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JPH0379658B2 - - Google Patents
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JPH0379658B2 - - Google Patents

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Publication number
JPH0379658B2
JPH0379658B2 JP57119561A JP11956182A JPH0379658B2 JP H0379658 B2 JPH0379658 B2 JP H0379658B2 JP 57119561 A JP57119561 A JP 57119561A JP 11956182 A JP11956182 A JP 11956182A JP H0379658 B2 JPH0379658 B2 JP H0379658B2
Authority
JP
Japan
Prior art keywords
signal
transfer function
excitation
vibration
excitation force
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 - Lifetime
Application number
JP57119561A
Other languages
Japanese (ja)
Other versions
JPS5910821A (en
Inventor
Akitaka Ikeuchi
Masaaki Shirai
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.)
JFE Engineering Corp
Original Assignee
Nippon Kokan Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nippon Kokan Ltd filed Critical Nippon Kokan Ltd
Priority to JP57119561A priority Critical patent/JPS5910821A/en
Publication of JPS5910821A publication Critical patent/JPS5910821A/en
Publication of JPH0379658B2 publication Critical patent/JPH0379658B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H15/00Measuring mechanical or acoustic impedance

Landscapes

  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Description

【発明の詳細な説明】 本発明は、構造物の伝達関数を測定する伝達関
数測定方法の改良に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement in a transfer function measuring method for measuring a transfer function of a structure.

構造物の伝達関数は、構造物に加振力を与えた
後、そのときの加振力信号と応答信号とを同時に
測定すれば、これら両信号から計算によつて求め
ることができる。
The transfer function of a structure can be determined by calculation from the excitation force signal and response signal, which are simultaneously measured after applying an excitation force to the structure.

構造物に対して加振力を与える加振法には、専
ら、正弦波掃引加振法、ランダム加振法、
インパルス加振法等が用いられている。
Excitation methods that apply excitation force to structures include sine wave sweep excitation method, random excitation method,
Impulse vibration method etc. are used.

以下、これらの加振法について述べる。先ず、
正弦波掃引加振法は、第1図に示すように正弦
波信号Sを供給して動電型加振機、油圧加振機、
不平衡重錘型起振機等1(以下、単に加振機と略
称する)を駆動することにより、該加振機1によ
つて構造物2に加振力を与える。そして、このと
き構造物2に接する加速度計3から得られる応答
信号である加速度信号4とロードセル5によつて
検出された加振力信号6とを機械インピーダンス
測定装置7に取り込み、ここで、そのときの周波
数における伝達関数8を求める方法である。
These vibration methods will be described below. First of all,
In the sine wave sweep excitation method, as shown in Fig. 1, a sine wave signal S is supplied to an electrodynamic vibrator, a hydraulic vibrator,
By driving an unbalanced weight type vibration exciter 1 (hereinafter simply referred to as a vibration exciter), an excitation force is applied to the structure 2 by the vibration exciter 1. At this time, the acceleration signal 4, which is a response signal obtained from the accelerometer 3 in contact with the structure 2, and the excitation force signal 6 detected by the load cell 5 are taken into the mechanical impedance measuring device 7, where the This is a method of finding the transfer function 8 at the frequency of .

なお、正弦波信号Sを連続的に変化させれば、
伝達関数8の周波数応答が一般にはボード線図の
形で得られる。
In addition, if the sine wave signal S is continuously changed,
The frequency response of the transfer function 8 is generally obtained in the form of a Bode plot.

次に、ランダム加振法は、第2図に示すよう
に正弦波信号Sの代りに周波数帯域の充分に広い
ランダム波信号RSを用いて加振機1を駆動し、
構造物2に加振力を与える。そして、同様に加速
度信号4と加振力信号6とを取り込んでフーリエ
変換装置9でフーリエ変換等の処理を行なつて伝
達関数8を求める方法である。
Next, in the random vibration method, as shown in FIG. 2, the vibration exciter 1 is driven using a random wave signal RS with a sufficiently wide frequency band instead of the sine wave signal S.
Apply an excitation force to the structure 2. Similarly, the acceleration signal 4 and the excitation force signal 6 are taken in, and a Fourier transform device 9 performs processing such as Fourier transform to obtain the transfer function 8.

