[go: up one dir, main page]

TWI289655B - Heat pipe - Google Patents

Heat pipe Download PDF

Info

Publication number
TWI289655B
TWI289655B TW95122728A TW95122728A TWI289655B TW I289655 B TWI289655 B TW I289655B TW 95122728 A TW95122728 A TW 95122728A TW 95122728 A TW95122728 A TW 95122728A TW I289655 B TWI289655 B TW I289655B
Authority
TW
Taiwan
Prior art keywords
section
heat pipe
heat
pipe
evaporating
Prior art date
Application number
TW95122728A
Other languages
English (en)
Other versions
TW200801436A (en
Inventor
Tay-Jian Liu
Chao-Nien Tung
Chuen-Shu Hou
Original Assignee
Foxconn Tech Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Foxconn Tech Co Ltd filed Critical Foxconn Tech Co Ltd
Priority to TW95122728A priority Critical patent/TWI289655B/zh
Application granted granted Critical
Publication of TWI289655B publication Critical patent/TWI289655B/zh
Publication of TW200801436A publication Critical patent/TW200801436A/zh

Links

Landscapes

  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Description

1289655 九、發明說明: 【發明所屬之技術領域】 本發明係關於一種熱傳導裝置,尤其係—種 【先前技術】 … 熱管因體積小、可快速輸送大量熱能、構造 量輕、無需外加作用力、壽命長、低熱阻、可遠距^ ^ 生’符合目前電腦散熱模組的需求,因此被廣泛用= 決散熱問題。其基本構造係在密閉管材内壁概以易吸收工 作流體的毛細結構層,而其中央的空間則為空洞狀離 =抽=的密閉管材内注人相當於毛細結構層孔“積 的工作流體。 償 熱官依吸熱或散熱等功能位置可區分為蒸發段、絕熱 段、冷卻段三大區段。上述熱管的工作原理是:在墓奸 之毛細結構内之飽和工作介質,吸收外部熱源的熱量= 發,由於蒸汽產生的壓差使蒸汽快速移動至冷卻段。而& 汽在冷卻段放熱而冷卻凝縮成液體。此時,凝縮的工作= 體被吸收於冷卻段之毛細結構内,由於冷卻段經絕敎段: 蒸發段的毛細管間的壓差,而回歸於冷卻段。上述工作流 體的移動及回歸過程循環運作,從而蒸發段不斷^ 向冷卻段持續性的傳輸熱量。 ^ 1見」熱管的三大區段的功能皆不同,而為了充分發 揮熱管的三大區段各自功能,使得熱管傳埶性 " 各段相應之毛細結構應滿足不同之結構需求,為此^界^ 6 1289655 I ' 在努力去改善。 【發明内容】 有馨於此,有必也 -種熱A,^.八傳熱性能較好的熱管。 該金屬管體沿管體長度方二為體」 者之間的絕熱段;適量工作;段、冷凝段及位於兩 及毛細結構,其設置於該“二入於該密封腔室内; 的脉它 n s , 屬s體内部並填滿對應蒸發段 的腔至’且至少對應絕熱段形成有蒸汽通道。 該熱管與習知熱管相 分的毛細結構係填滿的,右::有如下優點:由於蒸發段部 处而γ 、、、、 |於提昇熱管蒸發段的吸熱性 、#曰、、度並可增大回流毛細力而提高冷凝液體的 速度,從而使得熱管整體傳熱性能大幅提昇。 【實施方式】 、下 >“、、附圖,對本發明熱管予以進一步說明。 ,月 > 閱圖1及圖2 ’圖1係本發明熱管的第—實施例之 縱向截面圖’目2A係圖1中π_π部分的橫向截面圖,圖 2Β係圖1中ΠΚ[Ι1部分的橫向截面圖。該熱管包括-内有 密封腔室的管體10,其内壁面呈光滑或設有微溝槽,該管 體10内α卩设有毛細結構2〇,該腔室除了毛細結構2〇以外 的玉間則為蒸Α通道30,並管體1〇内部封入有適量工作流 體(圖未不)且可適度抽至一定的真空度。該管體10沿管 體長度方向依據其各段的使用功能可分為蒸發段4〇、冷凝 段60及位於二者之間的絕熱段5〇。 7 1289655 , ' 可以理解地’該熱管的支撐件可為如圖4a所示的沿隔 離層70周面與管體1Q管壁之間向熱管長度方向延伸的數 個ώ肋狀支撐件80a,或者如圖4Bm示的數個空心管狀支 • 撐件80b。 _請參閱圖5,係本發明熱管的第二實施例之縱向截面 圖。該實施例與第一實施例的區別在於,熱管蒸發段4〇a 位於,體l〇a中部,而冷凝段6〇a具有兩個並位於熱管兩 端,瘵發段40a與二冷凝段6〇a之間設有二絕熱段5〇a。該 冷凝段60a的填滿的毛細結構2〇a與未填滿的毛細結構之 間設有一導角23。 請參閱圖6,係本發明熱管的第三實施例之縱向截面 〜圖。該實施例與第二實施例的區別在於,該熱管兩端彎曲 -後熱管整體呈u字型,即二冷凝段6〇b平行並與蒸發段4〇b 垂直,而一絶熱段5〇b位於蒸發段4〇b兩側的彎角處。 還可以理解地,本發明上述各實施例中的毛細結構除 •了填滿以外的部分皆位於熱管中心、,而實際上該毛細結構 亦可以沿熱官内壁設置;該熱管亦可以打扁形成扁平狀, 尤其蒸發段呈扁平狀。 具有上述特徵的本發明熱管,由於蒸發段部分的毛細 結構係填滿的,有利於提昇熱管蒸發段的吸熱性能而提高 蒸發速度並可增大回流毛細力而提高冷凝液體的回流速 度,從而使得熱管整體傳熱性能大幅提昇。 综上所述,本發明符合發明專利要件,爰依法提出專 9

