TW200925599A - Fatigue testing device - Google Patents

Fatigue testing device Download PDF

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Publication number
TW200925599A
TW200925599A TW97137660A TW97137660A TW200925599A TW 200925599 A TW200925599 A TW 200925599A TW 97137660 A TW97137660 A TW 97137660A TW 97137660 A TW97137660 A TW 97137660A TW 200925599 A TW200925599 A TW 200925599A
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TW
Taiwan
Prior art keywords
workpiece
servo motor
testing device
force
load
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Application number
TW97137660A
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Chinese (zh)
Inventor
Kazuyoshi Tashiro
Sigeru Matsumoto
Hiroshi Miyashita
Kazuhiro Murauchi
Original Assignee
Kokusai Keisokuki Kk
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Publication of TW200925599A publication Critical patent/TW200925599A/en

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/32Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces
    • G01N3/38Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces generated by electromagnetic means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0014Type of force applied
    • G01N2203/0021Torsional
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0058Kind of property studied
    • G01N2203/0069Fatigue, creep, strain-stress relations or elastic constants
    • G01N2203/0073Fatigue
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02Details not specific for a particular testing method
    • G01N2203/06Indicating or recording means; Sensing means
    • G01N2203/067Parameter measured for estimating the property
    • G01N2203/0676Force, weight, load, energy, speed or acceleration

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

Provided is a fatigue testing device which can acquire such an amplitude of the angle of an axis of rotation of a servomotor automatically and quickly as to be set when a test is done with the fluctuation widths of a force to be applied to a work being adjusted constant. The fatigue testing device comprises deformation detecting means for measuring the deformation of the work, force measuring means for measuring the magnitude of the force to be applied to the work, spring constant calculating means for calculating the spring constant of the work, while increasing the amplitude of the angle of the rotation axis of the servomotor gradually, on the basis of the measurement results of the deformation detecting means and the force measuring means, and control means for controlling the servomotor on the basis of the spring constant calculated by the spring constant calculating means, so that the amplitude of the magnitude of the force to be applied to the work may be a predetermined magnitude.

