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JP4456682B2 - Non-contact flow velocity detection method and apparatus - Google Patents
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JP4456682B2 - Non-contact flow velocity detection method and apparatus - Google Patents

Non-contact flow velocity detection method and apparatus Download PDF

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JP4456682B2
JP4456682B2 JP34141698A JP34141698A JP4456682B2 JP 4456682 B2 JP4456682 B2 JP 4456682B2 JP 34141698 A JP34141698 A JP 34141698A JP 34141698 A JP34141698 A JP 34141698A JP 4456682 B2 JP4456682 B2 JP 4456682B2
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voltage
gap
flow velocity
conductive fluid
eddy current
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JP2000162228A (en
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由多可 平賀
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Nippon Steel Nisshin Co Ltd
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Nisshin Steel Co Ltd
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Description

【0001】
【発明の属する技術分野】
本発明は、非接触流速検出方法及び装置に関し、特に、金属の連続鋳造設備の自由表面下の導電性流体の流速の誤成分を、予め検出した湯面と検知コイル間の予知ギャップの関数として求めた値を用いて除去することにより高精度な流速を得るための新規な改良に関する。
【0002】
【従来の技術】
従来、特開平9−33554号公報にも開示されているように、溶融金属の連続鋳造設備用に提案されている非接触流速検出器について図8に基づき説明する。
従来の非接触流速検出器は、測定対象の導電性流体30に低周波磁場φ0を印加するための前記励磁コイル4を湯面18に対して非接触に配置し、その周辺に励磁コイル4と導電性流体30との作用によって生じる磁場を検出する検知コイル6から構成される。
この際、低周波発振器1及び高周波発振器2からの低周波及び高周波が増幅器3を介して励磁コイル4に印加され、励磁コイル4からの低周波磁場φ0が導電性流体30に入射することにより、導電性流体30には、渦電流が形成される。また導電性流体30がある速度で移動している場合には、低周波磁場φ0と速度との作用によって生じる誘導電流が形成される。したがって、励磁コイル4の周辺に配置された検知コイル6には誘導電流によって生じた速度成分磁束φvと速度とは関係のない渦電流によって生じた渦電流磁束φsとが検出される。この2つの磁束φsと、φvが検知コイル6を貫くことにより、検知コイル6には渦電流成分電圧esと速度成分電圧evとが検出された起電圧として出力される。
ここでこの2つの成分は位相が互いに90゜異なるため、高周波フィルタ7aと低周波フィルタ7bを介して整流回路8と位相整流回路9bにより、検出された起電圧6aから、速度成分電圧と渦電流成分電圧とに分離し、ギャップ補正回路10bを経て速度成分電圧からなる流速Vを取り出す方法を採用していた。
【0003】
【発明が解決しようとする課題】
しかしながら、上述した従来技術では、位相整流回路を介してのみ起電圧から分離し速度成分電圧を取り出す方法であり、この方法では完全に速度成分電圧と渦電流成分電圧とを分離することができず、速度成分電圧には渦電流成分電圧が残留した状態で出力されていた。この速度成分電圧に残留する渦電流成分電圧起因の成分を単に残留成分△esとする。また、この渦電流成分電圧は流速検出器ヘッドと導電性流体の湯面間とで存在する傾きや、導電性流体の湯面形状、例えば流動によって生じるうねりや波立ちにより変動することがある。
これは傾きや波立ちによって、検知コイル面内で導電性流体との距離(ギャップ)のずれが生じ、それに伴い検知コイルを貫く渦電流成分磁場が変化し、その結果、渦電流成分電圧が変動することになる。上述したように、この渦電流成分電圧は位相整流しても速度成分電圧に残留するため、導電性流体が静止した状態においても、見かけ上、速度成分電圧ev(=△es)が生じていることになる。そのため、残留成分△esにより流速に関わらず、湯面形状に応じて見かけ上、速度成分電圧evが変化するため流速検出の測定精度の低下(図9で示される)を招く原因となり、特に自由表面下での測定を困難にする原因となっていた。
【0004】
本発明は、以上のような課題を解決するためになされたもので、特に、金属の連続鋳造設備の自由表面下の導電性流体の流速の誤差分を、予め検出した湯面と検知コイル間の予知ギャップの関数として求めた値を用いて除去することにより高精度な流速を得るようにした非接触流速検出方法及び装置を提供することを目的とする。
【0005】
【課題を解決するための手段】
本発明による非接触流速検出方法は、測定対象である導電性流体に対して、非接触に配置したコアの励磁コイルに低周波発振器と高周波発振器からの2つの交流電流が印加されることで生じた低周波磁場と高周波磁場が導電性流体に入射することにより、前記励磁コイルで発生した低周波磁場を妨げる方向に生じた磁束が鎖交することにより発生する渦電流成分電圧esと、前記励磁コイルからの低周波磁場と測定対象である導電性流体が相対移動することにより生じた速度成分電圧evとを検出するための検知コイルを有する流速検出器ヘッドを用いて前記導電性流体の流速を得るようにした非接触流速検出方法において、前記検知コイルにより起電圧(速度成分電圧ev+渦電流成分電圧es+ギャップ分電圧eo+誤差分△esよりなる)を測定し、前記起電圧のうち、渦電流成分電圧esは位相整流により分離されて出力され、ギャップ分電圧eoは高周波磁界の整流で除去し、前記渦電流成分電圧esのうちの前記誤差分△esを、△es=α・esと定め、前記αは前記導電性流体の湯面と前記検知コイル間のギャップを予め得た予知ギャップの関数として求めた値を用いて除去することにより、前記導電性流体の前記流速を得る方法であり、また、前記予知ギャップは、前記導電性流体が静止している状態で測定する方法であり、また、本発明による非接触流速検出装置は、測定対象である導電性流体に対して、非接触に配置したコアの励磁コイルに低周波発振器と高周波発振器からの2つの交流電流が印加されることで生じた低周波磁場と高周波磁場が導電性流体に入射することにより、前記励磁コイルで発生した低周波磁場を妨げる方向に生じた磁束が鎖交することにより発生する渦電流成分電圧esと、前記励磁コイルからの低周波磁場と測定対象である導電性流体が相対移動することにより生じた速度成分電圧evとを検出するための検知コイルを有する流速検出器ヘッドを用いて前記導電性流体の流速を得るようにした非接触流速検出装置において、前記検知コイルからの検知電圧に対して低周波フィルタを経た後に位相整流を行うことにより渦電流成分電圧と速度成分電圧とを分離するための位相整流回路と、前記検知コイルで検知され高周波フィルタを介して得られたギャップ信号電圧の値を基に導電性流体とのギャップを求め、このギャップ変化に伴う速度成分電圧及び渦電流成分電圧の変化を補正するため、前記位相整流回路で取り出した速度成分電圧と渦電流成分電圧を補正するためのギャップ補正回路と、前記ギャップ補正回路に接続された演算回路とを備え、前記ギャップ補正回路を介して出力された速度成分電圧から渦電流成分電圧の誤差分△esを△es=α・esと定め、前記αは前記導電性流体の湯面と前記検知コイル間の間隔を予め得た予知ギャップの関数として求めた値を用いて除去し、前記演算回路から前記導電性流体の流速を得るようにした構成である。
【0006】
【発明の実施の形態】
以下、図面と共に本発明による非接触流速検出方法及び装置の好適な実施の形態について説明する。なお、従来例と同一又は同等部分については同一符号を用いて説明する。
図1において符号15で示されるものはコア5、励磁コイル4及び検知コイル6とからなる流速検出器ヘッドであり、この励磁コイル4には、低周波発振器1及び高周波発振器2からの低周波及び高周波が増幅器3を介して励磁コイル4に印加されている。なお、このコア5は正逆交互に180度位置をかえて検出するように構成されている。
【0007】
前記検知コイル6から得られた起電圧eは、高周波フィルタ7a及び整流回路8を介して第1ギャップ補正回路10aに印加されると共に、低周波フィルタ7b、1対の位相整流回路9a,9bを経て第1、第2ギャップ補正回路10a,10bに印加され、各ギャップ補正回路10a,10bの出力は演算回路16に入力されて流速Vが出力されるように構成されている。
【0008】
次に、動作について述べる。まず、励磁コイル4からの低周波交流磁場により、導電性流体30には渦電流が形成され、それに伴い低周波磁場と打ち消し合う方向の磁束φsa,φsbが図2の如く形成される。
ここで流速検出器ヘッド15と導電性流体30の湯面18が平滑な場合では、流速検出器ヘッド15の底部面と湯面18間の距離すなわちギャップ20が何れの点においても同一であるため、流れ21の上流側、下流側に形成される渦電流による磁束φsa,φsbは、検知コイル6に対して互いに打ち消し合う方向に作用しており、磁束φsa,φsbの差分が検出される。なお、φoは励磁磁束、φvは速度成分磁束である。
しかしながら、流速検出器ヘッド15の設置時に湯面18との傾きがある場合や流動によって湯面18にうねり、波立ちがある場合のように流速検出器ヘッド15の底部面と湯面18間のギャップ20が異なる時、磁束φsa,φsbの差分が増加し、渦電流成分電圧esも増加する。さらに湯面形状が連続的に変動している場合には、この渦電流成分電圧esも変動する。従来、この渦電流成分電圧esは起電圧eから位相整流して分離する信号処理を行うが、完全に分離・除去されず、残留し流速検出に際しては、大きな外乱となる。
そこで本発明では、この外乱の原因である渦電流によって生じる磁束φsa,φsbの差分により発生する渦電流成分電圧esより速度成分電圧evの補正を行う。補正処理を行うため、各位相整流回路9a,9bを介して起電圧eより渦電流成分電圧esと速度成分電圧evを分離し、この渦電流成分電圧esから残留成分を求め、速度成分電圧evから減算処理を行う。
この残留成分すなわち誤差分△esと渦電流成分電圧esとは次式で規定できる。
△es=α・es (1)
ここでαは、残留率であり、予め求めた係数である。すなわち予め静止湯面上での検知コイル6と湯面18との間のギャップを予知ギャップ20Aとして測定を行い、この予知ギャップ20Aの関数として後述のように求めた値を用いる。従って、求める速度成分電圧evは、式(1)より次式で示される。
ev=evt−α・es (2)
式(2)に基づいて渦電流成分電圧esにより、常に速度成分電圧evを補正することにより、自由表面下においても、精度よく流速Vを検出することができる。なお、この予知ギャップ20Aは湯面18が静止状態に限らず流れている場合でも可である。
【0009】
次に、前述の誤差分α・esのαの決め方について述べる。
コア5を180度回転させながら正逆の位置で起電圧eを測定する場合、検知コイル6には、
e(起電圧)=ev(速度分)+es(渦電流分)+eo(ギャップ分電圧)+△es(誤差分)が発生するため、位相整流でesを除去し正逆の速度成分の和を1/2し、高周波磁界の整流でeoを除去するが(これまでは従来方法と同じ)、誤差分△esについては、渦電流に比例するものとし、△es=α・esとして除去することで精度良い流速Vを得ている。
すなわち、本願は、前述の従来技術に加えて、検出器の傾きによる誤差を補正するもので、その補正におけるαの決め方を図4から図7を用いて説明する。
まず、静止湯面状へ検出器ヘッド15を設置し、ギャップ長毎(コア5のNS極先端の中心位置と静止湯面距離)に検出器ヘッド15のN/S極の傾きを変化させて、傾きと渦電流成分電圧esの関係を図4の如くプロットする。
次に、湯面18にある一定の流速を与え、検出器ヘッド15(α=1とする)と従来流速計(例えば周知の助川電工製の接触型)にて両検出器による流速を測定する。
この場合、本発明の検出器ヘッド15はギャップ長毎に傾きを変化させて測定するが、ギャップ及び傾きに対応して、従来流速計は一定であるので検出器ヘッド15の測定速度は変化して差が生じる。
その差(残留率αに相当する)を、水平設置時の検出器ヘッド15の検出電圧と従来検出器の速度の関係から、当該差を逆算して電圧に換算しその電圧を残留成分として、図5のような傾きと残留成分△esのプロット図を作成する。
図6は、前記図4と図5を同一ギャップ、傾きで、渦電流成分電圧esを残留成分で整理し、プロットし直したものである。この図から分かるように、各ギャップ毎の残留成分は渦電流成分電圧と比例関係にあり、各ギャップ毎に直線近似でき、ギャップによって傾きが異なることが明らかである。
上記ギャップ毎の傾き(残留率αに相当)をプロットしたものが図7である。このプロットから残留率αは、ギャップの2次近似式で表されることが分かり、検出器ヘッド15の設置位置によって、検出器ヘッド15の傾きに左右されずαを決定でき精度を向上することができる。すなわち、このαは導電性流体30の湯面18と検知コイル6間の間隔から予め得た予知ギャップ20Aの関数として求めた値を用いている。
【0010】
【実施例】
