JPS621221B2 - - Google Patents

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Publication number
JPS621221B2
JPS621221B2 JP55004912A JP491280A JPS621221B2 JP S621221 B2 JPS621221 B2 JP S621221B2 JP 55004912 A JP55004912 A JP 55004912A JP 491280 A JP491280 A JP 491280A JP S621221 B2 JPS621221 B2 JP S621221B2
Authority
JP
Japan
Prior art keywords
current meter
flow
turbulence
value
equation
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
JP55004912A
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Japanese (ja)
Other versions
JPS56101560A (en
Inventor
Rikya Takeda
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP491280A priority Critical patent/JPS56101560A/en
Publication of JPS56101560A publication Critical patent/JPS56101560A/en
Publication of JPS621221B2 publication Critical patent/JPS621221B2/ja
Granted legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/02Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer
    • G01P5/06Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer using rotation of vanes
    • G01P5/07Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer using rotation of vanes with electrical coupling to the indicating device

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

従来はげしい渦流を伴う乱れた流れを取扱う現
場試験においては、定常流の場合に規定されてい
る各種測定法がそのまま適用されている。これら
による測定誤差は不明であるから、高精度の測定
結果は得られない。 本発明はこの欠点を除去するために、大流量の
直接計測に最適といわれている流速計法を取扱
い、物性値の異なる各種流体の定常流の広範な流
速域に適用できる翼車形流速計(以下流速計と呼
ぶ)の校正式を提示し、されに乱れ度の大きい流
れに対しても使用でき得るようその一般化と高精
度化をはかり、現場試験にも適用可能な流速計に
よる乱流測定法の確立を目的とするものである。 従来流速計の水用校正式は定常な流れにおい
て、指示流速Vを翼車の回転数nの一次関数と仮
定し、式中の常数αおよびβの値がそれぞれえい
航水槽試験により定められている。 V=an+β (1) (1)式のaおよびβの各値は、流体の密度ρ、動
粘度νおよびレイノルズ数Re(Re=VtR/ν,tR= 翼の外径点においての弦長)の各値が大きく変化
するとき、これらの影響を受けて、それぞれが変
化しなければならない。にもかかわらず、αおよ
びβについての換算式は不明であるから、それは
指示誤差発生の要因になつている。さらに、(1)式
はそのままはげしい渦流を伴う乱れた流れに適用
されると、上記の物性値の変化による影響のみな
らず流れの乱れ度の変化による影響も大きく受け
るので現場試験に対する適応性は不明である。 翼車形流速計校正式に関する解析 上述の欠点を除去するために、まず各種流体の
定常な流れを取扱い、レイノルズ数を用いて流れ
の状態を定義する。流速計翼車のμo(=UR/
V=翼端の周連/流速)はRe数の関数fを用い
て次式のように表わす。 μo=f(Re) (2) さらに、つきの無次元量を定義する。 X′=Re−(Re)s, Y′=Re−(Re)s/μo−(μo)s(3) (3)式において、(Re)sは翼車がはじめて定常
回転するときのRe数、(μo)sは(Re)sにお
いてのμoの値である。これら(Re)sおよび
(μo)sの各値は翼車のトルクおよびスラスト
を表示する基礎式により導出することができる。
理想形流速計については、双曲線関数の関係が適
用できる。 第1図は流速計のRe〜μo曲線と双曲線の関
係図例である。同図において、直角座標x,yは
それぞれRe,μoを示し、原点o、双曲線の両
漸近線はx=a′,y=b′とする。同図上Aは流速
計の設計諸元値x=(Re)dおよびy=(μo)
d、Bは(Re)s、Eは(Re)d、A′は点Aよ
り直線y=b′に下した垂線の足で、添字dは設計
点を示す。さらに線分BAの延長線とy=b′との
交点をC、∠ABE=∠ACA′=∠βとする。直線
AB上AC=BDになる点をDとし、点Dを通りy
軸に平行線DNを引き、x軸、y=b′との交点を
それぞれB′,Nとする。また翼車のμoの最大値
を(μo)maxとし、 y=b′≒(μo)max (4) とおくことは可能であり、(μo)maxの値は設
計ビツチから定められる。このとき、翼車の滑り
率S.R.はつぎのように定義することができる。 S.R.=(μo)d/(μo)max (5) 第1図において
Conventionally, in field tests that deal with turbulent flows accompanied by severe vortices, various measurement methods prescribed for steady flows are applied as they are. Since measurement errors caused by these are unknown, highly accurate measurement results cannot be obtained. In order to eliminate this drawback, the present invention deals with the current meter method, which is said to be optimal for direct measurement of large flow rates, and uses a vane wheel type current meter that can be applied to a wide flow velocity range of steady flows of various fluids with different physical properties. We present a calibration formula for a current meter (hereinafter referred to as a current meter), and aim to generalize and improve its accuracy so that it can be used for flows with a large degree of turbulence. The purpose is to establish a flow measurement method. The water calibration formula for conventional current meters assumes that the indicated flow velocity V is a linear function of the impeller rotation speed n in a steady flow, and the values of the constants α and β in the formula are determined by towing water tank tests. . V=an+β (1) The values of a and β in equation (1) are the fluid density ρ, kinematic viscosity ν, and Reynolds number Re (Re=VtR/ν, tR= chord length at the outer diameter point of the blade) When each value of , changes significantly, each must change under these influences. Nevertheless, since the conversion formula for α and β is unknown, this becomes a factor in the occurrence of indication errors. Furthermore, if Equation (1) is applied as is to a turbulent flow with violent vortices, it will be affected not only by changes in the physical property values mentioned above but also by changes in the degree of turbulence of the flow, making it less applicable to field tests. It is unknown. Analysis of the calibration formula for the impeller-type current meter In order to eliminate the above-mentioned drawbacks, we first treat the steady flow of various fluids and define the flow state using the Reynolds number. μo of the current meter impeller (=UR/
V=circumference of the blade tip/flow velocity) is expressed as follows using the function f of the Re number. μo=f(Re) (2) Furthermore, define the dimensionless quantity with. X′=Re−(Re)s, Y′=Re−(Re)s/μo−(μo)s(3) In equation (3), (Re)s is the Re when the impeller rotates steadily for the first time. The number (μo)s is the value of μo at (Re)s. The values of (Re)s and (μo)s can be derived from basic equations representing the torque and thrust of the impeller.
For an ideal current meter, a hyperbolic function relationship can be applied. FIG. 1 is an example of the relationship between the Re~μo curve of a current meter and a hyperbola. In the figure, rectangular coordinates x and y indicate Re and μo, respectively, and the origin o and both asymptotes of the hyperbola are x=a' and y=b'. A in the same figure is the design specification value of the current meter x = (Re) d and y = (μo)
d and B are (Re)s, E is (Re)d, A' is the leg of the perpendicular line drawn from point A to straight line y=b', and the subscript d indicates the design point. Furthermore, let C be the intersection of the extension of line segment BA and y=b', and ∠ABE=∠ACA'=∠β. straight line
Let D be the point where AC=BD on AB, pass through point D and y
Draw a parallel line DN to the axis, and let the intersections with the x-axis and y=b' be B' and N, respectively. Furthermore, it is possible to set the maximum value of μo of the impeller as (μo)max, and to set y=b′≒(μo)max (4), and the value of (μo)max is determined from the design bit. At this time, the slip rate SR of the impeller can be defined as follows. SR=(μo)d/(μo)max (5) In Fig. 1

