JPS62267643A - Fatigue testing machine - Google Patents

Fatigue testing machine

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Publication number
JPS62267643A
JPS62267643A JP11083586A JP11083586A JPS62267643A JP S62267643 A JPS62267643 A JP S62267643A JP 11083586 A JP11083586 A JP 11083586A JP 11083586 A JP11083586 A JP 11083586A JP S62267643 A JPS62267643 A JP S62267643A
Authority
JP
Japan
Prior art keywords
signal
load
reference signal
test piece
error signal
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.)
Pending
Application number
JP11083586A
Other languages
Japanese (ja)
Inventor
Michio Kumazawa
熊沢 道夫
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP11083586A priority Critical patent/JPS62267643A/en
Publication of JPS62267643A publication Critical patent/JPS62267643A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To control so as to keep a load for working on a test piece constant, by supplying an error signal corresponding to the difference of a load signal for working the test piece and a reference signal, and an instruction signal corresponding to the sum of said error signal and the reference signal, to a servo-valve. CONSTITUTION:When a test piece 1 is attached between a load cell 2 and a frame 7, and a reference signal 16 corresponding to a test load condition being a target is generated by a reference signal generator 15, a fatigue testing machine starts to operate. An arithmetic unit 19 outputs the reference signal 16 as an instruction signal 20 to a servo-valve 9. As a result, a load works on the test piece 1 and a load signal 5 is transmitted to an error signal generator 17. In such a state, a difference between the reference signal 16 and the load signal 5 is calculated, an error signal 18 corresponding to this difference is transmitted to the arithmetic unit 19, and the arithmetic unit 19 stores this error signal 18. Subsequently, an instruction signal corresponding to the sum of the error signal and the reference signal is generated, and by this instruction signal, the servo-valve is operated.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は疲労試験機に関するものである。[Detailed description of the invention] [Industrial application field] This invention relates to a fatigue testing machine.

〔従来の技術〕[Conventional technology]

第4図は、例えば、エムティニスジャパン株式会社のカ
タログに示された従来の疲労試験機を一部ブロック図で
示す構成図である。図において。
FIG. 4 is a partial block diagram of a conventional fatigue testing machine shown in a catalog of Mtinis Japan Co., Ltd., for example. In fig.

(りは試験の対象物である試験片、(2)は試験片(1
)に作用する荷重を電気的に検出するロードセル、(3
)はロードセル出力、(4)はロードセル出力を増幅す
る増幅器、(5)は増幅された荷重信号、(6)は荷重
指示計、(7)は試験片(1)とロードセル(2)を取
り付けて保持するフレーム、(8)はフレーム(7)に
固定されて試験片(りに荷重を与える油圧アクチュエー
タ、(9)は油圧アクチュエータ(8)の動作を制御す
るサーボ弁、 (10)は油圧アクチュエータ(8)を
動作させるための油圧発生装置、(11)は試験片(1
)に付加する荷重の大きさ、波形の形などを設定する後
述の命令信号を発生するファンクションゼネレータ、(
12)は上述の命令信号、(13)は命令信号(12)
と荷重信号(5)を比較すると共に命令信号(12)ど
うりの荷重が試験片(1)に付加されるようにサーボ弁
(9)に後述の信号を与えるコントローラ、(1りはコ
ントローラ出力であるサーボ弁動作信号である。
(ri is the test piece which is the object of the test, (2) is the test piece (1
), a load cell that electrically detects the load acting on (3).
) is the load cell output, (4) is the amplifier that amplifies the load cell output, (5) is the amplified load signal, (6) is the load indicator, and (7) is the test piece (1) and load cell (2) attached. (8) is a hydraulic actuator that is fixed to the frame (7) and applies a load to the test piece, (9) is a servo valve that controls the operation of the hydraulic actuator (8), (10) is a hydraulic Hydraulic pressure generator (11) for operating the actuator (8) is the test piece (1
), a function generator that generates a command signal (described later) that sets the size of the load to be applied, the shape of the waveform, etc.;
12) is the above command signal, (13) is the command signal (12)
A controller that compares the load signal (5) with the command signal (12) and provides the signal described below to the servo valve (9) so that the load corresponding to the command signal (12) is applied to the test piece (1). is the servo valve operation signal.