流速検出器ヘッド15を測定対象である溶融したウッドメタル(メルティング・ポイント=70℃)溶湯100℃の湯面18に対して非接触に配置し、流速の測定を行った。なお、湯面18は自由表面である。100Hzの低周波発振器1および20kHz高周波発振器2より励磁コイル4に高低2つの交流磁場を印加した。このとき検知コイル6からの起電圧eは、周波数の違いにより高周波成分の信号と低周波成分の信号とに弁別される。低周波成分の信号は、各位相整流回路9a,9bにより速度成分電圧evと渦電流成分電圧esとに分離し、高周波フィルタ7a、整流回路8を通して得られるギャップ信号によりギャップ変化による出力変動であるギャップ分電圧eoを補正した補正後の速度成分電圧evと渦電流成分電圧esが出力される。すなわち、前記各ギャップ補正回路10a,10bでは、検知コイル6で検知され高周波フィルタ7aを介して得られたギャップ分電圧eoの値を基に導電性流体30とのギャップを求め、このギャップ変化に伴う速度成分電圧ev及び渦電流成分電圧esの変化を補正するため、各位相整流回路9a,9bで取り出した速度成分電圧evと渦電流成分電圧esを補正している。さらに速度成分電圧evは演算回路16により渦電流成分電圧esの値に基づき、渦電流成分に起因した外乱成分が除去される。演算回路16では、式(1)と式(2)で示されるようにギャップ補正後の速度成分電圧evtより、渦電流成分電圧esより求めた残留成分△esを減算することにより正味の速度成分電圧evが速度信号として出力される。
ギャップ補正のみを行った場合での速度成分電圧(evt)を流速に変換した結果を図9(従来方法)に、渦電流成分による残留成分の補正を行った場合の結果を図3(本発明方法)に示す。図中には参照として同時に測定した浸漬タイプの流速計の測定値(点線で薄く示される)も示した。図9,3に示されるように残留成分の補正を行うことにより非接触流速計の精度は著しく向上したことが明らかである。なお、図1の各部に信号の内容を式で表記した。
【0011】
【発明の効果】
本発明による非接触流速検出方法及び装置は、以上のように構成されているため、次のような効果を得ることができる。すなわち、起電圧(e)のうちの渦電流成分電圧(es)は位相整流で除去し、ギャップ電圧分(eo)は高周波磁界の整流で除去し、誤差分(△es)を、△es=α・esとし、αを予知ギャップ(20A)の関数として求めた値を用いて除去することにより高精度の流速(V)を求めることができる。
【図面の簡単な説明】
【図1】 本発明による非接触検出方法を適用した装置を示す構成図である。
【図2】 図1の動作を示す説明図である。
【図3】 図1の方法による流速/時間特性図である。
【図4】 本発明による渦電流電圧成分検出特性図である。
【図5】 本発明による流速検出器ヘッド/湯面間の傾きの影響特性図である。
【図6】 本発明による渦電流成分電圧と残留成分との関係特性図である。
【図7】 本発明による残留率と予知ギャップとの関係特性図である。
【図8】 従来方法を適用した装置を示す構成図である。
【図9】 図8の従来方法の流速/時間特性図である。
【符号の説明】
1 低周波発振器
2 高周波発振器
3 増幅器
4 励磁コイル
5 コア
6 検知コイル
7a 高周波フィルタ
7b 低周波フィルタ
8 整流回路
9a,9b 位相整流回路
10a,10b ギャップ補正回路
30 導電性流体
φo 励磁磁束
φs 渦電流磁束
φv 速度成分磁束
15 流速検出器ヘッド
16 演算回路
18 湯面
20 ギャップ
20A 予知ギャップ
21 溶融金属の流れ
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a non-contact flow velocity detection method and apparatus, and more particularly, to an erroneous component of the flow velocity of a conductive fluid below the free surface of a continuous metal casting facility as a function of a prediction gap between a molten metal surface and a detection coil. The present invention relates to a novel improvement for obtaining a highly accurate flow rate by removing using the obtained value.
[0002]
[Prior art]
Conventionally, as disclosed in Japanese Patent Laid-Open No. 9-33554, a non-contact flow rate detector proposed for a molten metal continuous casting facility will be described with reference to FIG.
In the conventional non-contact flow velocity detector, the excitation coil 4 for applying the low frequency magnetic field φ0 to the conductive fluid 30 to be measured is disposed in a non-contact manner with respect to the molten metal surface 18, and the excitation coil 4 and The detection coil 6 is configured to detect a magnetic field generated by the action with the conductive fluid 30.
At this time, the low frequency and high frequency from the low frequency oscillator 1 and the high frequency oscillator 2 are applied to the excitation coil 4 via the amplifier 3, and the low frequency magnetic field φ 0 from the excitation coil 4 is incident on the conductive fluid 30. An eddy current is formed in the conductive fluid 30. In addition, when the conductive fluid 30 moves at a certain speed, an induced current generated by the action of the low frequency magnetic field φ0 and the speed is formed. Therefore, the detection coil 6 arranged around the exciting coil 4 detects the velocity component magnetic flux φv generated by the induced current and the eddy current magnetic flux φs generated by the eddy current unrelated to the velocity. When these two magnetic fluxes φs and φv pass through the detection coil 6, eddy current component voltage es and velocity component voltage ev are output to the detection coil 6 as detected electromotive voltages.