Description

200925599 六、發明說明: 【發明所屬之技術領域】 本發明係關於一種將扭力、拉伸、壓縮、彎曲方向 之反覆負載施加於工件的疲勞測試裝置。 【先前技術】 對材料施加反覆負載而計測其材料之疲勞強度的 疲勞測試裝置,係利用使用記載於日本特開昭63 _ 37233號公報之祠服馬達者。飼服馬達係藉由將成為目 標之角度(目標角度)輸入祠服放大器,而使伺服馬達 之旋轉轴的相位移動於其角度者。在伺服馬達中設有用 於檢測旋轉轴之相位變化的旋轉編碼器,伺服放大器依 據從旋轉編碼器之檢測值判斷之旋轉轴的相位與目標 角度之差分,來設定賦予伺服馬達之驅動電力。 進行扭力測試之扭力測試裝置係藉由設於把持工 件一端的卡盤與伺服馬達之旋轉軸之間的減速機(減速 齒輪等),放大伺服馬達之力矩而賦予工件。此外,進 行拉伸、壓縮、彎曲測試之萬能測試裝置,係在伺服馬 達之旋轉軸上設置進给螺絲機構等的直動變換器,而將 伺服馬達之旋轉運動變換成直進運動。 【發明内容】 此種疲勞測試裝置中,係將施加之力(力矩或負 載)、變位、速度或加速度之變動幅度(上限及/或下 限)保持一定,而將反覆負載施加於工件。但是,因為 伺服馬達係控制其旋轉軸之角度者,所以將施加之力的 變動幅度保持一定而進行測試時,在進行反覆測試之 200925599 :2作業者以手動操作而施加 鈀加希望之力 认戰於工件,估計為了 動作)。、要之做馬相旋_之角度(嘗試 以手動操作進行此種嘗試動 ,得需要之伺服馬達旋轉軸】c此外, 者,在工件上過度施加力,可能在長時間。再 破損。 长旨δ式動作中導致工件 本發明係為了解決上述問題 Ο 明之目的為提供—種疲勞賴裝置,亦即,本發 1將:加於工件之力的變動幅度保持—以速= 時’須設定之他馬達的旋轉轴之角度振=進订測试 為了達成上述目的,本 力計測手段,其係二====: 其係使伺服馬達之旋轉軸的角度振二; 曰加而反轉_ ’依制服馬達錢轉肖纽測手 ,運异施加於工件之力與伺服馬達之旋轉 例常?;及控制手段,其係依據 1由比例*數運鼻手段所運算之比例常數,控制伺服馬 達,ί施加於工件之力的大小之振幅成為指定之大小。 藉由此種構成,可自動且迅速地求出比例常數,並 依據該比例常數而以適切之角度振幅使伺服馬達驅 動。此外,因為使伺服馬達之旋轉轴的角度振幅逐漸增 加,所以不致於不慎施加過大的力於工件上,而發生工 件之破損。 此外’比例常數運算手段宜構成依據伺服馬達之旋 轉轴的角度變動概略停止時的伺服馬達之旋轉轴的旋 轉角度及力計測手段之計測結果,來運算比例常數。亦 即’由於伺服馬達之旋轉軸的角速度快,即工件之變形 4 200925599 速度大時,容易發生計測誤差,因此,藉由在工件之變 形速度低,亦即在工件大致靜止之狀態下以施加於工件 之力的大小與伺服馬達之旋轉軸的旋轉角度來運算比 例常數,可更正確地求出伺服馬達之角度振幅。 此外’力計測手段應構成至少計測2次施加於工件 之力的大小,且比例常數運算手段應構成將第一次計測 時之伺服馬達的旋轉軸之旋轉角度與第二次計測時之 伺服馬達的旋轉軸之旋轉角度之差除第一次計測時之 力的大小與第二次計測時之力的大小之差的值,作為工 件之彈性常數。如拉伸測試及壓縮測試時,因為在將工 件安裝於測試裝置之時點,會在工件上發生翹曲’伺服 馬達之旋轉軸的旋轉角度不見得係對應於自然狀態時 之變形量。而按照本發明時,係依據以不同之力使工件 變形時之變形量的差與力大小之差,可更正確地算出比 例常數。 此外,疲勞測試裝置宜構成可沿著第一方向以及與 第一方向相反之第二方向兩者,而在工件上施加負载, 比例常數運算手段運算工件在第一方向變形時之第一 比例常數,與工件在第二方向變形時之第二比例常數, 且控制手段控制伺服馬達,於工件在第一方向變形時, 將以第一比例常數除指定之大小而獲得之變形量成為 工件變形量之上限,並控制前述伺服馬違,於工件在第 一方向變形時,將以第二比例常數除指定之大小而獲得 之變形量成為工件變形量之上限。亦即,如在將拉伸負 載施加於工件之疲勞測試中,使工件在拉伸方向(第一 方向)變形時,與從該狀態解除負載(使工件在第二方 白變形)時,可咸比例常數不同。因而,如本發明之構 成,宜分別求出第一比例常數與第二比例常數。 200925599 此外,如疲勞測試裝置係在工件上施加扭力負載之 扭力測試裝置,且施加於工件之力係工件之旋轉轴周圍 的力矩。 或是,疲勞測試裝置係經由進給螺絲機構,而在工 件上施加拉伸、壓縮或彎曲負載的萬能測試裝置,且施 加於工件之力係施加於工件之負載的進給螺絲機構的 進給方向成分。 如以上所述,按照本發明而實現可自動且迅速地獲 得將施加於工件之力的變動幅度保持一定而進行測試 〇 時,須設定之伺服馬達的旋轉軸之角度振幅的疲勞測試 裝置。 【實施方式】 以下,就本發明之實施例,使用圖式詳細作說明。 第一圖係顯示本發明第一實施例之疲勞測試裝置的區 塊圖者。本實施例之疲勞測試裝置係可在測試片(工件) 上反覆地施加扭力負載的疲勞測試裝置。 如第一圖所示,本實施例之疲勞測試裝置具有:在 © 工件W上施加扭力負載之裝置本體10,用於驅動裝置 本體10之伺服馬達12的伺服放大器20,及控制伺服放 大器20之控制部30。 裝置本體10具有:卡盤11a、lib、伺服馬達12、 減速機13、力矩感測器14及角度感測器15。卡盤11a 及lib從兩端把持工件W。減速機13配置於伺服馬達 12之驅動軸與一方之卡盤11a之間,增大伺服馬達12 之驅動軸的力矩而賦予工件W。此外,另一方之卡盤lib 經由力矩感測器14而固定於無圖示之裝置本體的框架。 在以上說明之構成中,驅動伺服馬達12時,在被 200925599 卡盤lla、lib把持之工件w上施加扭力負 藉由力矩感測器14計測。此外,角度咸哭大小 速㈣之輸出轴’檢测在卡盤lla4 = ;於減 力角度。 %之工件W的扭 伺服馬達12藉由伺服放大器20控制。亦g,_ 放大器20依據從控制部30傳送之設定角度伺月^ ❻200925599 VI. Description of the Invention: [Technical Field] The present invention relates to a fatigue testing device for applying a reverse load in a torsion, tension, compression, and bending direction to a workpiece. [Prior Art] A fatigue tester that measures the fatigue strength of a material by applying a load to a material is used by a motor that is described in Japanese Laid-Open Patent Publication No. S63-37233. The feeding motor moves the phase of the rotating shaft of the servo motor to its angle by inputting the target angle (target angle) into the servo amplifier. The servo motor is provided with a rotary encoder for detecting a phase change of the rotary shaft, and the servo amplifier sets the drive power applied to the servo motor based on the difference between the phase of the rotary shaft determined from the detected value of the rotary encoder and the target angle. The torque test device for performing the torque test is provided to the workpiece by amplifying the torque of the servo motor by a speed reducer (reduction gear or the like) provided between the chuck at one end of the gripping workpiece and the rotary shaft of the servo motor. Further, the universal testing device for performing the stretching, compression, and bending tests is to provide a linear motion converter such as a feed screw mechanism on the rotary shaft of the servo motor, and convert the rotary motion of the servo motor into a linear motion. SUMMARY OF THE INVENTION In such a fatigue test apparatus, a variable load (torque or load), a displacement, a speed, or an acceleration fluctuation range (upper limit and/or a lower limit) is kept constant, and a reverse load is applied to a workpiece. However, since the servo motor controls the angle of the rotation axis, when the test is performed while the fluctuation range of the applied force is kept constant, the operator performs the repeated test at 200925599: 2, and the operator applies the palladium with the manual operation. Battle on the artifact, estimated for action). If you want to do this kind of trial with a manual operation, you need the servo motor rotation axis. c In addition, if the force is excessively applied to the workpiece, it may be damaged for a long time. The present invention has been made in order to solve the above problems. The purpose of the present invention is to provide a fatigue-reducing device, that is, the present invention will: maintain the variation of the force applied to the workpiece - at speed = when it is required Angle vibration of the rotating shaft of the motor = binding test In order to achieve the above purpose, the force measuring means, the system is two ====: which makes the angle of the rotating shaft of the servo motor vibrate; According to the uniform motor money to turn to the New York tester, the force applied to the workpiece and the rotation of the servo motor are often used; and the control method is based on a proportional constant calculated by the proportional* number of nose means to control the servo motor. The amplitude of the force applied to the workpiece is a specified size. With this configuration, the proportionality constant can be automatically and quickly determined, and the servo motor can be driven with an appropriate angular amplitude in accordance with the proportional constant. In addition, since the angular amplitude of the rotating shaft of the servo motor is gradually increased, excessive force is not inadvertently applied to the workpiece, and the workpiece is broken. Further, the 'proportional constant calculation means should be based on the angle of the rotating shaft of the servo motor. The proportional constant is calculated by changing the rotation angle of the rotating shaft of the servo motor and the measurement result of the force measuring means when the fluctuation is stopped. That is, because the angular velocity of the rotating shaft of the servo motor is fast, that is, the deformation of the workpiece 4 200925599, the speed is easy. Since the measurement error occurs, the proportional constant can be calculated by calculating the proportionality constant when the deformation speed of the workpiece is low, that is, the magnitude of the force applied to the workpiece and the rotation angle of the rotation axis of the servo motor in a state where the workpiece is substantially stationary. The angular amplitude of the servo motor is determined. In addition, the force measuring means should be configured to measure the magnitude of the force applied to the workpiece at least twice, and the proportional constant calculation means should constitute the rotation angle of the rotating shaft of the servo motor during the first measurement. The difference between the rotation angles of the rotary axes of the servo motor during the second measurement, except the first count The value of the difference between the magnitude of the force and the force of the second measurement, as the elastic constant of the workpiece. For example, in the tensile test and the compression test, because the workpiece is mounted on the test device, it will be on the workpiece. Warpage occurs. The rotation angle of the rotating shaft of the servo motor does not necessarily correspond to the amount of deformation in the natural state. According to the present invention, the difference between the amount of deformation and the magnitude of the force when the workpiece is deformed by different forces is used. In addition, the fatigue test device should be configured to be both movable along the first direction and the second direction opposite to the first direction, and a load is applied to the workpiece, and the proportional constant operation means the workpiece is calculated. a first proportional constant when deforming in one direction, and a second proportional constant when the workpiece is deformed in the second direction, and the control means controls the servo motor to divide the first proportional constant by a specified size when the workpiece is deformed in the first direction The obtained deformation amount becomes the upper limit of the deformation amount of the workpiece, and controls the aforementioned servo horse violation. When the workpiece is deformed in the first direction, the second ratio is often In addition to the amount of deformation of the specified size to obtain the deformation amount becomes the upper limit of the workpiece. That is, as in the fatigue test in which a tensile load is applied to the workpiece, when the workpiece is deformed in the stretching direction (first direction), and when the load is released from the state (the workpiece is deformed in the second direction), The salt ratio constant is different. Therefore, as in the constitution of the present invention, the first proportional constant and the second proportional constant should be separately determined. 200925599 In addition, a fatigue testing device is a torque testing device that applies a torsional load on a workpiece, and the force applied to the workpiece is the moment around the rotating shaft of the workpiece. Alternatively, the fatigue testing device is a universal testing device that applies a tensile, compressive or bending load to the workpiece via a feed screw mechanism, and the force applied to the workpiece is fed by a feed screw mechanism applied to the load of the workpiece. Directional component. As described above, according to the present invention, it is possible to automatically and quickly obtain a fatigue test apparatus which can set the angular amplitude of the rotary shaft of the servo motor when the fluctuation range of the force applied to the workpiece is kept constant. [Embodiment] Hereinafter, embodiments of the present invention will be described in detail using the drawings. The first figure shows a block diagram of the fatigue test apparatus of the first embodiment of the present invention. The fatigue testing device of this embodiment is a fatigue testing device that can repeatedly apply a torsional load on a test piece (workpiece). As shown in the first figure, the fatigue testing apparatus of the present embodiment has a device body 10 for applying a torsional load on the workpiece W, a servo amplifier 20 for driving the servo motor 12 of the apparatus body 10, and a servo amplifier 20 for controlling Control unit 30. The apparatus body 10 has chucks 11a, lib, a servo motor 12, a speed reducer 13, a torque sensor 14, and an angle sensor 15. The chucks 11a and 11b hold the workpiece W from both ends. The speed reducer 13 is disposed between the drive shaft of the servo motor 12 and one of the chucks 11a, and increases the torque of the drive shaft of the servo motor 12 to be applied to the workpiece W. Further, the other chuck lib is fixed to the frame of the apparatus body (not shown) via the torque sensor 14. In the configuration described above, when the servo motor 12 is driven, the torque is applied to the workpiece w held by the 200925599 chucks 11a, 11b, and is measured by the torque sensor 14. In addition, the angle of the salty crying speed (four) of the output shaft 'detected at the chuck lla4 = ; at the force reduction angle. The twist of the workpiece W of % is controlled by the servo amplifier 20. Also, the _ amplifier 20 is based on the set angle transmitted from the control unit 30.

