TW200902971A - Universal testing machine, linear actuator and torsion testing machine - Google Patents

Universal testing machine, linear actuator and torsion testing machine Download PDF

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Publication number
TW200902971A
TW200902971A TW097114106A TW97114106A TW200902971A TW 200902971 A TW200902971 A TW 200902971A TW 097114106 A TW097114106 A TW 097114106A TW 97114106 A TW97114106 A TW 97114106A TW 200902971 A TW200902971 A TW 200902971A
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Taiwan
Prior art keywords
servo motor
feed screw
fixed
drive shaft
shaft
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TW097114106A
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Chinese (zh)
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TWI428595B (en
Inventor
Sigeru Matsumoto
Hiroshi Miyashita
Kazuhiro Murauchi
Masanobu Hasegawa
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Kokusai Keisokuki Kk
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Priority claimed from JP2007110134A external-priority patent/JP2008267939A/en
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Publication of TW200902971A publication Critical patent/TW200902971A/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
    • G01N3/02Details
    • 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
    • G01N3/34Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces generated by mechanical means, e.g. hammer blows
    • 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
    • G01N3/08Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
    • 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
    • G01N3/26Investigating twisting or coiling properties

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  • Physics & Mathematics (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)
  • Transmission Devices (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

In a general-purpose test device and a linear actuator which drive a cross head by a servo motor and a feed screw mechanism, the servo motor and a linear guide of the feed screw mechanism are fixed to a single support plate. It is preferable that a drive shaft of the servo motor be coupled to the feed screw by a rigid coupling or a semi-rigid coupling. Moreover, in a twist test device which applies a twist load to a test piece by the servo motor and a speed reduction mechanism, both of the servo motor and the speed reduction mechanism are fixed to a first support member as a single member. It is preferable that a drive shaft of the servo motor be coupled to an input shaft of the speed reduction mechanism by the rigid coupling or the semi-rigid coupling.

Description

200902971 九、發明說明: 【發明所屬之技術領域】 本發明係關於一種通用測試機台、適於該通用測試 機台之線性驅動器及扭力測試機台。 【先前技術】 以往,為了評估材料及構造物的強度、剛性等,係 利用在材料等上施加拉伸、壓縮及/或彎曲應力的材料 測試機台。此種材料測試機台,一般而言稱為通用測試 機台。通用測試機台例如記載於日本特開第 2003-106965號及日本特開第2003-90786號(均納入曰 本公開專利公報中)的機台。 記載於日本特開第2003-106965號及日本特開第 2003-90786號之通用測試機台,具有:固定於機台框架 之固定部、對機台框架可在指定方向(如上下方向)移 動地構成之十字頭、及用於使該十字頭移動之驅動裝 置。拉伸測試係將測試片之一端固定於固定部,將另一 端固定於十字頭,藉由驅動十字頭於從固定部離開之方 向而進行。此外,壓縮測試係在十字頭與固定部夾著測 試片之狀態下,藉由將十字頭以接近固定部之方式驅動 而進行。彎曲測試如以固定部或十字頭之一方兩點支撐 測試片,以另一方一點支撐測試片,將十字頭以接近於 固定部之方式驅動而進行(三點彎曲測試)。 驅動通用測試機台之十字頭的驅動裝置,例如有記 載於日本特開第2003-106965號之電動式線性驅動器, 及記載於日本特開第2003-90786號之油壓式線性驅動 器等。使用油壓式線性驅動器之測試機台係構成藉由使 用泵將高壓工作油送入油缸之裝置,或是從油缸除去工 200902971 作油之策置等,而驅動聯結於十字頭之油缸。如 為油壓式線性驅動器係藉由油壓缸直接驅動十 者以反應延遲小,可輕易以高似希望之振動波= 使十字頭振動,可以短時間進行疲勞測試。反之 ^ 油壓式線性驅動ϋ之测試機台在使用中存在因 沒漏及油霧等射周邊環境污_、岐置工作油槽導致 設備大型化、因驅動器定期維修及工作油更換而產生營 運成本增大及大畺消耗天然資源、及泵產生噪音的問 題。200902971 IX. INSTRUCTIONS: TECHNICAL FIELD The present invention relates to a universal testing machine, a linear driver and a torque testing machine suitable for the universal testing machine. [Prior Art] Conventionally, in order to evaluate the strength and rigidity of materials and structures, a material testing machine for applying tensile, compressive, and/or bending stress to materials or the like has been used. This type of material testing machine is generally referred to as a universal test machine. A general-purpose test machine is described, for example, in a machine that is described in Japanese Laid-Open Patent Publication No. 2003-106965 and Japanese Patent Laid-Open No. 2003-90786 (both incorporated herein by reference). The universal testing machine described in Japanese Laid-Open Patent Publication No. 2003-106965 and Japanese Patent Laid-Open No. 2003-90786 has a fixing portion fixed to the machine frame, and can move in a specified direction (upward direction) to the machine frame. A crosshead formed by the ground and a driving device for moving the crosshead. The tensile test is to fix one end of the test piece to the fixed portion and the other end to the crosshead, by driving the crosshead in a direction away from the fixed portion. Further, the compression test is performed by driving the crosshead close to the fixed portion in a state where the crosshead and the fixed portion sandwich the test piece. The bending test is performed by supporting the test piece at one of two points of the fixed portion or the crosshead, supporting the test piece at the other point, and driving the crosshead in a manner close to the fixed portion (three-point bending test). For example, there is an electric linear actuator that is described in Japanese Laid-Open Patent Publication No. 2003-106965, and a hydraulic linear actuator described in Japanese Laid-Open Patent Publication No. 2003-90786. The test machine system using the hydraulic linear actuator constitutes a cylinder that is coupled to the crosshead by using a pump to feed the high-pressure working oil into the cylinder, or by removing the cylinder from the cylinder. For example, the hydraulic linear actuator is driven directly by the hydraulic cylinder to have a small reaction delay, and the vibration wave can be easily oscillated with high hopeful vibrations. The fatigue test can be performed in a short time. On the other hand, the test machine of the hydraulic type linear drive 在 has the use of the surrounding environment due to no leakage and oil mist, and the operation of the oil sump causes the equipment to be enlarged, and the operator is regularly repaired and the working oil is replaced. The cost increases and the consumption of natural resources and the noise generated by the pump.