さらに、インパルス加振法は、第3図に示す
ようにハンマ等10を用いて構造物2を打撃し、
このときの加速度信号4および加振力信号6とか
らフーリエ変換等の処理によつて伝達関数8を求
める方法である。この方法は、ハンマ等10で構
造物2を打撃した時、そのインパルス状の打撃力
が広い周波数成分をもつていることを利用したも
のである。
Furthermore, in the impulse vibration method, as shown in FIG. 3, the structure 2 is hit with a hammer or the like 10,
This is a method of determining the transfer function 8 from the acceleration signal 4 and the excitation force signal 6 at this time through processing such as Fourier transformation. This method utilizes the fact that when the structure 2 is struck with a hammer or the like 10, the impulse-like striking force has a wide frequency component.

しかして、以上述べた3つの方法のうち、の
方法の場合には加振機1が不要であり、しかも短
時間で伝達関数8を計測できる利点をもつている
が、大きな加振力を得ることができない。このた
め、橋梁や高層建築物のように大型構造物2の場
合には利用できない。従つて、かかる構造物2の
場合には、回転不平衡重錘型起振機などの大型加
振機1を用いて伝達関数8を計測するのが通例と
なつているが、計測準備や測定に要する時間が長
くならざるを得ない。
Of the three methods described above, method 1 does not require the vibrator 1 and has the advantage of being able to measure the transfer function 8 in a short time, but it requires a large excitation force. I can't. Therefore, it cannot be used for large structures 2 such as bridges and high-rise buildings. Therefore, in the case of such a structure 2, it is customary to measure the transfer function 8 using a large-sized exciter 1 such as a rotating unbalanced weight type exciter. The time it takes to do so has to become longer.

ところで、大型構造物2における振動実験方法
には自由振動実験があり、引き網法、ロケツト法
など多くの種類の手法がある。これらの手法は、
ワイヤとウインチあるいはロケツトの推進力など
を利用して初期変位を与え、この変位を解放した
時の自由振動から振動特性を求めるものであり、
加振力の性質からステツプ加振とも呼ばれ、構造
物2の固有振動数、減衰係数が求められる。
By the way, there is a free vibration experiment as a vibration experiment method for the large structure 2, and there are many types of methods such as a seine method and a rocket method. These methods are
It uses a wire and the propulsion force of a winch or a rocket to apply an initial displacement, and when this displacement is released, the vibration characteristics are determined from the free vibration.
It is also called step vibration due to the nature of the excitation force, and the natural frequency and damping coefficient of the structure 2 are determined.

すなわち、かかる従来のステツプ加振による方
法は、後述する第6図と同様にロードセル11を
用いて加振力を測定することによつて行つてい
る。但し、このロードセルによる測定値には打ち
切り誤差が発生するために、伝達関数の計算には
使用できず、単に参考データとして用いるにすぎ
ない。ゆえに、従来の振動試験では、伝達関数を
求めることはせず、単に構造物の自由振動、つま
り変位、速度、加速度の何れか1つの波形を観祭
し、その周期から固有振動数を算出したり、或い
は自由振動波形のパワースペクトルを計算し固有
振動数を求める方法をとつている。
That is, the conventional step vibration method is carried out by measuring the vibration force using a load cell 11 as shown in FIG. 6, which will be described later. However, since a truncation error occurs in the measured value by this load cell, it cannot be used for calculating the transfer function, and is merely used as reference data. Therefore, in conventional vibration testing, the transfer function is not determined, but the free vibration of the structure, that is, the waveform of one of displacement, velocity, and acceleration, is observed and the natural frequency is calculated from the period. Alternatively, the natural frequency is determined by calculating the power spectrum of the free vibration waveform.

従つて、この方法は、前述のインパルス加振法
と同様に、加振機2が不要であり、短時間で計測
できる利点を有し、しかも容易に大きな加振力を
得ることができるが、正確に伝達関数8を求める
ことはできない。その理由は、以下の通りであ
る。先ず、参考のために、第4図に本来のステツ
プ関数とそのフーリエスペクトルを示す。第4図
aはステツプ関数の時間波形を示し、同図b,c
はそのフーリエスペクトルのそれぞれ振巾および
位相を示す図である。さて、実際の加振力は第5
図aに示すように近似的にはステツプ関数となつ
ている。ところが、これをそのまま有限フーリエ
変換しても打ち切り誤差が生じて正しい演算を行
うことができない。
Therefore, like the above-mentioned impulse excitation method, this method does not require the vibrator 2, has the advantage of being able to measure in a short time, and can easily obtain a large excitation force; It is not possible to accurately determine the transfer function 8. The reason is as follows. First, for reference, FIG. 4 shows the original step function and its Fourier spectrum. Figure 4a shows the time waveform of the step function, and Figure 4b and c
are diagrams showing the amplitude and phase of the Fourier spectrum, respectively. Now, the actual excitation force is the fifth
As shown in Figure a, it is approximately a step function. However, even if this is directly subjected to finite Fourier transformation, a truncation error will occur, making it impossible to perform correct calculations.