之伺服馬達的旋轉軸角度),產生用於驅動司服馬、達9 ^ 之驅動電力,並將其送至伺服馬達12使其驅動伺服 馬達12中設有用於檢測伺服馬達12之旋轉軸的轉數及 角度等之旋轉編碼器12a。旋轉編碼器i2a之訊號輪出 連接於飼服放大器20 ’伺服放大器20依據旋轉編^器 12a之計測結果進行驅動電力之回授控制。 其久’就控制部3 0之構成作說明。第二圖係本實 施例之控制部30的區塊圖。如第二圖所示,本實施例 之控制部30具有:控制器31、訊號變換手段32、a/d 變換手段33、力矩感測器用放大器34a、角度感測器用 放大器34b、操作手段35、波形發生電路36、軟碟驅動 器(FDD) 37、記憶體38及類比埠39。另外,在第一 圖及第二圖中,控制部30係記載了一個區塊,不過實 際上係藉由複數個單元而形成。如力矩感測器用放大器 34a及角度感測器用放大器34b分別作為獨立之單元而 形成。此外,操作手段35係設於包含控制器31之單元 的機盒側面之控制面板,不過,亦可為經由電缓而連接 於控制器31之獨立的單元(如個人電腦)。 本實施例之控制部30係參照藉由力矩感測器14、 角度感測器15 (均如第一圖)而檢測出之工件W的力 矩及角度,以力矩或角度之隨時間變動顯示希望之波形 的方式,而傳送設定角度至伺服放大器20(第一圖)者。 200925599 賦予工件w之作用(負載及變形量)的波形使用 作手段35作設定。操作手段35如具備:鍵盤等之輸又 手段,及用於確認該輸入手段之輸入結果的顯示手^, 本實施例之疲勞測試裝置的作業者可操作操作手段X乃 來設定進行反覆扭力測試時之力矩、角度或角速度又的範 圍。如可設定正弦波狀地進行來回扭力運動時之角度變 動的振幅。操作手段35之設定結果傳送至 ^ 並保存於記憶體38。 二 ’ ❹The rotation axis angle of the servo motor generates driving power for driving the servo horse, and sends it to the servo motor 12 to drive the servo motor 12 to be provided with a rotating shaft for detecting the servo motor 12. Rotary encoder 12a of number of revolutions and angles. The signal encoder of the rotary encoder i2a is connected to the feeding amplifier 20'. The servo amplifier 20 performs feedback control of the driving power in accordance with the measurement result of the rotary encoder 12a. The configuration of the control unit 30 will be described for a long time. The second drawing is a block diagram of the control unit 30 of the present embodiment. As shown in the second figure, the control unit 30 of the present embodiment includes a controller 31, a signal conversion means 32, an a/d conversion means 33, a torque sensor amplifier 34a, an angle sensor amplifier 34b, an operation means 35, The waveform generating circuit 36, the floppy disk drive (FDD) 37, the memory 38, and the analog 埠39. Further, in the first diagram and the second diagram, the control unit 30 describes one block, but actually it is formed by a plurality of units. For example, the torque sensor amplifier 34a and the angle sensor amplifier 34b are formed as separate units. Further, the operation means 35 is provided on the control panel on the side of the casing of the unit including the controller 31, but may be a separate unit (e.g., a personal computer) connected to the controller 31 via electric power. The control unit 30 of the present embodiment refers to the moment and angle of the workpiece W detected by the torque sensor 14 and the angle sensor 15 (both as shown in the first figure), and displays the hope with time or time of the moment or angle. In the manner of the waveform, the set angle is transmitted to the servo amplifier 20 (first figure). 200925599 The waveform that gives the action w (load and deformation amount) of the workpiece w is set by means 35. The operation means 35 includes a means for inputting a keyboard or the like, and a display means for confirming the input result of the input means. The operator of the fatigue test apparatus of the present embodiment can operate the operation means X to set the reverse torque test. The range of moments, angles or angular velocities. For example, the amplitude of the angular change when the back and forth torque motion is performed in a sinusoidal wave shape can be set. The setting result of the operation means 35 is transmitted to ^ and stored in the memory 38. Two ‘ ❹

