TW201702544A - Vortex tube device - Google Patents

Vortex tube device Download PDF

Info

Publication number
TW201702544A
TW201702544A TW104121617A TW104121617A TW201702544A TW 201702544 A TW201702544 A TW 201702544A TW 104121617 A TW104121617 A TW 104121617A TW 104121617 A TW104121617 A TW 104121617A TW 201702544 A TW201702544 A TW 201702544A
Authority
TW
Taiwan
Prior art keywords
vortex tube
tube device
end member
flow guiding
hole
Prior art date
Application number
TW104121617A
Other languages
Chinese (zh)
Other versions
TWI576551B (en
Inventor
王勇智
謝錚玟
黃庭強
廖文能
Original Assignee
宏碁股份有限公司
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 宏碁股份有限公司 filed Critical 宏碁股份有限公司
Priority to TW104121617A priority Critical patent/TWI576551B/en
Publication of TW201702544A publication Critical patent/TW201702544A/en
Application granted granted Critical
Publication of TWI576551B publication Critical patent/TWI576551B/en

Links

Abstract

A vortex tube device is provided, including a main body, a hot end member, a cold end member, and a first guiding element. The man body has a first inlet and an extending portion extending along a longitudinal axis of the vortex tube device. The hot end member is connected to the extending portion, the cold end member is connected to the main body, and the hot and cold end members are disposed on opposite sides of the main body. An air flows into the main body via the first inlet and is exhausted through the hot and cold end members. The first guiding element is disposed in the main body, having a first through hole, a first surface, and several channels formed on the first surface and surrounding the first through hole. The channels respectively have a slope for guiding the air into the extending portion.

Description

渦流管裝置 Vortex tube device

本發明是有關於一種渦流管裝置,特別係有關於一種設有導流元件之渦流管裝置。 The present invention relates to a vortex tube device, and more particularly to a vortex tube device provided with a flow guiding element.

一般冷凍空調所使用的方式為壓縮式的蒸氣循環,這是利用冷媒蒸發吸熱的特性,使用壓縮機將冷媒蒸汽加壓液化後循環使用。此外,利用渦流管(vortex tube)也能產生冷凍的效果,其中渦流管不需要設置散熱鰭片且故障性低,同時不需熱機時間,也不必使用電力驅動。 Generally, the method used in the refrigerating air-conditioning system is a compression type steam cycle, which is characterized in that the refrigerant is used to evaporate and absorb heat, and the compressor is used to liquefy the refrigerant vapor and then circulate it. In addition, the effect of freezing can also be produced by using a vortex tube, in which the vortex tube does not need to be provided with fins and has low failure, and does not require heat time or electric drive.

渦流管可以應用的地方很多,只要有高壓空氣作為氣體來源,就可以產生冷空氣或熱空氣。第1圖即是一種典型的渦流管設計,其中在渦流管兩端分別設有一冷空氣出口C和一熱空氣出口H,操作時可將高壓空氣由噴嘴N注入渦流管中(如第1圖中的箭頭A所示),由於管內的壓力接近大氣壓,因此離開噴嘴N後之空氣會迅速膨脹,且在渦流管內形成一個強制渦流(forced vortex),此時接近渦流管中心部分的空氣會對外側部分的空氣做功而使其本身溫度下降;相反地,接近渦流管外側部份的空氣溫度則會上升。如第1圖所示,在典型的渦流管內,接近渦流管中心的部分為冷空氣,而接近渦輪管外側的部分則為熱空氣,其中冷空氣和熱空氣可分別從渦流管兩端 的冷空氣出口C和熱空氣出口H而各自被分離出來。然而,傳統的渦流管裝置必須另外準備壓縮氣體或透過空氣泵浦來產生高壓氣體,因此成本較高且不利於裝置的小型化。 Vortex tubes can be used in many places. As long as high-pressure air is used as a gas source, cold air or hot air can be generated. Figure 1 is a typical vortex tube design in which a cold air outlet C and a hot air outlet H are respectively disposed at both ends of the vortex tube, and high pressure air can be injected into the vortex tube from the nozzle N during operation (as shown in Fig. 1). In the arrow A in the middle), since the pressure in the tube is close to the atmospheric pressure, the air leaving the nozzle N will expand rapidly, and a forced vortex is formed in the vortex tube, and the air near the center of the vortex tube is approached. The air in the outer portion is operated to lower its own temperature; conversely, the temperature of the air near the outer portion of the vortex tube rises. As shown in Fig. 1, in a typical vortex tube, the portion near the center of the vortex tube is cold air, and the portion near the outside of the turbine tube is hot air, wherein cold air and hot air can be respectively from both ends of the vortex tube. The cold air outlet C and the hot air outlet H are each separated. However, the conventional vortex tube device must separately prepare compressed gas or air-pumped to generate high-pressure gas, which is costly and is not conducive to miniaturization of the device.