電動式線性驅動器使用例如記載於日本特開第 2:〇3_'。6965产之細進給螺桿機構。因為進給螺桿機 才可ίτ易承文大負载,且精確地移動驅動對象,所以, 其他電動式驅動11 (採用線性馬達及齒輪齒條 機構者)比較,適於通用測試機台。 動二驅動機構之電動式線性驅 構即可驅動衫M _式娜馬達與進給螺桿機 型果之碩,所以,可以說與需要工作油槽及大 境的負擔!^驅動器的测試機台比較,在對機台周圍環 勢。、s、呂運成本、及測試機台小型化等方面具有優 剛性^外係為了評估長條狀構件之指定轴周圍的強度、 扭力測气邊=代通用測試機台,而使用扭力測試機台。 周圍的扭矩Γ係在兩端支撐測試片,在一端施加支撐軸 記載於日本护而扭ΐ專測試片者。此種扭力測試機台如有 之機台。寸開平第10·2746〇9號(曰本公開專利公報) 载於日本特開平第10-274609號之扭力測試機台 6 200902971 係在基座上固定框架,在該框架之水平面上設有一對支 撐構件(在垂直方向擴大之板狀構件)。各支撐構件中 安裝有用於在兩端把持測試片的卡盤。安裝於一方支撐 構件的卡盤經由減速機構及聯結器而與伺服馬達之驅 動軸聯結。此外,安裝於另一方支撐構件之卡盤與支撐 構件成為一體,藉由把持測試片之一端,而固定於另一 方之支撐構件。因此,藉由驅動伺服馬達,可扭轉被卡 盤把持之測試片。 一般而言,伺服馬達適合以低扭矩且高速地使驅動 軸旋轉。另外,扭力測試機台中,須以高扭矩且較低速 扭轉測試片。因而,使用伺服馬達之扭力測試機台中, 可在伺服馬達之驅動軸與卡盤之間設置蝸輪等之減速 機構,進行使用伺服馬達之高扭矩的扭力測試。 一種使用上述通用測試機台及扭力測試機台而一 般性進行的測試,例如疲勞測試。所謂疲勞測試,係在 測試片上反覆施加負載(應變),計測直到測試片破損 的周期次數等者。此種疲勞測試中,為了可在短時間完 成測試,須儘可能增加每單位時間之反覆負載的周期次 【發明内容】 (發明所欲解決之問題) 如前述,使用進給螺桿機構之通用測試機台需要聯 結伺服馬達之驅動軸與進給螺桿。同樣地,扭力測試機 台需要聯結伺服馬達之驅動軸與減速機構之輸入軸。一 般而言,聯結進給螺桿或減速機構之輸入軸與伺服馬達 的驅動軸時,需要將聯結之兩軸高度精確地定位(定 7 200902971 心)。但是,以通常之加工 之誤差)製作時,在伺服及組合精度(如±1〇〇μηι程度 產生無法忽略程度的輛偏^達之驅動軸與進給螺桿之間 由高剛性材料所形成之剛二(,心或偏角)。因而,以 生大的彎曲應力,而無 聯、、、。器聯結兩軸時,軸上發 轴平滑地旋皁專。因❿,弁_進給螺桿及減速機構之輪 機台中’係藉由可吸收輛測試機台或挺力挪 驅動轴。軟性二 ==輪入軸與飼服 前述之f曲應力,而可將接頭,藉由彈性體J 之旋如轉,滑地傳達== 之聯結器,所以除了 f:; = :由,體而傳、 扭矩。使用軟性聯結器卜’亦吸收某種程度J 器時,以高周期來回旋轉運動輸不太高之聯結 f:時,聯結器無法追隨輪入軸4』=卜轉 時,無法使輸出軸以高周期來回旋轉運t與輪出細 如此,耩由電動伺服馬達與 t回之通用測試機台中,無法高周期忿 地施予測試片。因而1前無法以使用進給二正確 通用測試機台在短時間進行疲勞測試,此種用、樽之 使用油壓驅動機構之通用測試機台。同樣地,=只能 機而將測試>;之1連接於而馬達的=滅迷 無法在短時間進行疲勞測試。 ㊇成機台 (解決問題之骏置) 本發明係為了解決上述問題。亦即,本發明 之目的 200902971 t提,一種可進行高精確度之組合,藉由使用高剛性 ,結器,可以高反覆速度將負載施加於測試片之 = 試機台、扭力測試機台、及可適用於此種通用測試機: 之電動式驅動器。 為了解決上述問題,本發明之通用測試機台及 式驅動器,在支撐板上固定有伺服馬達及線性導軌: 此,伺服馬達及線性導軌將支撐板作為基準,而直二 裝於支撐板上,將各構件以相對高精確度定位,: 高位置精確度容易。 、、隹持 此外,本發明之扭力測試機台具有:框架,政 定於機台之基座上;伺服馬達;減速機構;聯結’器j 係聯結減速機構之輪入軸與前述伺服馬達之驅動 ^ 一把持部,其係把持固定於減速機構之輸出軸的測讀= 之一端,第二把持部,其係把持固定於框架之測= 另一端;及第一支撐構件,其係固定於框架上,' 的 定伺服馬達及減速機構。藉此,藉由將第一支撐固 \ 為基準而安裝伺服馬達及減速機構,容易確保^構件2 精確度。 【實施方式】 =下,就本發明之實施例,使用圖式加以詳細說 明。第一圖係本發明第一實施例之通用測試機台的前視 圖。如第一圖所示,本實施例之測試機台i中設有··固 定於基座B之機台框架部10,與測試片之上端(或是安 裝於測試片上部之失具)抵接的固定部2〇,及與測試片 之下部(或是安裝於測試片下部之失具)抵接的邛移動 部 30。 '、 9 200902971 本實施例中,機台框架10具有:從基座B概略垂 直方向朝上延伸之一對腳部11,從該腳部11之各個上 端概略垂直方向朝上延伸之一對導桿12,及以聯結兩導 桿12之上端的方式而設置的頂部13。 在頂部13之概略中央部設有貫穿孔13a。該貫穿孔 13a中插通有使固定部20在上下方向移動用之進給螺桿 22。在頂部13之上設有與進給螺桿22卡合之螺母23a。 符號24a係可轉動地支撐螺母23a用的逕向滚珠軸承。 此外,逕向滾珠轴承24a之外輪嵌入以無圖示之螺栓固 定於頂部13之上面的軸承支撐部24b,且兩者成為一 體。同樣地,螺母23a嵌入逕向滾珠軸承24a之内輪而 兩者成為一體。因而,螺母23a可對軸承支撐部24b旋 轉,不過無法在螺母23a之上下方向及逕向方向移動。 因此,使螺母23a旋轉時,與螺母23a卡合之進給螺桿 22在上下方向移動。 在頂部13之上配置有用於驅動螺母23a之馬達 25。馬達25之驅動軸25a被收納於齒輪盒26内。齒輪 盒26係具有用於將輸入軸(馬達25之驅動轴25a)之 旋轉減速,而傳達於輸出軸26a之熟知的齒輪機構之構 件。如第一圖所示,齒輪盒26之輸出轴從齒輪盒26之 下端垂直朝下地延伸。亦即,齒輪盒26具有將延伸於 水平方向之驅動軸25a的旋轉運動轉換成延伸於垂直方 向之輸出軸26a的旋轉運動之功能。 齒輪盒26之輸出軸26a上安裝有主動皮帶輪26b。 此外,在螺母23a上安裝有從動皮帶輪23b。主動皮帶 輪26b與從動皮帶輪23b上架設無端皮帶27,主動皮帶 輪26b之旋轉經由無端皮帶27而傳達至從動皮帶輪 200902971 23b。 因此’藉由驅動馬達25而使馬達25之驅動軸25a 旋轉,可使螺母23a旋轉,並使進給螺桿22上下移動。 在進給螺桿22之下端懸掛固定部2〇之上部載台 21。在上部載台21之圖中左右兩端形成有延伸於上^ 方向之貫穿孔2U。在該貫穿孔2la中插通有導桿12。 因此,上部載台21之移動方向僅限定於上下方白。 在固定部20之上部載台21的时左右方°向兩端 (比貫穿孔2la外侧之位置)形成有在水平方向(圖中 從表面向背面之方向)穿孔之螺栓孔21b。從貫穿孔21& 之側面向上部載台21之圖中左右方向外侧擴大,而盥 螺栓孔21b正交之切槽狀的長孔形成於上部載台21,^ 過第-圖中並未圖示。因此’在螺拴孔m中插 21c而旋緊時,貫穿孔21a之直徑變小,貫穿孔仏 内周面爽住導桿I2。結果,上部載台固定於導。 此外’從該狀態旋鬆螺栓21c時,可驅動馬達乃而 部載台21上下移動。 —使用進行以上說明之上部載台21的上下移動及固 疋之機構,係為了因應測試片之 :,。與可移動部30之間距。另外,測:而 ΪΪΓ傳唯由導桿12支撐,試而發生之負載幾 23a、也向滾珠輪承-及軸 口 1The electric linear actuator is described, for example, in Japanese Patent Laid-Open No. 2: 〇 3_'. The fine feed screw mechanism produced by 6965. Because the feed screw machine can load large loads and accurately move the drive object, other electric drives 11 (using linear motors and rack and pinion mechanisms) are suitable for general-purpose test machines. The electric linear drive of the second drive mechanism can drive the M-type motor and the feed screw model, so it can be said that it requires a working oil tank and the burden of the environment! ^ The test bench of the drive is compared to the ring around the machine. , s, Lu Yun cost, and test machine miniaturization, etc. have excellent rigidity ^ external system in order to evaluate the strength around the specified shaft of the long strip member, torsion test gas side = generation universal test machine, and use the torque test machine station. The surrounding torque is supported at both ends by a test piece, and a support shaft is applied at one end. Such a torque test machine has a machine. 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 Support member (plate member that expands in the vertical direction). A chuck for holding the test piece at both ends is mounted in each of the support members. The chuck attached to one of the support members is coupled to the drive shaft of the servo motor via a speed reduction mechanism and a coupler. Further, the chuck attached to the other supporting member is integrated with the supporting member, and is fixed to the other supporting member by holding one end of the test piece. Therefore, by driving the servo motor, the test piece held by the chuck can be twisted. In general, the servo motor is adapted to rotate the drive shaft with low torque and high speed. In addition, in the torque test machine, the test piece must be twisted at a high torque and at a lower speed. Therefore, in the torque test machine using the servo motor, a speed reduction mechanism such as a worm wheel can be provided between the drive shaft of the servo motor and the chuck to perform a high torque torque test using the servo motor. A test that is generally performed using the above-described universal test machine and torque test machine, such as fatigue test. In the so-called fatigue test, the load (strain) is applied repeatedly on the test piece, and the number of cycles until the test piece is broken is measured. In such a fatigue test, in order to complete the test in a short time, it is necessary to increase the cycle time of the repeated load per unit time as much as possible [Inventive content] (Problems to be solved by the invention) As described above, the universal test using the feed screw mechanism The machine needs to connect the drive shaft of the servo motor with the feed screw. Similarly, the torque test machine needs to couple the drive shaft of the servo motor with the input shaft of the speed reduction mechanism. In general, when coupling the input shaft of the feed screw or reduction mechanism to the drive shaft of the servo motor, it is necessary to accurately position the two axes of the coupling (set 7 200902971 hearts). However, when it is produced by the usual processing error, the servo and the combination precision (such as ±1〇〇μηι) can be made of a highly rigid material between the drive shaft and the feed screw which are not negligible. Just two (, heart or declination). Therefore, in the case of large bending stress, and without the coupling, the two axes of the coupling, the shaft on the shaft smoothly spins the soap. Because ❿, 弁 _ feed screw And the engine platform of the speed reduction mechanism 'by the absorbable test machine or the force to move the drive shaft. Soft two == wheel and shaft feeding the