TW200411146A - Jet flow meter - Google Patents

Jet flow meter Download PDF

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TW200411146A
TW200411146A TW91138079A TW91138079A TW200411146A TW 200411146 A TW200411146 A TW 200411146A TW 91138079 A TW91138079 A TW 91138079A TW 91138079 A TW91138079 A TW 91138079A TW 200411146 A TW200411146 A TW 200411146A
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Taiwan
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fluid
flow
micro
jet
sensing element
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TW91138079A
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Chinese (zh)
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TW580564B (en
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Shiang-Fu Chen
Shih-Chi Kuo
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Ind Tech Res Inst
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Abstract

There is provided a jet flow meter, which includes the following three major parts: a buffer chamber, a micro channel and a fluid oscillating chamber. The buffer chamber is provided to make the fluid smoothly enter the jet flow meter from the flowing field. Then, fluid enters the micro channel from the buffer chamber. The micro channel has multi-threaded micro flow elements for detecting the flowing field of micro flow. Finally, fluid enters the fluid oscillating chamber from the micro channel. When the Renault number of flowing field reaches the status of transition flow, the fluid becomes unstable. By measuring the frequency of fluid oscillation, it is able to derive the flowing fields of middle and high flows. This jetflow meter is combined with the micro flow and the measurement of middle and high flows to expand the dynamic measurement range of the flow meter.

Description

200411146200411146

五、發明說明(1) 【發明所屬之技術領域】 本發明是關於一種射流流量計,應用於流場中之流 量量測。 【先前技術】 目前流量計的應用範圍非常廣泛,例如:在日常生、、舌中 每個家庭都會使用到的瓦斯表、醫院所使用的啤吸器中之 的氣體流量控制、汽車用的空氣調節器、實驗室或&工廠 中氣瓶之流量計等’都需使用到流量計。然而,針對不^ 領域之應用,會有不同需求的流量計量範圍。 目前研發出來的流量計主要是應用於瓦斯表中 以下 針對不同型式的流量計結構及其量測原理作一簡介· 〇)美國專利第4, 244, 230號所提出來的射流震流量 計,請參考「第1圖」所示,首先,在流體的入口丨〇 1彤 成一個高深寬比的流道,此流道的截面形狀既窄又深,^ 使流經其中的流體形成一個面的流體喷出來。合户 來的時候,在出口20漸縮到漸寬的地方,由於;;=於二 =體30之凹槽31會造成流體不穩定的現象,而產::: 效應,會造成流體偏擺的現象,在流體由出口^ 出的弟一瞬間,流體可能會往左擺,或是往右擺, = 達效應。而在凹槽31的左右兩侧設置有‘ ^ f感測器40 ’由於流體震盛感測器4 = 率:與流體的體積流率呈線性關係、,因此,; 算得出流體的質量流率。,流阻越大時由; 政果越好,而流體震盪感測器4〇感測的效果也越佳= 200411146 五、發明說明(2) ' 此專利在流體出口 20的前端設置有阻擋體3〇,以增加流體 的不穩定性。本發明的缺點是必須以流阻來換取顯著的震 靈效應’而且必須要有足夠的壓損(pressure i〇se)才會 造成流體震盪的效果。 (2 )由美國專利第5,3 9 6,8 0 9號所揭露之流量計,請參考 「第2圖」所示,其設計原理與前述專利相同,但其與前 述專利最大的不同點在於:此專利在震盪室凹槽3 1的正中 間再加入一個流體震盪感測器4 〇,其主要的作用在於提高 流體震盪的感測解析度,尤其是在流體流量較小、震盪不 甚明顯的時候’即可有效的改善並提高流量計的精確性。 (3 )而在美國專利第5,3 6 3,7 0 4號所揭露之流量計,請參 考「第3圖」所示,此專利的主要目的在於改善美國專利 第5,3 9 6,8 0 9號所揭露之流量計的缺點··因為當流體的流速 變快時,雖然流體震盪的效果變好,但是在凹槽3 1内卻會 產生紊亂的渦流(v 〇 r t e X ),此滿流會使凹槽3 1内的流體變 得更加混亂,連帶影響流體震盪感測器40所量測之訊雜比 變得不明顯。所以此專利為改善這個缺點,便在凹槽3 1的 兩侧各挖一個旁通道(B y p a s s ) 3 2,使凹槽3 1内所產生的滿 流可由旁通道32流出,降低凹槽31内流體的亂流,以提高 流體產生震盪時的訊雜比。 (4)根據美國專利第5, 1 57, 974號所揭露之小型化微電腦 瓦斯表,請參考「第4圖」所示,其核心技術即為射流流 量計,將射流流量計應用於瓦斯表中的最大好處在於··瓦 斯基本上並不甚乾淨,且容易囤積雜質於流量計結構中,V. Description of the invention (1) [Technical field to which the invention belongs] The present invention relates to a jet flow meter, which is applied to flow measurement in a flow field. [Prior art] current meter wide range of applications, for example: each family will use the gas to daily life ,, table tongue, beer aspirator used in the hospital of the gas flow control, automotive air-conditioning Flowmeters are used in gas generators, laboratories or & factories. However, for applications in different fields, there will be different flow measurement ranges. The currently developed flowmeters are mainly used in gas meters to make a brief introduction to the different types of flowmeter structures and their measuring principles. 〇) Jet shock flowmeters proposed in US Patent No. 4,244, 230, Please refer to "Figure 1". First, a high-aspect-ratio flow channel is formed at the inlet of the fluid. The cross-sectional shape of this flow channel is narrow and deep, so that the fluid flowing through it forms a surface. Fluid squirting out. When the household comes, when the outlet 20 gradually shrinks to a gradually wider place, because ;; = 于 二 = the groove 31 of the body 30 will cause the phenomenon of fluid instability, and the production :: effect will cause the fluid to sway At the moment when the fluid exits from the outlet ^, the fluid may swing to the left or to the right, = the effect. The '^ f sensor 40' is provided on the left and right sides of the groove 31 because the fluid shock sensor 4 = rate: linear relationship with the volumetric flow rate of the fluid, so; rate. The greater the flow resistance, the better; the better the political result, and the better the effect of the fluid shock sensor 4 = 200411146 V. Description of the invention (2) 'This patent is provided with a blocking body at the front end of the fluid outlet 20. 30 to increase fluid instability. The disadvantage of the present invention is that the fluid resistance must be exchanged for a significant shock effect 'and that there must be sufficient pressure loss to cause the fluid shock effect. (2) disclosed by the U.S. Patent of the 5,3 6,8 0 9 9 flowmeter shown refer to "FIG. 2", the design principle of the same patent, but the aforementioned patent biggest difference The reason is that this patent adds a fluid oscillating sensor 40 in the middle of the groove 31 of the oscillating chamber. Its main function is to improve the resolution of fluid oscillating sensing, especially when the fluid flow is small and the oscillating is not very When it is obvious, it can effectively improve and improve the accuracy of the flow meter. (3) disclosed in U.S. Patent No. 6 5,3 3,7 0 of the first flow meter 4, shown refer to "FIG. 3", the main purpose of this patent is to improve U.S. Patent No. 5,3 96, the disadvantage of the disclosed flowmeter 80 · 9 because when the fluid flow rate becomes faster, although the effect of the fluid shocks better, but it will generate a vortex disorder (v 〇rte X) in the recess 31, the fluid 31 will flow over this recess became more chaotic, thus influencing the fluid shock sensor 40 measuring the amount of to-noise ratio becomes inconspicuous. Therefore, this patent is to improve this disadvantage, it is on both sides of each recess 31 digging a bypass passage (B ypass) 3 2, so that full flow recess 31 may be generated by the bypass passage 32 flows, reducing the groove 31 Turbulent flow of the internal fluid to increase the signal-to-noise ratio of the fluid when it oscillates. (4) According to U.S. Patent No. 5, 157, 974 disclosed the size of the gas meter microcomputer, refer to "FIG. 4", the core technology is the fluidic flowmeter, the flowmeter is applied to the gas jet table The biggest advantage is that the gas is basically not very clean and it is easy to accumulate impurities in the flowmeter structure.