この打ち切り誤差は、有限長さの信号をフーリ
エ変換する際に発生するものであつて、次のよう
に定義できる。有限長さの信号をフーリエ変換す
る際には、その信号が無限に繰り返されていると
解釈されます。このことは、信号が終わつたとこ
ろから、再び同じ信号が連続して始まつていると
見なされます。しかし、一般的には信号の終わり
の部分と始まりの部分とは滑らかな状態で連続し
ていません。そのために、信号に不連続点が生
じ、フーリエスペクトルに乱れが発生します。こ
れが打ち切り誤差であります。
This truncation error occurs when a finite length signal is Fourier transformed, and can be defined as follows. When a signal of finite length is Fourier transformed, the signal is interpreted as repeating itself infinitely. This is considered to be the same continuous signal starting again from where the signal ended. However, in general, the end and beginning parts of a signal are not smoothly continuous. This results in discontinuities in the signal and disturbances in the Fourier spectrum. This is the truncation error.

よつて、以上のように打ち切り誤差が発生した
ときには、第4図bに示すようにならずに第5図
bのようになつてしまう。このため、この加振力
を実際に1自由度系(固有振動数:約20Hz)に与
えた時の応答を測定し、それらから伝達関数8を
求めると、第5図cのように本来共振点(山)が
1つであるにも拘らず疑似的な共振点が1つ多く
現れ、しかも共振点に無関係に位相が変動してい
るとから、非常に誤差の大きなものになつてしま
う。
Therefore, when a truncation error occurs as described above, the result will not be as shown in FIG. 4b but as shown in FIG. 5b. Therefore, when this excitation force is actually applied to a one-degree-of-freedom system (natural frequency: approximately 20Hz), the response is measured and the transfer function 8 is determined from them. Although there is only one point (mountain), one more pseudo resonance point appears, and the phase fluctuates regardless of the resonance point, resulting in a very large error.

本発明は上記実情にかんがみてなされたもの
で、簡便な加振法であるステツプ加振法を用いる
とともに、この加振法によつて得られた信号をフ
イルタを通すことによりインパルス応答に近似さ
せた正しい伝達関数を求めることができる構造物
の伝達関数測定方法を提供することを目的とす
る。
The present invention was made in view of the above circumstances, and uses a step excitation method, which is a simple excitation method, and approximates an impulse response by passing the signal obtained by this excitation method through a filter. The purpose of the present invention is to provide a method for measuring the transfer function of a structure by which a correct transfer function can be determined.

以下、本発明方法の実施例を説明する前に、先
ず、従来のステツプ加振法によつて伝達関数を正
確に求められなかつた理由を述べる。従来のステ
ツプ加振法では、ステツプ状の加振力信号をサン
プリングしてデイジタル量に変換し、このデイジ
タル信号にフーリエ変換を施すものであるが、こ
のフーリエ変換を施す際にデータ長が有限である
ことから打ち切り誤差が生ずるためである。即
ち、第5図aにおいて時間零では信号の大きさは
零であるが、データ長の最後(第5図aの時間
2)には信号の大きさが1となる。このため、有
限フーリエ変換を実行すると、データが不連続と
なり、打ち切り誤差が発生する。
Before explaining the embodiments of the method of the present invention, the reason why the transfer function could not be accurately determined by the conventional step excitation method will be explained below. In the conventional step excitation method, a step-like excitation force signal is sampled and converted into a digital quantity, and this digital signal is subjected to Fourier transformation. This is because a truncation error occurs due to certain reasons. That is, the magnitude of the signal is zero at time zero in FIG. 5a, but the magnitude of the signal becomes 1 at the end of the data length (time 2 in FIG. 5a). Therefore, when the finite Fourier transform is performed, the data becomes discontinuous and a truncation error occurs.