本發明之一實施例提供一種渦流管裝置,包括一本體、一熱端構件、一冷端構件以及一第一導流元件。前述本體具有一第一入風口以及一長條狀之延伸部,其中延伸部朝渦流管裝置之一縱軸方向延伸。前述熱端構件連接延伸部,前述冷端構件連接本體,其中冷端構件與熱端構件位於本體之相反側。一氣體自第一入風口進入本體,並經由冷端構件與熱端構件排出渦流管裝置。前述第一導流元件設置於本體內,具有一第一通孔、一第一表面以及複數個通道,其中前述通道形成於第一表面且圍繞第一通孔,且前述通道底部分別形成有一斜面,用以導引氣體進入本體之延伸部。 One embodiment of the present invention provides a vortex tube device including a body, a hot end member, a cold end member, and a first flow guiding member. The body has a first air inlet and an elongated extension, wherein the extension extends toward one of the longitudinal axes of the vortex tube device. The hot end member connects the extension, the cold end member connects to the body, wherein the cold end member and the hot end member are located on opposite sides of the body. A gas enters the body from the first air inlet and exits the vortex tube device via the cold end member and the hot end member. The first flow guiding element is disposed in the body, and has a first through hole, a first surface, and a plurality of channels, wherein the channel is formed on the first surface and surrounds the first through hole, and the bottom of the channel is respectively formed with a slope For guiding the gas into the extension of the body.

於一實施例中,前述本體更具有一第二入風口,氣體自第一、第二入風口進入本體,並經由前述通道導引進入延伸部。 In an embodiment, the body further has a second air inlet, and the gas enters the body from the first and second air inlets and is guided into the extension via the foregoing passage.

於一實施例中,前述第一、第二入風口之間形成一鈍角。 In an embodiment, an obtuse angle is formed between the first and second air inlets.

於一實施例中,前述鈍角介於100~150度。 In one embodiment, the obtuse angle is between 100 and 150 degrees.

於一實施例中,前述渦流管裝置更包括一第二導流元件,連接延伸部和第一導流元件,且第二導流元件具有一第二表面,第一、第二表面垂直於前述縱軸方向且相互抵接。 In one embodiment, the vortex tube device further includes a second flow guiding element connecting the extension portion and the first flow guiding element, and the second flow guiding element has a second surface, the first and second surfaces being perpendicular to the foregoing The longitudinal axis direction and abut each other.

於一實施例中,前述第二導流元件具有一第二通 孔,與第一通孔相通,且第二通孔朝熱端構件方向形成一漸擴結構。 In an embodiment, the second flow guiding element has a second pass The hole communicates with the first through hole, and the second through hole forms a diverging structure toward the hot end member.

於一實施例中,前述通道呈放射狀排列。 In one embodiment, the channels are radially arranged.

於一實施例中,前述每一通道具有一入口端以及一出口端,氣體自入口端進入通道後再經由出口端離開通道,其中入口端的寬度大於出口端的寬度。 In one embodiment, each of the channels has an inlet end and an outlet end. The gas enters the channel from the inlet end and exits the channel via the outlet end, wherein the width of the inlet end is greater than the width of the outlet end.

於一實施例中,前述熱端構件可相對於本體沿前述縱軸方向滑動。 In one embodiment, the hot end member is slidable relative to the body in the direction of the longitudinal axis.

於一實施例中,前述熱端構件具有複數個氣孔,一部分之氣體經由前述氣孔排出渦流管裝置。 In one embodiment, the hot end member has a plurality of air holes, and a portion of the gas is discharged from the vortex tube device via the air holes.

為使本發明之上述目的、特徵和優點能更明顯易懂,下文特舉較佳實施例並配合所附圖式做詳細說明。 The above described objects, features and advantages of the present invention will become more apparent from the description of the appended claims.