第6頁 200411146 五、發明說明(3) 而射流流量計可以采,丨田、去^ 使流量計的量測= : = :震盛藉以清洗瓦斯表内部, 盈感測器40放置於流道。此射流流量計是將流體震 時,由於流道5。突:m口處’當流體通過此流道50 訊號,計算流體時;Ϊ流體震盪f測器40所量測到的 項專利的發明相對於前可^异成流,的流量。此 流體震盪的現象發生時,所二:、:是為了避免當 專利的發明卻也造成Τ另-個缺點‘ 儿的減弱,所以,此專利所提出 且明顯地提高訊雜比。 工不此有效 (;)「L在圖曰本/利,Τ'2_9號所揭露的流量計,請參 5 w」斤不 結構设計大致與美國專利第 沾157, 9 74號所揭露之小型化微電腦瓦斯表相同,其主 ^構想是將流體震盪感測器4〇設置於震盪室入口 6〇 a、 的位置,其主要的目的在於增加感測流體震盪的頻 =二但此專利的缺點是:只要上游流場之壓力發生變動, 此就會成δίΐ號的铁判而造成流場計量的不準確。 2)在日本專利第JP20 0 1 -20 8 575號所揭露的流量計,其 ^構之立體圖請參考「第6圖」所示,此專利的基本原理 又然疋利用流體不穩定的現象,來推算流體之質量流率。 $漸縮段70先造成流體的加速,再經由高深寬比的流道造 f所謂的近似二維流場,以產生流體不穩定的現象,並造 、灰體週期性的震盪,而達到流體計量的功能。但此項專 200411146 五、發明說明(4) 利與前述日本專利第JP4-262209號所揭露的流量計有相同 的缺點:此流量計易受到上游流場壓力的影響,而造成感 測震氣的誤差。 在上述這些流量計中,其量測範圍都相當有限,無法 量測到一個較大的流量範圍。而且,當須量測微流量流場 時,所使用的管徑也必須跟著減小,如此一來,會造成报 大的壓力損失。Page 6 200411146 V. Description of the invention (3) And the jet flow meter can be used. 丨 Field, go ^ to make the flow meter measurement =: =: Zhen Sheng used to clean the inside of the gas meter, and the profit sensor 40 was placed in the flow channel. . This jet flow meter is due to the flow path 5 when the fluid is shaken. Burst: at the mouth of m 'when the fluid passes through the flow channel 50 signal to calculate the fluid; the patented invention measured by the fluid oscillating f-detector 40 is different from the flow that can be different. When this phenomenon of fluid turbulence occurs, the second :: is to avoid the weakening of the patented invention but also another disadvantage ′. Therefore, this patent proposes and significantly improves the noise-to-noise ratio. The work is not effective (;) "L is shown in the figure / benefit, the flowmeter disclosed in T'2_9, please refer to 5w" The structure design is roughly the same as that disclosed in US Patent No. 157, 9 74 The miniaturized microcomputer gas meter is the same. The main idea is to set the fluid shock sensor 40 at the entrance of the shock chamber 60a. The main purpose is to increase the frequency of sensing fluid shock = 2. But this patent The disadvantage is that as long as the pressure in the upstream flow field changes, this will become the iron judgment of δίΐ and cause inaccurate flow field measurement. 2) For the flow chart of the flowmeter disclosed in Japanese Patent No. JP20 0 1 -20 8 575, please refer to "Figure 6" for the three-dimensional structure of the flowmeter. The basic principle of this patent again utilizes the phenomenon of fluid instability. To estimate the mass flow rate of the fluid. The $ grading section 70 first causes the acceleration of the fluid, and then creates a so-called approximately two-dimensional flow field through the high-aspect-ratio flow channel to generate a fluid instability phenomenon, and the gray body is periodically oscillated to achieve fluid metering. Functions. However, this patent 200411146 V. Description of the invention (4) has the same disadvantages as the flowmeter disclosed in the aforementioned Japanese Patent No. JP4-262209: This flowmeter is easily affected by the pressure of the upstream flow field, which causes the vibration gas to be sensed. The error. In these flowmeters, the measurement range is quite limited, and a large flow range cannot be measured. In addition, when the micro-flow field needs to be measured, the diameter of the pipe used must be reduced accordingly. This will cause a large pressure loss.