そこで、本発明方法は打ち切り誤差を除去して
簡便なステツプ加振法により伝達関数を測定する
ものであり、第6図はその一実施例を示す図であ
る。このステツプ加振法は、ロードセル11を介
して構造物12に引張力Fを加えて構造物12に
初期変位を与えた後、ロードセル11と構造物1
2とを切り離すことにより構造物12にステツプ
状変位を与え、このときの加速度および加振力を
構造物12に接する加速度計13とロードセル1
1を用いて検出する。そして、加速度計13で検
出した加速度信号14とロードセル11で検出し
た加振力信号15とをそれぞれ適宜な遮断周波数
特性を有するハイ・パスフイルタ16,17を通
過させて低周波信号成分をカツトする。しかる
後、両フイルタ16,17の出力をフーリエ変換
装置18によりフーリエ変換等の処理を行なえ
ば、正確に伝達関数19を求めることができる。
Therefore, the method of the present invention removes the truncation error and measures the transfer function by a simple step excitation method, and FIG. 6 is a diagram showing one embodiment thereof. In this step vibration method, a tensile force F is applied to the structure 12 via the load cell 11 to give an initial displacement to the structure 12, and then the load cell 11 and the structure 1 are
By separating the structure 12 from the structure 12, a step-like displacement is applied to the structure 12, and the acceleration and excitation force at this time are transferred to the accelerometer 13 and the load cell 1 that are in contact with the structure 12.
Detect using 1. Then, the acceleration signal 14 detected by the accelerometer 13 and the excitation force signal 15 detected by the load cell 11 are passed through high pass filters 16 and 17 having appropriate cutoff frequency characteristics, respectively, to cut out low frequency signal components. Thereafter, if the outputs of both filters 16 and 17 are subjected to processing such as Fourier transform using the Fourier transform device 18, the transfer function 19 can be accurately determined.

この理由は以下の通りである。即ち、従来のス
テツプ加振では、第4図aのように信号の始まり
は0ですが、終わりは0でない。このため、この
信号を繰り返すと不連続点が生じ、打ち切り誤差
の原因となります。ところが、第6図のようにハ
イパスフイルタ16,17を設ければ、加振力は
第7図aに示すように変換され、信号の始まりと
終わりがともに0になりますので、これを繰り返
し並べたとしても、その接続点には不連続は生じ
ません、従つて、伝達関数が正確に求められる。
The reason for this is as follows. That is, in conventional step vibration, the signal starts at 0, but the end is not 0, as shown in FIG. 4a. Therefore, repeating this signal creates discontinuities that cause truncation errors. However, if high-pass filters 16 and 17 are provided as shown in Figure 6, the excitation force will be converted as shown in Figure 7a, and both the beginning and end of the signal will be 0, so this can be repeated and arranged. Even if there is no discontinuity at the connection point, the transfer function can be determined accurately.

つまり、第5図aの信号をハイ・パスフイルタ
16,17を通過させれば、第7図aに示すよう
にステツプ状の信号ではなく、時間零のときと時
間2のときにそれぞれ振巾の等しい信号を得るこ
とができ、このような信号を有限フーリエ変換を
行なつても打ち切り誤差が生ずることがなく、第
7図bに示すように正しい結果が得られる。従つ
て、第6図の構成にて構造物12の伝達関数を計
測すれば、第7図cのような結果が得られインパ
ルス加振法による測定結果(第7図d参照)とほ
ぼ等しい値が得られる。すなわち、第7図dは従
来から十分に信頼性が保証されているインパルス
加振法による測定結果であり、これに対して第7
図cは共振点が1つだけ現れ、かつ、その共振点
では位相が180゜から−180゜に向けて1回だけ変動
し、第7図dとほぼ同様な測定結果を得ることが
できる。
In other words, if the signal in FIG. 5a is passed through the high pass filters 16 and 17, it will not be a step-like signal as shown in FIG. Equal signals can be obtained, and even when such signals are subjected to finite Fourier transformation, no truncation error occurs, and correct results are obtained as shown in FIG. 7b. Therefore, if the transfer function of the structure 12 is measured with the configuration shown in FIG. 6, the result shown in FIG. is obtained. In other words, Fig. 7d shows the measurement results using the impulse excitation method, which has been sufficiently reliable in the past;
In Fig. 7(c), only one resonance point appears, and at that resonance point, the phase changes only once from 180° to -180°, and almost the same measurement results as in Fig. 7(d) can be obtained.