10‧‧‧本體 10‧‧‧ Ontology

11‧‧‧第一入風口 11‧‧‧First air inlet

12‧‧‧第二入風口 12‧‧‧Second air inlet

13‧‧‧延伸部 13‧‧‧Extension

131‧‧‧內壁 131‧‧‧ inner wall

14‧‧‧連通孔 14‧‧‧Connected holes

20‧‧‧第一導流元件 20‧‧‧First flow guiding element

21‧‧‧第一表面 21‧‧‧ first surface

22‧‧‧通道 22‧‧‧ channel

221‧‧‧斜面 221‧‧‧Bevel

222‧‧‧入口端 222‧‧‧ entrance end

223‧‧‧出口端 223‧‧‧export end

23‧‧‧第一通孔 23‧‧‧First through hole

30‧‧‧熱端出風構件 30‧‧‧hot end outlet components

31‧‧‧腔室 31‧‧‧ chamber

32‧‧‧氣孔 32‧‧‧ stomata

40‧‧‧第二導流元件 40‧‧‧Second flow guiding element

41‧‧‧第二表面 41‧‧‧ second surface

42‧‧‧第二通孔 42‧‧‧Second through hole

50‧‧‧冷端出風構件 50‧‧‧Cold end outlet member

100‧‧‧渦流管裝置 100‧‧‧Vortex tube device

C‧‧‧冷空氣出口 C‧‧‧Cold air outlet

H‧‧‧熱空氣出口 H‧‧‧hot air outlet

L‧‧‧中心線 L‧‧‧ center line

N‧‧‧噴嘴 N‧‧‧ nozzle

A、A1、A2、A3‧‧‧箭頭 A, A1, A2, A3‧‧‧ arrows

D、d‧‧‧寬度 D, d‧‧‧ width

第1圖表示一習知渦流管之示意圖;第2A、2B圖表示本發明一實施例之渦流管裝置爆炸圖;第3A、3B圖表示本發明一實施例之渦流管裝置組裝後的立體圖;第3C圖表示本發明一實施例之渦流管裝置剖面示意圖;第3D圖表示氣體透過通道底部的斜面導引進入第二導流元件中央的第二通孔之示意圖;第4A圖表示本發明一實施例之第一導流元件立體圖;以及第4B、4C圖表示第4A圖中之第一導流元件不同視角的示意圖。 1 is a schematic view showing a conventional vortex tube; 2A and 2B are views showing an exploded view of a vortex tube device according to an embodiment of the present invention; and FIGS. 3A and 3B are perspective views showing an assembled vortex tube device according to an embodiment of the present invention; 3C is a schematic cross-sectional view showing a vortex tube device according to an embodiment of the present invention; FIG. 3D is a view showing a second through hole in the center of the second flow guiding member guided by a slope of the bottom of the gas transmission passage; FIG. 4A is a view showing the present invention; A perspective view of the first flow guiding element of the embodiment; and FIGS. 4B and 4C are schematic views showing different viewing angles of the first flow guiding element in FIG. 4A.

茲配合圖式說明本發明之較佳實施例。 The preferred embodiment of the invention is described in conjunction with the drawings.

有關本發明之前述及其他技術內容、特點與功效,在以下配合參考圖式之一較佳實施例的詳細說明中,將可清楚的呈現。以下實施例中所提到的方向用語,例如:上、下、左、右、前或後等,僅是參考附加圖式的方向。因此,使用的方向用語是用來說明並非用來限制本發明。 The above and other technical contents, features and advantages of the present invention will be apparent from the following detailed description of the preferred embodiments. The directional terms mentioned in the following embodiments, such as up, down, left, right, front or back, etc., are only directions referring to the additional drawings. Therefore, the directional terminology used is for the purpose of illustration and not limitation.