【表】 なお、(4)式のa′の符号はつぎの条件から定められ
る。
[Table] Note that the sign of a' in equation (4) is determined from the following conditions.

【表】 ∠A′NB′の二等分線と双曲線の交点をQとし、
NQをhとすると、C=h2/2である。 第1図に示している双曲線は (Re−a′)(μo−b′)=−C (8) かくして、流速計のX′−Y′応答は(3)式と(8)式
からつぎのように示される。 X″/Y+X′/Y〔(Re)s−a′〕 +X′〔(μo)s−b′〕 +〔(Re)s−a′〕〔(μo)s−b′〕 =−C (9) 流速計の諸元値が定められると、(μo)s
0を仮定することができるので(9)式は直線的応答
を示す。 Y′=1/b′X′+(Re)s−a′/b′ (10) この結果、各種流体の定常流において(2)式は成
立し、流速計の校正式はレイノルズ数の関数によ
り表示することが可能になる。
[Table] Let Q be the intersection of the bisector of ∠A′NB′ and the hyperbola,
When NQ is h, C=h 2 /2. The hyperbola shown in Figure 1 is (Re−a′)(μo−b′)=−C (8) Thus, the X′−Y′ response of the current meter is It is shown as follows. X''/Y+X'/Y[(Re)s-a'] +X'[(μo)s-b'] +[(Re)s-a'][(μo)s-b'] =-C ( 9) Once the specifications of the current meter are determined, (μo)s
Since 0 can be assumed, equation (9) shows a linear response. Y' = 1/b' This makes it possible to display.