aforementioned f-bend stress, and the joint can be made by the elastic body J Rotate and sleekly convey the == coupling, so except for f:; = : by, body, torque. Use soft couplings to absorb some degree of J, and rotate back and forth with high cycle When the coupling f is not too high, the coupling cannot follow the wheel into the shaft 4 』= When turning, the output shaft cannot be rotated back and forth in a high cycle, and the wheel is fine. This is common to the electric servo motor and t-turn. In the test machine, the test piece cannot be applied in a high cycle. Use the feed two correct universal test machine to perform the fatigue test in a short time. This type of test machine uses the universal test machine of the hydraulic drive mechanism. Similarly, the test can only be connected to the test. However, the motor====================================================================================================== The combination, by using high rigidity, the knotter, can apply the load to the test piece at a high repetitive speed = test machine, torque test machine, and electric drive that can be applied to such a universal test machine: In the above problem, the universal test machine and the drive of the present invention have a servo motor and a linear guide fixed on the support plate: the servo motor and the linear guide use the support plate as a reference, and the straight two are mounted on the support plate, The component is positioned with relatively high precision, and the position accuracy is easy. In addition, the torque testing machine of the present invention has a frame, which is fixed on the base of the machine; a motor; a speed reduction mechanism; a coupling shaft of the coupling mechanism of the speed reduction mechanism and a driving portion of the servo motor, which is held at one end of the output shaft of the speed reduction mechanism, and the second holding portion. It is fixed to the frame of the test = the other end; and the first support member is fixed to the frame, the fixed servo motor and the speed reduction mechanism. Thereby, the servo is mounted by using the first support as a reference The motor and the speed reduction mechanism are easy to ensure the accuracy of the member 2. [Embodiment] = The following is a detailed description of the embodiment of the present invention, which is a general testing machine of the first embodiment of the present invention. As shown in the first figure, the test machine table i of the present embodiment is provided with the machine frame portion 10 fixed to the base B, and the upper end of the test piece (or the upper portion of the test piece). The fixed portion 2A that abuts and the moving portion 30 that abuts against the lower portion of the test piece (or the missing piece attached to the lower portion of the test piece). ', 9 200902971 In the present embodiment, the machine frame 10 has a pair of leg portions 11 extending upward from a substantially vertical direction of the base B, and a pair of guides extending upward from a substantially vertical direction of the upper ends of the leg portions 11 The rod 12 and the top portion 13 are provided in such a manner as to join the upper ends of the two guide rods 12. A through hole 13a is provided in a schematic central portion of the top portion 13. The feed screw 22 for moving the fixing portion 20 in the vertical direction is inserted into the through hole 13a. A nut 23a that engages with the feed screw 22 is provided above the top portion 13. Reference numeral 24a is a radial ball bearing for rotatably supporting the nut 23a. Further, the outer ring of the radial ball bearing 24a is fitted to the bearing support portion 24b fixed to the upper portion 13 by a bolt (not shown), and the two are integrally formed. Similarly, the nut 23a is fitted into the inner ring of the radial ball bearing 24a and the two are integrated. Therefore, the nut 23a can rotate the bearing support portion 24b, but cannot move in the downward direction and the radial direction of the nut 23a. Therefore, when the nut 23a is rotated, the feed screw 22 engaged with the nut 23a moves in the vertical direction. A motor 25 for driving the nut 23a is disposed above the top portion 13. The drive shaft 25a of the motor 25 is housed in the gear case 26. The gear case 26 has a member for decelerating the rotation of the input shaft (the drive shaft 25a of the motor 25) and transmitting it to the well-known gear mechanism of the output shaft 26a. As shown in the first figure, the output shaft of the gear case 26 extends vertically downward from the lower end of the gear case 26. That is, the gear case 26 has a function of converting the rotational motion of the drive shaft 25a extending in the horizontal direction into the rotational motion of the output shaft 26a extending in the vertical direction. A drive pulley 26b is mounted on the output shaft 26a of the gear case 26. Further, a driven pulley 23b is attached to the nut 23a. The endless belt 27 is erected on the drive pulley 26b and the driven pulley 23b, and the rotation of the drive pulley 26b is transmitted to the driven pulley 200902971 23b via the endless belt 27. Therefore, by rotating the drive shaft 25a of the motor 25 by the drive motor 25, the nut 23a can be rotated and the feed screw 22 can be moved up and down. The upper stage 21 of the fixing portion 2 is suspended at the lower end of the feed screw 22. In the upper and lower ends of the upper stage 21, a through hole 2U extending in the upper direction is formed. A guide rod 12 is inserted into the through hole 21a. Therefore, the moving direction of the upper stage 21 is limited only to the upper and lower sides. Bolt holes 21b that are perforated in the horizontal direction (the direction from the front surface to the back surface in the drawing) are formed at both ends in the right and left directions of the upper stage of the fixing portion 20 (the position outside the through hole 21a). The side surface of the through hole 21 & is enlarged to the outside in the left-right direction in the figure of the upper stage 21, and the slotted long hole orthogonal to the bolt hole 21b is formed in the upper stage 21, and is not shown in the figure - Show. Therefore, when the screw hole m is inserted into the screw hole m and tightened, the diameter of the through hole 21a becomes small, and the inner peripheral surface of the through hole 爽 cools the guide rod I2. As a result, the upper stage is fixed to the guide. Further, when the bolt 21c is loosened from this state, the motor can be driven and the stage 21 can be moved up and down. - The mechanism for performing the up-and-down movement and the fixing of the upper stage 21 as described above is used in response to the test piece. The distance from the movable portion 30. In addition, the test: and the rumor is only supported by the guide rod 12, the load of the test occurs 23a, also to the ball bearing - and the shaft 1

