy originating from the electronic component. This heat transfer is then transmitted to the heat transfer fin 20 and then to the core structure #1〇. Since the heat energy is transmitted to the core-like lion with pores, the working fluid existing in the fine hole is vaporized, and then the gas passage disposed on the core structure 1 is passed through the gas line to the condenser. The vinegar (4) is liquefied after the condenser towel is radiated outward, and then supplied to the core structure via the liquid line. The above process is repeated to cool the electronic component. 201020498 (S4) and operation of the joint assembly structure (S6) The operation may be performed in the same manner, and then the operation of joining the heat transfer plates (S7) may be performed separately. Alternatively, the operation of forming the heat transfer fins (S2) of forming the core structure (the operation of forming the component unit) (forming the assembly) Operation of the structure (S5), subsequently, the operation of joining the component units (S4) 'the operation of connecting the wheel structure (s6) and the operation of the connecting plate (S7) can be simultaneously performed in the same process. Method mentioned in the examples The operation of the evaporator for the loop type thermal system manufactured will be briefly described below. The efficiency of the manufacturing method of the evaporator previously used for the loop heat pipe system will be described below. According to the practice of the present invention For example, the heat transfer fins are coupled to the core structure to form: a separate member 'the core structure and the heat transfer plate are interconnected to form a component unit, and the plurality of component units are horizontally arranged to form a component structure and then the group = structure Then, it is connected to the heat transfer plate. Therefore, the core structure and the heat transfer fins of various shapes and sizes can be manufactured to minimize the thermal contact resistance between the core structure and the heat transfer fin 23 201020498 Wjpu sheet. Compared with the prior art, all the protrusions of the prior art are directly formed on the heat transfer plate, but in the embodiment, since the heat transfer fins are made of independent members, the shape can be formed more complicated. Heats the fins and forms heat transfer fins having a very thin thickness. According to the prior art, the adhesion between the core structures and the heat dissipation fins can only be adjusted between the core structure and the heat transfer fins. Capacity Tolerance or the like increases, limiting the increase in adhesion between the core structure and the heat transfer fins. However, in an embodiment of the invention, the core structure and heat transfer fins The adhesion between the two can be increased to promote the generation of gas and the evaporator has excellent efficiency. Similarly, in the embodiment of the present invention, the thickness of the heat transfer fin can be easily adjusted, and can be found to be suitable for The size of the gas passage is used. Further, the heat transfer fin can be manufactured according to the thickness of the core structure, so that a thin core structure can be used to appropriately adjust the gas generation region and the heat transfer region to obtain the most Optimum structure. In the embodiment of the present invention, the above-mentioned optimum structure which is easy to perform can maximize the addition domain and the gas generation region, and the core structure includes heat transfer fins of the protrusions. The thermal contact resistance between the two is minimized. As such, the total thermal impedance of the loop heat pipe system can be reduced. If the core structure is composed of metal, the connection between the core structure and the heat transfer fin f and the heat transfer fin and the heat transfer plate cannot be simply combined with the actual contact surface. Achieved, but should be achieved by metal coupling achieved by one or both of heat and pressure. As such, the thermal contact resistance of the contact interface 24 201020498 can be reduced. According to a conventional technique, after the sintered core structure is formed, the sintered core structure is physically embedded and joined between the protrusions as the base of the heat transfer fin. Thereby, even if the size of the contact surface between the sintered core structure and the substrate can be increased, the connection in the contact surface between the sintered core structure and the protrusion of the substrate is by point contact instead of The surface contact is achieved, and the state of the contact surface is deteriorated, so that the actual thermal impedance in the contact surface