Since these two components are 90 ° out of phase with each other, the speed component voltage and the eddy current are detected from the electromotive voltage 6a detected by the rectifier circuit 8 and the phase rectifier circuit 9b via the high frequency filter 7a and the low frequency filter 7b. A method of taking out the flow velocity V composed of the velocity component voltage through the gap correction circuit 10b is used.
[0003]
[Problems to be solved by the invention]
However, the above-described prior art is a method of extracting the velocity component voltage by separating it from the electromotive voltage only through the phase rectifier circuit, and this method cannot completely separate the velocity component voltage and the eddy current component voltage. The velocity component voltage was output with the eddy current component voltage remaining. The component resulting from the eddy current component voltage remaining in the velocity component voltage is simply referred to as a residual component Δes. In addition, the eddy current component voltage may fluctuate due to an inclination existing between the flow velocity detector head and the molten metal surface of the conductive fluid, or a molten metal surface shape of the conductive fluid, for example, undulation or ripple caused by flow.
This is caused by a deviation in the distance (gap) from the conductive fluid in the sensing coil surface due to inclination or undulation, and the eddy current component magnetic field penetrating the sensing coil changes accordingly, and as a result, the eddy current component voltage fluctuates. It will be. As described above, since this eddy current component voltage remains in the velocity component voltage even when phase rectified, the velocity component voltage ev (= Δes) is apparently generated even when the conductive fluid is stationary. It will be. For this reason, the residual component Δes apparently changes according to the shape of the molten metal surface regardless of the flow rate, so that the velocity component voltage ev changes, causing a decrease in the measurement accuracy of the flow velocity detection (shown in FIG. 9). It was the cause that made measurement under the surface difficult.
[0004]
The present invention has been made to solve the above-described problems. In particular, an error in the flow velocity of the conductive fluid below the free surface of the continuous casting equipment for metal is detected between the molten metal surface and the detection coil. It is an object of the present invention to provide a non-contact flow velocity detection method and apparatus capable of obtaining a highly accurate flow velocity by removing using a value obtained as a function of the prediction gap.