上部載”1之重量的程度即可U 、晶二二之間距時,雖可精確地驅動進給螺桿,不 刀之強度降低。但是,本實施例中,因為大幅 超過上部載台21重量之負載不致施加於進給螺桿及^ 200902971 母,所以採用問, ^ HI 20鱼小之進給螺桿及螺母,可精確地調整 固疋'20與可,部3〇之間隔。 把持二片之下部安裝有於拉伸測試時 Π牛28。該附件28中内藏負載傳感器 ⑽σ於剛試時計測施加於測試片之負載。另 二載:21 2專下感Α作為與附件獨立之構件時,亦可在上 = 安裝負載傳感器,進—步將附件28安 裝於負載傳感器之下部而構成。 ^'ATm 0 f 接而固定工作台33。圖:! U之上藉由焊 的下邱入闲悝垃认體而§,工作台33之侧面33a 的下心肋接於腳部上面 33之下面33b與腳部n + 儿且坪接工作口 33經由腳部η而剛體支=側面Ub。藉此’工作台 工作…it,第一圖)。 測試時,_加於^^ 充分大_板,且在 κ 在該工作台33之下,經tt3G之負载實質地視為剛體。 祠服馬達35。如圖在、、、達撐框架37而固定有AC 有複數肋條37a。而後,|^達支撐框架37之側壁形成 37a的上端與工作台%错由將馬達支撐框架37及肋條 馬達支撐框架37 “ ^面2焊接’卫作台33與 馬達35係本發明群獨而一體化。此外,該AC祠服 輸出AC伺服馬達,择^之可而速反轉運動的高 低内部之慣性,可以最9大、/先前之AC伺服馬達大幅減 回旋轉運動。 建500Hz之反覆率使驅動轴來 此外’在工作台幻之上配置有藉由AC舰馬達 12 200902971 35而可在上下方向移動地構成的下部載台31。 一由下部載台31、經由剛性聯結器34而聯結於Ac 伺服馬達35之驅動軸35a的滾珠螺桿36、及線性導執 4〇構成進給螺桿機構。線性導軌係將下部載台31之 移動方向j堇限制在上下方向而導引的元件。線性導軌4〇 具有:導引框42、一對執道44及移動塊牝。導引框“ 糟由螺栓等而固定於工作台33之上面33c。導引框42 於垂直方向之一對側壁42a,以及在上端聯 二各側壁42a之上部壁面42b ’全體成為倒u字狀的形 42a内4係延伸於垂直方向的軌道,且較於側壁 裁Mi 此外’各—個移動塊46分別固定於下部 入°心二中左右兩端,且與其各個對應之軌道44卡 :=移動,46之移動係藉由執道44導引,因此; 邛載口 31之移動方向僅限定於上下方向。 J I3載口 31藉由滾珠螺桿機 二 部埋入具備滾珠循環二 螺桿36上部之螺;旱部t螺二用:母4?形成於滚珠 31藉由線性導執4 〇導引,:述,由於下部載台 因此使滾珠,6二,; ’與滾珠螺桿用螺母叫-體化之下 該開口部42c,其上端之+ —邛42c。下部載台31貫穿 42b上側。因此,下部心於比上部壁面 部载台21之附件28十字碩3〗b與安裝於上 相對。於拉伸測試時,測試片經由 200902971 卡盤而安裝於十字頭31b。此外,於壓縮、彎曲測試時, 測試片或夾具被放置於十字頭31b上。 滾珠螺桿36之下部成為軸部36b,其並未形成用於 與滾珠絲槓用螺母31a卡合之溝。該軸部36b經由剛性 聯結器34而聯結於AC伺服馬達35之驅動軸35a。本 實施例之剛性聯結器34係構成滚珠螺桿36之軸部36b 周圍(亦即AC伺服馬達35之驅動轴35a周圍)的扭力 剛性極高,而可以高度反應性將施加於AC伺服馬達乃 之驅動軸35a的扭矩傳達至滾珠螺桿36,不過其詳細 成於後述。 —其次’就阶!·生聯結器34之構造作說明 顯示剛性聯結器34及细山口你 之AC飼服馬達性f、=34而彼此聯結 36b的放大剖面圖乾動轴祝與滾珠螺桿36之轴部 為中形之齡請全體成 亦即,筒狀本體3Π·亦即,階梯形厚度之圓筒)。 之軸部36b W上部開D、A .具備從上插入滾珠螺桿36 備從下插入AC伺服V^34C的上部圓筒部%,及具 撕之下部圓筒部=達^之驅動軸祝的下部開口部 之轴部36b的直^ tbA^本貝施例巾’由於滾珠螺桿36 因此,上部圓筒;34=服馬,35之挪 小。 34a之外徑比下部圓筒部34b之外經 之上ί:別筒部、之下部及下部圓筒部 35之驅動軸35at t 軸/娜及AC伺服馬達 的罝乜概略相等。因而,在狹窄部 200902971 及3奸之内周面、以及滚珠螺桿36之軸部36b與AC伺 服馬達35之驅動軸35a的外周幾乎無間隙的狀態下,滾 珠螺桿36之軸部36b與AC伺服馬達35之驅動軸35a 被收容於狹窄部34e及34f。 上部開口部34c及下部開口部34d之直徑構成分別 比滚珠螺桿36之軸部36b及AC伺服馬達35之驅動軸 的外位大。為了將上部開口部34c及下部開口部34d 分別固定於滾珠螺桿36之軸部3沾及Ac伺服馬達35 之驅動軸35a ’而使用固定用環及14〇。 固疋用環130具有·内輪132、外輪134及螺栓136。 内輪132之外周面132a成為直徑朝下而變小之錐形面。 =二之内周面咖成為比滾珠螺桿36之軸 部36b的外徑稍大程度之圓筒面。在内輪 成1擴大於半徑方向外侧的凸緣部1奴。凸緣部mc 中設有複數個在上下方向插$ 、’When the weight of the upper load "1" is U and the distance between the crystals and the second is small, although the feed screw can be accurately driven, the strength of the non-knife is lowered. However, in this embodiment, since the weight of the upper stage 21 is significantly exceeded The load is not applied to the feed screw and ^200902971 mother, so the request, ^ HI 20 fish small feed screw and nut, can accurately adjust the solid 疋 '20 and can be, the interval between the 3 。. The yak 28 is installed during the tensile test. The load sensor (10) σ is included in the attachment 28 to measure the load applied to the test piece at the time of the test. The other two load: 21 2 special sensation as a separate component from the attachment, It can also be installed on the upper = install load sensor, and then attach the attachment 28 to the lower part of the load sensor. ^'ATm 0 f Connect and fix the workbench 33. Fig.: U above the U.下 认 认 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , 'Workbench work...it, first picture.) When testing, _added to ^^ _ plate, and under κ under the table 33, the load by tt3G is substantially regarded as a rigid body. The motor 35 is attached to the frame 37, and the AC has a plurality of ribs 37a. The upper end of the side wall forming 37a of the support frame 37 is offset from the table by the motor support frame 37 and the rib motor support frame 37. The "face 2 welding" table 33 and the motor 35 are integrated into the present invention. . In addition, the AC servo output AC servo motor can select the high and low internal inertia of the reverse speed, which can greatly reduce the rotary motion of the 9th/previous AC servo motor. A repetition rate of 500 Hz is established to drive the drive shaft. Further, a lower stage 31 which is configured to be movable in the vertical direction by the AC ship motor 12 200902971 35 is disposed on the table top. A ball screw 36 and a linear guide 4 that are coupled to the drive shaft 35a of the Ac servo motor 35 via the rigid coupling 34 via the lower stage 31 constitute a feed screw mechanism. The linear guide is an element that guides the movement direction j of the lower stage 31 to the upper and lower directions. The linear guide 4 has a guide frame 42, a pair of obstructions 44, and a moving block 牝. The guide frame is fixed to the upper surface 33c of the table 33 by bolts or the like. The guide frame 42 is in the vertical direction, the pair of side walls 42a, and the upper end side wall 42a upper wall surface 42b are all inverted. In the shape 42a, the 4 series extends in the vertical direction of the track, and is smaller than the side wall. In addition, each of the moving blocks 46 is fixed to the left and right ends of the lower part of the center, and the corresponding track 44 is: The movement of 46 is guided by the obstruction 44. Therefore, the moving direction of the load port 31 is limited to the up and down direction. The J I3 carrier 31 is embedded in the upper part of the ball screw machine 36 by the ball screw machine. The snail; the dry part of the t screw: the mother 4? is formed on the ball 31 by the linear guide 4 〇 guide: said, because the lower stage thus makes the ball, 6 two; 'with the ball screw nut called - The opening portion 42c has an upper end of the opening 42c. The lower stage 31 penetrates the upper side of the 42b. Therefore, the lower core is more than the attachment 28 of the upper wall surface stage 21 and is mounted on the upper side. During the tensile test, the test piece is mounted on the ten via the 200902971 chuck. Further, in the compression and bending test, the test piece or the jig is placed on the crosshead 31b. The lower portion of the ball screw 36 becomes the shaft portion 36b which is not formed to be engaged with the ball screw nut 31a. The shaft portion 36b is coupled to the drive shaft 35a of the AC servo motor 35 via the rigid coupling 34. The rigid coupling 34 of the present embodiment is formed around the shaft portion 36b of the ball screw 36 (i.e., the drive of the AC servo motor 35). The torque around the shaft 35a is extremely high, and the torque applied to the AC servomotor or the drive shaft 35a can be transmitted to the ball screw 36 with high reactivity, but the details are as follows. - Secondly, the order is! The structure of the device 34 is shown in an enlarged cross-sectional view showing the rigid coupling 34 and the fine Yamaguchi AC clothing motor f, = 34 and the coupling 36b. The axis of the shaft and the shaft of the ball screw 36 are medium-sized. That is, the cylindrical body 3Π, that is, the cylinder having a stepped thickness). The upper portion of the shaft portion 36b W is opened D, A. The upper portion of the ball screw 36 is inserted from above, and the upper portion of the AC servo V^34C is inserted from below. % of the cylinder, and a cylinder with a tear = The diameter of the shaft portion 36b of the lower opening portion of the drive shaft of the drive shaft is as follows: due to the ball screw 36, the upper cylinder; 34 = the service horse, the movement of 35 is small. The drive shaft 35at t-axis/na of the other cylindrical portion, the lower portion, and the lower cylindrical portion 35 are substantially equal to the outer diameter of the lower cylindrical portion 34b, and the AC servo motor is substantially equal to the lower cylindrical portion 34b. Therefore, in the narrow portion 20000221 and The shaft portion 36b of the ball screw 36 and the drive shaft 35a of the AC servo motor 35 are in a state in which the inner peripheral surface of the ball and the shaft portion 36b of the ball screw 36 and the outer circumference of the drive shaft 35a of the AC servo motor 35 have almost no gap. It is accommodated in the narrow portions 34e and 34f. The diameters of the upper opening portion 34c and the lower opening portion 34d are larger than the outer positions of the shaft portion 36b of the ball screw 36 and the drive shaft of the AC servo motor 35, respectively. In order to fix the upper opening portion 34c and the lower opening portion 34d to the shaft portion 3 of the ball screw 36 and the drive shaft 35a' of the Ac servo motor 35, the fixing ring and the 14'' are used. The fixing ring 130 has an inner wheel 132, an outer wheel 134, and a bolt 136. The outer peripheral surface 132a of the inner ring 132 has a tapered surface whose diameter is reduced downward. The inner peripheral surface of the second surface is a cylindrical surface slightly larger than the outer diameter of the shaft portion 36b of the ball screw 36. The inner wheel is made up of a flange portion 1 that is enlarged to the outside in the radial direction. A plurality of flange portions mc are inserted in the vertical direction, $,