此外、,波形發生電路36係以希望之周期、時序而 產生正弦波、三角波、矩形波等之訊號波形的電路。更 具體而言,f⑴為將時間t作為自變數之函數時,係將公 式s=f(t)表示之值s依序輸出至控制器31者。另外,上 述公式中,如波形係正弦波時,周期設為τ,相位設為 =則'f(t)=sin(27t(t—a)/T)。此時,周期 τ 及相位 a 可错由操作操作手段35而設定成任意之值。 控制器31將從波形發生電路36傳送至控制器31 =值乘上,由操作手段35而設定之值,來運算目標波 =,並運算應從該目標波形送至伺服放大器20之設定 度。而後,操作手段35所設定之經運算的設定角度 及由訊號變換手段32而傳送至伺服放大器2〇。Further, the waveform generating circuit 36 is a circuit that generates signal waveforms such as sine waves, triangular waves, and rectangular waves in a desired cycle and timing. More specifically, when f(1) is a function of the time t as a self-variable, the value s expressed by the equation s=f(t) is sequentially output to the controller 31. Further, in the above formula, if the waveform is a sine wave, the period is set to τ, and the phase is set to = then 'f(t) = sin(27t(t - a) / T). At this time, the period τ and the phase a can be set to an arbitrary value by the operation operation means 35. The controller 31 transmits the value from the waveform generation circuit 36 to the controller 31 = value multiplied by the operation means 35 to calculate the target wave = and calculates the set value to be sent from the target waveform to the servo amplifier 20. Then, the calculated set angle set by the operating means 35 is transmitted to the servo amplifier 2 via the signal converting means 32.

藉由以上之構成,可驅動伺服馬達12,使工件W =扭力角按照正弦波、三角波或矩形波之規定的波形變 動0 ,本實施例之疲勞測試裝置1,在進行以作| 所設定之力矩的振幅(設定力矩振幅)在工件w上方 ^覆負載之疲勞測試時,可自動地設定伺服馬達1 於旋轉軸的角度變動之振幅。就其程序參照第三圖說日 ;下另外,第二圖係橫軸為時間t,縱軸為伺服馬i; 8 200925599 12之旋轉軸之角度θ的圖。 為了可如上述地以設定力矩振幅在工件w上施力 反覆負載,本實施例中,係在疲勞測試之前計測工件^ 之彈性常數。其次說明其具體之計測方法。首先,將工 件w安裝於卡盤lla、ub上,其次驅動伺服馬達 而後,在伺服馬達開始驅動之初,以充分小之 變動的振幅驅動伺服馬達12之旋轉轴。其後使 广 之角度振幅逐漸增加。此時,藉由力矩感測器14 ❹ ❹ 施加於工件w之力矩。此外,旋轉軸之角度的變、 T係-定’而與振幅無關。 周』 12 A、Fb、匕、〜及此時伺服馬達 H疋轉轴的角度Θα、Θβ、%、θ〇。此時,點A $ ”Iff始測試時之旋轉軸的角度〇朝-個方向2 正的方向)變動時進行計測者,而點β t 變ς朝與該正方向相反之方向(以下,稱為 變動時進行計測者。 ;万向) 二子點*只%例中如第三圖所示,係控制 ^ 线轉轴㈣動成為正弦波狀。因而,從刮 :始經過時間T/4+nT(n:自然數)後,在正^ 侧’旋轉軸的角速度為0 =方向 間3Τ/4 + ΠΤ後,在正之方 舳^ 過時 細、κ施例中’將從測試開始經過9Τ/4後設為點A,。 、、里過 11T/4 後設為點 B,,將 將經過15T/4後設為點〇將紅過137/4後5又為點C, 工件5人二A〜D之計測值,藉由數式1運〜 件W在正及負方向的力矩與飼服馬達的旋轉^ = 200925599 比的比例常數sP、sN。 [數式1] sP=^ θ,-θ, c — Fd -FbAccording to the above configuration, the servo motor 12 can be driven to vary the workpiece W = torque angle by a predetermined waveform of a sine wave, a triangular wave or a rectangular wave. The fatigue test apparatus 1 of the present embodiment is set to perform the operation of | The amplitude of the torque (set torque amplitude) can automatically set the amplitude of the angular variation of the servo motor 1 on the rotating shaft when the fatigue test of the load over the workpiece w is applied. For the procedure, refer to the third figure for the day; in addition, the second graph is the time axis t, the vertical axis is the servo horse i; 8 200925599 12 is the angle θ of the rotation axis. In order to apply a force to the workpiece w to apply a load to the load w as described above, in the present embodiment, the spring constant of the workpiece ^ is measured before the fatigue test. Next, the specific measurement method will be described. First, the workpiece w is attached to the chucks 11a and ub, and after the servo motor is driven, the rotary shaft of the servo motor 12 is driven with a sufficiently small amplitude at the beginning of the start of driving of the servo motor. Thereafter, the amplitude of the wide angle is gradually increased. At this time, the moment applied to the workpiece w by the torque sensor 14 ❹ 。. Further, the change in the angle of the rotation axis, T-set, is independent of the amplitude. Weeks 12 A, Fb, 匕, ~ and the angle Θα, Θβ, %, θ〇 of the servo motor H疋 shaft at this time. At this time, when the point A $ "Iff starts to test, the angle of the rotation axis 〇 changes in the positive direction of the direction 2", the measurement is performed, and the point β t changes toward the direction opposite to the positive direction (hereinafter, For the change, the measurement is performed. ; Universal direction) The second sub-point * Only in the example of the third example, the control shaft rotation axis (four) movement becomes a sinusoidal wave. Therefore, the elapsed time from the scraping: T/4+ After nT(n: natural number), the angular velocity of the 'rotation axis' on the positive side is 0 = 3Τ/4 + 方向 between the directions, and in the positive square 过 ^ 细 , , , , , , , , , , , , , , , 4 is set to point A, . , , after 11T/4, set to point B, will be set after 15T/4, point will be red, 137/4, then 5 is point C, workpiece 5 people two The measured values of A to D are the proportional constants sP and sN of the ratio of the torque in the positive and negative directions to the rotation of the feeding motor ^ = 200925599 by the formula 1 [S1] sP=^ θ, -θ, c — Fd -Fb