従来の疲労試験機は上述したように構成されており、試
験片(1)がロードセル(2)とフレーム(7)の間に
取り付けられて、ファンクションゼネレータ(11)を
動作させると、予め設定された一定振幅、一定肩波数の
命令信号(12)が発生し、この命令信号(12) j
こ対応する荷重となるようコントローラ(13)はサー
ボ弁(9)に対してサーボ弁動作信号(1りを送り、サ
ーボ弁(9)はこれを受けてこのサーボ弁動作信号(1
4)に対応した油圧量を油圧アクチュエータ(8)に与
えるよう動作する。以下、命令信号(12)と荷重信号
(5)の差が最小になるようコントローラ(13)はサ
ーボ弁(9)に連続修正信号をサーボ弁動作信号として
与え続けて、荷重振幅一定の試験が行なわれる。
The conventional fatigue testing machine is configured as described above, and when the test piece (1) is attached between the load cell (2) and the frame (7) and the function generator (11) is operated, the preset A command signal (12) with a constant amplitude and a constant shoulder wave number is generated, and this command signal (12) j
The controller (13) sends a servo valve operation signal (1) to the servo valve (9) to achieve the corresponding load, and the servo valve (9) receives this and sends this servo valve operation signal (1).
The hydraulic actuator (8) operates to apply a hydraulic pressure amount corresponding to (4) to the hydraulic actuator (8). Thereafter, the controller (13) continues to give a continuous correction signal to the servo valve (9) as a servo valve operation signal so that the difference between the command signal (12) and the load signal (5) is minimized, and a test with a constant load amplitude is performed. It is done.

以上の制御系のブロック図は第5図のように示され、い
わゆるネガティブフィードバック方式の制御系である。
A block diagram of the above control system is shown in FIG. 5, and is a so-called negative feedback type control system.

また、この制御系の疲労試験機の性能曲線は1周知のよ
うに、油圧発生装置(1o)の容量が決まれば、第6図
のように一定の試験片変位と繰返し速度の関係として与
えられる。
In addition, as is well known, the performance curve of the fatigue testing machine for this control system is given as the relationship between constant specimen displacement and repetition rate, as shown in Figure 6, once the capacity of the hydraulic pressure generator (1o) is determined. .

〔発明が解決しよtとする問題点〕[Problems that the invention is intended to solve]

従来の疲労試験機では、一定繰返し速度での試験中暑こ
試験片(1)にき裂が生じて試験片(1)の剛性が低下
し、その変形量が大きくなって第6図に示す制御不安定
領域に入ると、試験片(りに作用する荷重が低下すると
いう問題点があり、また、低下した荷重を初期の目標値
に設定しようとすると、荷重波形が乱れて精度の良い疲
労試験が行なえないなどの問題点があり、更にこのよう
な場合に精度良く試験を行なおうとすれば、ファンクシ
ョンゼネレータ(11)を再調整して繰返し速度を小さ
くする。必要があり、結果的に試験効率が悪くなる問題
点があった。
In conventional fatigue testing machines, cracks occur in the heat test piece (1) during the test at a constant repetition rate, the rigidity of the test piece (1) decreases, and the amount of deformation increases, resulting in the control shown in Figure 6. When the test piece enters the unstable region, there is a problem that the load acting on the test piece decreases, and if you try to set the decreased load to the initial target value, the load waveform becomes distorted, making it difficult to perform accurate fatigue tests. In addition, if you want to perform a test with high accuracy in such a case, it is necessary to readjust the function generator (11) and reduce the repetition rate.As a result, the test There was a problem that the efficiency deteriorated.

この発明は、上述したような問題点を解決するためにな
されたもので、試験荷重条件に対応する命令信号を一度
設定すると、その後は試験片の剛性が試験中に変化して
も安定にかつ試験荷重値、荷重波形が変化することな(
、試験が可能な疲労試験機を得ることを目的にしている
This invention was made to solve the above-mentioned problems, and once the command signal corresponding to the test load condition is set, the stiffness of the test piece remains stable even if it changes during the test. The test load value and load waveform will not change (
The purpose is to obtain a fatigue testing machine that can perform , tests.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係る疲労試験機は、試験片に作用する荷重値
、荷重波形が、設定された試験条件と一致するように、
基準信号を発生する基準信号発生器と、試験片に作用す
る荷重に対応する荷重信号と基準信号の差に対応する誤
差信号を発生する誤差信号発生器と、基準信号と誤差信
号の和に対応する命令信号を発生する演算装置とを設け
たものである。
The fatigue testing machine according to the present invention is configured such that the load value and load waveform acting on the test piece match the set test conditions.
A reference signal generator that generates a reference signal, an error signal generator that generates an error signal that corresponds to the difference between the load signal that corresponds to the load acting on the test piece and the reference signal, and the sum of the reference signal and error signal. The system is equipped with an arithmetic unit that generates a command signal to perform the operation.