is relatively high, and it is difficult to smoothly transfer heat from the heat source to the sintered core structure. However, in the present embodiment, the contact surface between the core structure and the heat transfer fins is not achieved by a simple physical connection, but is achieved by metal face bonding in which the metal is slightly thermally melted. Thus, by comparing the conventional techniques, the thermal contact resistance in the present embodiment can be greatly reduced, so that the electronic component, i.e., the heat source, can be operated at a low temperature. ^ '' At the same time, in this embodiment, the core structure and the heat transfer fins are not in direct contact with the heat source. Therefore, the structure of the heat transfer film can be freely adjusted, and the thickness and width of the core structure are . In other words, in forming the heat transfer fin and the core structure, the thickness and the entire width of each of the core structure and the heat transfer sheet can be easily adjusted so that the heat transfer region and the gas generation region are as large as possible. . When heating and pressure are simultaneously applied to connect the core structure and the heat transfer fins to each other, the interconnection becomes very hard and the thermal impedance of the contact interface is lowered. Similarly, since the assembly structure is horizontally pressurized, the pore diameter of the fine 25 201020498 hole in the core structure is reduced, thereby increasing the capillary suction force, and as a result, the working fluid can smoothly flow. According to an embodiment of the invention, the shape of the heat transfer fins can be varied and the spacers can be disposed between the component units. Due to this configuration, the shape of each component can be freely changed so that the gas can be smoothly discharged to the outside. 21 to 23 are other embodiments of the present invention, which respectively correspond to a modified heat transfer fin 2〇c, a component unit 3〇c, and a component structure 4. Compared with the heat transfer fin of FIG. 9, the heat transfer fins 2〇c of this embodiment do not include the protrusions placed on the side of the heat transfer fins 2〇c, only the protrusions 28c on the other side, and one Bottom member 24c. 22 to 23 are respectively a component unit 30c corresponding to 10% of a heat transfer fin 2〇c-like structure, and a schematic view of the assembly unit 4〇c formed by the assembly unit 3〇. In the embodiment of the present invention, the above method can also be used to manufacture the component structure 40c. The present invention has been disclosed in the above embodiments, but it is not intended to limit the application of the present invention. The figure defines the schematic of the general loop heat pipe system. Fig. 2 to Fig. 4 are schematic diagrams of the prior art. The contact between the interface and the core structure in Fig. 2 to Fig. 4 26 201020498 Fig. 6 is a perspective exploded view of the evaporator manufactured by the method for manufacturing the circuit of the actual circuit and the steaming of the pipeline. Fig. 7 is a flow chart showing the manufacturing method of the loop type heat pipe green shouting device of the present invention. 8. Figures 9 and 10 are schematic diagrams of the corresponding core structure, heat transfer and component unit. Figure 11 is a cross section of the powder interface between the core structure and the heat transfer front. Figure 12 is a schematic diagram of the structure of the component. Inhibition - implementation of the financial group hiding material meaning and the implementation of the invention - the implementation of the financial component structure and = 17 and Figure 18 is the application of horizontal pressure to the structure of the assembly 19 is the hair (four) - real scarf & ^ The structure of the frame of the frame · the meaning of the four-sided = 20 - component structure connection _ heat transfer plate schematic. The film: two 23 respectively correspond to the invention - the embodiment _ piece assembly early, and the component structure Fig. 4 [Description of main component symbols] 1 '114 ·_Evaporator 1〇· 'Swim structure 12: Intermediate core structure 14, 16: Spacer 27 201020498 15,17: Gas channel 18: Fine Holes 20, 20a, 20b, 20c: heat transfer fins 22: core structure connectors 24, 24a, 24b, 24c: bottom members 26, 28, 26a, 26b, 28a, 28b, 28c, 120: protrusions 29 The bottom surface 30, 30a, 30b, 30c of the module unit: the unit unit 40, 40a, 40b, 40c: the assembly structure 42: the quadrilateral frame 50: the heat transfer plate 60: the cover member 62: the gas line connection hole 64: the liquid line connection hole 110: loop heat pipe system 112: condenser 116: gas line 118: liquid line 410: core structure D0: The compressed diameter of the pores D1: diameter of the pores compressed