其次,依據計測之SP、SN,決定以設定力矩振幅在 工件W上施加反覆負載用之伺服馬達12的旋轉軸之角 度變動的上限值與下限值。亦即,分別將正方向侧之設 定力矩振幅設為FSP,將負方向側之設定力矩振幅設為 FSN,並將伺服馬達12之旋轉軸的角度變動之上限值與 下限值分別設為ΘΡ、ΘΝ,而藉由以下之數式2運算ΘΡ、 ΘΝ。 [數式2]Then, based on the measured SP and SN, the upper limit and the lower limit of the angular variation of the rotational axis of the servo motor 12 for the reverse load are applied to the workpiece W by the set torque amplitude. In other words, the set torque amplitude on the positive side is FSP, the set torque amplitude on the negative side is FSN, and the upper and lower limits of the angular variation of the rotational axis of the servo motor 12 are respectively set. ΘΡ, ΘΝ, and ΘΡ, ΘΝ by the following formula 2. [Expression 2]

a _ ^SNa _ ^SN

ΘΝ—TΘΝ—T

而後,依據求出之θρ、ΘΝ,以伺服馬達12之旋轉 軸的角度變動滿足數式3之方式,藉由變更賦予伺服放 大器20之設定角度Θ,可依據希望之設定力矩振幅,在 工件上賦予反覆負載。 [數式3] 200925599 裝置‘ :月之尤發明的第—實施例係關於扭力測試 轉明即使:使非:定於上述構成者。亦即, 置中仍可、達之其他型式的疲勞測試裝 試裝置二可本發明第二實施例的疲勞測 置。 申壓縮或考曲負載的所謂萬能測試裝 圖去第Γΐ係顯不本實施例之疲勞測試裝置igi的區棟Then, according to the obtained θρ, ΘΝ, the angle variation of the rotation axis of the servo motor 12 satisfies the formula 3, and by changing the set angle 赋予 given to the servo amplifier 20, the workpiece amplitude can be set according to the desired torque amplitude. Give a repeat load. [Expression 3] 200925599 Apparatus ‘: The first embodiment of the invention is related to the torque test. Even if it is: the non-conformity is determined by the above-mentioned constituents. That is, the fatigue test apparatus 2 of the other type which is still available in the center can be used for the fatigue measurement of the second embodiment of the present invention. The so-called universal test package for compressing or testing the load is shown in the third section of the fatigue test device igi of the present embodiment.

❹ 例之疲勞測試裝置可在測試片(工件)上 反覆地施加拉伸、壓縮或彎曲負載。 如第四圖所示,本實施例之測試裝置101具有:在 工件W上施力口負載之裝置本體11〇,用於驅動裝置本體 :1〇之飼服馬達112的伺服放大器12〇,及控制伺服放大 器120之控制部13〇。裝置本體u〇具有:框架ln、伺 服馬達112、直動變換器113、負載傳感器U4、變位感 測器115及接合器118a及118b。 直動變換器113係用於將伺服馬達112之旋轉軸的 知:轉運動變換成直進方向之運動者。且具有:進給螺絲 113a、螺母113b、一對導軌113c、及分別對應於導軌 113c的移動塊113d。螺母U3b與進給螺絲113a結合。 此外’移動塊113d固定於螺母113b。移動塊113d可沿 著對應之導軌113c而移動,並且無法移動於其以外方 向。因而,移動塊113d及螺母113b之運動限定於沿著 導執113c伸出之方向的一個自由度。再者,因為進給螺 絲113a之轴方向係與導轨113()伸出之方向平行(亦即 上下方向),所以藉由伺服馬達112使進給螺絲113&轉 動時,螺母113b沿著導軌i13c而移動。如第四圖所示, 伺服馬達112固定於框架m之平台部Ula之下,此 11 200925599 外’導轨113c固定於平台部ma之上。 對平台部仙上下運動。科,在螺母之上安 保持工件w用的下部接合器118a。 上部載台116從框架ηι之頂板lllb 此:卜’在平台部ma之上面設有伸出於圖中的上下方面二掛導 桿117C。在上部载台116之左右方向端部形成有在 方向穿孔之貫穿孔116a,導桿117c通過該貫穿孔11如。 因而,上部載台116可沿著導桿117c而在上下方向The fatigue test device of the example can repeatedly apply tensile, compressive or bending loads on the test piece (workpiece). As shown in the fourth figure, the test apparatus 101 of the present embodiment has a device body 11A that applies a load on the workpiece W, and is used to drive the apparatus body: a servo amplifier 12A of the feeding motor 112, and The control unit 13 of the servo amplifier 120 is controlled. The apparatus body 〇 has a frame ln, a servo motor 112, a linear motion converter 113, a load sensor U4, a displacement sensor 115, and adapters 118a and 118b. The linear motion converter 113 is for converting the known rotational motion of the rotational axis of the servo motor 112 into a motion in the straight forward direction. Further, it has a feed screw 113a, a nut 113b, a pair of guide rails 113c, and a moving block 113d corresponding to the guide rail 113c. The nut U3b is coupled to the feed screw 113a. Further, the moving block 113d is fixed to the nut 113b. The moving block 113d is movable along the corresponding guide rail 113c and cannot be moved in the other direction. Thus, the movement of the moving block 113d and the nut 113b is limited to one degree of freedom in the direction in which the guide 113c protrudes. Furthermore, since the axial direction of the feed screw 113a is parallel to the direction in which the guide rail 113 () protrudes (i.e., the up and down direction), when the feed screw 113& is rotated by the servo motor 112, the nut 113b is along the guide rail. I13c moves. As shown in the fourth figure, the servo motor 112 is fixed to the platform portion U1 of the frame m, and the 11 200925599 outer 'rail 113c is fixed to the platform portion ma. Move up and down on the platform. The lower adapter 118a for holding the workpiece w is placed over the nut. The upper stage 116 is provided with a top plate 111b of the frame ηι. This is provided on the upper surface of the platform portion ma with the upper and lower side guide bars 117C extending from the figure. A through hole 116a that is perforated in the direction is formed at an end portion of the upper stage 116 in the left-right direction, and the guide rod 117c passes through the through hole 11, for example. Thus, the upper stage 116 can be in the up and down direction along the guide bar 117c