〔作 用〕[For production]

この発明では、上述した荷重信号と基準信号の差に対応
する誤差信号、およびこの誤差信号と基準信号の和に対
応する命令信号をサーボ弁へ供給することにより、試験
片に作用する荷重一定の制御が行われる。
In this invention, by supplying an error signal corresponding to the difference between the above-mentioned load signal and the reference signal and a command signal corresponding to the sum of this error signal and the reference signal to the servo valve, the load acting on the test piece is constant. Control takes place.

〔実施例〕〔Example〕

以下、この発明に係る疲労試験機の一実施例を図につい
て説明する。第1図はこの発明の一実施例を一部ブロッ
ク図で示す構成図であり、(1)〜(1G)は第4図に
示したものと全く同じである。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a fatigue testing machine according to the present invention will be described below with reference to the drawings. FIG. 1 is a block diagram partially showing an embodiment of the present invention, and (1) to (1G) are exactly the same as those shown in FIG.

(15)は設定された試験条件に対応する基準信号を発
生するための基準信号発生器% (16)はこの基準信
号発生器によって発生された基準信号、(17)は増幅
器(4)によって発生された荷重信号(5)と基準信号
(16)を比較すると共にこれらの差に対応する誤差信
号を発生するための誤差信号発生器、(1a)はこの誤
差信号発生器(17)によって発生された誤差信号s 
(19)は前述した基準信号(16)と誤差信号(18
)を加算すると共にこれらの和に対応する命令信号を発
生するための演算装置% (20)はこの演算装置(1
つによって発生された命令信号である。
(15) is a reference signal generator for generating a reference signal corresponding to the set test conditions. (16) is a reference signal generated by this reference signal generator, and (17) is a reference signal generated by amplifier (4). An error signal generator (1a) for comparing the loaded load signal (5) and the reference signal (16) and generating an error signal corresponding to the difference between them is generated by this error signal generator (17). error signal s
(19) is the reference signal (16) and error signal (18) mentioned above.
) and generates a command signal corresponding to the sum of these sums.
This is a command signal generated by one.

上述したよう化構成された疲労試験機において、試験片
(1)をロードセル(2)とフレーム(7)の間に取り
付けて目標とする試験荷重条件に対応する基準信号(1
6)を基準信号発生器(15)に発生させると、疲労試
験機が動作し始める。
In the fatigue testing machine configured as described above, the test piece (1) is attached between the load cell (2) and the frame (7), and the reference signal (1) corresponding to the target test load condition is applied.
6) is generated in the reference signal generator (15), the fatigue tester starts operating.

第1回目の負荷では、それ以前の荷重信号(5)が不明
であるため、演算装置(1つは基準信号(16)を命令
信号(20)としてサーボ弁(9)に出力する。この結
果、試験片(りには荷重が作用して荷重信号(5)が誤
差信号発生器(17)へ伝送される。なお、上述した試
験片(1)暑ζ作用する荷重は、負荷系の剛性や油圧源
の性能などにより、基準信号(16)どうりの波形や大
きさにはならず、試験条件どうりの荷重負荷は一般に行
なわれない。次に、誤差信号発生器(17)は、基準信
号(16)と上述した荷重信号(5)の差を計算し、こ
れ薯ζ対応する誤差信号(18)を演算装置(19)に
伝送し、演算装置はこの誤差信号(18)を記憶する。
In the first load, since the previous load signal (5) is unknown, the calculation device (one outputs the reference signal (16) as the command signal (20) to the servo valve (9). , a load acts on the test piece (ri), and a load signal (5) is transmitted to the error signal generator (17).The load applied to the test piece (1) mentioned above depends on the stiffness of the load system. The waveform and size of the standard signal (16) will not be the same depending on the performance of the hydraulic power source and the hydraulic power source, and the load will not be applied according to the test conditions.Next, the error signal generator (17) The difference between the reference signal (16) and the above-mentioned load signal (5) is calculated, and the corresponding error signal (18) is transmitted to the calculation device (19), which stores this error signal (18). do.

以上で第1回目の負荷過程が終る。This completes the first loading process.