Claims (1)

1289655 • ' 8·如申請專利範圍第1至6中任一項所述之熱管,其中 該蒸發段位於管體的中部而管體兩端部位為冷凝段。 9·如申請專利範圍第8項所述之熱管,其中該熱管彎曲 呈U字型。 10·如申請專利範圍第1項所述之熱管,其中該毛細結構 係由複數波浪狀金屬薄片與平板狀金屬薄片在管體 周向上弧形、考曲後在管體徑向上交替堆疊形成,該二 ► 種金屬薄片對應蒸發段及冷凝段部位均設有供各金 屬薄片之間液體流道相通的通道。 12
TW95122728A 2006-06-23 2006-06-23 Heat pipe TWI289655B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW95122728A TWI289655B (en) 2006-06-23 2006-06-23 Heat pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW95122728A TWI289655B (en) 2006-06-23 2006-06-23 Heat pipe

Publications (2)

Publication Number Publication Date
TWI289655B true TWI289655B (en) 2007-11-11
TW200801436A TW200801436A (en) 2008-01-01

Family

ID=39295712

Family Applications (1)

Application Number Title Priority Date Filing Date
TW95122728A TWI289655B (en) 2006-06-23 2006-06-23 Heat pipe

Country Status (1)

Country Link
TW (1) TWI289655B (zh)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9909448B2 (en) 2015-04-15 2018-03-06 General Electric Company Gas turbine engine component with integrated heat pipe
US10356945B2 (en) 2015-01-08 2019-07-16 General Electric Company System and method for thermal management using vapor chamber
US10365047B2 (en) 2016-06-21 2019-07-30 Ge Aviation Systems Llc Electronics cooling with multi-phase heat exchange and heat spreader
US10660236B2 (en) 2014-04-08 2020-05-19 General Electric Company Systems and methods for using additive manufacturing for thermal management
CN114046680A (zh) * 2021-11-23 2022-02-15 联想(北京)有限公司 热管及其制作方法
US11260953B2 (en) 2019-11-15 2022-03-01 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11260976B2 (en) 2019-11-15 2022-03-01 General Electric Company System for reducing thermal stresses in a leading edge of a high speed vehicle
US11267551B2 (en) 2019-11-15 2022-03-08 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11352120B2 (en) 2019-11-15 2022-06-07 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11407488B2 (en) 2020-12-14 2022-08-09 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11427330B2 (en) 2019-11-15 2022-08-30 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11577817B2 (en) 2021-02-11 2023-02-14 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11745847B2 (en) 2020-12-08 2023-09-05 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US12040690B2 (en) 2020-08-31 2024-07-16 General Electric Company Cooling a stator housing of an electric machine