❹ 動&此t藉由旋緊設於上部載台116之無圖示的螺检, 可縮小貫穿孔116a之内徑,藉此,可對導桿m 上部載台116。 疋 在上部載台116之下面安裝用於從上方保持工件w 的上部接合器U8b。本實施例藉由在上部接合器U8b 與下部接合器118a之間保持工件W的狀態下,使螺母 113b上下運動,可在工件w上施加負載。另外,丄部 及下部接合器118a、118b分別構成可對上部载台116 及螺母113b裝卸,可依應施加於工件w之負載的種類 選擇適切之接合器。因為第四圖係在工件w上施加壓縮 負載的構成,所以上部接合器U8b之下面及下部接合 器的上面形成平面狀。在工件w上施加拉伸負載時使 用設置了把持工件W之卡盤的接合器118a、li8b。進 行三點彎曲測試時’係組合壓縮測試用之接合器與三點 %曲用之爽具而使用。 此外,上部載台116從框架111之頂板Ulb藉由進 給螺絲117a懸掛。在頂板lllb中埋入可與進給螺絲117a 結合而旋轉之螺母(未顯示於圖)。螺母藉由配置於頂 板Ulb之馬達117b而旋轉驅動。此外,藉由連結進給 螺絲117a與上部載台116之鏈環(link),進給螺絲117a 12 200925599 對上部載台116不在其軸周圍旋轉。因此,在旋鬆上部 載台116之螺栓,而可移動上部載台116之狀態下,藉 由馬達117b使該螺母轉動,可在上下方向驅動進給螺 絲117a及與該進給螺絲117a連結之上部載台116。該 功能使用於配合工件w之尺寸調整接合器118a、118b 之間隔時。亦即,進行測試時,旋緊螺栓,而將上部載 台116固定於導桿117c。 以上說明之構成中’以接合器118a、118b保持工件 W而驅動祠服馬達1· 12時’在工件w上施加拉伸、壓 縮或彎曲負載,其大小藉由負載傳感器114計測。此外, 變位感測器115係檢測下部接合器之變位,亦即檢測工 件W之變形量的感測器(如插入旋轉編碼器之測微儀 (dial gauge))。 與第一實施例同樣地藉由伺服放大器120控制伺服 馬達112。亦即,祠服放大器12〇依據從控制部13〇傳 送之目標值(作為目標之伺服馬達的旋轉轴角度)產生 用於驅動伺服馬達112之驅動電力,並將其送至伺服馬 達112使其驅動。伺服馬達ip中設有用於檢測伺服馬 達112之旋轉軸的轉數及角度等之旋轉編碼器U2a。旋 轉編碼器112a之訊號輸出連接於伺服放大器12〇,伺服 放大器120依據旋轉編碼器i12a之計測結果進行回授控 制。 其次,說明控制部130之構成。第五圖係本實施例 之控制部130的區塊圖。如圖所示,本實施例之控制部 130除了可分別連接負載傳感器來取代力矩感測器,及 變位感測器來取代角度感測器之外,與第三圖所示之本 發明的第一實施例相同。因此,控制部130中,在與本 發明之第一實施例相同或類似的構成要素上註記相同 13 200925599 符號,並省略關於控制部13〇之詳細說明。 本:施例之控制部130係參照藉由負載傳感器ιΐ4 及變位感測”15 (均記栽於第四圖)檢測出之工件w 的負載及變形以負載或變形量之隨時間變動顯示希 望之波形的方式’傳送^定角度至飼服放大器12〇 (第 一圖)。 —賦予工件w之作用的波形使用操作手段35來設 疋。本y施例之測試裝置101的作業者可操作操作手段❹ & amp t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t t上 An upper adapter U8b for holding the workpiece w from above is mounted under the upper stage 116. In the present embodiment, the nut 113b is moved up and down in a state where the workpiece W is held between the upper adapter U8b and the lower adapter 118a, and a load can be applied to the workpiece w. Further, each of the crotch portion and the lower adapters 118a and 118b is configured to be detachable from the upper stage 116 and the nut 113b, and an appropriate adapter can be selected depending on the type of load applied to the workpiece w. Since the fourth figure is a configuration in which a compressive load is applied to the workpiece w, the lower surface of the upper adapter U8b and the upper surface of the lower adapter are formed in a planar shape. When the tensile load is applied to the workpiece w, the adapters 118a and li8b provided with the chuck for holding the workpiece W are used. When the three-point bending test is performed, the adapter for the combined compression test and the three-point fastener are used. Further, the upper stage 116 is suspended from the top plate U1b of the frame 111 by a feed screw 117a. A nut (not shown) that can be rotated in conjunction with the feed screw 117a is embedded in the top plate 111b. The nut is rotationally driven by a motor 117b disposed on the top plate U1b. Further, by connecting the link of the feed screw 117a and the upper stage 116, the feed screws 117a 12 200925599 rotate the upper stage 116 around its axis. Therefore, when the bolt of the upper stage 116 is loosened and the upper stage 116 is moved, the nut is rotated by the motor 117b, and the feed screw 117a can be driven in the up-and-down direction and coupled to the feed screw 117a. Upper stage 116. This function is used to adjust the spacing of the adapters 118a, 118b in accordance with the size of the workpiece w. That is, when the test is performed, the bolt is tightened, and the upper stage 116 is fixed to the guide rod 117c. In the above-described configuration, when the workpiece W is held by the adapters 118a and 118b and the servo motor 1·12 is driven, a tensile, compressive or bending load is applied to the workpiece w, and the magnitude thereof is measured by the load cell 114. Further, the displacement sensor 115 detects a displacement of the lower adapter, that is, a sensor that detects the amount of deformation of the workpiece W (e.g., a dial gauge inserted into the rotary encoder). The servo motor 112 is controlled by the servo amplifier 120 as in the first embodiment. That is, the servo amplifier 12 generates driving power for driving the servo motor 112 in accordance with the target value transmitted from the control unit 13 (the rotation axis angle of the target servo motor), and sends it to the servo motor 112 to cause it. drive. The servo motor ip is provided with a rotary encoder U2a for detecting the number of revolutions, the angle, and the like of the rotary shaft of the servo motor 112. The signal output of the rotary encoder 112a is connected to the servo amplifier 12A, and the servo amplifier 120 performs feedback control based on the measurement result of the rotary encoder i12a. Next, the configuration of the control unit 130 will be described. The fifth diagram is a block diagram of the control unit 130 of the present embodiment. As shown in the figure, the control unit 130 of the present embodiment can be used in addition to the torque sensor instead of the torque sensor, and the displacement sensor instead of the angle sensor, and the present invention shown in the third figure. The first embodiment is the same. Therefore, in the control unit 130, the same or similar constituent elements as those of the first embodiment of the present invention are denoted by the same reference numeral 13 200925599, and the detailed description of the control unit 13A is omitted. The control unit 130 of the embodiment refers to the load and deformation of the workpiece w detected by the load sensor ι 4 and the displacement sensing "15 (all recorded in the fourth figure), and displays the load or the amount of deformation with time. The desired waveform mode is 'transmitted to the feeding amplifier 12 〇 (first figure). - The waveform imparted to the workpiece w is set by the operating means 35. The operator of the testing apparatus 101 of the present embodiment can Operational means