首先請一併參閱第2A、2B以及3A、3B圖,本發明一實施例之渦流管裝置100主要係裝設於筆記型電腦、桌上型電腦或其他各種類型的電子裝置中,用以取代傳統的散熱風扇,藉以對電子裝置內部的電子元件進行散熱。前述渦流管裝置100包括一本體10、一第一導流元件20、一熱端構件30、一第二導流元件40以及一冷端構件50。應了解的是,前述本體10、第一導流元件20、熱端構件30、第二導流元件40以及冷端構件50皆呈中空結構,其中本體10具有第一入風口11、一第二入風口12、一長條狀之延伸部13以及一連通孔14,且延伸部13係朝渦流管裝置100之縱軸方向(X軸方向)延伸。此外,前述熱端構件30插設於延伸部13之一端,且熱端構件30內部形成有一腔室31,該腔室31與本體10的連通孔14相通。在本實施例中,前述熱端構件30可相對於本體10沿渦流管裝置100之縱軸方向(X軸方向)滑動,藉此可調整並控制由熱端構件30及冷端構件50所排出之氣體溫度和流量。 First, please refer to FIGS. 2A, 2B and 3A, 3B. The vortex tube device 100 according to an embodiment of the present invention is mainly installed in a notebook computer, a desktop computer or other various types of electronic devices to replace A conventional cooling fan is used to dissipate heat from electronic components inside an electronic device. The vortex tube device 100 includes a body 10, a first flow guiding member 20, a hot end member 30, a second flow guiding member 40, and a cold end member 50. It should be understood that the body 10, the first flow guiding element 20, the hot end member 30, the second flow guiding element 40, and the cold end member 50 are all hollow structures, wherein the body 10 has a first air inlet 11 and a second The air inlet 12, an elongated extension 13 and a communication hole 14 extend in the longitudinal direction (X-axis direction) of the vortex tube device 100. In addition, the hot end member 30 is inserted into one end of the extending portion 13, and a cavity 31 is formed inside the hot end member 30, and the chamber 31 communicates with the communication hole 14 of the body 10. In the present embodiment, the hot end member 30 is slidable relative to the body 10 in the longitudinal axis direction (X-axis direction) of the vortex tube device 100, whereby the hot end member 30 and the cold end member 50 can be adjusted and controlled. Gas temperature and flow rate.

前述第一導流元件20及第二導流元件40主要係用以將自第一、第二入風口11、12所注入之氣體導引到本體10的 延伸部13內,其中第一導流元件20具有一第一表面21,第一表面21垂直於渦流管裝置100之縱軸方向(X軸方向),且在第一表面21上形成有複數個凹陷且呈放射狀排列之通道22;第二導流元件40則連接第一導流元件20與本體10之延伸部13,並且具有一第二表面41,且第二表面41同樣垂直於渦流管裝置100之縱軸方向(X軸方向),前述第一、第二表面21、41於組裝時係相互抵接;如第2A、2B圖所示,前述第一導流元件20具有一第一通孔23,且第二導流元件40具有一第二通孔42,組裝時第一、第二導流元件20、40係容置於本體10內,且第一、第二通孔23、42與本體10的連通孔14相通。於一實施例中,前述第一、第二導流元件20、40也可以整合成為單一構件並以一體成形的方式製作,藉此可節省製造及組裝成本。 The first flow guiding element 20 and the second flow guiding element 40 are mainly used to guide the gas injected from the first and second air inlets 11 and 12 to the body 10 . In the extending portion 13, wherein the first flow guiding member 20 has a first surface 21, the first surface 21 is perpendicular to the longitudinal axis direction (X-axis direction) of the vortex tube device 100, and a plurality of the first surface 21 are formed on the first surface 21. a recessed and radially arranged channel 22; the second flow guiding element 40 connects the first flow guiding element 20 with the extension 13 of the body 10 and has a second surface 41, and the second surface 41 is also perpendicular to the vortex tube In the longitudinal direction of the device 100 (X-axis direction), the first and second surfaces 21 and 41 abut each other during assembly; as shown in FIGS. 2A and 2B, the first flow guiding element 20 has a first The through hole 23, and the second flow guiding element 40 has a second through hole 42. When assembled, the first and second flow guiding elements 20, 40 are received in the body 10, and the first and second through holes 23, 42 communicates with the communication hole 14 of the body 10. In one embodiment, the first and second flow guiding members 20, 40 may be integrated into a single member and fabricated in an integrally formed manner, thereby saving manufacturing and assembly costs.