而且’目前一般家用流量計所需量測的範圍為〇 · 3公升 /小時~ 3 0 0 0公升/小時,其動態量測範圍((^11&111丨(^1^11以) 達到1 0 0 0 0 : 1,然而目前所研發出的流量計,並無任何單 一的流量計可量測到如此大的範圍。 【發明内容】 莶π以上 種射流流量計 量感測元件, 的動態量測範 本發明之 衝室、微流道 流量計中之流 道,在微流道 微流量之流體 雷諾數到達過 會產生不穩定 流體震盈的頻 習知技術的問題’本發明之目的在於提供一 ,其結合量測微流量的微管道及多線型微流 與量測中高流量的流體震盪器,以達到較大 圍。And 'Currently, the measurement range of general household flow meters is from 0.3 liters / hour to 3 0 0 liters / hour, and its dynamic measurement range ((^ 11 & 111 丨 (^ 1 ^ 11)) reaches 1 0 0 0 0: 1, however, there is no single flowmeter that can measure such a large range of the flowmeters currently developed. [Contents of the Invention] The dynamic quantities of 莶 π or more jet flowmeters for measuring sensing elements Testing the flow channel in the flushing chamber and micro-channel flowmeter of the present invention, and the problem of the frequency-recognized technology that generates unstable fluid shock when the Reynolds number of the micro-flow channel and the micro-flow reaches the 'the purpose of the present invention is to provide First, it combines micro-pipes for measuring micro-flow and multi-line micro-flows and fluid oscillators for measuring medium and high-flow to achieve a larger circumference.

射流流量計,其包括有三個主要的部份:缓 及流體震盪室。緩衝室是使由流場進入射流 體平順著’流體進入與其相連接的微流 内設置有多線型微流量感測元件,用以感測 ;最後,流體進入流體震盪室冬 渡流(Transition n〇w)的狀態時:^體便 的現象,而造成流體之偏擺震盪,利用量測 率,即可推算中高流量流體之量測。Fluidic flowmeter, which comprises three main parts: the slow and fluid shock room. The buffer chamber is such that a multi-line micro-flow sensing element is provided in the micro-flow connected to the fluid to enter the fluid smoothly into the fluid flow. Finally, the fluid enters the fluid oscillating chamber in winter. 〇w): the phenomenon of diarrhea, which causes the fluid to oscillate. Using the measurement rate, you can estimate the measurement of medium and high flow fluids.