❹ 35 ’來设疋進行反覆測試時之負載、變形量等的變動幅 度。如可設定在工彳W上施加正弦波狀之反覆壓縮變位 時的變位振幅。 控制器31在從波形發生電路36傳送至控制器31 之值中乘上藉由操作手段35所設定之值,運算目標值, 比較該目標值與負載傳感器114檢測出之負載,或是比 較變位感測器115檢測出之變形量(或是此等之時間微 分值的變形速度),運算應送至伺服放大器120之設定 角度。運算出之設定角度經由訊號變換手段32而傳送 至伺服放大器120。 藉由以上之構成,可以施加於工件W之負載或工件 W之變形量按照正弦波、三角波或矩形波之規定波形而 變動的方式驅動伺服馬達112。 此外’與第一實施例同樣地,本實施例之萬能測試 裝置101以作業者所設定之負載的振幅(設定負載振幅) 在工件w上施加反覆負載的疲勞測試時,可自動地設定 飼服馬達12之旋轉軸的角度變動振幅。該構成與參照 第三圖而說明之本發明的實施例大致相同。因此,本實 施例中亦參照第三圖作說明。 為了可如上述地以設定力矩振幅在工件W上施加 14 200925599 反覆負載,本實施例中,係在疲勞測試之前計測工件w 之彈性常數。具體之計測方法說明如下。首先,將工件 W安裝於測試裝置101,其次驅動伺服馬達12。而後, 在伺服馬達12開始驅動之初,以充分小之角度變動的 振幅驅動伺服馬達12之旋轉軸。其後使旋轉軸之角度 振幅逐漸增加。此時,藉由力矩感測器14檢測施加於 工件W之力矩。此外,旋轉軸之角度的變動周期T係 一定,而與振幅無關。 其次,在第三圖中之四處的點A、B、C及D計測 ❹ 施加於工件W之負載PA、PB、Pc、PD及此時伺服馬達 12之旋轉轴的角度Θα、Θβ、〇c、〇d。此時’點A及C 係角度從開始測試時之旋轉軸的角度0朝一個方向(以 下,定義為正的方向)變動時進行計測者,而點B及D 係角度朝與該正方向相反之方向(以下,稱為負的方向) 變動時進行計測者。 此外,點A〜D均是伺服馬達12之旋轉軸的變動概 略停止的時點。本實施例中如第三圖所示,係控制伺服 馬達12之旋轉軸的變動成為正弦波狀。因而,從測試 β 開始經過時間T/4 + nT (η :自然數)後,在正之方向 侧,旋轉軸的角速度為0。同樣地,從測試開始經過時 間3Τ/4 + ηΤ後,在正之方向侧,旋轉軸的角速度為0。 本實施例中,將從測試開始經過9Τ/4後設為點A,將 經過11T/4後設為點B,將經過13T/4後設為點C, 將經過15T/4後設為點D。 其次,使用在點A〜D之計測值,藉由數式4運算 工件W在正及負方向的彈性常數SP、SN。 [數式4] 15 200925599❹ 35 ’ Set the amplitude of the load, the amount of deformation, etc. during the repeated test. For example, the displacement amplitude when a sinusoidal reverse compression displacement is applied to the workpiece W can be set. The controller 31 multiplies the value set by the operation means 35 by the value transmitted from the waveform generating circuit 36 to the controller 31, calculates the target value, compares the target value with the load detected by the load sensor 114, or compares it. The amount of deformation detected by the bit sensor 115 (or the deformation rate of the time differential value) is calculated and sent to the set angle of the servo amplifier 120. The calculated set angle is transmitted to the servo amplifier 120 via the signal conversion means 32. According to the above configuration, the servo motor 112 can be driven such that the load applied to the workpiece W or the deformation amount of the workpiece W fluctuates according to a predetermined waveform of a sine wave, a triangular wave or a rectangular wave. Further, in the same manner as the first embodiment, the universal testing device 101 of the present embodiment can automatically set the feeding service when the fatigue test of the load is applied to the workpiece w by the amplitude of the load set by the operator (set load amplitude). The angular variation amplitude of the rotation axis of the motor 12. This configuration is substantially the same as the embodiment of the present invention described with reference to the third drawing. Therefore, this embodiment is also described with reference to the third figure. In order to apply the 14200925599 reverse load to the workpiece W with the set torque amplitude as described above, in this embodiment, the spring constant of the workpiece w is measured before the fatigue test. The specific measurement methods are described below. First, the workpiece W is mounted on the test device 101, and the servo motor 12 is driven next. Then, at the beginning of the start of driving of the servo motor 12, the rotation shaft of the servo motor 12 is driven at an amplitude that is sufficiently small to vary. Thereafter, the angular amplitude of the rotating shaft is gradually increased. At this time, the moment applied to the workpiece W is detected by the torque sensor 14. Further, the fluctuation period T of the angle of the rotation axis is constant regardless of the amplitude. Next, the points A, B, C, and D at four points in the third figure measure the loads PA, PB, Pc, PD applied to the workpiece W and the angles 旋转α, Θβ, 〇c of the rotation axis of the servo motor 12 at this time. , 〇d. At this time, the angles of the points A and C are measured from the angle 0 of the rotation axis at the start of the test in one direction (hereinafter, defined as a positive direction), and the angles of the points B and D are opposite to the positive direction. When the direction (hereinafter referred to as the negative direction) changes, the measurement is performed. Further, each of the points A to D is a point at which the fluctuation of the rotation axis of the servo motor 12 is substantially stopped. In the present embodiment, as shown in the third figure, the fluctuation of the rotation axis of the servo motor 12 is controlled to be sinusoidal. Therefore, after the elapsed time T/4 + nT (η : natural number) from the test β, the angular velocity of the rotating shaft is 0 on the positive side. Similarly, after the elapsed time from the start of the test, 3 Τ / 4 + η , , the angular velocity of the rotary shaft is 0 on the positive direction side. In this embodiment, it will be set to point A after 9Τ/4 from the start of the test, to point B after 11T/4, to point C after 13T/4, and to the point after 15T/4. D. Next, using the measured values at points A to D, the elastic constants SP and SN of the workpiece W in the positive and negative directions are calculated by the equation 4. [Expression 4] 15 200925599

Pc-Pa P θ.-θκPc-Pa P θ.-θκ

PD -PB N ΘΌ-ΘΒ 其次,依據計測之SP、SN,決定以設定負載振幅在 工件W上施加反覆負載用之伺服馬達12的旋轉軸之角 度變動的上限值與下限值。亦即,分別將正方向侧之設 定負載振幅設為PSP,將負方向側之設定負載振幅設為 PSN,並將伺服馬達12之旋轉軸的角度變動之上限值與 下限值分別設為ΘΡ、ΘΝ,而藉由以下之數式5運算ΘΡ、 ΘΝ。 [數式5] 而後,依據求出之θρ、ΘΝ,以伺服馬達12之旋轉 軸的角度變動滿足前述數式3之方式,藉由變更賦予伺 服放大器20之設定角度Θ,可依據希望之設定負載振 幅,在工件上賦予反覆負載。 【圖式簡單說明】 第一圖係顯示本發明第一實施例之疲勞測試裝置 的概要者。 第二圖係本發明第一實施例之疲勞測試裝置的控 制部之區塊圖。 第三圖係顯示本發明之第一及第二實施例中之伺 16 200925599 服馬達的旋轉軸之角度變動圖。 第四圖係顯示本發明第二實施例之疲勞測試裝置 的概要者。 第五圖係本發明第二實施例之疲勞測試裝置的控 制部之區塊圖。 【主要元件符號說明】 1 疲勞測試裝置 10 裝置本體 12 伺服馬達 20 伺服放大器 30 控制部 31 控制器 33 A/D變換手段 35 操作手段 37 軟碟驅動器(FDD) W 工件 17PD - PB N ΘΌ - ΘΒ Next, based on the measured SP and SN, the upper limit and the lower limit of the angular variation of the rotational axis of the servo motor 12 for applying the load to the workpiece W are determined by setting the load amplitude. In other words, the set load amplitude on the positive side is PSP, the set load amplitude on the negative side is PSN, and the upper and lower limits of the angular variation of the rotational axis of the servo motor 12 are respectively set. ΘΡ, ΘΝ, and ΘΡ, ΘΝ by the following formula 5. [Expression 5] Then, according to the obtained θρ, ΘΝ, the angular variation of the rotation axis of the servo motor 12 satisfies the above Expression 3, and the setting angle 赋予 given to the servo amplifier 20 can be changed according to the desired setting. The load amplitude gives a repetitive load on the workpiece. BRIEF DESCRIPTION OF THE DRAWINGS The first figure shows an outline of a fatigue testing apparatus according to a first embodiment of the present invention. The second drawing is a block diagram of the control unit of the fatigue testing apparatus of the first embodiment of the present invention. The third figure shows an angle variation diagram of the rotation axis of the servo motor of the servo motor of the first and second embodiments of the present invention. The fourth figure shows an overview of the fatigue testing apparatus of the second embodiment of the present invention. Fig. 5 is a block diagram of a control portion of the fatigue testing device of the second embodiment of the present invention. [Explanation of main component symbols] 1 Fatigue test device 10 Device body 12 Servo motor 20 Servo amplifier 30 Control unit 31 Controller 33 A/D converter 35 Operating means 37 Disk drive (FDD) W Workpiece 17