由第3A、3B圖中可以看出,本實施例係藉由設置 第一入風口11以及第二入風口12,可同時注入兩股氣體到本體10內,其中第一、第二入風口11、12之間形成有一鈍角θ,該鈍角θ的範圍約介於100~150度(例如120度),惟入風口之數量及其間的夾角並不以此為限。如前所述,透過第一、第二入風口11、12所導入之氣流可產生疊加之效果以增加整體進氣壓力值,故本發明相較於傳統單一入風口的渦流管設計而言,能有效降低輸入氣體的壓力需求。舉例而言,當使用兩個以上的入風口時,可不需再額外準備壓縮氣體或透過空氣泵浦來產生高壓氣體,反之利用電子裝置內部現成的散熱風扇驅動即可作為氣體來源,如此一來不僅能大幅降低成本,同時也可有助於達 到電子裝置的小型化。 As can be seen from the figures 3A and 3B, this embodiment is set by The first air inlet 11 and the second air inlet 12 can simultaneously inject two gases into the body 10, wherein an obtuse angle θ is formed between the first and second air inlets 11, 12, and the obtuse angle θ ranges from about 100. ~150 degrees (for example, 120 degrees), but the number of inlets and the angle between them are not limited to this. As described above, the airflow introduced through the first and second air inlets 11, 12 can produce a superimposed effect to increase the overall intake pressure value, so the present invention is compared with the vortex tube design of the conventional single air inlet. Can effectively reduce the pressure requirements of the input gas. For example, when more than two air inlets are used, it is not necessary to additionally prepare compressed gas or air pumping to generate high-pressure gas, and vice versa, using a ready-made cooling fan inside the electronic device as a gas source, thus Not only can it significantly reduce costs, but it can also help To the miniaturization of electronic devices.

接著請一併參閱第3C、3D圖,其中第3C圖為本發 明一實施例之渦流管裝置剖面示意圖,當氣體經由第一、第二入風口11、12同時導入本體10後(如第3C、3D圖中的箭頭A1所示),可經過第一導流元件20上的通道22導引而流向第二導流元件40中央的第二通孔42,接著並透過漸擴之第二通孔42導引氣體至延伸部13的內壁131以形成渦流。當氣流持續往熱端構件30的方向(X軸方向)運動並經過本體10的連通孔14而到達熱端構件30的腔室31時,一部分氣體(熱空氣)會從腔室31經由熱端構件30上的氣孔32排出渦流管裝置100(如第3C圖中箭頭A2所示),另一部分接近渦流管裝置100中心處的氣體(冷空氣)則會形成由熱端返回的冷渦流,並沿著-X軸方向依序流過連通孔14、第二通孔42以及第一通孔23,最後再經由與第一導流元件20相連接之冷端構件50排出渦流管裝置100(如第3C圖中箭頭A3所示),藉以針對電子裝置內部之一發熱源或電子元件進行冷卻降溫。 Please refer to the 3C and 3D diagrams together. The 3C figure is the same. A schematic cross-sectional view of the vortex tube device of the first embodiment, after the gas is simultaneously introduced into the body 10 via the first and second air inlets 11, 12 (as indicated by an arrow A1 in the 3C and 3D drawings), the first diversion can be performed. The passage 22 on the member 20 is guided to the second through hole 42 in the center of the second flow guiding member 40, and then guided through the diverging second through hole 42 to the inner wall 131 of the extending portion 13 to form a vortex. When the airflow continues to move in the direction of the hot end member 30 (X-axis direction) and passes through the communication hole 14 of the body 10 to reach the chamber 31 of the hot end member 30, a part of the gas (hot air) passes from the chamber 31 via the hot end. The air vent 32 on the member 30 exits the vortex tube device 100 (as indicated by arrow A2 in Fig. 3C), and another portion of the gas (cold air) near the center of the vortex tube device 100 forms a cold vortex returning from the hot end, and Flowing through the communication hole 14, the second through hole 42 and the first through hole 23 in the -X axis direction, and finally discharging the vortex tube device 100 via the cold end member 50 connected to the first flow guiding member 20 (eg In Fig. 3C, the arrow A3 is shown) for cooling and cooling of a heat source or an electronic component inside the electronic device.

由第3D圖中可以看出,前述第一導流元件20上的 通道22底部形成有一斜面221,從第一、第二入風口11、12所注入之氣體可透過通道22底部的斜面221導引而進入第二導流元件40中央的第二通孔42。由於本實施例中的第二通孔42係朝熱端構件30方向(X軸方向)形成一漸擴結構,藉此可有助於將第二通孔42內的氣體導引至本體10之延伸部13的內壁131,以使氣體能與延伸部13的內壁131作用而形成熱渦流,進而可提 升渦流管裝置100的效率。 As can be seen from the 3D figure, the aforementioned first flow guiding element 20 A slope 221 is formed at the bottom of the passage 22. The gas injected from the first and second air inlets 11, 12 can be guided through the slope 221 at the bottom of the passage 22 to enter the second through hole 42 in the center of the second flow guiding member 40. Since the second through hole 42 in the embodiment forms a diverging structure toward the hot end member 30 (X-axis direction), the gas in the second through hole 42 can be guided to the body 10. The inner wall 131 of the extending portion 13 is configured to allow gas to interact with the inner wall 131 of the extending portion 13 to form a thermal vortex, thereby providing The efficiency of the vortex tube device 100.