200411146 五、發明說明(5)200411146 V. Description of Invention (5)

本發明所研發之射流流量計具有下列之優點: (1 )不同於一般的瓦斯流量計,此射流流里ό十的内部没有 任何可動元件,因此,不會因為長久的使用而造成量測的 誤差,且所產生的壓損較小。 (2 )針對量測中高流量的流體震盪室的部份,其對於不同 種類液體的流量量测,只需將量測的結果乘上一個校正因 子(即液體的密度)便可得到其流量,不需像一般的浮子流 量計還需依照不同的液體更換不同的浮子,可方便使用者 之操作,且大大地提升量測的準確性。除此之外,當流體 在流體震盪室中產生震盪時,亦可清除流量計内的髒東The jet flowmeter developed by the present invention has the following advantages: (1) Unlike ordinary gas flowmeters, there is no movable element inside the jet flow, so it will not cause measurement due to long-term use. Error, and the resulting pressure loss is small. (2) the fluid portion of the shock chamber for measuring high flow, which flow measurements for different types of liquids, the measurement results simply multiplied by a correction factor (i.e., the density of the liquid) flow can be obtained which, There is no need to replace different floats according to different liquids like ordinary float flow meters, which is convenient for users to operate and greatly improves the measurement accuracy. In addition, the shock generated when the fluid in the fluid chamber of the shock, the host can remove dirty meter

省 西,以維持量測時的準確性。 (3 )由於此射流流量計在微流量量測時,係利用多線型的 流量感测元件並配合飛行時間(T i m e 〇 f f 1 i gh t)原理進行 量測,所以能精確地量測到流體瞬時的速度。 (4)本發明之微管道中設置的多線型微流量感測元件,與 流體震盪室中所使用的單線型流體震盪感測元件,皆係利 用多晶矽材質製作,所以其具有低耗電量、高靈敏度的特 性,且易於和互補式金氧半導體(complementai_y Metal Oxide Semiconductor ; CMOS)電路相整合。 (5 ) —般所見的流量計通常都會生 ^ ^ ㈢乂成流體極大的壓力損 失,然而本發明之射流流量計其髀 吉&由、*从μ ^ 1 α ^人* L 、體知輕巧、成本低廉,1 直接串連於管路中且不會造成管路的壓阻。 (6 )本發明之射流流量計應用於 = 之膜式氣量計中,因其機械或可丛=,可以消除S ^ 勒件模組的磨擦阻力或ϊWest Province, in order to maintain accuracy in measurement. (3) Since this jet flow meter uses a multi-line flow sensing element in conjunction with the time-of-flight (T ime ff 1 i gh t) principle when measuring micro-flow, it can accurately measure The instantaneous velocity of the fluid. (4) The multi-line micro-flow sensing element provided in the micro-pipe of the present invention and the single-line fluid vibration sensing element used in the fluid oscillating chamber are made of polycrystalline silicon material, so it has low power consumption, High sensitivity and easy integration with complementary metal oxide semiconductor (CMOS) circuits. (5)-The flowmeters that are generally seen usually generate a great pressure loss in the fluid, but the jet flowmeter of the present invention is well-known by, * from μ ^ 1 α ^ person * L, the body knows Lightweight and low cost, 1 directly connected in the pipeline without causing piezoresistance in the pipeline. (6) The jet flow meter of the present invention is applied to a film-type gas meter, because of its mechanical or clustering, it can eliminate the friction resistance or ϊ of the S ^ module.

200411146 五、發明說明(6) 隙所造成之内部洩漏的問題。 【實施方式】 本發明所研發之射流流量計,係裝設於流場中,以量 測流場内之流體流量,其上視圖請參考「第7圖」所示, 其包括有三個主要的部份··缓衝室8 〇、微流道90,以及流 體晨盈至1 0 0。此緩衝室8 〇的主要功能是將流進此射流流 ϊ計的流場穩定,使其平順地流進射流流量計中,而不要 直接衝入微流道9 〇中,以免影響量測之結果。 而在微流道9 〇的部份,主要是藉由一些設置於微流道 9〇中的感測元件,量測微流量之流體;當微流道9〇中的感 測元件已無法感測到流體的流速時,便藉由與其相連接的 =體震盈室1 〇〇來量測中高流量的流體。所α,此射流流 =计不僅I量測微流量的流場,還可量測中高流量的流 場,其涵蓋的動態量測範圍較習知之流量計廣。 在緩衝室80中,其包括有第一入口81、第'一出口82, 及個5又置於鄰近第一入口 81處的擋體83,流體由第一入 口81進入緩衝室80中,並藉由擋體83的設置可使流體平順 地進入緩衝室80,而不會直接衝到微流道9〇中。 微流道90連接於緩衝室80的第一出口81,而使流體流 入其中,而第一出口81連接到微流道90的地方是以漸縮管 的型式,使流體自動加速流過微流道9〇。此微流道9〇中設 置有多線型微流量感測元件9丨,透過量測流體之飛行時間 (Tlme n UM)的方式,可量測微流量之流體。 請參考「第8圖」所示,此多線型微流量感測元件91200411146 V. Description of the invention (6) Internal leakage caused by gaps. [Embodiment] The jet flowmeter developed by the present invention is installed in the flow field to measure the fluid flow in the flow field. For the top view, please refer to "Figure 7", which includes three main parts Parts ... buffer chamber 80, microchannel 90, and fluid morning surplus to 100. The main function of the buffer chamber 80 is to stabilize the flow field flowing into the jet flow meter, so that it flows smoothly into the jet flow meter, instead of directly rushing into the microchannel 90, so as not to affect the measurement. result. In the micro-channel portion 9 billion, primarily provided by some of the sensing elements in the micro-channel 9〇, the measured amount of fluid in the micro flow; 9〇 micro channel when the sensing element is not sensing when measuring the flow rate of fluid, then by sEISMIC = 1 thousand and surplus chamber connected thereto to the amount of fluid in the high flow rate measurement. So, this jet flow = not only measures the flow field of micro flow, but also the flow field of medium and high flow, which covers a wider dynamic measurement range than the conventional flow meter. In the buffer chamber 80, which includes a first inlet 81, 'an outlet 82, and a stopper 5 and 83 disposed adjacent the first inlet 81, the fluid from the first inlet 81 into the buffer chamber 80, and With the arrangement of the blocking body 83, the fluid can smoothly enter the buffer chamber 80 without being flushed directly into the microchannel 90. The micro-flow channel 90 is connected to the first outlet 81 of the buffer chamber 80 to allow fluid to flow therein, and the place where the first outlet 81 is connected to the micro-flow channel 90 is a tapered tube type, which automatically accelerates the fluid to flow through the micro-flow Road 90. A multi-line micro-flow sensing element 9 丨 is set in the micro-fluidic channel 90, and the micro-fluid can be measured by measuring the time of flight (Tlme n UM) of the fluid. Please refer to "Figure 8", this multi-line micro flow sensor 91