【表】 上記の(10)式が直線的応答を示すことから、(8)式
および(11)式は定常流の場合良好な校正式になる。 つぎに流速計が各種流体の乱流による影響を受
ける場合、流れの乱れ度T.F.の値(乱れの強さ
と大きさを包含した値)によつて流体の速度場の
変動は規定することができる。このとき、T.F.
=1は定常流の場合である。校正式として(8)式ま
たは(11)式を保持する良好な流速計は、流れの乱れ
度T.F.が一定値の場合、乱流に対しても直線的
応答を示すことが期待できる。流速計が各種の乱
れ度T.F.の値によつて影響を受けると、受ける
影響度に対応してそのμo―Re曲線は変化す
る。そこで、流れのT.F.の値に対する流速計の
応答関係(1−μpT/μo)はつぎのように仮定され る。 1μpT/μo=F1(Re)・F2(T.F.) (12) ここに示しているμpTは乱れの影響を受けたμ
oの値、F1およびF2はそれぞれReおよびT.F.の
関数である。 さらにつきの無次元量を定義する。 X″=1−μpT/μo (13) Y″=Re(1−μpT/μo) (14) 前述している定常流の場合、すなわちT.F.=
1のμo〜Re曲線は直線的応答を示しており、
乱れの影響を受ける場合のμpT〜Re曲線は経験
に基づくと定常流の場合と同様にほぼ直線的応答
を示す。この直線はつぎのように表わせる。 Y″=ATX″+Cr (15) (15)式に示している符号はつぎのようなもの
である。 X″〜Y″座標においてATは直線の勾配、Crは
直線の切片である。(15)式を書き換えると、 (μo−μpT)(Re−AT)=μoCT (16) (16)式を(12)式に代入すると右辺の関数関
係はつぎのように表わされる。 (1−μpT/μo)=1/Re−A・CT (17) (17)式を書き換えると、 μpT=μo(1−C/Re−A) (18) (18)式が各種流体の乱れた流れの影響を受け
る流速計の校正式である。 (18)式に示しているATおよびCTの各値は、
流速計による実測値を適用すると容易に定めるこ
とができる。すなわち、乱れた流れの場合、
(Re)Sの値を(Re)sTとすれば、ATの値はほぼ
(Re)sTの値に等しい。 AT(Re)sT (19) さらにCTは(12)式と(17)式からつぎのように
示すことができる。 CT=F3(T.F.) (20) ここに示しているF3はT.F.の関数である。こ
の関数は実測値に基づくとつぎのように示すこと
が可能になる。 CT=ψ(T.F.−1)〓 (21) (21)式に示している符号はつぎのように定義
する。φは横軸に(T.F.−1)を取り、縦軸を
Tとした両対数座標における直線の勾配、ψは
その切片である。(18)式に(19)式および
(21)式を代入すると、各種流体の乱れた流れの
影響を受ける流速計の実用的校正式は次式により
示される。 μpT=μo〔1−ψ(T.F.−1)〓/Re−(R
e)sT〕(22) (22)式は定常流の場合、すなわちT.F.=1
では、μpT=μoとなり、このとき(12)式により示
される応答は零である。 μpT=μo (23) 上記のことは、本解析において考慮した境界条
件であり、それは満足されている。 本発明翼車形流速計による乱流測定法の特徴上
述の流速計校正式の理論を適用した実施例につい
て、流れの流速および流量の計測に関する重要な
特徴を簡単に記述する。 1 定常流の場合 流速計は市販中良好な性能を示すといわれてい
る水用小形ott流速計No.3を用いて、各種流体の
各物性値が大きく異なつている空気、水および油
の流れを取扱い、これらの定常流における流速計
の特性へ検討を加える。 第2図は、横軸にレイノルズ数Reをとり、縦
軸をμoとした小形ott流速計の特性曲線図を示
す。同図には、空気、水および油の各実測値の例
がそれぞれ記号×、△および○の順序で記入され
てある。 第3図は使用した小形ott流速計の概略説明図
の例で、翼車の主要諸元値の例は、翼車外径=5
cm、平板翼3枚、ピツチ=25cm、翼面積=1914
mm、翼角32゜10′、面積比=0.985、節弦比=
1.187、材質=アラルダイトである。上記諸元値
に基づいて、本発明による校正式(11)式の計算結果
は次式のようになる。
[Table] Since equation (10) above shows a linear response, equations (8) and (11) are good calibration equations for steady flow. Next, when the current meter is affected by turbulent flow of various fluids, the fluctuation of the fluid velocity field can be specified by the value of the flow turbulence degree TF (a value that includes the strength and size of the turbulence). . At this time, TF
=1 is for steady flow. A good current meter that maintains equation (8) or equation (11) as a calibration formula can be expected to show a linear response even to turbulent flow when the flow turbulence degree TF is a constant value. When the current meter is influenced by various values of the degree of turbulence TF, its μo-Re curve changes in accordance with the degree of influence. Therefore, the response relationship (1-μ pT /μo) of the current meter to the value of TF of the flow is assumed as follows. 1μ pT /μo=F 1 (Re)・F 2 (TF) (12) μ pT shown here is μ affected by disturbance.
The values of o, F 1 and F 2 are functions of Re and TF, respectively. Furthermore, we define the dimensionless quantity with. X″=1−μ pT /μo (13) Y″=Re(1−μ pT /μo) (14) In the case of the steady flow described above, that is, TF=
The μo~Re curve of 1 shows a linear response,
Based on experience, the μ pT ~Re curve under the influence of turbulence shows an almost linear response, similar to the steady flow case. This straight line can be expressed as follows. Y″=A T X″+Cr (15) The signs shown in equation (15) are as follows. In the X″ to Y″ coordinates, A T is the slope of the straight line, and Cr is the intercept of the straight line. Rewriting equation (15), (μo−μ pT )(Re−A T )=μoC T (16) Substituting equation (16) into equation (12), the functional relationship on the right side is expressed as follows. (1-μ pT / μo) = 1/Re-A T・C T (17) Rewriting equation (17), μ pT = μo (1-C T /Re-A T ) (18) (18) This is the calibration formula for current meters that are affected by turbulent flows of various fluids. Each value of A T and C T shown in equation (18) is
It can be easily determined by applying actual measurements using a current meter. That is, in the case of turbulent flow,
If the value of (Re) S is (Re) sT , then the value of A T is approximately equal to the value of (Re) sT . A T (Re) sT (19) Furthermore, C T can be expressed as follows from equations (12) and (17). C T =F 3 (TF) (20) F 3 shown here is a function of TF. Based on actual measurements, this function can be expressed as follows. C T =ψ(TF-1) (21) The signs shown in equation (21) are defined as follows. φ is the slope of a straight line in log-logarithmic coordinates with (TF-1) on the horizontal axis and C T on the vertical axis, and ψ is its intercept. Substituting equations (19) and (21) into equation (18), the practical calibration formula for a current meter that is affected by the turbulent flow of various fluids is shown by the following equation. μ pT = μo [1-ψ(T.F.-1)=/Re-(R
e) sT ] (22) Equation (22) is for steady flow, that is, TF = 1
Then, μ pT =μo, and at this time, the response shown by equation (12) is zero. μ pT = μo (23) The above is the boundary condition considered in this analysis, and it is satisfied. Characteristics of the turbulence measurement method using the impeller-type current meter of the present invention Regarding an embodiment to which the theory of the above-mentioned current meter calibration formula is applied, important characteristics regarding the measurement of flow velocity and flow rate will be briefly described. 1 In the case of steady flow The current meter is a small OTT current meter for water, No. 3, which is said to have good performance on the market. We will discuss the characteristics of current meters in these steady flows. FIG. 2 shows a characteristic curve diagram of a small ott current meter with Reynolds number Re on the horizontal axis and μo on the vertical axis. In the figure, examples of measured values for air, water, and oil are written in the order of symbols x, △, and ○, respectively. Figure 3 is an example of a schematic explanatory diagram of the small ott current meter used, and an example of the main specifications of the impeller is as follows: outer diameter of the impeller = 5
cm, 3 flat blades, pitch = 25cm, blade area = 1914
mm, blade angle 32°10′, area ratio = 0.985, chord ratio =
1.187, material = araldite. Based on the above specification values, the calculation result of the calibration formula (11) according to the present invention is as follows.