[0005]
[Means for Solving the Problems]
The non-contact flow velocity detection method according to the present invention is generated by applying two alternating currents from a low-frequency oscillator and a high-frequency oscillator to a core exciting coil arranged in a non-contact manner with respect to a conductive fluid to be measured. The eddy current component voltage es generated by the linkage of the magnetic flux generated in the direction that interferes with the low frequency magnetic field generated by the excitation coil when the low frequency magnetic field and the high frequency magnetic field are incident on the conductive fluid, and the excitation The flow velocity of the conductive fluid is measured by using a flow velocity detector head having a detection coil for detecting a low frequency magnetic field from the coil and a velocity component voltage ev generated by relative movement of the conductive fluid to be measured. In the non-contact flow velocity detection method obtained, an electromotive force (speed component voltage ev + eddy current component voltage es + gap voltage eo + error Δes) is generated by the detection coil. ) Was measured, among the electromotive voltage, eddy current component voltage es is outputted are separated Ri by the phase commutation gap portion voltage eo is removed by rectification of high-frequency magnetic field, of the eddy current component voltage es The error Δes is defined as Δes = α · es, where α is removed using a value obtained as a function of a prediction gap obtained in advance for the gap between the molten metal surface of the conductive fluid and the detection coil. Thus, the flow velocity of the conductive fluid is obtained, and the prediction gap is a method of measuring the conductive fluid in a stationary state, and the non-contact flow velocity detection device according to the present invention. Is a low-frequency magnetic field and a high-frequency magnetic field generated by applying two alternating currents from a low-frequency oscillator and a high-frequency oscillator to a core exciting coil arranged in a non-contact manner with respect to a conductive fluid to be measured. For conductive fluid The eddy current component voltage es generated when the magnetic flux generated in the direction that hinders the low-frequency magnetic field generated in the excitation coil is interlinked, and the low-frequency magnetic field from the excitation coil and the conductivity to be measured In the non-contact flow velocity detection device, wherein the flow velocity of the conductive fluid is obtained using a flow velocity detector head having a detection coil for detecting the velocity component voltage ev generated by relative movement of the conductive fluid, A phase rectification circuit for separating an eddy current component voltage and a velocity component voltage by performing phase rectification on the detection voltage from the detection coil after passing through a low frequency filter, and detected by the detection coil via a high frequency filter Based on the value of the gap signal voltage obtained in this way, the gap with the conductive fluid is obtained, and the change in the velocity component voltage and eddy current component voltage accompanying this gap change. For correcting the velocity component voltage and the eddy current component voltage extracted by the phase rectifier circuit, and an arithmetic circuit connected to the gap correction circuit, and through the gap correction circuit determined from the velocity component voltage outputted error component △ es eddy current component voltage △ es = α · es Te, the alpha got previously the spacing between the sensing coil and the molten metal surface of the conductive fluid The value obtained as a function of the prediction gap is removed, and the flow velocity of the conductive fluid is obtained from the arithmetic circuit.
[0006]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, preferred embodiments of a non-contact flow velocity detection method and apparatus according to the present invention will be described with reference to the drawings. The same or equivalent parts as those in the conventional example will be described using the same reference numerals.
A reference numeral 15 in FIG. 1 indicates a flow velocity detector head including a core 5, an excitation coil 4 and a detection coil 6, and the excitation coil 4 includes a low frequency and a low frequency from the low frequency oscillator 1 and the high frequency oscillator 2. A high frequency is applied to the exciting coil 4 via the amplifier 3. The core 5 is configured to detect by changing the position 180 degrees alternately forward and reverse.
[0007]
The electromotive voltage e obtained from the detection coil 6 is applied to the first gap correction circuit 10a via the high-frequency filter 7a and the rectifier circuit 8, and the low-frequency filter 7b and the pair of phase rectifier circuits 9a and 9b. Then, it is applied to the first and second gap correction circuits 10a and 10b, and the outputs of the gap correction circuits 10a and 10b are input to the arithmetic circuit 16 to output the flow velocity V.
[0008]
Next, the operation will be described. First, an eddy current is formed in the conductive fluid 30 by the low-frequency AC magnetic field from the exciting coil 4, and accordingly magnetic fluxes φsa and φsb in a direction that cancels the low-frequency magnetic field are formed as shown in FIG.
Here, when the flow velocity detector head 15 and the molten metal surface 18 of the conductive fluid 30 are smooth, the distance between the bottom surface of the flow velocity detector head 15 and the molten metal surface 18, that is, the gap 20 is the same at any point. The magnetic fluxes φsa and φsb due to the eddy currents formed on the upstream side and the downstream side of the flow 21 act in a direction that cancels each other, and the difference between the magnetic fluxes φsa and φsb is detected. Note that φo is an excitation magnetic flux, and φv is a velocity component magnetic flux.
However, when the flow velocity detector head 15 is installed, the gap between the bottom surface of the flow velocity detector head 15 and the molten metal surface 18, such as when there is an inclination with the molten metal surface 18 or when the molten metal undulates and flows due to flow. When 20 is different, the difference between the magnetic fluxes φsa and φsb increases, and the eddy current component voltage es also increases. Further, when the molten metal surface shape continuously varies, the eddy current component voltage es also varies. Conventionally, the eddy current component voltage es is subjected to signal processing for phase rectification and separation from the electromotive voltage e. However, the eddy current component voltage es is not completely separated / removed, and remains and becomes a great disturbance when detecting the flow velocity.