再請一併參閱第4A~4C圖,本實施例中之第一導流 元件20係形成有六個深度不盡相同且圍繞著第一通孔23呈放射狀排列的通道22,惟前述通道22的長度、寬度及深度仍可依設計需求而調整成具有相同或不同之尺寸,其中從第一、第二入風口11、12所注入之氣體可透過該些通道22底部的斜面221導引而進入第二導流元件40中央的第二通孔42;如第4C圖所示,前述每一通道22皆具有圓弧狀之入口端222及出口端223,其中第二導流元件40外側的氣體經由入口端222進入通道22後,再透過第二導流元件40內側的出口端223離開通道22,又前述入口端222的寬度D係大於出口端223的寬度d,藉此可有助於渦流的形成。又,由第4C圖中可以看出,本實施例中之每一通道22皆具有一中心線L,該些中心線L不相交於同一點,且與一內切圓相切。 Please refer to the 4A~4C diagram again, the first diversion in this embodiment. The element 20 is formed with six channels 22 of different depths and arranged radially around the first through holes 23, but the length, width and depth of the channels 22 can still be adjusted to have the same or different according to design requirements. Dimensions, wherein the gas injected from the first and second air inlets 11, 12 can be guided through the inclined surface 221 at the bottom of the channels 22 to enter the second through hole 42 in the center of the second flow guiding element 40; as shown in FIG. 4C As shown, each of the channels 22 has an arc-shaped inlet end 222 and an outlet end 223. The gas outside the second flow guiding element 40 enters the channel 22 via the inlet end 222 and then passes through the inside of the second flow guiding element 40. The exit end 223 exits the passage 22, and the width D of the aforementioned inlet end 222 is greater than the width d of the outlet end 223, thereby facilitating the formation of eddy currents. Moreover, as can be seen from FIG. 4C, each of the channels 22 in this embodiment has a center line L that does not intersect at the same point and is tangent to an inscribed circle.

綜上所述,本發明藉由設置兩個以上的入風口, 可同時導入兩股氣流到本體內,且導入之氣流可產生疊加效果以提升整體進氣壓力值,故本發明相較於傳統單一入風口的渦流管設計而言,能有效降低輸入氣體的壓力需求,進而可大幅降低成本並有助於達到電子裝置的小型化。此外,本發明藉由在第一導流元件表面形成複數個以放射狀排列之通道,同時搭配兩個以上的入風口設計,更可有效導引氣體到本體內部以產生渦流,進而能提升渦流管裝置的整體效率。 In summary, the present invention provides more than two air inlets. Two airflows can be introduced into the body at the same time, and the introduced airflow can generate a superimposed effect to increase the overall intake pressure value. Therefore, the present invention can effectively reduce the pressure of the input gas compared with the vortex tube design of the conventional single air inlet. Demand, in turn, can significantly reduce costs and help to achieve miniaturization of electronic devices. In addition, the present invention can form a plurality of radially arranged channels on the surface of the first flow guiding element, and simultaneously design with two or more air inlets, thereby effectively guiding the gas into the body to generate eddy current, thereby improving The overall efficiency of the vortex tube device.

雖然本發明已以較佳實施例揭露於上,然其並非 用以限定本發明,任何熟習此項工藝者,在不脫離本發明之精神和範圍內,當可作些許之更動與潤飾,因此本發明之保護範圍當視後附之申請專利範圍所界定者為準。 Although the invention has been disclosed in the preferred embodiments, it is not The scope of the present invention is defined by the scope of the appended claims, and the scope of the present invention is defined by the scope of the appended claims. Prevail.