【表】 (24)式による計算例は、実測値との比較のた
めに第2図中に実線を用いて記入してある。 さらに、第2図中には、従来一般に使用されて
いる水用校正式(1)式に基づく水用ott社校正式の
計算結果の例が点線により示されてある。上記の
実測値に対する両校正式の適用結果へ検討を加え
る。各種流体の定常流へ本発明による校正式を適
用すると、第2図に示しているように、(24)式
による計算結果はそれぞれの始動流速付近を除い
て、それぞれの広い流速範囲で良好な精度を保持
し、その指示誤差は±0.2%以下の値を示す。こ
れに比べて、ott社の水用校正式による計算結果
は、Re<104の場合、指示誤差が1%から30%の
値、Re>104では±0.5%以下の値となり、計測結
果の不正確さが明らかになつている。しかも、前
述のように、従来の校正式は各種流体に対する適
用性が不明である。よつて、本発明になる校正式
は各種流体の流れの広い流速の範囲で良好な精度
を示すことが認められる。 2 乱流の場合 本発明になる校正式は、自然のはげしい渦流を
伴う乱れた流れに対する適用性を考慮して、流れ
の乱れ度T.F.の値が大きく相違する水流へ適用
される。この場合、T.F.の値は球による計測法
によつて定められ、その値を大きく変化させるた
めに乱流格子(金網)が使用される。 使用流速計は、前記の小形ott流速計No.3を用
い、静止水中におけるえい航試験結果を定常流の
場合とし、それはT.F.=1と定義される。 第4図は、T.F.の各値をもつ乱流の影響を受
けるott流速計(4種類No.1,2,3,4)の実
測値に基づいたRe〜μo曲線図の例である。同
図に示している各記号はT.F.値が大きく異なつ
た場合の各流れを示し、T.F.の各値は、◎=
1.0,□=2.3,△=2.8,×=3.1で、●および〇は
気流の場合を示している。 前述のottNo.3の諸元値を用いると、本発明に
なる乱流用校正式(18)式または(22)式は次式
のように示される。 μpT=μo{1−43.9(T.F.−1)77/Re−(Re)s〔4.96×10−2(T.F.−1)
71+1〕}(25) T.F.=1の場合 μo=0.628−290/Re−388,(Re)s=850 (25)式を用いて計算した結果の例は第4図中
に実線で示してある。同図から、本発明になる校
正式は良好な精度を保持し、その指示誤差の値は
流速計の始動流速付近で±0.5%以下、流速が速
くなると±0.2%以下となり、流れの広い速度域
に対して適応することが明らかとなつた。 上述のことは、従来不明とされてきたはげしい
渦流を伴う乱れた流れを取扱う現場試験の場合、
その流速および流量が良好な精度で計測可能なこ
とを示している。 3 現場試験の場合 上記のように、本発明になる乱流用校正式は室
内実験によつて良好な精度を保持することが認め
られる。そこで、自然の渦流を伴うはげしい乱れ
を取扱う現場試験に対する本校正式の適応性の検
討を行う。 現場試験は第5図に示す中国電力株式会社広水
力発電所放水路の途中に3種類の測定器を取り付
けて同時測定を行つた。測定器は前述の小形ott
流速計No.3、流れの乱れ度とその方向も計測でき
る5孔探子球、および検定した標準ビトー管であ
る。 第5図は広発電所てい形放水路(上底=2670
mm、下底=1942mm、高さ=2000mm、長さ=40m)
と測定装置の平面図、正面図および断面説明図の
例で、図中に示している説明用の符号は使用した
器具と水路の概略寸法である。なお、同図中に示
す水路断面において点線は流量Q=6m3/Sの場
合に平均水深が1.4mQ=3.5m3/Sでは、0.8mを
示し、ott流速計O.C.、ピトー管Pおよび探子球
Sはそれぞれの支持棒O.C.S.,P.S.およびS.S.に
固定され、それらは各スライダーSLにより上下
および左右の方向へ自由に移動できるように設置
してある。 第6図は、上記の測定装置を用い、放水路にお
いて測定断面の中心線上での乱れと流速を測定し
た結果の例で、この場合の流量は6m3/S,45
m3/Sおよび3.5m3/Sである。 同図は横軸に流速をとり、縦軸には、放水路の
水位が示されてあり、図中の符号はそれぞれott
流速計およびピトー管によるもので、経験からピ
トー管による指示流速がほほ実流速として取扱わ
れている。さらに、ott流速計の実測値へ本発明
になる乱流校正式を適用した場合、流速計による
流れの乱れ度の値は探子球による実測値とほぼ等
しくなり、またその指示流速の値は、ピトー管に
よる指示流速の値に等しくなる。 第6図において、流れの乱れ度の各値の例は
ott流速計(校正式を適用しない)による各実測
値の左側に示してあり、またピトー管の指示流速
曲線とott流速計が示す流速曲線(校正式を適用
しない)の横座標間の距離がott流速計の指示誤
差である。 上述のことから、本発明になる流速計の乱流校
正式は、自然のはげしい渦流を伴う乱れた流れを
取扱う現場試験に適用されると、流れの流速のみ
ならずその乱れ度も良好な精度で計測できること
を明らかに示している。 4 試作水用小形流速計の場合 市販中の流速計を取扱い、前記の1,2および
3に基づくと、本発明になる校正式(11)式および
(18)式は、流れに対する実施試験へ良好な精度
を保持し、従来の流速計による計測法の欠陥を改
善する特徴を示している。さらに、新しく水用小
形流速計を設計製作し、その実施試験を行い、上
述している適応性を確認するために検討を加え
る。 第7図は、試作した水用小形流速計とその流速
指示装置の概略説明図例。 第7図において、流速計本体に設置してある回
転数発振器は翼車軸の抵抗トルクを軽減するため
に新しく工夫した非接触形である。すなわち、発
光ダイオードからの投光は本体内翼車軸の一端
(他端は翼車)に取付けたスリツトを通して光ダ
イオードにより感知できる。スリツトは翼車の回
転とともに回転するように製作してあるので、ス
リツトによる投光しや断回数が電気回路における
パルスとして受光部に受信できる構造となつてい
る。この回路はリード線から増幅器を通してデジ
タルカウンターに接続しているので流速に対する
翼車の回転数が計測できる。 上記の試作流速計に対する実施試験結果の例を
第8図に示す。第8図は横軸にレイノルズ数Re
をとり、縦軸には翼車のμoの値を示した試作流
速計のRe〜μo曲線例。試作4枚平板翼車の諸
元値は、外径=15mm、ボス径=6mm、翼角=30
゜、翼弦長=10.4mm、面積比=1.0、ピツチ=
11.78cmである。比較のため、試作流速計の諸元
値を用いて、校正式式を計算すると次式のよう
になる。 さらに、第8図に示してある実線は、(26)式
による計算値で、同図から流速計の始動流速の近
傍を除いて、計算値と実測値(〇は中国工業技術
試験所小形えい航水槽および広島大学えい航水
槽)はたいへん良好な精度で一致していることが
認められる。 上述のことから試作流速計に対する本発明にな
る校正式の適応性は良好なものと確認できる。な
お、乱流に対する適応性も同様な結果を得てい
る。 以上説明したように、この発明翼車形流速計の
校正式を各種流体の定常流および乱れた流れに適
用できるように、新しい無次元量を定義し、校正
式に対する解析を行い、各種流体の物性値の変化
による影響や乱れた流れの影響を除去することに
よつて、自然のはげしい乱れた渦流を取扱う現場
試験に対する計測を高精度化出来る効果がある。
よつて、本発明の現場試験に対する適用法は、乱
流測定法3に詳述したように上記の流速計とピト
ー管(または乱流特性の相異なる流速計2個)を
併用すると容易に乱流の流速ならびに流量を決定
することがでる。