Therefore, in the present invention, the velocity component voltage ev is corrected from the eddy current component voltage es generated by the difference between the magnetic fluxes φsa and φsb generated by the eddy current that is the cause of the disturbance. In order to perform the correction process, the eddy current component voltage es and the velocity component voltage ev are separated from the electromotive voltage e through the phase rectifier circuits 9a and 9b, the residual component is obtained from the eddy current component voltage es, and the velocity component voltage ev Subtract processing from.
The residual component, that is, the error Δes and the eddy current component voltage es can be defined by the following equation.
△ es = α ・ es (1)
Here, α is a residual ratio, which is a coefficient obtained in advance. That is, the gap between the detection coil 6 and the molten metal surface 18 on the static molten metal surface is measured in advance as a prediction gap 20A, and a value obtained as described below is used as a function of the prediction gap 20A. Therefore, the speed component voltage ev to be obtained is expressed by the following equation from the equation (1).
ev = evt−α · es (2)
By always correcting the velocity component voltage ev by the eddy current component voltage es based on the equation (2), the flow velocity V can be detected with high accuracy even under the free surface. Note that the prediction gap 20A is possible even when the molten metal surface 18 is flowing in a stationary state.
[0009]
Next, how to determine α of the above-mentioned error α · es will be described.
When measuring the electromotive voltage e at the forward and reverse positions while rotating the core 5 180 degrees,
e (electromotive voltage) = ev (speed min) + es (eddy current component) + eo order (gap portion voltage) + △ es (error component) is generated, the sum of the velocity components of the forward and reverse removed es phase rectifier ½, and eo is removed by rectification of the high-frequency magnetic field (the same as the conventional method so far), but the error Δes is proportional to the eddy current and is removed as Δes = α · es. Thus, the flow velocity V with high accuracy is obtained.
That is, the present application corrects an error due to the inclination of the detector in addition to the above-described conventional technique, and how to determine α in the correction will be described with reference to FIGS.
First, the detector head 15 is installed in the shape of a stationary molten metal surface, and the inclination of the N / S pole of the detector head 15 is changed for each gap length (the center position of the NS pole tip of the core 5 and the stationary molten metal surface distance). The relationship between the slope and the eddy current component voltage es is plotted as shown in FIG.
Next, a certain flow velocity is given to the molten metal surface 18, and the flow velocity by both detectors is measured with a detector head 15 (α = 1) and a conventional flowmeter (for example, a contact type manufactured by well-known Sukegawa Electric Works). .
In this case, the detector head 15 of the present invention performs measurement while changing the inclination for each gap length. However, the measurement speed of the detector head 15 changes corresponding to the gap and inclination because the conventional anemometer is constant. Difference.
The difference (corresponding to the residual rate α) is converted back to a voltage by back-calculating the difference from the relationship between the detection voltage of the detector head 15 during horizontal installation and the speed of the conventional detector, and the voltage is used as a residual component. A plot of the slope and the residual component Δes as shown in FIG. 5 is created.
FIG. 6 is a graph obtained by rearranging and plotting FIG. 4 and FIG. 5 with the same gap and inclination and the eddy current component voltage es by the residual component. As can be seen from this figure, the residual component for each gap is proportional to the eddy current component voltage and can be linearly approximated for each gap, and it is clear that the slope varies depending on the gap.
FIG. 7 is a plot of the slope for each gap (corresponding to the residual rate α). From this plot, it can be seen that the residual rate α is expressed by a quadratic approximate expression of the gap, and α can be determined regardless of the inclination of the detector head 15 according to the installation position of the detector head 15 and the accuracy can be improved. Can do. That is, α is a value obtained as a function of the prediction gap 20A obtained in advance from the distance between the molten metal surface 18 of the conductive fluid 30 and the detection coil 6.
[0010]
【Example】
The flow velocity detector head 15 was placed in a non-contact manner with respect to the molten metal surface (melting point = 70 ° C.) molten metal 100 ° C. 18 to be measured, and the flow velocity was measured. The hot water surface 18 is a free surface. Two alternating magnetic fields were applied to the exciting coil 4 from the low frequency oscillator 1 of 100 Hz and the high frequency oscillator 2 of 20 kHz. At this time, the electromotive voltage e from the detection coil 6 is discriminated into a high-frequency component signal and a low-frequency component signal according to the difference in frequency. The low frequency component signal is separated into the speed component voltage ev and the eddy current component voltage es by the phase rectifier circuits 9a and 9b, and output fluctuation due to a gap change by the gap signal obtained through the high frequency filter 7a and the rectifier circuit 8. The corrected speed component voltage ev and eddy current component voltage es obtained by correcting the gap voltage eo are output. That is, each of the gap correction circuits 10a and 10b obtains a gap from the conductive fluid 30 based on the value of the gap voltage eo detected by the detection coil 6 and obtained through the high frequency filter 7a. In order to correct the accompanying changes in the velocity component voltage ev and the eddy current component voltage es, the velocity component voltage ev and the eddy current component voltage es extracted by the phase rectifier circuits 9a and 9b are corrected. Further, the velocity component voltage ev is removed from the disturbance component due to the eddy current component based on the value of the eddy current component voltage es by the arithmetic circuit 16. In the arithmetic circuit 16, the net velocity component is obtained by subtracting the residual component Δes obtained from the eddy current component voltage es from the velocity component voltage evt after gap correction as shown in the equations (1) and (2). The voltage ev is output as a speed signal.