10‧‧‧本體 10‧‧‧ Ontology

11‧‧‧第一入風口 11‧‧‧First air inlet

12‧‧‧第二入風口 12‧‧‧Second air inlet

13‧‧‧延伸部 13‧‧‧Extension

131‧‧‧內壁 131‧‧‧ inner wall

14‧‧‧連通孔 14‧‧‧Connected holes

20‧‧‧第一導流元件 20‧‧‧First flow guiding element

22‧‧‧通道 22‧‧‧ channel

23‧‧‧第一通孔 23‧‧‧First through hole

30‧‧‧熱端出風構件 30‧‧‧hot end outlet components

31‧‧‧腔室 31‧‧‧ chamber

32‧‧‧氣孔 32‧‧‧ stomata

40‧‧‧第二導流元件 40‧‧‧Second flow guiding element

41‧‧‧第二表面 41‧‧‧ second surface

42‧‧‧第二通孔 42‧‧‧Second through hole

50‧‧‧冷端出風構件 50‧‧‧Cold end outlet member

100‧‧‧渦流管裝置 100‧‧‧Vortex tube device

A1、A2、A3‧‧‧箭頭 A1, A2, A3‧‧‧ arrows

Claims (10)

一種渦流管裝置,包括:一本體,具有一第一入風口以及一長條狀之延伸部,其中該延伸部朝該渦流管裝置之一縱軸方向延伸;一熱端構件,連接該延伸部;一冷端構件,連接該本體,其中該冷端構件與該熱端構件位於該本體之相反側,一氣體自該第一入風口進入該本體,並經由該冷端構件與該熱端構件排出該渦流管裝置;以及一第一導流元件,設置於該本體內,具有一第一通孔以及複數個通道,其中該些通道圍繞該第一通孔,且該些通道分別形成有一斜面,用以導引該氣體進入該本體之該延伸部。 A vortex tube device comprising: a body having a first air inlet and an elongated extension, wherein the extension extends toward a longitudinal axis of the vortex tube device; and a hot end member connecting the extension a cold end member coupled to the body, wherein the cold end member and the hot end member are located on opposite sides of the body, a gas entering the body from the first air inlet, and the cold end member and the hot end member Discharging the vortex tube device; and a first flow guiding element disposed in the body, having a first through hole and a plurality of channels, wherein the channels surround the first through hole, and the channels are respectively formed with a slope And guiding the gas into the extension of the body. 如申請專利範圍第1項所述之渦流管裝置,其中,該本體更具有一第二入風口,該氣體自該第一、第二入風口進入該本體,並經由該些通道導引進入該延伸部。 The vortex tube device of claim 1, wherein the body further has a second air inlet, and the gas enters the body from the first and second air inlets, and is guided into the body through the channels. Extension. 如申請專利範圍第2項所述之渦流管裝置,其中,該第一、第二入風口之間形成一鈍角。 The vortex tube device of claim 2, wherein an obtuse angle is formed between the first and second air inlets. 如申請專利範圍第3項所述之渦流管裝置,其中,該鈍角介於100~150度。 The vortex tube device of claim 3, wherein the obtuse angle is between 100 and 150 degrees. 如申請專利範圍第1項所述之渦流管裝置,其中,該渦流管裝置更包括一第二導流元件,連接該延伸部和該第一導流元件,且該第一、第二導流元件相互抵接。 The vortex tube device of claim 1, wherein the vortex tube device further comprises a second flow guiding element connecting the extension portion and the first flow guiding element, and the first and second flow guiding The components abut each other. 如申請專利範圍第5項所述之渦流管裝置,其中,該第二導流元件具有一第二通孔,與該第一通孔相通,且該第二通孔朝該熱端構件方向形成一漸擴結構。 The vortex tube device of claim 5, wherein the second flow guiding member has a second through hole communicating with the first through hole, and the second through hole is formed toward the hot end member. A gradually expanding structure. 如申請專利範圍第1項所述之渦流管裝置,其中,該些通道分別具有一中心線,且該些中心線不相交於同一點。 The vortex tube device of claim 1, wherein the channels each have a center line, and the center lines do not intersect at the same point. 如申請專利範圍第7項所述之渦流管裝置,其中,每一該通道具有一入口端以及一出口端,氣體自該入口端進入該通道後再經由該出口端離開該通道,其中該入口端的寬度大於該出口端的寬度。 The vortex tube device of claim 7, wherein each of the passages has an inlet end and an outlet end, and the gas enters the passage from the inlet end and exits the passage via the outlet end, wherein the inlet The width of the end is greater than the width of the outlet end. 如申請專利範圍第1項所述之渦流管裝置,其中,該熱端構件可相對於該本體沿該縱軸方向滑動。 The vortex tube device of claim 1, wherein the hot end member is slidable relative to the body in the longitudinal direction. 如申請專利範圍第1項所述之渦流管裝置,其中,該熱端構件具有複數個氣孔,一部分之該氣體經由該些氣孔排出該渦流管裝置。 The vortex tube device of claim 1, wherein the hot end member has a plurality of air holes through which a portion of the gas is discharged from the vortex tube device.
TW104121617A 2015-07-03 2015-07-03 Vortex tube device TWI576551B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW104121617A TWI576551B (en) 2015-07-03 2015-07-03 Vortex tube device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW104121617A TWI576551B (en) 2015-07-03 2015-07-03 Vortex tube device