[Table] An example of calculation using equation (24) is shown using a solid line in Figure 2 for comparison with actual measured values. Further, in FIG. 2, an example of the calculation result of the water calibration formula based on the water calibration formula (1) which has been commonly used in the past is shown by a dotted line. We will now consider the results of applying both calibration formulas to the above measured values. When the calibration formula according to the present invention is applied to the steady flow of various fluids, as shown in Figure 2, the calculation results using equation (24) are good over a wide flow velocity range, except around the starting flow velocity. Precision is maintained and the indication error is less than ±0.2%. In comparison, the calculation results using OTT's water calibration formula show that when Re < 10 4 , the indication error is between 1% and 30%, and when Re > 10 4 , the error is less than ±0.5%, and the measurement result is The inaccuracy of is becoming clear. Moreover, as mentioned above, the applicability of the conventional calibration formula to various fluids is unclear. Therefore, it is recognized that the calibration formula according to the present invention exhibits good accuracy over a wide range of flow velocities of various fluid flows. 2 Case of Turbulent Flow The calibration formula according to the present invention is applied to water flows in which the values of the degree of turbulence TF of the flows differ greatly, taking into consideration its applicability to turbulent flows accompanied by violent natural vortices. In this case, the value of TF is determined by the sphere measurement method, and a turbulence grid (wire mesh) is used to significantly change the value. The current meter used is the above-mentioned small ott current meter No. 3, and the towing test results in still water are assumed to be a steady flow, which is defined as TF=1. FIG. 4 is an example of a Re~μo curve diagram based on actual measurement values of OTT current meters (four types No. 1, 2, 3, and 4) that are affected by turbulence having various values of TF. Each symbol shown in the figure indicates each flow when the TF value differs greatly, and each value of TF is ◎=
1.0, □=2.3, △=2.8, ×=3.1, and ● and ○ indicate the case of airflow. Using the above-mentioned specification values of ott No. 3, the turbulent flow calibration equation (18) or (22) according to the present invention is expressed as the following equation. μ pT =μo{1-43.9(T.F.-1) 2 . 77 /Re-(Re)s [ 4.96×10-2 (T.F.-1)
3 . 71 +1]} (25) When TF=1 μo=0.628-290/Re-388, (Re)s=850 An example of the result calculated using equation (25) is shown by the solid line in Figure 4. be. From the same figure, the calibration formula according to the present invention maintains good accuracy, and the value of the indication error is less than ±0.5% near the starting flow velocity of the current meter, and less than ±0.2% when the flow velocity increases, and the value of the indication error is ±0.2% or less when the flow velocity increases. It has become clear that it is adaptable to various areas. The above is true in the case of field tests that deal with turbulent flows accompanied by violent vortices, which have been thought to be unknown in the past.
This shows that the flow rate and flow rate can be measured with good accuracy. 3. Case of Field Test As mentioned above, the turbulent flow calibration formula according to the present invention has been found to maintain good accuracy through laboratory experiments. Therefore, we will examine the formal suitability of our school for field tests that deal with violent turbulence accompanied by natural vortices. In the field test, three types of measuring instruments were installed in the middle of the Chugoku Electric Power Company's Hiroshi Hydroelectric Power Station tailrace channel as shown in Figure 5, and measurements were taken simultaneously. The measuring device is the small ott mentioned above.
These are a No. 3 current meter, a five-hole probe ball that can measure the degree and direction of flow turbulence, and a certified standard Vitot tube. Figure 5 shows the Hiro Power Plant's trough-shaped spillway (top = 2670
mm, bottom = 1942mm, height = 2000mm, length = 40m)