第10頁 200411146 五、發明說明(7) 係由數個感測元件所組成,當流體流入微流道9 〇時,其第 一個接觸到的感測元件是一個加熱元件(Heater ) 9 1 a,而 其下游設置有與加熱元件9 1 a不同距離的溫度感測元件 91 b,當流體的流速改變時,可以在不同位置的溫度感測 元件9 1 b感測到其速度。Page 10 200411146 V. Description of the invention (7) It consists of several sensing elements. When the fluid flows into the microfluidic channel 90, the first sensing element it touches is a heater 9 1 a, and a temperature sensing element 91 b at a different distance from the heating element 9 1 a is disposed downstream thereof, and when the flow velocity of the fluid is changed, the temperature sensing element 9 1 b at a different position can sense its velocity.

其量測流體之流量的原理為:將此加熱元件9 1 a瞬時加 熱一段時間,而在加熱元件9 1 a上所產生的熱波會隨著流 體的移動而往下游移動,而在微流道9 0下游的溫度感測元 件9 1 b便會感測到此熱波。由於在設置此溫度感測元件9 j b 時,我們便知道每個溫度感測元件9 1 b與加熱元件9 1 a間的 距離大小,且也知道加熱元件9 1 a加熱與溫度感測元件9 1 b 感測到熱波中間的時間差,如此一來,便可計算流體之流 速,進而推算出流體之流量。 流體震盪室100中包括有第二入口 101、第二出口 1 0 2,及二個相對稱的障礙物1 〇 3。此第二入口 1 〇 1與微流 道9 0的另一端相連接,以使流體流入流體震盪室1 〇 〇中, 而第二出口 1 0 2則是與流場相連通。The principle of measuring the flow rate of fluid is: the heating element 9 1 a is heated instantaneously for a period of time, and the heat wave generated on the heating element 9 1 a will move downstream with the movement of the fluid, and the micro-flow The temperature sensing element 9 1 b downstream of the channel 90 will sense the heat wave. Since when setting this temperature sensing element 9 jb, we know the distance between each temperature sensing element 9 1 b and the heating element 9 1 a, and also know the heating element 9 1 a heating and temperature sensing element 9 1 b The time difference in the middle of the heat wave is sensed. In this way, the flow velocity of the fluid can be calculated, and the flow rate of the fluid can be calculated. The fluid oscillating chamber 100 includes a second inlet 101, a second outlet 102, and two symmetric obstacles 103. The second inlet 101 is connected to the other end of the microchannel 90, so that the fluid flows into the fluid oscillating chamber 100, and the second outlet 102 is in communication with the flow field.