Publications (2)

Publication Number Publication Date
TW201702544A true TW201702544A (en) 2017-01-16
TWI576551B TWI576551B (en) 2017-04-01

Family

ID=58401094

Family Applications (1)

Application Number Title Priority Date Filing Date
TW104121617A TWI576551B (en) 2015-07-03 2015-07-03 Vortex tube device

Country Status (1)

Country Link
TW (1) TWI576551B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112622718A (en) * 2019-10-08 2021-04-09 B/E航空公司 Multi-stage vortex tube assembly for low pressure and low flow applications
CN113418311A (en) * 2021-05-21 2021-09-21 武汉理工大学 Pasteurization device based on vortex tube effect
CN114984729A (en) * 2022-06-17 2022-09-02 蔡登� Vortex type cold and hot gas separation device
CN112622718B (en) * 2019-10-08 2024-05-10 B/E航空公司 Multi-stage vortex tube assembly for low pressure and low flow applications

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021012045A1 (en) * 2019-07-22 2021-01-28 Nex Flow Air Products Corp. Vortex tube cooling system and method of using same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2790310A (en) * 1954-11-23 1957-04-30 Garrett Corp Axial flow vortex tube mechanism
US3173273A (en) * 1962-11-27 1965-03-16 Charles D Fulton Vortex tube
US6494935B2 (en) * 2000-12-14 2002-12-17 Vortex Aircon, Inc. Vortex generator
CN104654647B (en) * 2015-01-28 2017-01-18 北京航空航天大学 Adaptive frozen-blocking prevention vortex tube within all cold flow rate range

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112622718A (en) * 2019-10-08 2021-04-09 B/E航空公司 Multi-stage vortex tube assembly for low pressure and low flow applications
CN112622718B (en) * 2019-10-08 2024-05-10 B/E航空公司 Multi-stage vortex tube assembly for low pressure and low flow applications
CN113418311A (en) * 2021-05-21 2021-09-21 武汉理工大学 Pasteurization device based on vortex tube effect
CN114984729A (en) * 2022-06-17 2022-09-02 蔡登� Vortex type cold and hot gas separation device

Also Published As

Publication number Publication date
TWI576551B (en) 2017-04-01

Similar Documents

Publication Publication Date Title
TWI576551B (en) Vortex tube device
BR102016005385A2 (en) heat exchanger
CN105637632B (en) Cooler and the semiconductor module for using the cooler
TWI815494B (en) Two phase cold plate
WO2018009259A3 (en) Gas turbine engine having a surface cooler with ogv oriented fin angles
CN107448298A (en) For the improved pitted cabin inner surface of tool that conducts heat
US20130312938A1 (en) Heat pipe with vaporized working fluid flow accelerator
CN205013288U (en) Helical -lobe compressor and organism thereof
MX2017015002A (en) Enhanced vapor injection air conditioning system.
EP3214380A1 (en) Air conditioner
AU2019339973B2 (en) Stator assembly, motor having same and wind power generator set
US11959624B2 (en) Light emitting device
WO2018024185A1 (en) Heat exchange device
JPWO2019073584A1 (en) Compressor housing and turbocharger provided with the compressor housing
CN205027001U (en) Knockout, compressor and indirect heating equipment
CN204404235U (en) A kind of gas-turbine combustion chamber changeover portion with cooling structure
JP2005294802A (en) Heat dissipation module
KR102007794B1 (en) Noise reduction type double pipe heat exchanger
KR101980632B1 (en) Cooler Assembly Having Reducing Cooling Loss, and Generator Having The Same
TW201706764A (en) Cooling device
CN103744497B (en) A kind of cooling system
CN109259408B (en) Handle air inlet type hair dryer
TW202024855A (en) Electronic device, heat dissipation system and heat dissipation module thereof
TWI792414B (en) Vortex Heat Exchanger
TWM561391U (en) Water-filling and degassing structure of water-cooling device