第2回目の負荷では、演算装置(19)は記憶しておい
た第1回目の誤差信号(18)と基準信号(16)の和
を命令信号(20)としてサーボ弁(9)に伝送し、第
2回目の負荷が行なわれる。この場合、命令信号(20
)は、基準信号(16)と第1回目の負荷の誤差信号(
18)の和であるため、第1回目の負荷より基準信号(
16)に近づいた負荷が行なわれ、その荷重信号(5)
は第1回目の負荷と同様に誤差信号発生器(17)へ伝
送され、基準信号(16)との差が計算され、誤差信号
(18)として演算装置(19)へ伝送、記憶され、第
2回目の負荷過程が終る。以後、同様に負荷が繰返され
、制御系のゲインで決まる繰返し回数後、基準信号(1
6)どうりの負荷が実行される。
In the second load, the arithmetic unit (19) transmits the memorized sum of the first error signal (18) and the reference signal (16) to the servo valve (9) as a command signal (20). , a second load is performed. In this case, the command signal (20
) is the reference signal (16) and the first load error signal (
18), the reference signal (
16) is performed, and the load signal (5)
is transmitted to the error signal generator (17) in the same way as the first load, the difference with the reference signal (16) is calculated, and transmitted and stored as an error signal (18) to the arithmetic unit (19). The second loading process is completed. Thereafter, the load is repeated in the same way, and after the number of repetitions determined by the gain of the control system, the reference signal (1
6) Different loads are executed.

なお、従来の疲労試験機では、リアルタイムで連続的に
命令信号が修正されて荷重制御が行なわれるが、この発
明の疲労試験機では、1回の負荷重で命令信号(20)
の修正が行なわれる。第2図にこの発明による疲労試験
機の制御系のブロック図を示し、そして第3図に上述し
た各信号の対応関係を示す。例えば第3図(a)に示す
ような基準信号を疲労試験機に入力して第3図(1))
のような荷重信号が得られた場合1次の負荷に対する誤
差信号は第3図(C)、そして命令信号は第3図(d)
のように設定される。このように、基準信号と誤差信号
にもとづいた制御が行なわれるため、この発明による疲
労試験機では、第6図に示したような振幅−繰返し速度
特性に制限のない制御ができる。
In addition, in a conventional fatigue testing machine, load control is performed by continuously modifying the command signal in real time, but in the fatigue testing machine of the present invention, the command signal (20) is corrected in one load.
Corrections will be made. FIG. 2 shows a block diagram of the control system of the fatigue testing machine according to the present invention, and FIG. 3 shows the correspondence of the above-mentioned signals. For example, by inputting a reference signal as shown in Fig. 3(a) into a fatigue tester, Fig. 3(1))
When a load signal like this is obtained, the error signal for the primary load is shown in Figure 3 (C), and the command signal is shown in Figure 3 (d).
It is set as follows. As described above, since control is performed based on the reference signal and error signal, the fatigue tester according to the present invention can control the amplitude-repetition rate characteristic without restrictions as shown in FIG.

なお、上記実施例では、試験片薯ζ作用する荷重を一定
とする制御系について述べたが、試験片の変形量や油圧
アクチュエータの変位量を一定に制御する場合でも上記
と同様の効果がある。
In addition, in the above example, a control system was described in which the load acting on the test piece was kept constant, but the same effect as described above can be obtained even when the amount of deformation of the test piece or the amount of displacement of the hydraulic actuator is controlled to be constant. .

〔発明の効果〕〔Effect of the invention〕

以上のように、この発FJAζζよれば基準信号を発生
する基準信号発生器、基準信号と荷重信号の差iζ対応
する誤差信号を発生する誤差信号発生器。
As described above, according to this output FJAζζ, there is a reference signal generator that generates a reference signal, and an error signal generator that generates an error signal corresponding to the difference iζ between the reference signal and the load signal.

および誤差信号と基準信号の和に対応する命令信号を発
生し、この命令信号でサーボ弁を動作させる演算装置を
設けたので、試験片の剛性の変化が生じても、初期化設
定した荷重の大きさや波形が変化することなく、疲労試
験を実行することができ、非常に高精度で材料の疲労特
性を求めることができる効果がある。
Since we have installed a calculation device that generates a command signal corresponding to the sum of the error signal and the reference signal and operates the servo valve using this command signal, even if the stiffness of the test piece changes, the initialized load can be maintained It is possible to perform fatigue tests without changing the size or waveform, and has the effect of determining the fatigue properties of materials with extremely high accuracy.