Examples of a plan view, a front view, and a cross-sectional explanatory view of the measuring device are shown, and the explanatory symbols shown in the figures indicate the approximate dimensions of the instruments and water channels used. In addition, in the cross section of the waterway shown in the same figure, the dotted line indicates an average water depth of 1.4 m when the flow rate Q = 6 m 3 /S and 0.8 m when Q = 3.5 m 3 /S. The balls S are fixed to respective support rods OCS, PS, and SS, and these are installed so that they can be freely moved vertically and horizontally by each slider SL. Figure 6 shows an example of the results of measuring the turbulence and flow velocity on the center line of the measurement cross section in the spillway using the above measuring device, and the flow rate in this case is 6 m 3 /S, 45
m 3 /S and 3.5m 3 /S. In this figure, the horizontal axis shows the flow velocity, and the vertical axis shows the water level in the spillway.
It is determined by a current meter and a pitot tube, and based on experience, the flow rate indicated by the pitot tube is treated as the actual flow rate. Furthermore, when the turbulence calibration formula of the present invention is applied to the actual measurement value of the OTT current meter, the value of the degree of turbulence of the flow measured by the current meter becomes almost equal to the actual value measured by the probe ball, and the value of the indicated flow velocity is It is equal to the flow rate indicated by the pitot tube. In Figure 6, examples of each value of flow turbulence are
The distance between the indicated velocity curve of the Pitot tube and the abscissa of the velocity curve indicated by the OTT velocity meter (without the calibration formula applied) is shown to the left of each actual value measured by the OTT velocimeter (no calibration formula applied). This is the reading error of the ott current meter. From the above, when the turbulence calibration formula of the current meter according to the present invention is applied to field tests that handle turbulent flows accompanied by violent natural vortices, it is possible to obtain good accuracy in not only the flow velocity but also the degree of turbulence. This clearly shows that it can be measured with 4 In the case of a prototype small-sized current meter for water Using a commercially available current meter, and based on 1, 2, and 3 above, the calibration equations (11) and (18) of the present invention can be applied to the actual flow test. It maintains good accuracy and exhibits characteristics that improve the deficiencies of conventional current measurement methods. Furthermore, we will design and manufacture a new small water velocity meter, conduct practical tests, and conduct studies to confirm the above-mentioned adaptability. FIG. 7 is an example of a schematic explanatory diagram of a prototype small current meter for water and its flow rate indicating device. In Fig. 7, the rotational speed oscillator installed in the main body of the current meter is a newly devised non-contact type to reduce the resistance torque of the blade axle. That is, the light emitted from the light emitting diode can be sensed by the photodiode through a slit attached to one end of the blade axle in the main body (the other end is the blade wheel). Since the slit is manufactured to rotate with the rotation of the impeller, the structure is such that the number of light projections and breaks caused by the slit can be received by the light receiving section as pulses in the electric circuit. Since this circuit is connected to a digital counter from the lead wire through an amplifier, it is possible to measure the number of revolutions of the impeller relative to the flow velocity. FIG. 8 shows an example of the test results for the above prototype current meter. In Figure 8, the horizontal axis is the Reynolds number Re.