FIG. 9 (conventional method) shows the result of converting the velocity component voltage (evt) into the flow velocity when only the gap correction is performed, and FIG. 3 shows the result when the residual component is corrected by the eddy current component. Method). In the figure, the measured value of the immersion type anemometer (simultaneously indicated by a dotted line) is also shown as a reference. As shown in FIGS. 9 and 3, it is apparent that the accuracy of the non-contact velocimeter is remarkably improved by correcting the residual component. It should be noted that the contents of the signal are represented by equations in each part of FIG.
[0011]
【The invention's effect】
Since the non-contact flow velocity detection method and apparatus according to the present invention are configured as described above, the following effects can be obtained. That is, the eddy current component voltage (es) in the electromotive voltage (e) is removed by phase rectification, the gap voltage (eo) is removed by rectification of the high-frequency magnetic field, and the error (Δes) is Δes = By using α · es and removing α using a value obtained as a function of the prediction gap (20A), a highly accurate flow velocity (V) can be obtained.
[Brief description of the drawings]
FIG. 1 is a configuration diagram showing an apparatus to which a non-contact detection method according to the present invention is applied.
FIG. 2 is an explanatory diagram showing the operation of FIG. 1;
FIG. 3 is a flow velocity / time characteristic diagram according to the method of FIG. 1;
FIG. 4 is an eddy current voltage component detection characteristic diagram according to the present invention.
FIG. 5 is an influence characteristic diagram of the inclination between the flow velocity detector head and the molten metal surface according to the present invention.
FIG. 6 is a relationship characteristic diagram between an eddy current component voltage and a residual component according to the present invention.
FIG. 7 is a relationship characteristic diagram between a residual rate and a prediction gap according to the present invention.
FIG. 8 is a configuration diagram showing an apparatus to which a conventional method is applied.
FIG. 9 is a flow velocity / time characteristic diagram of the conventional method of FIG.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Low frequency oscillator 2 High frequency oscillator 3 Amplifier 4 Excitation coil 5 Core 6 Detection coil 7a High frequency filter 7b Low frequency filter 8 Rectifier circuit 9a, 9b Phase rectifier circuit 10a, 10b Gap correction circuit 30 Conductive fluid φo Excitation magnetic flux φs Eddy current magnetic flux φv velocity component magnetic flux 15 flow velocity detector head 16 arithmetic circuit 18 molten metal surface 20 gap 20A prediction gap 21 flow of molten metal

Claims (3)

測定対象である導電性流体に対して、非接触に配置したコア(5)の励磁コイル(4)に低周波発振器(1)と高周波発振器(2)からの2つの交流電流が印加されることで生じた低周波磁場と高周波磁場が導電性流体(30)に入射することにより、前記励磁コイル(4)で発生した低周波磁場を妨げる方向に生じた磁束が鎖交することにより発生する渦電流成分電圧(es)と、前記励磁コイル(4)からの低周波磁場と測定対象である導電性流体(30)が相対移動することにより生じた速度成分電圧(ev)とを検出するための検知コイル(6)を有する流速検出器ヘッド(15)を用いて前記導電性流体(30)の流速(V)を得るようにした非接触流速検出方法において、前記検知コイル(6)により起電圧e(速度成分電圧ev+渦電流成分電圧es+ギャップ分電圧eo+誤差分△esよりなる)を測定し、前記起電圧(e)のうち、渦電流成分電圧(es)は位相整流により分離されて出力され、ギャップ分電圧(eo)は高周波磁界の整流で除去し、前記渦電流成分電圧(es)のうちの前記誤差分(△es)を、△es=α・esと定め、前記αは前記導電性流体(30)の湯面(18)と前記検知コイル(6)間のギャップ(20)を予め得た予知ギャップ(20A)の関数として求めた値を用い、除去することにより、前記導電性流体(30)の前記流速(V)を得ることを特徴とする非接触流速検出方法。Two alternating currents from the low-frequency oscillator (1) and the high-frequency oscillator (2) are applied to the exciting coil (4) of the core (5) placed in non-contact with the conductive fluid to be measured. The low-frequency magnetic field and the high-frequency magnetic field generated in step 1 are incident on the conductive fluid (30), and the vortex generated by the linkage of the magnetic flux generated in the direction that interferes with the low-frequency magnetic field generated in the excitation coil (4). Current component voltage (es) and velocity component voltage (ev) generated by relative movement of the low-frequency magnetic field from the excitation coil (4) and the conductive fluid (30) to be measured are detected. In the non-contact flow velocity detection method in which the flow velocity (V) of the conductive fluid (30) is obtained using a flow velocity detector head (15) having a detection coil (6), an