以上詳記したように本発明によれば、ステツプ
加振法で得られた信号をハイ・パスフイルタを通
過させた後フーリエ変換等の処理を施すことによ
り、打ち切り誤差の影響を受けない正確な伝達関
数を求めることができ、また大型構造物であつて
も比較的簡易なステツプ加振法を用いて伝達関数
を測定できる構造物の伝達関数測定方法を提供で
きる。
As detailed above, according to the present invention, the signal obtained by the step excitation method is passed through a high-pass filter and then subjected to processing such as Fourier transformation, thereby achieving accurate transmission that is not affected by truncation errors. It is possible to provide a method for measuring a transfer function of a structure, which can obtain a function, and can also measure a transfer function of a large structure using a relatively simple step excitation method.

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

第1図ないし第3図はそれぞれ従来の異なる加
振法を説明する構成図、第4図a〜cは本来のス
テツプ関数およびそのフーリエスペクトルを説明
する図、第5図a〜cは従来の加振法を実際に適
用して得られたステツプ関数、フーリエスペクト
ルおよび伝達関数特性図、第6図は本発明方法の
一実施例を説明する構成図、第7図a〜cは本方
法によつて得られた特性図、第7図dはインパル
ス加振法によつて得られた伝達関数特性図であ
る。 11……ロードセル、12……構造物、13…
…加速度計、16,17……ハイ・パスフイル
タ、18……フーリエ変換装置、19……伝達関
数。
Figures 1 to 3 are block diagrams explaining different conventional excitation methods, Figures 4 a to c are diagrams explaining the original step function and its Fourier spectrum, and Figures 5 a to c are diagrams explaining conventional excitation methods. The step function, Fourier spectrum, and transfer function characteristic diagram obtained by actually applying the excitation method. Figure 6 is a block diagram explaining one embodiment of the method of the present invention. Figures 7 a to c are diagrams of the method according to the present invention. The characteristic diagram thus obtained, FIG. 7d, is a transfer function characteristic diagram obtained by the impulse excitation method. 11...Load cell, 12...Structure, 13...
... accelerometer, 16, 17 ... high pass filter, 18 ... Fourier transform device, 19 ... transfer function.

Claims (1)

【特許請求の範囲】[Claims] 1 ロードセルを介して構造物にステツプ状変位
を与え、このとき前記構造物から得られる加速度
信号を前記構造物に取り付けた加速度計で検出
し、また前記構造物に作用する加振力信号をロー
ドセルによつて検出した後、これら加速度信号お
よび加振力信号をそれぞれハイ・パスフイルタを
通過させ、これら両ハイ・パスフイルタから出力
された両信号をフーリエ変換して伝達関数を求め
ることを特徴とする構造物の伝達関数測定方法。
1 A step-like displacement is applied to a structure via a load cell, an acceleration signal obtained from the structure is detected by an accelerometer attached to the structure, and an excitation force signal acting on the structure is detected by the load cell. A structure characterized in that the acceleration signal and the excitation force signal are passed through a high-pass filter, and the transfer function is obtained by Fourier-transforming both signals output from the high-pass filters. A method for measuring the transfer function of objects.
JP57119561A 1982-07-09 1982-07-09 Transfer function measurement method for structures Granted JPS5910821A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57119561A JPS5910821A (en) 1982-07-09 1982-07-09 Transfer function measurement method for structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57119561A JPS5910821A (en) 1982-07-09 1982-07-09 Transfer function measurement method for structures

Publications (2)

Publication Number Publication Date
JPS5910821A JPS5910821A (en) 1984-01-20
JPH0379658B2 true JPH0379658B2 (en) 1991-12-19

Family

ID=14764367

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57119561A Granted JPS5910821A (en) 1982-07-09 1982-07-09 Transfer function measurement method for structures

Country Status (1)

Country Link
JP (1) JPS5910821A (en)

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JPS6415082A (en) * 1986-11-14 1989-01-19 Sigma Shoji Kk Roulette play apparatus
JP3398582B2 (en) * 1997-10-08 2003-04-21 富士通株式会社 Vibration analysis method and analyzer for disk device housing
JP2011240045A (en) * 2010-05-20 2011-12-01 Juno Gaming Co Ltd Game device

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