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10660236B2 (en) 2014-04-08 2020-05-19 General Electric Company Systems and methods for using additive manufacturing for thermal management
US10356945B2 (en) 2015-01-08 2019-07-16 General Electric Company System and method for thermal management using vapor chamber
US9909448B2 (en) 2015-04-15 2018-03-06 General Electric Company Gas turbine engine component with integrated heat pipe
US10365047B2 (en) 2016-06-21 2019-07-30 Ge Aviation Systems Llc Electronics cooling with multi-phase heat exchange and heat spreader
US11035621B2 (en) 2016-06-21 2021-06-15 Ge Aviation Systems Llc Electronics cooling with multi-phase heat exchange and heat spreader
US11267551B2 (en) 2019-11-15 2022-03-08 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11260953B2 (en) 2019-11-15 2022-03-01 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11260976B2 (en) 2019-11-15 2022-03-01 General Electric Company System for reducing thermal stresses in a leading edge of a high speed vehicle
US11352120B2 (en) 2019-11-15 2022-06-07 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11427330B2 (en) 2019-11-15 2022-08-30 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US12040690B2 (en) 2020-08-31 2024-07-16 General Electric Company Cooling a stator housing of an electric machine
US12525851B2 (en) 2020-08-31 2026-01-13 General Electric Company Cooling a stator housing of an electric machine
US11745847B2 (en) 2020-12-08 2023-09-05 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11407488B2 (en) 2020-12-14 2022-08-09 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11577817B2 (en) 2021-02-11 2023-02-14 General Electric Company System and method for cooling a leading edge of a high speed vehicle
CN114046680A (zh) * 2021-11-23 2022-02-15 联想(北京)有限公司 热管及其制作方法

Also Published As

Publication number Publication date
TW200801436A (en) 2008-01-01

Similar Documents

Publication Publication Date Title
TWI289655B (en) Heat pipe
CN101093151B (zh) 热管
KR100495699B1 (ko) 판형 열전달장치 및 그 제조방법
US8622118B2 (en) Loop heat pipe
JP3451737B2 (ja) 沸騰冷却装置
RU2005137166A (ru) Охлаждающее устройство пластинчатого типа для предотвращения высыхания
EP2713132A1 (en) A vapor-based heat transfer apparatus
US20080078530A1 (en) Loop heat pipe with flexible artery mesh
CN106949763A (zh) 一种平板热管
US20070240852A1 (en) Heat pipe with heat reservoirs at both evaporating and condensing sections thereof
CN102202488A (zh) 热管散热装置
TW201712286A (zh) 均熱板
US20180038659A1 (en) Heat pipe
CN107764118A (zh) 一种平板热管
JP3166568U (ja) 径方向排流機能を備えたヒートパイプ
CN114777540A (zh) 一种多级v形沟槽吸液芯热二极管及其加工方法
CN112113450A (zh) 一种用于航天电子散热用的振荡复合式毛细芯均热板结构
CN207881538U (zh) 一种平板热管
JP2011094822A (ja) ループ型ヒートパイプ及びこれを備えた電子機器
JP2015172474A (ja) 自励振動ヒートパイプ
JP4277312B2 (ja) サーモサイフォン
JP2006189239A (ja) ヒートパイプ
JP2005156011A5 (zh)
JP2000193385A (ja) 平面型ヒートパイプ
CN201122068Y (zh) 具有双重毛细组织的热管结构

Legal Events

Date Code Title Description
MM4A Annulment or lapse of patent due to non-payment of fees