electromotive voltage is generated by the detection coil (6). e (consisting of velocity component voltage ev + eddy current component voltage es + gap voltage eo + error Δes) Constant and, among the induced voltage (e), an eddy current component voltage (es) is outputted are separated Ri by the phase commutation gap portion voltage (eo) is removed in the rectification of the high frequency magnetic field, the eddy current components The error (Δes) of the voltage (es) is defined as Δes = α · es, where α is between the molten metal surface (18) of the conductive fluid (30) and the detection coil (6). Non-contact flow velocity characterized in that the flow velocity (V) of the conductive fluid (30) is obtained by removing the gap (20) using a value obtained as a function of the prediction gap (20A) obtained in advance. Detection method. 前記予知ギャップ(20A)は、前記導電性流体(30)が静止している状態で測定することを特徴とする請求項1記載の非接触流速検出方法。  The non-contact flow velocity detection method according to claim 1, wherein the prediction gap (20A) is measured in a state where the conductive fluid (30) is stationary. 測定対象である導電性流体(30)に対して、非接触に配置したコア(5)の励磁コイル(4)に低周波発振器(1)と高周波発振器(2)からの2つの交流電流が印加されることで生じた低周波磁場と高周波磁場が導電性流体(30)に入射することにより、前記励磁コイル(4)で発生した低周波磁場を妨げる方向に生じた磁束が鎖交することにより発生する渦電流成分電圧(es)と、前記励磁コイル(4)からの低周波磁場と測定対象である導電性流体(30)が相対移動することにより生じた速度成分電圧(ev)とを検出するための検知コイル(6)を有する流速検出器ヘッド(15)を用いて前記導電性流体(30)の流速(V)を得るようにした非接触流速検出装置において、前記検知コイル(6)からの検知電圧に対して低周波フィルタ(7b)を経た後に位相整流を行うことにより渦電流成分電圧と速度成分電圧とを分離するための位相整流回路(9a,9b)と、前記検知コイル(6)で検知され高周波フィルタ(7a)を介して得られたギャップ分電圧(eo)の値を基に導電性流体(30)とのギャップを求め、このギャップ変化に伴う速度成分電圧(ev)及び渦電流成分電圧(es)の変化を補正するため、前記位相整流回路(9a,9b)で取り出した速度成分電圧(ev)と渦電流成分電圧(es)を補正するためのギャップ補正回路(10a,10b)と、前記ギャップ補正回路(10a,10b)に接続された演算回路(16)とを備え、前記ギャップ補正回路(10a,10b)を介して出力された速度成分電圧(ev)から渦電流成分電圧(es)の誤差分△esを、△es=α・esと定め、前記αは前記導電性流体(30)の湯面(18)と前記検知コイル(6)間の間隔を予め得た予知ギャップ(20A)の関数として求めた値を用いて除去し、前記演算回路(16)から前記導電性流体(30)の流速(V)を得るように構成したことを特徴とする非接触流速検出装置。Two AC currents from the low-frequency oscillator (1) and high-frequency oscillator (2) are applied to the exciting coil (4) of the core (5) arranged in a non-contact manner with respect to the conductive fluid (30) to be measured. The low-frequency magnetic field and the high-frequency magnetic field generated as a result of being incident on the conductive fluid (30), the magnetic flux generated in the direction that interferes with the low-frequency magnetic field generated in the excitation coil (4) is interlinked. Detects the eddy current component voltage (es) generated and the velocity component voltage (ev) generated by the relative movement of the low-frequency magnetic field from the excitation coil (4) and the conductive fluid (30) to be measured. In the non-contact flow velocity detection device that obtains the flow velocity (V) of the conductive fluid (30) using the flow velocity detector head (15) having the detection coil (6) for the detection coil (6) The eddy current component voltage and velocity are generated by phase rectification after passing through the low-frequency filter (7b) for the detected voltage from The phase rectifier circuit (9a, 9b) for separating the voltage and the conductivity based on the value of the gap voltage (eo) detected by the detection coil (6) and obtained through the high frequency filter (7a) The velocity component extracted by the phase rectifier circuit (9a, 9b) in order to obtain the gap with the fluid (30) and correct the change in the velocity component voltage (ev) and the eddy current component voltage (es) due to the gap change. A gap correction circuit (10a, 10b) for correcting the voltage (ev) and the eddy current component voltage (es), and an arithmetic circuit (16) connected to the gap correction circuit (10a, 10b), gap correction circuit (10a, 10b) the error of △ es of velocity component voltage output through the (ev) from the eddy current component voltage (es), defined as △ es = α · es, the alpha is the conductivity The distance between the hot water surface (18) of the ionic fluid (30) and the detection coil (6) is removed using a value obtained as a function of the prediction gap (20A) obtained in advance, from the arithmetic circuit (16). A non-contact flow velocity detection device configured to obtain a flow velocity (V) of the conductive fluid (30).
JP34141698A 1998-12-01 1998-12-01 Non-contact flow velocity detection method and apparatus Expired - Lifetime JP4456682B2 (en)

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