Claims (1)

200925599 七、申請專利範圍: 1. 一種疲勞測試裝置,係藉由伺服馬達而在工件上施加 反覆負載,且具有: 力計測手段,其係計測施加於該工件之力的大 小; 比例常數運算手段,其係使前述伺服馬達之旋轉 軸的旋轉角度振幅逐漸增加而反轉驅動,依據前述伺 服馬達之旋轉角度及前述力計測手段的計測結果,運 算施加於該工件之力與前述伺服馬達之旋轉軸的旋 © 轉角度之比的比例常數;及 控制手段,其係依據藉由前述比例常數運算手段 所運算之比例常數,控制前述伺服馬達,使施加於該 工件之力的大小之振幅成為指定之大小。 2. 如申請專利範圍第1項之疲勞測試裝置,其中前述比 例常數運算手段係依據前述伺服馬達之旋轉軸的角 度變動概略停止時的前述伺服馬達之旋轉軸的旋轉 角度及前述力計測手段之計測結果,來運算該比例常 數。 ® 3.如申請專利範圍第1項之疲勞測試裝置,其中前述力 計測手段至少計測2次施加於該工件之力的大小, 前述比例常數運算手段將第一次計測時之前述 伺服馬達的旋轉軸之旋轉角度與第二次計測時之前 述伺服馬達的旋轉軸之旋轉角度之差除第一次計測 時之力的大小與第二次計測時之力的大小之差的 值,作為該比例常數。 4.如申請專利範圍第1項之疲勞測試裝置,其中前述疲 勞測試裝置可沿著第一方向以及與該第一方向相反 之第二方向兩者,而在該工件上施加負載, 18 200925599 前述比例常數運算手段運算該工件在該第一方 向變形時之第一比例常數,與該工件在該第二方向變 形時之第二比例常數, 前述控制手段控制前述伺服馬達,於該工件在第 一方向變形時,將以該第一比例常數除該指定之大小 而獲得之變形量成為該工件變形量之上限,並控制前 述伺服馬達,於該工件在第二方向變形時,將以該第 二比例常數除該指定之大小而獲得之變形量成為該 工件變形量之上限。 ❹ 5.如申請專利範圍第1項之疲勞測試裝置,其中前述疲 勞測試裝置係在該工件上施加扭力負載之扭力測試 裝置, 且施加於該工件之力係該工件之旋轉軸周圍的 力矩。 6.如申請專利範圍第1項之疲勞測試裝置,其中前述疲 勞測試裝置係經由進給螺絲機構,而在該工件上施加 拉伸、壓縮或彎曲負載的萬能測試裝置, 且施加於該工件之力係施加於該工件之負載的 ® 該進給螺絲機構的進給方向成分。 19200925599 VII. Patent application scope: 1. A fatigue testing device, which applies a reverse load on a workpiece by a servo motor, and has: a force measuring means for measuring the magnitude of a force applied to the workpiece; The driving angle of the rotating shaft of the servo motor is gradually increased and the driving is reversed. The rotation of the servo motor and the measurement result of the force measuring means are used to calculate the force applied to the workpiece and the rotation of the servo motor. a proportionality constant of a ratio of a rotation angle of a shaft; and a control means for controlling the servo motor based on a proportionality constant calculated by the proportional constant calculation means to specify an amplitude of a force applied to the workpiece The size. 2. The fatigue test apparatus according to claim 1, wherein the proportional constant calculation means is based on a rotation angle of the rotation axis of the servo motor when the angular rotation of the rotation axis of the servo motor is substantially stopped, and the force measurement means The measurement result is used to calculate the proportionality constant. 3. The fatigue testing device according to claim 1, wherein the force measuring means measures the magnitude of the force applied to the workpiece at least twice, and the proportional constant calculating means rotates the servo motor in the first measurement. The ratio of the difference between the rotation angle of the shaft and the rotation angle of the rotation axis of the servo motor in the second measurement is the difference between the magnitude of the force at the time of the first measurement and the magnitude of the force at the second measurement. constant. 4. The fatigue testing device of claim 1, wherein the fatigue testing device is capable of applying a load on the workpiece along both the first direction and a second direction opposite the first direction, 18 200925599 The proportional constant calculation means calculates a first proportional constant of the workpiece when deformed in the first direction, and a second proportional constant when the workpiece is deformed in the second direction, and the control means controls the servo motor to be in the first When the direction is deformed, the deformation amount obtained by dividing the first proportional constant by the specified size becomes the upper limit of the deformation amount of the workpiece, and controls the servo motor, and when the workpiece is deformed in the second direction, the second The amount of deformation obtained by dividing the proportional constant by the specified size becomes the upper limit of the amount of deformation of the workpiece. 5. The fatigue testing device of claim 1, wherein the fatigue testing device is a torsion testing device that applies a torsional load on the workpiece, and the force applied to the workpiece is a moment around a rotating shaft of the workpiece. 6. The fatigue testing device of claim 1, wherein the fatigue testing device applies a universal testing device for tensile, compressive or bending loads on the workpiece via a feed screw mechanism, and applies to the workpiece. The force applied to the load of the workpiece is the feed direction component of the feed screw mechanism. 19
TW97137660A 2007-10-01 2008-10-01 Fatigue testing device TW200925599A (en)

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KR101329648B1 (en) 2012-01-04 2013-11-14 주식회사 엠브로지아 Fatigue testing apparatus
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