Claims (1)

201020498 七、申請專利範園: 括: '一種用於迴路式熱管系統的蒸發器的製造方法,包 形成多個具有細孔的蕊狀結構物 形成多個分別具有一連結至多個蕊狀結構物之一的 蕊狀結構物連結器的傳熱鰭片; 將每一個蕊狀結構物分別嵌入至每一個傳熱鰭片的 焱狀結構物連結器,從而形成多個組件單元; 施加至少熱及壓力之一至該組件單元,且將該蕊狀結 構物之一接觸面與該傳熱鰭片之一接觸面做互相連… 水平配置該些組件單元,使得每一組件單元的底面可 配置於一平面上,且形成一組件結構; 施加至少熱及壓力之一至該組件結構,並將該些組件 單元互相連接;以及 配置該組件結構至一具有一平板形狀的傳熱板之頂 面上,施加熱或施加熱及壓力至頂面上的該組件結構,並 將該組件結構之一接觸面及傳熱板之一接觸面做^結:、 2.如申請專利範圍第1項所述之用於迴路 統的蒸發器的製造方法,其中該多個蕊狀結構物^勺、 含使用-種自金屬粉末、非金屬粉末、金屬纖心= 金屬纖維所組成的集合中狀的材料,然後施 = 壓力之一至該選定的材料,從而形成多個夏 夕…、 的蕊狀結構物。 、希望的形狀 3_如申請專利範圍第2項所述之料迴路式熱管系 29 201020498 =的?,、、發^|的製造方法,其中該多個蕊狀 含以一熱塑性聚合物及一有機溶劑之-來與形成包 具有希望的形狀的蕊狀結構物。“物心形成多個 1如申請專利範圍第3項所述之用於 統,發器的製造方法,其中在形成多個^熱管系 的滋狀結構物之後,多個蕊狀結構物的形 的形狀 劑抽取法和熱解法之—來移除已混合使用溶 混合的有機溶劑。 …11聚合物或已 統的^發專利第1項所狀用於迴路式孰管系 _蕊狀、構物嵌入ΐ傳熱 ==該蕊狀結構物舆該軸片間二 ❹ 如申請專利範圍第!項所述之用 統的洛發H㈣造方m缝件 =包、3 =:元之間配置一中間蕊狀結 如申請專利範圍第〗項所述之肋迴路式 發器的製造方法,其愧组件結構的形成更包含土 結構上’從而使該蕊狀結構物中的 8.如U利朗第〗項所叙臉迴路式熱管系 30 201020498 的製造方法,其中該組件結構的形成更包含配 =力元件能在該組件結構的任一侧的方 孔的孔徑縮小。德件結構,並使該蕊狀結構物中的細 統的ί發如器申41^範所述之用於迴路式熱管系 φ i組件的形成’該組件單元的形成,以及 組件傳的互相連結,該些 *的連結皆同“:構與該傳熱板的接觸 .料及Λ傳熱41片之接觸面的互相連結是 .構“傳熱而後進行該組件結 結,接觸面的互相連 ❹與該傳熱板之接觸面的連結相連結’以及該組件結構201020498 VII. Application for Patent Park: Included: 'A manufacturing method for an evaporator for a loop heat pipe system, comprising forming a plurality of core structures having fine pores to form a plurality of core structures each having a joint to a plurality of core structures a heat transfer fin of the core structure connector; each of the core structures is respectively embedded in the braid structure connector of each heat transfer fin to form a plurality of component units; applying at least heat and One of the pressures to the component unit, and one of the contact faces of the core structure and the contact surface of the heat transfer fin are interconnected... The component units are horizontally arranged such that the bottom surface of each component unit can be disposed on one Forming a component structure in a plane; applying at least one of heat and pressure to the component structure, and interconnecting the component units; and arranging the component structure to a top surface of the heat transfer plate having a flat plate shape Heating or applying heat and pressure to the assembly structure on the top surface, and one of the contact surfaces of the assembly structure and one of the contact faces of the heat transfer plate is made: 2. Applying for a patent The method for manufacturing an evaporator for a circuit according to Item 1, wherein the plurality of core structures comprise a metal powder, a non-metal powder, a metal core, and a metal fiber. The medium-like material is collected, and then one of the pressures is applied to the selected material to form a plurality of core structures. a desired shape 3_, as in the manufacturing method of the loop-type heat pipe system 29 201020498, as described in claim 2, wherein the plurality of cores contain a thermoplastic polymer and a The organic solvent is used to form a core structure having a desired shape of the package. "The formation of a plurality of core structures as described in claim 3, wherein the shape of the plurality of core structures after forming a plurality of heat-generating structures The shape agent extraction method and the pyrolysis method are used to remove the organic solvent which has been mixed and mixed. The 11 polymer or the conventional method of the first method is used for the loop type fistula system. Embedding ΐ heat transfer == the core structure 舆 between the shafts ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ ❹ The middle core-like knot is a manufacturing method of the rib-loop hair-cutting device described in the scope of the patent application, wherein the formation of the 愧-component structure further comprises a soil structure, thereby making the core structure 8. such as U Lilangdi The method of manufacturing the face loop heat pipe system 30 201020498, wherein the formation of the component structure further comprises a reduction in the aperture of the square hole on either side of the component structure. The fineness of the core structure is as described in the instrument In the formation of the loop heat pipe system φ i component 'the formation of the component unit, and the mutual connection of the components, the links of the * are the same as: "contact with the heat transfer plate, contact with the material and heat transfer 41 pieces" The mutual interconnection of the surfaces is such that the heat transfer is followed by the junction of the components, the interconnection of the contact faces is connected with the connection of the contact faces of the heat transfer plates, and the structure of the assembly
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