此外,外輪m之内周面13=:,之螺则^ 面。外輪W之内周面134=直徑朝下變小之錐形 ⑽相同的錐角。此外,具^内輪I%之内周面 比上部開口部34c之直徑稍;二之外周面134b成為 中,與螺栓孔132d對應而开肉面。再者’外輪134 合之陰螺紋134c。此外,外有複數個與螺栓I36卡 端直獲(最大徑)比内輪132'134之内周* 134a的上 徑(最大禋)小。因而,使U内周面⑽的上端直 放置於外輪U4上時,内輪^隹形面抵接地將内輪132 為與外輪134之上面不接觸而之凸緣部砂的下面成 及内輪U2插入上部開口部^起的狀態。將外輪134 _間的間隙,緊固經由凸C與滾珠螺桿36之軸部 深# 132c之螺栓孔132d而 200902971 插入了陰螺紋134c之螺栓136時,内輪132之錐形面 132b從外輪134之錐形面134a承受半徑方向朝内之 力,内輪132之圓筒面132b強力壓迫滾珠螺桿36之軸 部36b。此外,此時外輪134之錐形面134a從内輪132 之錐形面132b承受半徑方向朝外之力,圓筒面134b強 力壓迫上部開口部34c。滾珠螺桿36之軸部36b藉由該 結果而發生之靜摩擦力,強固地固定於筒狀本體34B之 上部圓筒部34a,兩者形成一體化。另外,圖中分別顯 示各二組之螺栓136、螺栓孔132d及陰螺紋134c,不過, 實際上在將滾珠螺桿36之軸為中心的圓周上設有多數 個(如10組)。 同樣地,固定用環140具有:内輪142、外輪144 及螺栓146。内輪142之外周面142a成為直徑朝上而變 小之錐形面。此外,内輪142之内周面142b成為AC伺 服馬達35之驅動軸35a的外徑稍大程度之圓筒面。在内 輪142之下端形成有擴大於半徑方向外側的凸緣部 142c。凸緣部142c中設有複數個在上下方向插通螺栓 146之螺栓孔142d。外輪144之内周面144a成為直徑朝 上變小之錐形面。此外,外輪144之外周面144b成為 比下部開口部34d之直徑稍小的圓筒面。再者,外輪144 中,與螺栓孔142d對應而形成有複數個與螺栓146卡 合之陰螺紋144c。此外,外輪144之内周面144a的下 端直徑(最大徑)比内輪142之内周面142b的下端直 徑(最大徑)小。因而,使各錐形面抵接地將内輪142 放置於外輪144之下方時,内輪142之凸緣部142c的上 面成為與外輪144之下面不接觸而浮起的狀態。將外輪 144及内輪142插入下部開口部34d與AC伺服馬達35 16 200902971 ===固經由凸緣部-之螺栓孔 錐形面㈣從外輪累栓146時,内輪142之 内之力,内輪142之鬥;,® 144a承受半徑方向朝 35之驅動軸35a 強力壓迫从伺服馬達 從内輪142之錐此外,此時外輪144之錐形面144a 之驅動軸35a藉由,了4=:"4d。AC伺服馬達% 化。另外,圖中分別顧-夂间邛揚,兩者形成一體 及陰螺紋U4c,不:不二螺栓146、螺栓孔142d 驅動軸匕實際上在將AC伺服馬達35之 (如u)^ 轉中"軸為中心的圓周上設有多數個 的厚^地之上部圓筒部^及下部圓筒部34b 剛性與滾:蟫此,剛性聯結器34之連結部的扭力 等戋:复'、f及AC伺服馬達35之驅動軸35a相 = 因此,剛性聯結器34可以高度反應性將 =6 達35之驅動軸3元的扭矩傳達至滾珠 如第二圖所示,在工作纟33之中央設有貫穿孔 二袞珠螺桿36貫穿該貫穿孔33d。本實施例中,於 為了可旋轉地支樓承受推力方向之大負載的滚 琢螺样36,而在貫穿孔33d之位置設有輛承部丨5〇。以 下’就該輛承之構造作說明。 第四圖係工作台33之貫穿孔33d附近的縱刻面 圖。如圖示,在貫穿孔33d中嵌入有圓環形狀之第一轴 承安裝構件152。在第一軸承安裝構件152之上端形成 17 200902971 有擴大於半徑方向外侧之凸緣部152a。凸緣部152壮中 设有穿孔於上下方向之貫穿孔152b。工作台33上, 對應於貫穿孔152b之位置形成有陰螺紋33e。藉由將 栓158=插入貫穿孔152b及陰螺紋33e,其次旋緊螺拴 158a,第一轴承安裝構件152被固定於工作台幻上, 兩者形成一體化C5 此外’在滾珠螺桿36之螺桿部36a與軸部36b之間 °又有軸。卩36b側之直棱變小的階差。在該階差之 置有第一套環154。而後,在第-套環154之下依序梦 a又組合角浪珠軸承丨5丨及第二套環 155 °此外,在滚珠 螺桿36之轴部36b的中途形成有陽螺紋,將第— 環1=、組合角滾珠軸承151及第二套環155插通於滾 珠螺桿36之轴部36b後,藉由將螺母156安裳於滾珠 螺杯36之陽螺紋36c’而在第一套環154與第二套環155 之間支撐組合角滾珠轴承151之内輪。 此外’在第—軸承安裝構件152之下部配置有第二 =承女裝,件153。第二軸承安裝構件153藉由螺栓 扑而固疋於第—軸承安裝構件152。第二軸承安裝構 組合角滾珠轴承151係^ 151b之各正面相對地組合者( 153之上面與組合角滾珠軸承151之外輪抵接,而從 下方支撐組合角滾珠軸承151之外輪。 係使一對角滚珠軸承151a、 於拉伸測試時承受上方向之大負載,於壓In addition, the inner circumferential surface of the outer wheel m is 13 =:, and the screw is the surface. The inner peripheral surface 134 of the outer wheel W = the taper angle (10) having the same diameter as the diameter becomes smaller. Further, the inner circumferential surface of the inner wheel I% is slightly smaller than the diameter of the upper opening portion 34c, and the outer circumferential surface 134b is formed to correspond to the bolt hole 132d to open the meat surface. Furthermore, the outer wheel 134 is combined with the female thread 134c. In addition, there are a plurality of outer diameters (maximum diameters) which are smaller than the inner circumference* 134a of the inner wheel 132'134. Therefore, when the upper end of the U inner peripheral surface (10) is placed directly on the outer ring U4, the inner wheel surface is grounded, the inner wheel 132 is formed on the lower surface of the flange portion which is not in contact with the upper surface of the outer wheel 134, and the inner wheel U2 is inserted into the upper portion. The state in which the opening is raised. When the gap between the outer wheels 134_ is tightened through the bolt holes 132d of the shaft C and the shaft portion depth #132c of the ball screw 36, and the bolt 136 of the female thread 134c is inserted into the bolt 136, the tapered surface 132b of the inner wheel 132 is from the outer wheel 134. The tapered surface 134a receives a force inward in the radial direction, and the cylindrical surface 132b of the inner ring 132 strongly presses the shaft portion 36b of the ball screw 36. Further, at this time, the tapered surface 134a of the outer ring 134 receives a force directed outward in the radial direction from the tapered surface 132b of the inner ring 132, and the cylindrical surface 134b strongly presses the upper opening portion 34c. The shaft portion 36b of the ball screw 36 is firmly fixed to the upper cylindrical portion 34a of the tubular body 34B by the static friction generated by the result, and the two are integrated. Further, the two sets of the bolts 136, the bolt holes 132d, and the female threads 134c are respectively shown in the drawing, but actually, a plurality of (e.g., 10 sets) are provided on the circumference centering on the axis of the ball screw 36. Similarly, the fixing ring 140 has an inner wheel 142, an outer wheel 144, and a bolt 146. The outer peripheral surface 142a of the inner ring 142 has a tapered surface whose diameter is increased upward. Further, the inner circumferential surface 142b of the inner ring 142 is a cylindrical surface having a slightly larger outer diameter of the drive shaft 35a of the AC servo motor 35. A flange portion 142c enlarged in the radial direction outer side is formed at the lower end of the inner ring 142. A plurality of bolt holes 142d through which the bolts 146 are inserted in the vertical direction are provided in the flange portion 142c. The inner circumferential surface 144a of the outer ring 144 becomes a tapered surface whose diameter becomes smaller. Further, the outer circumferential surface 144b of the outer ring 144 is a cylindrical surface slightly smaller than the diameter of the lower opening portion 34d. Further, in the outer ring 144, a plurality of female threads 144c engaged with the bolts 146 are formed corresponding to the bolt holes 142d. Further, the diameter (maximum diameter) of the lower end of the inner circumferential surface 144a of the outer ring 144 is smaller than the diameter (maximum diameter) of the lower end of the inner circumferential surface 142b of the inner ring 142. Therefore, when the tapered surfaces are placed in contact with each other and the inner ring 142 is placed below the outer ring 144, the upper surface of the flange portion 142c of the inner ring 142 is in a state of being floated without coming into contact with the lower surface of the outer ring 144. The outer wheel 144 and the inner wheel 142 are inserted into the lower opening portion 34d and the AC servo motor 35 16 200902971 === the force of the inner wheel 142 when the ferrule 146 is 146 from the outer wheel through the flange portion of the flange portion. The 144a is driven by a drive shaft 35a with a radial direction toward 35. The cone is strongly pressed from the servo motor from the inner wheel 142. In addition, the drive shaft 35a of the tapered surface 144a of the outer wheel 144 is used by 4=:"4d . The AC servo motor is %. In addition, in the figure, the 夂-夂 邛 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , "The center of the circumference is provided with a plurality of thick upper ground cylindrical portions and lower cylindrical portions 34b rigid and rolled: Thus, the torque of the joint portion of the rigid coupling 34 is equal to: f and the drive shaft 35a of the AC servo motor 35 = Therefore, the rigid coupling 34 can highly transmit the torque of the drive shaft of 3 = 35 to 35 balls to the ball as shown in the second figure, at the center of the work 纟 33 A through-hole bead screw 36 is provided through the through hole 33d. In the present embodiment, the hoisting screw 36 is received at a position of the through hole 33d in order to receive the hoisting screw 36 of the large load in the thrust direction in the rotatable branch. The following is a description of the construction of the vehicle. The fourth drawing is a longitudinal plan view of the vicinity of the through hole 33d of the table 33. As shown in the figure, a first bearing mounting member 152 having an annular shape is fitted into the through hole 33d. At the upper end of the first bearing mounting member 152, a flange portion 152a which is enlarged to the outer side in the radial direction is formed. The flange portion 152 is provided with a through hole 152b that is perforated in the vertical direction. A female screw 33e is formed on the table 33 at a position corresponding to the through hole 152b. By inserting the bolt 158 = into the through hole 152b and the female thread 33e, and secondly tightening the thread 158a, the first bearing mounting member 152 is fixed to the table phantom, and the two form an integral C5. Further 'the screw at the ball screw 36 There is a shaft between the portion 36a and the shaft portion 36b. The straight edge of the 卩36b side becomes smaller. There is a first collar 154 between the steps. Then, under the first collar 154, the combination of the corner bearing 丨5丨 and the second collar 155 °, in addition, a male thread is formed in the middle of the shaft portion 36b of the ball screw 36, which will be the first Ring 1 =, the combined angular ball bearing 151 and the second collar 155 are inserted into the shaft portion 36b of the ball screw 36, and the first collar is placed on the male thread 36c' of the ball screw cup 36 by the nut 156. The inner wheel of the combined angular ball bearing 151 is supported between the 154 and the second collar 155. Further, a second female member, member 153, is disposed under the first bearing mounting member 152. The second bearing mounting member 153 is fixed to the first bearing mounting member 152 by bolting. The front surface of each of the second bearing mounting combined angular ball bearings 151 is integrally assembled (the upper surface of the 153 abuts against the outer wheel of the combined angular ball bearing 151, and the outer wheel of the combined angular ball bearing 151 is supported from below. Diagonal ball bearing 151a, subjected to a large load in the upward direction during tensile testing, at pressure