An example of the Re~μo curve of a prototype current meter, where the vertical axis shows the value of μo of the impeller. The specifications of the prototype 4-plate flat blade wheel are: outer diameter = 15 mm, boss diameter = 6 mm, blade angle = 30.
°, chord length = 10.4mm, area ratio = 1.0, pitch =
It is 11.78cm. For comparison, the calibration equation is calculated using the specification values of the prototype current meter and becomes as follows. Furthermore, the solid line shown in Figure 8 is the calculated value using equation (26). water tank and Hiroshima University towing tank) are found to agree with very good accuracy. From the above, it can be confirmed that the calibration formula of the present invention has good adaptability to the prototype current meter. Furthermore, similar results were obtained regarding adaptability to turbulence. As explained above, in order to be able to apply the calibration formula of this invention's impeller-type current meter to steady flow and turbulent flow of various fluids, we defined new dimensionless quantities, performed analysis on the calibration formula, and By eliminating the effects of changes in physical property values and the effects of turbulent flow, it is possible to improve the accuracy of measurements for field tests that deal with naturally violently turbulent vortex flows.
Therefore, as detailed in Turbulence Measurement Method 3, the method of applying the present invention to on-site tests is to easily detect turbulence by using the above-mentioned current meter and pitot tube (or two current meters with different turbulence characteristics) together. It is possible to determine the flow rate as well as the flow rate of the flow.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は翼車形流速計のRe〜μo曲線と双曲
線の関係図例を示す。第2図は小形ott流速計の
Re―μo曲線図例。第3図は、小形ott流速計の
概略説明例。同図中の記号は、 1……本体、2……支持棒、3……車軸、4…
…翼車、5……ボールベアリング、6……ベアリ
ング押え、7……ねじ込みプラグ、8……スプリ
ング、9……パルス発生器、10……信号発生
器。 第4図は乱流の影響を受ける小形ott流速計の
Re―μo曲線図例。 第5図は広発電所てい形放水路および測定装置
の一部破断平面図、正面図および断面説明図の
例。同図に示してある記号はS.G.……固定枠、F.
……整流器、S.……探子救、M.M.……多管マノ
メーター、V.P.……真空ポンプ、B.……足場、V.
……流速、O.C.o……ttmeter、D.C.……デジタ
ルカウンター、P.……ピトー管、P.T.……圧力タ
ンク、SL.……スライダー、S.S.……球の支持
棒、P.S.……ピトー管の支持棒、O.C.S.ottの支
持棒。 第6図は広発電所放水路の測定断面の中心線上
での実測例。 第7図は、試作水用小形流速計の概略説明図
例。なお、同図中の記号11は増幅器、12はデ
ジタルカウンター。 第8図は、試作流速計のRe―μo曲線図例。
FIG. 1 shows an example of the relationship between the Re~μo curve and the hyperbola of a vane wheel type current meter. Figure 2 shows a small OTT current meter.
Example of Re-μo curve diagram. Figure 3 is a schematic example of a small OTT current meter. The symbols in the figure are: 1...Main body, 2...Support rod, 3...Axle, 4...
... impeller, 5 ... ball bearing, 6 ... bearing holder, 7 ... threaded plug, 8 ... spring, 9 ... pulse generator, 10 ... signal generator. Figure 4 shows a small OTT current meter affected by turbulence.
Example of Re-μo curve diagram. FIG. 5 is an example of a partially cutaway plan view, front view, and cross-sectional explanatory view of the Hiroden Power Plant's rectangular spillway and measuring device. The symbols shown in the figure are SG...Fixed frame, F.
... Rectifier, S. ... Probe, MM ... Multi-tube manometer, VP ... Vacuum pump, B. ... Scaffolding, V.
...Flow rate, OCo...ttmeter, DC...Digital counter, P....Pitot tube, PT...Pressure tank, SL....Slider, SS...Ball support rod, PS...Pitot tube support rod , OCSott support bar. Figure 6 is an example of an actual measurement taken on the center line of the measurement cross section of the Hiroden Power Station spillway. FIG. 7 is an example of a schematic explanatory diagram of a prototype small-sized current meter for water. In addition, the symbol 11 in the figure is an amplifier, and the symbol 12 is a digital counter. Figure 8 is an example of the Re-μo curve diagram of the prototype current meter.