而設置此障礙物1 〇 3的目的,是將此流體震盪室丨〇 〇區 隔成二個回饋流旁通道丨〇 4,流體經由這二個回饋流旁通 道104分別由鄰近第二出口 1〇2處沿著此障礙物1〇3的外緣 而回到第二入口 1 0 1 ;而在其中一個障礙物1 03上,或是可 以在二個障礙物1〇3上,設置有單線型流體震盪感測元件 103a 此單線型流體震盛感測元件ma係為壓力感測器。 當流體由微流道90進入流體震盪室1 00時,若此時流This provided an obstacle 〇3 purpose is this turbulence fluid chamber Shu thousand and two reserved segment to bypass flow passage Shu 〇4, respectively, by the fluid adjacent the second outlet via a bypass flow passage which two reserved 104 〇2 along the outer edge of this obstacle 103 and return to the second entrance 101; and one of the obstacles 103, or two obstacles 103 can be provided with a single line type fluid shock sensing elements 103a-line type fluid shock Sheng this sensing element is a pressure sensor based ma. When the fluid enters the fluid oscillating chamber 100 from the microfluidic channel 90, if the fluid flows at this time

200411146 發明說明(8) 2的田^數到達過渡流的狀態(即流體的流量到達中高流 里)’飢體便會產生不穩定的現象,此即為孔達效應。此 效應^使知由第二入口 1 0 1流入的喷流左右震盪,而藉由 流經兩回饋流旁通道1 04之流體,可激發此喷流穩定且持 續地左右震盪。 田此嗔'流往右震盪或是往左震盈時,設置於障礙物 10 3上的單線刑^ ^ ^ 、 、长、、 〃IL體晨盪感測元件1 0 3 a會明顯地感測到有 ^體版過來(因為如果沒有流體擺動過來,流體的流量會200411146 Invention description (8) 2 The number of fields reaches the state of transitional flow (that is, the flow of fluid reaches the middle and high flow). The starvation body will produce instability, which is the Kongda effect. This effect ^ makes the jet flowing in from the second inlet 101 to oscillate left and right, and the fluid flowing through the two feedback side passages 104 can excite the jet to oscillate stably and continuously.田 此 嗔 'When the shock is flowing to the right or shaking to the left, the single-line penalty set on the obstacle 10 3 ^ ^ ^, 晨, 长,, 〃IL body morning swing sensing element 1 0 3 a will obviously feel It is detected that the body version comes over (because if there is no fluid swinging over, the fluid flow will be

很小抑°由於此單線型流體震盪感測元件1 〇3a是一個壓力 感測器,因jf ,& , b 匕對於有沒有流體經過可以很敏感地感測 出來,如此一爽, > ^ 便可有效k而訊雜比’而提高流量計的 精準I i本發明在流體震盪室100的第二出口 102處,設 计成漸縮管的妹ϋ λ ^ a j、、°構’使其可以在較小的流量時便能開始發 生震盪現象。 ★、=丨 1目、θ前的技術’我們已知:流場中由孔達效應所產生 白、/瓜豆晨靈之頻率和流體的體積流率呈線性關係,因此, 可以由單線划# _ ^ 斤、爪體晨盪感測元件1 〇 3 a所量測到噴流的震盪Very small because the single-line fluid vibration sensing element 1 03a is a pressure sensor, because jf, & b can be sensitively sensed for the presence or absence of fluid, so refreshing, > ^ It can effectively reduce the signal-to-noise ratio and improve the accuracy of the flow meter. The present invention is designed as a tapered tube at the second outlet 102 of the fluid oscillating chamber 100. λ ^ aj,, ° It can start to oscillate at small flows. ★, = 1 Shu mesh technique before θ 'we know: of the flow field generated by the orifice effect white / frequency and volume flow rate of the fluid guar morning spirits linear relationship, thus, can be drawn by a single wire # _ ^ The vibration of the jet flow measured by the jin, claw body morning swing sensor 1 〇3a

二;庚gp 5 lb流體的體積流率,再將此體積流率乘上流體 的被度即可得到流體的質量流率。 當流體的泊I h t .^ ^ ^ 里較小時,由於此時流場的雷諾數還未到 沾31 t抓的狀態’因此流體震盪室1 00不會發生流體震盪 治^ ’此時流體之流量計量是以微流道90中的多線型微 = 件91進行量測。當流場中的流量到達中高流量 ^ I7 ”田居數到達過渡流的狀態),以空氣為例,當流速Second; hept gp 5 lb fluid volume flow rate, and then multiply this volume flow rate by the fluid's degree to get the mass flow rate of the fluid. When the poise I ht. ^ ^ ^ Of the fluid is small, since the Reynolds number of the flow field has not reached the state of 31 t at this time, the fluid oscillation chamber 100 will not undergo fluid oscillation treatment ^ 'At this time the fluid The flow rate is measured by a multi-line micro-element 91 in the micro-channel 90. When the flow in the flow field reaches medium to high flow ^ I7 "The number of fields has reached the state of transitional flow), taking air as an example, when the flow velocity