角滚珠軸承,市 在本實施例中, 奢(正面組合)。本實施例中 έ二又卜万向之大負載。因而,構成以正 、、且合(使各背面相對地組合者)組合一對 而可支撐上下兩方向之推力負載。特別是 ,抓用正面組合之組合角滚珠軸承151, 200902971 可防止軸(滾珠螺桿36之 内部Jf卜力;中,轴承本身不生挽曲時輪承 之滾珠與内外輪的摩擦,而供給调滑油承151 滑油漏出,而在第一套環154盥二方止該潤 之間的餘隙,及第二套環心;二構件⑸ 間之餘隙t分別設有油封咖、、1571)。^裝f件153 潤滑油從第一軸承安裝構件152與 二了防止Angular ball bearing, city In this embodiment, luxury (front combination). In this embodiment, the second load is a large load. Therefore, the thrust load can be supported in the upper and lower directions by combining a pair of positive and negative (combining the back faces). In particular, the combined angular ball bearing 151, 200902971 with the front combination can prevent the shaft (the internal Jf force of the ball screw 36; in the middle of the bearing, the bearing itself does not have the friction of the ball and the inner and outer wheels of the wheel bearing, but the supply is adjusted. The oil bearing 151 oil leaks out, and the gap between the first ring 154 and the second ring is the second ring; the clearance between the two members (5) is respectively provided with oil seal, 1571 ). ^Loading f 153 lubricating oil from the first bearing mounting member 152 and two to prevent

154之間漏出,而在第—軸承安裝構件m盘;裝= 安裝構件154之間設有襯墊159。另 /笛弟厂軸承 裝構件153中形成有延伸於半徑方向之貫承安 ;;5=在從外部供給_油時者:通常係藉^ 其次,就本實施例之線性導軌4〇的軌道44及 塊46 (第二圖)之構成’使用圖式詳細作說明。第五 係在垂直於軌道44之長軸方向的一面(亦即水平面)Θ 切斷軌道44及移動塊46的剖面圖’第六圖係第五圖之 Ι—Ι剖面圖。如第五圖及第六圖所示,移動塊40中形成 有凹部以包圍軌道44,該凹部中形成有延伸於執道44 之轴方向的四條溝46a、46a,。該溝46a、46a,中收納 有多數個不銹鋼製之滾珠46b。在軌道44中,與移動塊 46之溝46a、46a’相對的位置’分別設有溝44a、44a,, 滾珠46b被夾在溝46a與溝44a,或是溝46a,與溝44a, 之間。溝46a、46a’、44a、44a’之剖面形狀係圓弧狀, 其曲率半徑與滚珠46b之半徑概略相等。因而,滚珠46b 在幾乎無游隙之狀態下,密合於溝46a、46a,、44a、44a,。 在移動塊46之内部設有與各個溝46a概略平行之4 19 200902971 條退出路& 46c、46c,。如第六圖所示,溝恤與退出路 徑46c之各個兩端經由u字形路徑偏而連接,藉由溝 46a、溝44a、退出路徑46c、及u字形路徑偏,而形 成使滾珠46b循環用之循環路徑。藉由溝4如,、溝4如, 及退出路徑46c,亦形成同樣之循環路徑。 因而,移動塊46對執道44移動時,多數個滾珠4仍 在溝46a、46a,、44a、44a,中轉動而在循環路徑中循環。 因而,即使在執道軸方向以外之方向施加大負載,由於 仍可以多數個滾珠支撐移動塊,並且藉由滾珠46b轉 動,減少軌道轴方向之阻力而保持,因此,可使移動塊 46對軌道44平滑地移動。另外,退出路徑46c及u字 形路徑46d之内徑比滾珠46b之直徑稍大。因而,在退 出路徑46c及U字形路徑46d與滾珠46b間發生的摩擦 力極小,藉此不妨礙滾珠46b之循環。 如圖所示,被溝46a與44a夾著的二列滾珠46b之 列形成接觸角概略為±45。之正面組合型之角滾珠軸承。 此時之接觸角係溝46a及44a與滾珠46b接觸之各接觸 ’’’古的連線,對線性導執的逕向方向(從移動塊向軌道之 方向,第五圖中之下方向)形成之角度。如此形成之角 滚珠轴承可支撐反逕向方向(從軌道向移動塊之方向, 第五圖中之上方向)及橫方向(與逕向方向及移動塊之 =退方向兩者正交的方向’第五圖中之左右方向)的負 同樣地’被溝46a,與44a,夾著之二列的滾珠46b之 列形成接觸角(溝46a,及44a,與滾珠46b接觸之各接觸 點的連線’對線性導軌的反逕向方向形成之角度)概略 為±45。之正面組合型之角滾珠軸承。該角滾珠軸承可支 20 200902971 撐逕向方向及横方向的負载。 此外’被溝46a與44a之一方(圖中左侧)與溝46a, 與44a’之一方(圖中左側)分別夹著之二列的滾珠46b 之列也形成正面組合型之角滾珠軸承。同樣地,被溝46& 與44a之另一方(圖中右側)與溝46a,與44a,之另—方 (圖中右側)分別夾著之二列的滚珠46b之列也形成正 面組合型之角滾珠轴承。 如此,本實施例中,具有多數個滚珠46b之正面組 合型的角滾珠軸承係對分別作用於逕向方向、反逕向方 向及橫方向的負載而支撐,而可充分支撐施加於軌道軸 方向以外方向之大負載。 其次’就本實施例之通用測試機台1的控制計測部 之構成作說明。第七圖係本實施例之通用測試機台i的 控制計測部200之區塊圖。本實施例之通用測試機台ι 可以短時間進行疲勞測試,並可在測試片上以短周期施 加反覆負載。 通用測試機台1之控制計測部200具有:設定值指 示單元210、驅動控制單元22〇及測定單元25〇。 设疋值指示單元210係用於指示如何使下部载台31 (第一圖)移動的單元。具體而言,係將下部載台31 從初期位置之變位量(目標位置)作為訊號而輸出,並 傳送至驅動控制單元220之單元。設定值指示單元 具有:輸入介面212及波形產生電路214。 輸入介面212係用於連接設定值指示單元21〇與無 圖示之工作站的介面。通用測試機台1之操作者操作^ 作站,而指示如何使下部載台31變位。如係進行靜熊 之拉伸測試時,操作者操作工作站,輸入施予下部载△ 21 200902971 31之變位速度,並送訊至輸入介面212。此外,進行在 測試片上施加反覆負載之疲勞測試時,操作者操作工作 站,輸入下部載台31之振幅、頻率及波形(使用正弦 波或三角波之波形等),並送訊至輸入介面212。輸入於 輸入介面212之指示傳送至波形產生電路214。 波形產生電路214解釋從輸入介面212送訊之指 示,逐次運算下部載台31從初期位置之變位量,並將 其送訊至驅動控制單元220。另外,進行疲勞測試時, 不限於以單一之正弦波或三角波的一定波形、頻率驅動 下部載台31,亦可依據從具有各種振幅或頻率之函數所 合成之函數來驅動下部載台31。如亦可依據乘以頻率不 同之正弦波的函數,使下部載台31之振幅隨時間變化 地驅動下部載台31。 下部載台31之變位量作為數位訊號而從波形產生 電路214輸出。因而,從波形產生電路214送訊至驅動 控制單元220之訊號,首先輸入D/A轉換器222而轉 換成類比訊號。其次,轉換成類比訊號之下部載台31 的變位量資訊傳送至放大器224。而後,放大器224將 從D/A轉換器222傳送之下部載台31的變位量資訊放 大而輸出。 如前述,本實施例中,AC伺服馬達35係藉由驅動 下部載台31而進行各種測試。此處,AC伺服馬達35 内藏有用於檢測驅動轴35a(第一圖)之轉數的編碼器, 編碼器檢測出之轉數送訊至驅動控制單元220之現在位 置運算電路226。 現在位置運算電路22 6依據A C伺服馬達3 5之編碼 器的檢測結果,運算下部載台31之現在位置而輸出。 22 200902971 而後,將放大器224之輪出與現在位 輸出的差分(亦即相當於下部載A 逆异電路226之 在位置之差的訊號)送訊至雷、、,31之目襟位置與現 电々IL產生電路228。 電流產生電路228依據收A gap 159 is provided between the 154 and the mounting member 154. In addition, the bearing member 153 of the Didi factory is formed with a transverse bearing extending in the radial direction; 5 = when the oil is supplied from the outside: usually by the second, the orbit of the linear guide 4 of the present embodiment The composition of 44 and block 46 (second figure) will be described in detail using the drawings. The fifth system is on the one side (i.e., the horizontal plane) perpendicular to the long axis direction of the track 44. The cross-sectional view of the cut track 44 and the moving block 46 is shown in the sixth figure as a cross-sectional view of the fifth figure. As shown in the fifth and sixth figures, the moving block 40 is formed with a recess to surround the rail 44, and four recesses 46a, 46a extending in the axial direction of the lane 44 are formed in the recess. The grooves 46a and 46a accommodate a plurality of balls 46b made of stainless steel. In the rail 44, a position 44' opposite to the groove 46a, 46a' of the moving block 46 is provided with a groove 44a, 44a, respectively, and the ball 46b is sandwiched between the groove 46a and the groove 44a, or between the groove 46a and the groove 44a. . The grooves 46a, 46a', 44a, and 44a' have a circular arc shape in cross section, and the radius of curvature is substantially equal to the radius of the balls 46b. Therefore, the balls 46b are in close contact with the grooves 46a, 46a, 44a, 44a in a state where there is almost no play. Inside the moving block 46, there are 4 19 200902971 exit paths & 46c, 46c which are substantially parallel to the respective grooves 46a. As shown in the sixth figure, the two ends of the groove and the exit path 46c are connected by a U-shaped path, and the groove 46a, the groove 44a, the exit path 46c, and the u-shaped path are offset to form the ball 46b for circulation. The loop path. The same circulation path is also formed by the grooves 4 such as, the grooves 4, and the exit path 46c. Therefore, when the moving block 46 moves to the lane 44, the plurality of balls 4 are still rotated in the grooves 46a, 46a, 44a, 44a to circulate in the circulation path. Therefore, even if a large load is applied in a direction other than the direction of the axis of the road, since the moving block can be supported by a plurality of balls and is held by the rotation of the balls 46b to reduce the resistance in the direction of the track axis, the moving block 46 can be made to the track. 44 moves smoothly. Further, the inner diameter of the exit path 46c and the u-shaped path 46d is slightly larger than the diameter of the ball 46b. Therefore, the frictional force generated between the exit path 46c and the U-shaped path 46d and the ball 46b is extremely small, thereby preventing the circulation of the balls 46b. As shown in the figure, the contact angle between the rows of the two rows of balls 46b sandwiched by the grooves 46a and 44a is ±45. The front combined angular ball bearing. At this time, the contacts of the contact angle grooves 46a and 44a are in contact with the balls 46b, and the radial direction of the linear guide (from the moving block to the track, in the lower direction of the fifth figure) The angle of formation. The angular ball bearing thus formed can support the reverse radial direction (the direction from the track to the moving block, the upper direction in the fifth figure) and the lateral direction (the direction orthogonal to both the radial direction and the direction of the moving block = the retreating direction) The negative direction of the 'left-right direction in the fifth figure' is similarly formed by the groove 46a, and the row of the balls 46b of the two rows sandwiched by 44a (the grooves 46a, 44a, and the contact points of the balls 46b) The connection 'the angle formed by the reverse radial direction of the linear guide rails' is roughly ±45. The front combined angular ball bearing. The angular ball bearing can support 20 200902971 to support the radial direction and the lateral direction. Further, the row of the balls 46b of the two rows which are sandwiched by one of the grooves 46a and 44a (the left side in the drawing) and one of the grooves 46a and 44a' (the left side in the drawing) also form a front combined type angular ball bearing. Similarly, the rows of the balls 46b of the other row (the right side in the figure) of the groove 46& and 44a (the right side in the figure) and the groove 46a, and the other side (the right side in the figure) of 44a are also formed into a front combination type. Angular ball bearings. As described above, in the present embodiment, the front side combined type angular ball bearing having a plurality of balls 46b is supported by the load acting in the radial direction, the reverse radial direction, and the lateral direction, respectively, and can be sufficiently supported to be applied to the track axis direction. Large load in the direction of the outside. Next, the configuration of the control measuring unit of the universal testing machine 1 of the present embodiment will be described. The seventh diagram is a block diagram of the control measuring unit 200 of the universal test machine i of the present embodiment. The universal test machine ι of this embodiment can perform the fatigue test in a short time, and can apply the reverse load on the test piece in a short cycle. The control measurement unit 200 of the universal test machine 1 has a set value indicating unit 210, a drive control unit 22, and a measuring unit 25A. The threshold value indicating unit 210 is a unit for indicating how to move the lower stage 31 (first map). Specifically, the displacement amount (target position) of the lower stage 31 from the initial position is output as a signal, and is transmitted to the unit of the drive control unit 220. The set value indicating unit has an input interface 212 and a waveform generating circuit 214. The input interface 212 is for connecting the interface of the set value indicating unit 21 and the workstation (not shown). The operator of the universal test machine 1 operates the station and instructs how to displace the lower stage 31. If the static bear tensile test is performed, the operator operates the workstation, inputs the displacement speed applied to the lower load Δ 21 200902971 31, and sends it to the input interface 212. Further, when performing a fatigue test in which a reverse load is applied to the test piece, the operator operates the work station, inputs the amplitude, frequency, and waveform of the lower stage 31 (using a waveform of a sine wave or a triangular wave, etc.), and transmits it to the input interface 212. The indication input to the input interface 212 is passed to the waveform generation circuit 214. The waveform generating circuit 214 interprets the indication sent from the input interface 212, successively calculates the amount of displacement of the lower stage 31 from the initial position, and sends it to the drive control unit 220. Further, when performing the fatigue test, the lower stage 31 is not limited to being driven by a constant waveform or frequency of a single sine wave or a triangular wave, and the lower stage 31 may be driven by a function synthesized from functions having various amplitudes or frequencies. The lower stage 31 can be driven with the amplitude of the lower stage 31 as a function of time, as a function of multiplying the sine waves of different frequencies. The displacement amount of the lower stage 31 is output from the waveform generating circuit 214 as a digital signal. Thus, the signal sent from the waveform generating circuit 214 to the drive control unit 220 is first input to the D/A converter 222 and converted into an analog signal. Next, the amount of displacement information converted to the lower stage stage 31 of the analog signal is transmitted to the amplifier 224. Then, the amplifier 224 expands and outputs the displacement amount information transmitted from the D/A converter 222 to the lower stage 31. As described above, in the present embodiment, the AC servo motor 35 performs various tests by driving the lower stage 31. Here, the AC servo motor 35 incorporates an encoder for detecting the number of revolutions of the drive shaft 35a (first figure), and the number of revolutions detected by the encoder is sent to the current position operation circuit 226 of the drive control unit 220. The position calculating circuit 22 6 calculates the current position of the lower stage 31 based on the detection result of the encoder of the A C servo motor 35, and outputs it. 22 200902971 Then, the difference between the round-out of the amplifier 224 and the current bit output (that is, the signal corresponding to the difference between the positions of the lower-loaded A-reverse circuit 226) is sent to the target position of the thunder, and 31. The power 々 IL generating circuit 228. The current generating circuit 228 is based on