Claims (1)

【特許請求の範囲】 1 次式 u0T=u0〔1−ψ(T.F.−1)〓/Re−(Re
ST〕 〔但し u0=翼端の周速/流速、u0T=乱れの影響を受
けるu0の値、T.F.=流れの乱れ度、Re=翼車の
レイノルズ数、(Re)ST=乱れた流れにおける翼
車の始動レイノルズ数、φ=実験定数、ψ=実験
定数、〕 により、乱れ度の異なる乱れた流れがそれぞれ翼
車形流速計の指示流速に及ぼす影響度を除去する
ことを特徴とする翼車形流速計による乱流測定
法。
[Claims] Linear equation u 0T = u 0 [1-ψ(T.F.-1)=/Re-(Re
) ST ] [However, u 0 = circumferential speed of blade tip/flow velocity, u 0T = value of u 0 affected by turbulence, TF = degree of turbulence of flow, Re = Reynolds number of impeller, (Re) ST = turbulence The starting Reynolds number of the impeller in a given flow, φ=experimental constant, ψ=experimental constant,] is characterized by eliminating the influence of turbulent flows with different degrees of turbulence on the indicated flow velocity of the impeller-type current meter. Turbulence measurement method using a vane wheel type current meter.
JP491280A 1980-01-19 1980-01-19 Turbulent flow measuring method by means of blade wheel current meter Granted JPS56101560A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP491280A JPS56101560A (en) 1980-01-19 1980-01-19 Turbulent flow measuring method by means of blade wheel current meter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP491280A JPS56101560A (en) 1980-01-19 1980-01-19 Turbulent flow measuring method by means of blade wheel current meter

Publications (2)

Publication Number Publication Date
JPS56101560A JPS56101560A (en) 1981-08-14
JPS621221B2 true JPS621221B2 (en) 1987-01-12

Family

ID=11596843

Family Applications (1)

Application Number Title Priority Date Filing Date
JP491280A Granted JPS56101560A (en) 1980-01-19 1980-01-19 Turbulent flow measuring method by means of blade wheel current meter

Country Status (1)

Country Link
JP (1) JPS56101560A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0242112U (en) * 1988-09-16 1990-03-23

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54781B2 (en) * 1972-08-30 1979-01-16

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0242112U (en) * 1988-09-16 1990-03-23

Also Published As

Publication number Publication date
JPS56101560A (en) 1981-08-14

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