第12頁 200411146 五、發明說明(9) ίΓΛ公二分鐘時’ &時流體震盪室100中之流體便開 ‘成的ή 1中現象’巾其量測則改為以流體震盈室1 〇 〇所 2=盪頻率,計算當時的瞬時體積流率,再經由 /爪里计异邏軏程式換算成瞬時流量。 =此L本發明所研發之射流流量計其動態量測範圍較 體浐相大中小流量的流場量測’且其機械結構簡單, 接見在所使用的浮子流量計之大小,因此’可直 接串接於流場管路中。 晶石夕在流量感測元件的部>,其材料是使用多 心的白金’使製作出來的加熱元件、溫度感測 有低耗電量、高靈敏度及易於和互補戎+ 路相整合的特性。 7互補式金虱+導體電 表氣i ν月:射流流量計其應用範圍很廣泛,例如:瓦斯 、 U ;里測流場中流體之瞬時流量。 非用來上限所定述本者於明僅%為本Λ明其中的較佳實施例而已,並 圍所作的均等變化盥丄即凡依本發明申請專利範 ]寺支化與修舞,皆為本發明專利範圍所涵蓋。 200411146 圖式簡單說明 第1圖為習知之射流震盪流量計的結構示意圖; 第2圖為習知之流量計的結構示意圖; 第3圖為習知之流量計的結構示意圖; 第4圖為習知之小型化微電腦瓦斯表的結構示意圖 第5圖為習知之流量計的結構示意圖; 第6圖為習知之流量計的結構示意圖; 第7圖為本發明之射流流量計的上視圖;及 第8圖為本發明之微管道的示意圖。 【圖式符號說明】Page 12 200411146 V. Description of the invention (9) When the fluid flow in the fluid vibration chamber 100 is opened at two minutes, the fluid will be opened. The phenomenon of the phenomenon "1" will be changed to the fluid shock chamber 1 〇〇 所 2 = Swing frequency, calculate the instantaneous volume flow rate at that time, and then convert it to instantaneous flow rate by using the squaring program. = L developed the present invention, this fluidic flowmeter dynamic fluid flow measurement range than the field of measurement with medium and small flow Chan 'and simple mechanical structure, the float met flowmeters used in size, thus' direct Connected in the flow field pipeline. Xi spar portion in the flow sensing element >, the material which is used platinum suspicious' made out of the heating elements, temperature sensing low power consumption, and high sensitivity and ease of integration with a complementary passage of Rong + characteristic. 7 Complementary golden lice + conductor meter gas i ν: Jet flowmeter has a wide range of applications, such as: gas, U; measure the instantaneous flow of fluid in the flow field. It ’s not the upper limit stated that the author is only %% of the best examples of this, and the equivalent changes made around it are all those who apply for patents according to the present invention] temple branching and dance, both are Covered by the patent scope of the present invention. 200411146 Brief description of the diagram. Figure 1 is a schematic diagram of a conventional jet oscillating flowmeter. Figure 2 is a schematic diagram of a conventional flowmeter. Figure 3 is a schematic diagram of a conventional flowmeter. Figure 4 is a conventional small-sized flowmeter. Structure of a chemical microcomputer gas meter. Figure 5 is a schematic diagram of a conventional flow meter. Figure 6 is a schematic diagram of a conventional flow meter. Figure 7 is a top view of a jet flow meter of the present invention. Schematic diagram of the microchannel of the present invention. [Illustration of Symbols]

第14頁 10 入口 20 出口 30 阻擋體 31 凹槽 32 旁通道 40 流體震盡感測器 50 流道 6 0a 震盪室入口 60b 震盪室入口 70 漸縮段 80 緩衝室 81 第一入口 82 第一出口 83 擋體 90 微管道 200411146 圖式簡單說明 91 91a 91b 100 101 102 103 103a 104 多線型微流量感測元件 加熱元件 溫度感測元件 流體震盪室 第二入口 第二出口 障礙物 早線型流體震盪感測元件 回饋流旁通道Page 14 10 Inlet 20 Outlet 30 Barrier 31 Groove 32 Side Channel 40 Fluid Shock Sensor 50 Flow Channel 6 0a Oscillation Chamber Entrance 60b Oscillation Chamber Entrance 70 Tapered Section 80 Buffer Chamber 81 First Entrance 82 First Exit 83 Block 90 Micro-tube 200411146 Simple illustration 91 91a 91b 100 101 102 103 103a 104 Multi-line micro-flow sensing element heating element temperature sensing element fluid oscillating chamber second entrance second exit obstacle early linear fluid oscillation sensing Component feedback side channel

第15頁Page 15

Claims (1)