朽服ms夕一如雷土 欠 机號,產生輪出至ΑΓ 伺服馬達35之二相電流,並將其輪 和出至AC 結果驅動AC伺服馬達35,而蚀卞 旬服馬達。 位置。 而使下部載台31到達目標 藉由驅動下部載台31而施加 由内藏於通用測試機台1之附件28、負載’藉 感器254,及取出負载傳感器254 =負载傳 用的橋接電路256來檢測。l ^λ訊 至工作站。工作站統計從輪出訊 ^如將時_作為橫轴,將施加於測試片之應, 縱轴的圖形而表示。 心 為 此外The sorrow of the sorrow is like a thunder. The machine is owed to the machine, and the two-phase current of the servo motor 35 is generated, and the wheel and the AC output are driven to the AC servo motor 35, and the motor is eclipsed. position. The lower stage 31 is caused to reach the target by driving the lower stage 31 to apply the bridge circuit 256 from the accessory 28 built in the universal test machine 1, the load susceptor 254, and the load sensor 254 = load transfer. To detect. l ^λ News to the workstation. The workstation statistics are sent from the round. If the time _ is taken as the horizontal axis, it will be applied to the test piece and the vertical axis. Heart for

值傳送至波形產生電=器258之輸出的負載 ,得达至波祕生電路214,因應負載而使下部載台31 之變位行動變化的所謂反饋控制。如下部載台31之變 位墨與負載值並非JL比關係’亦即測試片產生升降時, 可進行擴大下部載台之振幅等的控制。 藉由使1以上構成之通用測試機台1,可進行測試 片之靜態破瓌測試及疲勞測試等。此處,本實施例中係 使用反應性高’且高扭矩之AC伺服馬達35驅動下部載 台31。因而,通用測試機台丨可將最大達數百让1^之負 ,施加於測試片,此外,亦可以數百Hz之高頻而將反 覆負載施加於測試片。因此,採用本實施例之通用測試 機台1時,可在短時間内評估測試片之疲勞特性,且可 23 200902971 °某求細短測試時間。 於使t ’採財實_之構斜,田 AC^^SS, 下運動時ct二動 S於同,:=用3^ 二用下;=伺服馬達-之心^ 35a及滾珠螺桿36 達35之驅動軸 ‘:在同-板面上全部配::確度定心。此外’ 相斜位置。 度地^轉已定位之各元件的 進行^V採用本實施例之構成時,因发 運订AC伺服馬達%之驅 了目為可高精確度地 二’所以因定心誤差而作用^ ^及滚珠螺桿36的定 a及滾珠螺桿36的 ^ 司服馬達35之驅動轴 :聯結伺服馬達與進給‘曲應力較小。通常用 而:(橡膠及金;彈二器),,係使用藉由介有 ^攝成的軟性聯結器。 以吸收彎曲應力 '、可高精確度地進行2軸^定、細*例中,如上述,因 2料所形成的剛性聯結器C因:以可使用以剛性高 二用,AC祠服馬達35之=可以高反應性使 t 36之㈣36b。因此,即使以=扭矩傳達至滾珠 建3S之驅動軸35a來 同周期使AC伺服馬 追隨驅動車由 35a之口上轉,,二為滾珠螺桿36仍可正 巧剛性者,且以數十 ,即使測試片係鋼等 以上、速使十字頭3lb來回 24 200902971 運動時,仍可將所設定之負載(應變)正確地施加於測 試片。亦即,本實施例之通用測試機台1可在短時間進 行測試片之疲勞測試。 另外,本實施例中,如第二圖所示,係分別將軌道 44固定於導引框42,將移動塊46固定於下部載台而構 成,不過,亦可分別將移動塊固定於導引框,將軌道固 定於下部載台(亦即與進給螺桿卡合之螺母)而構成。 此外,本實施例中,使通用測試機台之十字頭上下 移動的機構係使用線性驅動器,不過,該線性驅動器除 了通用測試機台之外,如第八圖亦可利用於使汽車C在 上下方向激振用的激振測試機台Γ。亦即,根據本實施 型態係備有4組可移動部30與線性導軌40 (第一圖) 的線性驅動器,而將其分別固定於被基座B支撐的機台 框架部10’。而後,將各個十字頭31b固定於汽車C之 車輪W,藉由驅動可移動部30之AC伺服馬達35,可 使汽車C激振。此種激振測試機台可以高振動頻率激振 如汽車C之重量大的受測體。 此外,本實施例中,剛性聯結器34聯結滾珠螺桿 36之轴部36b與AC伺服馬達35之驅動軸35a (第三 圖)。但是,本發明並非限定於上述之構成,亦可使用 在扭力方向具有高剛性之其他聯結器。此種聯結器如為 其次說明之本發明第二實施例的半剛性聯結器。 將藉由半剛性聯結器聯結滾珠螺桿與AC伺服器之 驅動軸的通用測試機台,作為本發明之第二實施例而說 明於下。另外,本發明之第一實施例與第二實施例,僅 聯結滾珠螺桿與AC伺服馬達之驅動軸的聯結器不同, 其他均相同。因此,本實施例中,在與第一實施例相同 25 200902971 之構件或元件上賦予與第一實施例同一符號’而省略此 等之詳細說明。 第九圖係顯示本實施例中之半剛性聯結器3〇〇,及 經由該半剛性聯結器300而彼此聯結之Ac伺服馬達35 的驅動轴35a與滾珠螺桿36之軸部36b的放大剖面圖。 本實施例之半剛性聯結器300構成扭力剛性極高\可以 高反應性使施加於AC伺服馬達3 5之驅動軸3 5 &的扭矩 傳達至滾珠螺桿36。此外,構成藉由内部之樹脂構件而 柔軟地吸收長度方向之軸的變位,使從Ac伺服馬達% 之驅動轴35a傳導之^伺服器發生的軸方向振動大幅 衰減’而不易傳導至滾珠螺桿36。 如第九圖所示,半剛性聯結器3〇〇由尼龍製之内 外輪320及340、以及固定此等之複 數(本實把例係6個)螺栓382而構成。在遍 中央’於内部相互連絡之圓孔362a、地 圓孔—之内徑係可無間隙地插入AC,服馬= 上 驅動軸35a的大小,圓孔362b ^達35之 入滾珠螺桿36之軸部36b的大之^另成為=間隙地插 由於滾珠螺桿36之軸部36b的直徑比ac =㈣小,因此圓孔362b之外徑比圓孔―之 在内輪360之軸方向中央 周延伸於半徑方向朝外的=;^從^輪_之外 之兩面中央部分別形成有延伸於 攸凸緣部360a 部之外側面364、366成為隨形部。錐形 逐漸變小之圓錐狀的錐形面。此迎軸方向頂端而外徑 一對外輪I娜的中央分別形成= 26 200902971 内側面322、342的貫穿孔。外輪320與340分別將内 側面322、342之錐形面打開方向朝向内輪36〇側而配 置。外輪320、340之錐形形狀的内側面322、342分 別具有與内輪360之外側面364、366相同的錐角◦而 後’外輪320之内側面322與内輪36〇之外側面364、 外輪340之内側面342與内輪36〇之外侧面施重疊 地’在外輪320、34〇之貫穿孔中插入形成於内輪 的錐形部。The value is transferred to the load of the output of the waveform generating electric= 258, and the so-called feedback control which changes the displacement action of the lower stage 31 in response to the load is obtained. When the displacement ink and the load value of the following stage 31 are not in the JL ratio relationship, that is, when the test piece is lifted and lowered, the amplitude of the lower stage or the like can be controlled. By using the universal test machine 1 composed of one or more, the static break test and the fatigue test of the test piece can be performed. Here, in the present embodiment, the lower stage 31 is driven by the AC servo motor 35 having high reactivity and high torque. Therefore, the universal test machine can apply a maximum of several hundred to 1^ to the test piece, and a reverse load can be applied to the test piece at a high frequency of several hundred Hz. Therefore, when the universal test machine 1 of the present embodiment is used, the fatigue characteristics of the test piece can be evaluated in a short time, and 23 200902971 ° can be used for a short test time. In order to make t 'take the wealth _ the structure of the slant, field AC ^ ^ SS, ct second move S in the same movement, : = use 3 ^ two use; = servo motor - heart ^ 35a and ball screw 36 35 drive shaft ': all on the same - board surface:: accuracy centering. In addition, the 'inclined position. When the composition of the present embodiment is used, the operation of the present embodiment is based on the fact that the AC servo motor is shipped for a high degree of accuracy, so the effect is due to the centering error ^ ^ And the drive shaft of the ball screw 36 and the drive shaft of the ball screw 36: the servo motor and the feed 'torque stress are small. Usually used: (rubber and gold; two devices), the use of a soft coupling through the mediation. In the case of absorbing the bending stress ', it is possible to perform two-axis determination and fineness with high precision. As described above, the rigid coupling C formed by the two materials is used for the purpose of rigidity, and the AC 祠 motor 35 is used. = can be highly reactive to make t 36 (four) 36b. Therefore, even if the torque is transmitted to the drive shaft 35a of the ball 3S to make the AC servo horse follow the drive car up by the mouth of 35a, the second is that the ball screw 36 can still be rigid, and even if it is tested, even if it is tested When the sheet metal is equal to or higher than the speed of the crosshead 3lb back and forth 24 200902971, the set load (strain) can still be correctly applied to the test piece. That is, the universal test machine 1 of the present embodiment can perform the fatigue test of the test piece in a short time. In addition, in the present embodiment, as shown in the second figure, the rail 44 is fixed to the guide frame 42 and the moving block 46 is fixed to the lower stage. However, the moving block can be separately fixed to the guide. The frame is constructed by fixing the rail to the lower stage (that is, the nut that engages with the feed screw). In addition, in the embodiment, the mechanism for moving the cross head of the universal test machine up and down uses a linear driver. However, the linear drive can be used to make the car C up and down in addition to the universal test machine. The vibration tester for the direction excitation is Γ. That is, according to the present embodiment, the linear actuators of the four movable portions 30 and the linear guides 40 (first drawing) are provided, and are respectively fixed to the machine frame portion 10' supported by the base B. Then, the respective crossheads 31b are fixed to the wheels W of the car C, and the car C is excited by the AC servo motor 35 that drives the movable portion 30. This type of vibration test machine can excite a high vibration frequency such as the weight of the vehicle C. Further, in the present embodiment, the rigid coupling 34 couples the shaft portion 36b of the ball screw 36 with the drive shaft 35a of the AC servo motor 35 (third drawing). However, the present invention is not limited to the above configuration, and other couplers having high rigidity in the torque direction may be used. Such a coupler is the semi-rigid coupler of the second embodiment of the present invention which will be described next. A general-purpose test machine in which a ball screw and a drive shaft of an AC servo are coupled by a semi-rigid coupling is described as a second embodiment of the present invention. Further, in the first embodiment and the second embodiment of the present invention, only the coupling of the ball screw and the drive shaft of the AC servo motor is different, and the others are the same. Therefore, in the present embodiment, the same reference numerals as in the first embodiment are given to the members or elements of the same as the first embodiment 25 200902971, and the detailed description thereof will be omitted. The ninth drawing shows an enlarged sectional view of the semi-rigid coupling 3 in the present embodiment, and the drive shaft 35a of the Ac servo motor 35 and the shaft portion 36b of the ball screw 36 which are coupled to each other via the semi-rigid coupling 300. . The semi-rigid coupling 300 of the present embodiment constitutes a very high torque rigidity. The high reactivity makes the torque applied to the drive shafts 3 5 & of the AC servo motor 35 to the ball screw 36. In addition, the displacement of the shaft in the longitudinal direction is softly absorbed by the internal resin member, and the vibration in the axial direction caused by the servo that is transmitted from the drive shaft 35a of the Ac servo motor% is greatly attenuated, and is not easily transmitted to the ball screw. 36. As shown in the ninth figure, the semi-rigid coupling 3 is composed of inner and outer wheels 320 and 340 made of nylon, and a plurality of bolts 382 which are fixed to each other. The inner diameter of the circular hole 362a and the ground circular hole which are interconnected in the center is inserted into the AC without a gap, and the size of the upper drive shaft 35a is the size of the upper drive shaft 35a, and the round hole 362b is 35 into the ball screw 36. The larger diameter of the shaft portion 36b is inserted into the gap. Since the diameter of the shaft portion 36b of the ball screw 36 is smaller than ac = (four), the outer diameter of the circular hole 362b extends beyond the center of the inner circumference of the inner ring 360. The side surfaces 364 and 366 extending from the flange portion 360a are formed as the conforming portions, respectively, at the central portions of the two faces other than the wheel. Conical tapered conical surface that tapers. The top end of the axial direction and the outer diameter of the outer wheel Ia form a through hole of the inner side surface 322, 342 of = 26 200902971, respectively. The outer wheels 320 and 340 are disposed such that the tapered surface opening directions of the inner side surfaces 322, 342 are directed toward the inner side of the inner wheel 36. The tapered inner side surfaces 322, 342 of the outer wheels 320, 340 respectively have the same taper angle 与 as the outer sides 360, 366 of the inner wheel 360, and then the inner side 322 of the outer wheel 320 and the outer side 364 of the inner wheel 36, the outer wheel 340 The inner side surface 342 is overlapped with the outer side surface of the inner wheel 36'. The tapered portion formed in the inner wheel is inserted into the through hole of the outer wheel 320, 34'.

V:. 此外,在外輪34〇之貫穿孔的周圍,與形成於螺栓 382之頂端部的陽螺紋卡合的陰螺紋344,在將貫穿孔 之軸作為中心的圓周上等間隔地形成有複數個。此外, 外輪320與内輪360之凸緣部36〇a中,亦在對應於陰螺 紋344之位置分別形成有螺栓孔324、368。而後,6 個螺检382插通於外輪32〇之螺栓孔—及内輪36〇之 螺栓孔368 ’而與外輪34〇之陰螺紋344卡合。 、在内輪36〇之圓孔362a中,從下方插入AC伺服馬 達d之^動軸祝的頂端,在圓孔362b中,從上方插 入;义’、干36之軸部36b的頂端後,而緊固螺栓382 :被外輪320與外輪340從兩側強力夾著, 之2個錐形部分別深深嵌入外輪32〇、34〇 孔迎、鳥至从飼服馬達 == 螺桿36之軸部36b分別施加強側壓。因=圓孔 362b與驅動軸35a、滾珠蟫浐% * ±此在圓孔362a、 生強Λ之雜力 之轴部36b之間分別發 生強力之雜力,絲軸35a與 360而一體地聯結。結果,半剛性干36 t内輪 結部的扭力嶋與滾珠螺桿36及t 構成之聯 C伺服馬達35之驅 27 200902971 動軸35a相等或比其大。 性#之居巧掛此 在外輪320與340之間,僅以黏彈 紝哭3〇〇 1曰而形成之内輪支撐。此外,在半剛性聯In addition, the female screw 344 engaged with the male screw formed at the distal end portion of the bolt 382 around the through hole of the outer ring 34 is formed at equal intervals on the circumference centering the shaft of the through hole. One. Further, in the flange portion 36A of the outer ring 320 and the inner ring 360, bolt holes 324, 368 are formed at positions corresponding to the female threads 344, respectively. Then, the six screw gauges 382 are inserted into the bolt holes of the outer wheel 32 and the bolt holes 368' of the inner wheel 36 to engage with the female threads 344 of the outer wheel 34. In the round hole 362a of the inner ring 36, the top end of the AC servo motor d is inserted from below, and the hole 362b is inserted from above, and the top end of the shaft portion 36b of the stem 36 is closed. The fastening bolt 382 is strongly sandwiched by the outer wheel 320 and the outer wheel 340 from both sides, and the two tapered portions are deeply embedded in the outer wheel 32〇, 34, the hole, the bird to the feeding motor== the shaft of the screw 36 36b applies a strong side pressure, respectively. Since the round hole 362b and the drive shaft 35a, the ball 蟫浐% * ±, respectively, a strong force is generated between the round hole 362a and the shaft portion 36b of the force generating force, and the wire shafts 35a and 360 are integrally coupled. . As a result, the torsion force 半 of the semi-rigid dry 36 t inner wheel portion is equal to or larger than the ball screw 36 and the t-c servo motor 35. Sexuality # 挂 挂 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在In addition, in semi-rigid joint