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

第1図はこの発明の一実施例を一部ブロック図で示す構
成図、第2図はその制御系のブロック図。 第3図は第1図および第2図の各部に生じる信号の波形
図、第4図は従来の疲労試験機を一部ブロック図で示す
構成図、第5図はその制御系のブロック図、第6図は従
来の疲労試験機の性能曲線図である。 図において、(りは試験片、(2)はロードセル、(3
)はロードセル出力、(4)は増幅器、(5)は荷重信
号。 (6)は荷重指示計、(7)はフレーム、(8)は油圧
アクチュエータ、(9)はサーボ弁、 (10)は油圧
発生装置。 (11)はファンクションゼネレータ、 (12)は命
令信号、  (Ig)はコントローラ、(1りはサーボ
弁動作信号、(15)は基準信号発生器% (14)は
基準信号。 (17)は誤差信号発生器、(18)は誤差信号、(1
つは演算装置、(20)は命令信号である。 なお1図中、同一符号は同一、又は相当部分を示す。 第1図 不4図
FIG. 1 is a block diagram showing a partial block diagram of an embodiment of the present invention, and FIG. 2 is a block diagram of its control system. FIG. 3 is a waveform diagram of signals generated in each part of FIGS. 1 and 2, FIG. 4 is a block diagram showing a partial block diagram of a conventional fatigue testing machine, and FIG. 5 is a block diagram of its control system. FIG. 6 is a performance curve diagram of a conventional fatigue testing machine. In the figure, (ri is the test piece, (2) is the load cell, (3 is
) is the load cell output, (4) is the amplifier, and (5) is the load signal. (6) is a load indicator, (7) is a frame, (8) is a hydraulic actuator, (9) is a servo valve, and (10) is a hydraulic pressure generator. (11) is the function generator, (12) is the command signal, (Ig) is the controller, (1 is the servo valve operation signal, (15) is the reference signal generator% (14) is the reference signal. (17) is the error The signal generator, (18) is the error signal, (1
One is an arithmetic unit, and (20) is a command signal. In addition, in FIG. 1, the same reference numerals indicate the same or equivalent parts. Figure 1-4

Claims (1)

【特許請求の範囲】[Claims] 試験片に荷重を加えかつこの荷重に対応する荷重信号を
発生するための荷重付加・検出系と、設定された試験条
件に対応する基準信号を発生するための基準信号発生器
と、前記荷重信号と前記基準信号の差に対応する誤差信
号を発生するための誤差信号発生器と、前記基準信号と
前記誤差信号の和に対応する命令信号を発生し、この命
令信号を前記荷重付加・検出系へ供給するための演算装
置とを備えたことを特徴とする疲労試験機。
A load addition/detection system for applying a load to a test piece and generating a load signal corresponding to this load, a reference signal generator for generating a reference signal corresponding to set test conditions, and the load signal. and an error signal generator for generating an error signal corresponding to the difference between the reference signal and the reference signal, and generating a command signal corresponding to the sum of the reference signal and the error signal, and transmitting the command signal to the load addition/detection system. A fatigue testing machine characterized by being equipped with a computing device for supplying data to a computer.
JP11083586A 1986-05-16 1986-05-16 Fatigue testing machine Pending JPS62267643A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11083586A JPS62267643A (en) 1986-05-16 1986-05-16 Fatigue testing machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11083586A JPS62267643A (en) 1986-05-16 1986-05-16 Fatigue testing machine

Publications (1)

Publication Number Publication Date
JPS62267643A true JPS62267643A (en) 1987-11-20

Family

ID=14545869

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11083586A Pending JPS62267643A (en) 1986-05-16 1986-05-16 Fatigue testing machine

Country Status (1)

Country Link
JP (1) JPS62267643A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5396804A (en) * 1993-10-12 1995-03-14 Gas Research Institute Apparatus and method for force-controlled fatigue testing
AT414176B (en) * 2003-03-20 2006-09-15 Seibt Kristl & Co Gmbh DEVICE FOR EXPLORING A TEST WITH A PERIODIC CHANGING TEST SIZE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5396804A (en) * 1993-10-12 1995-03-14 Gas Research Institute Apparatus and method for force-controlled fatigue testing
AT414176B (en) * 2003-03-20 2006-09-15 Seibt Kristl & Co Gmbh DEVICE FOR EXPLORING A TEST WITH A PERIODIC CHANGING TEST SIZE

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