200411146200411146 六、申請專利範圍 測該流場内 i 一種射流流量計,裝設於一流場,用以量 之流體的流量,其包括有: 一緩衝室,其包括有一第一 抑卞斗枝 、n n 昂 八 一第一出口以及 坪近该弟一入口的一擋體,該流體由該第—入口進入該 緩衝室,並受到該擋體之JJ且ρ 承 士 版心沮枱而千順地進出該緩衝室; 、一微流道,連接於該緩衝室之該第一出口,而使該 流體加速流過,且該微流道中設置有一多線型微流量感 測元件;以及 一流體展盪室’其包括有一第二入口與第二出口, 该第一入口與该微流道的另一端相連接,而該第二出口 連通於該流場’且該流體震盪室内設置有二相對稱之障 礙物,而將該流體震盪室區隔形成二個回饋流旁通道’ 該流體經由二該回饋流旁通道分別由鄰近該第二出口處 沿著二該障礙物外緣而回到該第二入口; 其中一該障礙物設置有一單線型流體震盪感測元 件,當該流體流入該回饋型流體震盪室時,由於^達2 應的作用,會使該流體形成一喷流且左右震盪’藉3單 經各該回饋流旁通道之流體使該喷流穩定震盈’ 5 ^ < 線型流體震盪感測元件所量測之該喷流的震盈j出該射 推算該流體之流量,而該流體經由該第二出口/1料流 流流量計;且該多線型微流量感測元件你 Η Λ兮流體 ^ θ β年,即由滅 置之流體,當其無法量測該流體之流多/节㉟之流量。 2 ·如申請專利範圍第1項所述之射流流重J6. The scope of the patent application measures the flow field in the flow field. A jet flow meter is installed in the first-class field to measure the flow rate of the fluid, and includes: a buffer chamber, which includes a first damping bucket, an outlet and a stopper body floor near the brother an inlet of the fluid from this decision - entrance to the buffer chamber, and by JJ the stop member of and ρ bearing persons EDITION heart ju station and one thousand cis and out of the buffer chamber; A micro-flow channel connected to the first outlet of the buffer chamber to accelerate the flow of the fluid, and a multi-line micro-flow sensing element is provided in the micro-flow channel; and a fluid display chamber including: a second inlet and a second outlet, the first inlet and the other end of the micro channel is connected, and the second outlet in communication with the flow field 'and the fluid chamber is provided with two opposite shock referred obstacle, and The fluid oscillating chamber is partitioned to form two feedback side channels', and the fluid returns to the second inlet via the two feedback side channels along the outer edges of the two obstacles adjacent to the second outlet; The obstacle Was provided with a single line type fluid shock sensing element, when the fluid flows into the feedback type fluid shock chamber, since ^ of 2 corresponding action causes the fluid forms a jet of right and left shock 'by 3 single through each of the feedback The fluid in the side flow channel stabilizes the jet flow. 5 ^ < The shock of the jet flow measured by the linear fluid oscillating sensing element is used to estimate the flow rate of the fluid, and the fluid passes through the second Outlet / 1 flow flow meter; and the multi-line micro-flow sensing element you Η Λ Xi fluid ^ θ β years, that is, the destroyed fluid, when it is unable to measure the flow of the fluid . 2 · Jet weight as described in item 1 of the scope of patent application 第16頁 震盪室所量測之該喷流的震盪頻率推算3:^中另〆該 200411146Page 16 The oscillating frequency of the jet measured in the oscillating chamber is estimated at 3: ^ and the other is 200411146 六、申請專利範圍 ★〆該單 P早礙物亦設置有該單線型流體震盪感測元件’藉、 推算 線型流體震盪感測元件所量測之該喷流的震嚴頻率 該流體之流量。 由梦第一 3 ·如申請專利範圍第1項所述之射流流量計,其 μ 出口係為漸縮管的型式。 ^^第一 4·如申請專利範圍第丨項所述之射流流量計,其中瀛 出口係為漸縮管的型式。 > 少令 5 ·如申請專利範圍第丨項所述之射流流量計,其中瀛多备 型微流量感測元件包括有複數個微流量感測元件。 6·如申請專利範圍第4項所述之射流流量計,其中該流體 流經該微流道中第_個接觸的該微流量感測元件係為一加 熱元件,而其餘之該微流量感測元件係為溫度感測元件。 7 ·如申請專利範圍第4項所述之射流流量計,其中該加熱 元件係由多晶矽材質所組成。 8 8如申睛專利範圍第4項所述之射流流量計,其中該溫磨 感測元件係由多晶矽材質所組成。 9 ·如申睛專利範圍第1項所述之射流流量計,其中誃罝妗 型流體震盪感測元件係由多晶矽材質所組成。 7Sixth, the scope of patent application: 〆The single P early obstruction is also provided with the single-line fluid vibration sensing element ′, to estimate the vibration frequency of the jet measured by the linear fluid vibration sensing element and the flow rate of the fluid. From Dream First 3 · The jet flowmeter described in item 1 of the scope of patent application, the μ outlet is a type of tapered tube. ^^ First 4. The jet flowmeter as described in item 丨 of the patent application scope, wherein the 瀛 outlet is a type of tapered tube. > Lesser orders 5 · The jet flowmeter described in item 丨 of the patent application scope, wherein the multi-type micro-flow sensing element includes a plurality of micro-flow sensing elements. 6. The jet flowmeter as described in item 4 of the scope of the patent application, wherein the micro-flow sensing element that the fluid flows through the _th contact in the micro-flow channel is a heating element, and the remaining micro-flow sensing The element is a temperature sensing element. 7. The jet flow meter as described in item 4 of the scope of patent application, wherein the heating element is composed of polycrystalline silicon material. 88. The jet flowmeter as described in item 4 of the Shenjing patent scope, wherein the temperature-grinding sensing element is composed of polycrystalline silicon material. 9 · The jet flowmeter as described in item 1 of Shenjing's patent scope, in which the 誃 罝 妗 -type fluid vibration sensing element is composed of polycrystalline silicon material. 7
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