珠螺桿36之轴部=馬達35之驅動轴35a的頂端與滾 之間隔而聯結。因此的頂端離開微小(如約1毫米) 時,内輪360彈性傲开:從馬達施加壓縮軸之方向的力 之間隔狹窄,在半該驅動軸祝餘珠螺桿% 可113GG㈣㈣方向之力’ 內aim 珠ί扣36側之力大幅衰減。本實施例中, < = 。^動衰減率在驅動轴35a的固有振動數中概 措此,可使驅動軸35a之軸方向或軸之半徑 方向的振動有效地衰減。 另卜如上述’ AC飼服馬達35之驅動軸35a的頂 ^與滾珠螺# 36之軸部36b的頂端之間隔短達1毫米 辁度,此外,各軸之頂端的全周與内輪一體化。因而, 在返回方向充分地剛性聯結,可將AC伺服馬達35之驅 動軸35a的旋轉驅動正確地傳達至滾珠螺桿36。 以上說明之本發明的第一及第二實施例,係關於使 用進給螺桿機構的通用測試機台者。但是,本發明除了 通用測試機台之外’亦可適用於以下說明之本發明的第 三實施例之其他種類的材料測試機台中。 弟十圖係本發明第三實施例之扭力測試機台的前 視圖。此外’第Η 圖係本實施例之扭力測試機台的俯 視圖。本實施例之扭力測試機台501中,長條狀之測試 片S係在其長軸方向概略水平地藉由卡盤572、574之 爪572a、547a把持兩端的狀態下進行扭力測試。另外, 為了明確說明扭力測試機台501之構造,測試片s及把 28 200902971 =測試片之卡盤572、574僅顯示於第十圖中。亦即, 係測試片s及卡盤572、574被拆下狀態的扭 力測5式機台501之俯視圖。 下十圖所示’本實施例中,在固^於基座B上之 (“二:、510之上設有:用於固定支撐測試片S之-端 片$ p㈤固定端支撐部520,與可旋轉地支撐測試 拉i〜另鈿(驅動端)的驅動端支撐部530。而後, i測動端支撐部53G断旋圍之指定扭矩 、^ ,可在测試片S上施加扭力應力而扭轉。 F扣牲^端支撐部52G具有安裝凸緣527,其係用於安 ^巴^試片S之时端用的固^端側卡盤仍。從安 +27之與安裝了固定端侧卡盤572之面的相反側 ,支撐軸526延伸於概略水平方向。 562 由526之頂端聯結於扭矩計測用之負載傳感器 ―戚八^端。在支撐軸526之頂端與負載傳感器562之 緣,^形成有連接用之凸 '緣’藉由以螺栓固定各凸 Θ 撐軸526與負載傳感器562。負載傳感器 柄加^ 鳊固疋於固定端支撐部520之固定端侧的侧 二从2 L側框架522藉由螺栓固定、焊接等之裝置而 ,疋於固定端支撐部520之固定端支撐板521 。固定端支撐板521 0定於下部框架51〇上。此處, =架522係具有L字狀之剖面形狀的板狀構件,且其 ,洛部中形成有補強用之肋條522a。因而,側框架522 =為剛性高者。由於固定端支撐板521強固地固定於下 匚木510,因此側框架522可視為與基座b 一體之剛 體’不過詳細如後述。 如此,測5式片S之固定端經由固定端侧卡盤572、 29 200902971 安裝凸緣527、支撐軸526、負載傳感器562而固定於 側框架522。此處,固定端側卡盤572、安裝凸緣527、 支撐轴526、負載傳感器562對測試片S充分地提高扭 力剛性,藉由在測試片S之驅動端施予扭矩,可使測試 片S之内部發生因應扭矩大小之扭力應力。而後,藉由 負载傳感器562計測施加於測試片s之扭矩的大小。The shaft portion of the bead screw 36 = the tip end of the drive shaft 35a of the motor 35 is coupled to the gap of the roller. Therefore, when the tip is slightly small (for example, about 1 mm), the inner wheel 360 is elastic and proud: the interval of the force from the direction in which the motor applies the compression axis is narrow, and in the half of the drive shaft, the margin of the screw can be 113GG (four) (four) direction of force 'in aim The force of the side of the buckle is greatly reduced. In this embodiment, <=. The dynamic attenuation rate is roughly the same in the natural vibration number of the drive shaft 35a, and the vibration in the radial direction of the drive shaft 35a or the radial direction of the shaft can be effectively attenuated. Further, as described above, the distance between the top of the drive shaft 35a of the AC feeding motor 35 and the tip end of the shaft portion 36b of the ball screw #36 is as short as 1 mm, and the entire circumference of the top end of each shaft is integrated with the inner wheel. . Therefore, the rotational driving of the drive shaft 35a of the AC servo motor 35 can be accurately transmitted to the ball screw 36 by being sufficiently rigidly coupled in the return direction. The first and second embodiments of the present invention described above relate to a general-purpose test machine using a feed screw mechanism. However, the present invention can be applied to other types of material testing machines of the third embodiment of the present invention described below in addition to the general testing machine. Fig. 10 is a front view of a torque testing machine of a third embodiment of the present invention. Further, the figure is a top view of the torque test machine of the present embodiment. In the torque testing machine 501 of the present embodiment, the long test piece S is subjected to a torque test in a state where the longitudinal ends of the test pieces S are held horizontally by the claws 572a and 547a of the chucks 572 and 574 at both ends. In addition, in order to clarify the configuration of the torque testing machine 501, the test piece s and the chucks 572, 574 of the test piece 2009, 200902971 = test pieces are only shown in the tenth figure. That is, a plan view of the torque test type 5 machine 501 in which the test piece s and the chucks 572, 574 are removed is shown. In the present embodiment, in the present embodiment, it is fixed on the base B ("two:, 510 is provided with: an end piece $p (five) fixed end support portion 520 for fixing the supporting test piece S, And a driving end support portion 530 that rotatably supports the test pull i to the other end (drive end). Then, the i-measuring end support portion 53G breaks the specified torque of the circumference, and can apply a torsional stress on the test piece S. The F-buckle end support portion 52G has a mounting flange 527 which is used for the end of the clamp end of the test piece S. The mounting end is fixed from the +27 On the opposite side of the face of the end side chuck 572, the support shaft 526 extends in a substantially horizontal direction. The 562 is coupled to the load sensor for torque measurement at the top end of the 526. At the top end of the support shaft 526 and the load sensor 562 The edge is formed with a convex 'edge' for connecting by fixing each of the tenon shafts 526 and the load cell 562 by bolts. The load sensor handle is fixed to the side of the fixed end side of the fixed end support portion 520. 2 L side frame 522 is fixed to the fixed end of the fixed end support portion 520 by means of bolt fixing, welding, or the like. The plate 521. The fixed end support plate 521 0 is fixed to the lower frame 51. Here, the frame 522 is a plate-like member having an L-shaped cross-sectional shape, and a reinforcing rib 522a is formed in the base portion. Therefore, the side frame 522 = is rigid. Since the fixed end support plate 521 is strongly fixed to the lower eucalyptus 510, the side frame 522 can be regarded as a rigid body integral with the base b, but will be described later in detail. The fixed end of the sheet S is fixed to the side frame 522 via the fixed end side chuck 572, 29 200902971 mounting flange 527, the support shaft 526, and the load sensor 562. Here, the fixed end side chuck 572, the mounting flange 527, and the support The shaft 526 and the load sensor 562 sufficiently increase the torsional rigidity of the test piece S, and by applying a torque to the driving end of the test piece S, a torsional stress corresponding to the magnitude of the torque can be generated inside the test piece S. Then, by the load sensor 562 measures the magnitude of the torque applied to the test piece s.

此外,支撐軸526在其中途藉由固定端側軸承524 可旋轉地支撐。固定端側軸承524亦藉由螺栓固定、焊 接等之裝置而強固地固定於固定端支撐板521上。 其次,就用於將固定端支撐板521固定於下部框架 51〇的機構作說明。如第十一圖所示,在下部框架5j〇 有一對溝511 °使用該溝511與螺栓5、12而 將固疋鈿支撐板521固定於下部框架51〇。 =支樓板521上’沿著各溝511各設有7個(亦即合 j 14個)插通螺栓512之貫穿孔521a,藉由 穿孔521a之全部安裝螺栓512, 專貝 地固定於下部框架51〇。 口疋知切板切強固 其次,就藉由螺栓512而固定固定端支 構造詳細說明。第十二圖係第十一圖之:板521的 如第十二圖所示,溝511係下部5nb之寬产^面圖 之寬度大的附階差之溝。此外,蟬 2 邛511a 了六角扳手用夕二_&:?丨S19 & 检 係在頭部形成 用孜予用之六角孔512a的所謂附六角孔4 ㈣2與配置於溝511之下部5 C該= 母犯之尺寸僅比下部511b之寬度稍小母5 3卡合。螺 之寬度大’因此在螺栓512之頭部盘螺母^上部511a ,端切板521與溝511之上/二^ 芽板521強固地固定於下部框架510。 疋端支 30 200902971 其次,就驅動端支撐部530之構成作說明。 如第十圖所不,驅動端支撐部53〇具有安 537,其係用於安裝把持測試片s之驅 驅= 側卡盤574。在安裝凸緣537之與安裝了驅動 574之面相反側之面上設有減速機構536。具體而‘皿 係在減速機構536之輸出軸上形成有安裝凸緣幻7 :成 - 速機構536將其輸入軸之高速、低扭矩的旋轉運動轉^ 成輪出轴之低速、高扭矩的旋轉運動。輸出軸之 置 (' 動經由凸緣537、卡盤574而傳達至測試片s之驅動 §亥減速機構536固定於驅動端支撐部53〇之驅* 側之侧框架532。驅動端側之侧框架532藉由焊 = ,端支撐部53G之驅動端支撐板531之上而強固地= 疋。驅動端支撐板531藉由與固定端支撐板521同 固定裝置而固定於下部框架510上。此處,側框架’M2 係概略垂直於旋轉軸A之板狀的構件,且在藉由側框架 532與驅動端支撐板531而形成之角落部形成有補強用 肋條532a。該肋條532a亦焊接於驅動端支撐板531與 i" 驅動端側之側框架532。因此,側框架532與驅動端^ =板531以回剛性而一體化。如前述由於驅動端支撐板 1強固地固定於下部框架510,因此侧框架532可視 -為與基座B—體之剛體。 在下部框架51〇之中央部(溝511、511之間)形 ' =洞部514。在該空洞部514中設有用於使驅動端 @ ^ ^ 53〇對下部框架51 〇滑動於旋轉軸A方向的進給 有'干機,。如第十及第十一圖所示,在空洞部514中設 ,與旋轉轴A平行之方向延伸的進給螺桿544。進給 ’、才于544之兩端藉由一對軸承54s、S46 (第十圖)而可 31 200902971 旋轉地支撐。此外,在驅動端支撐板531之下面固定有 與該進給螺桿544卡合之螺母548。因而,在驅動端支 撐板531未固定於下部框架510之狀態(亦即旋鬆用於 固定驅動端支撐板531的螺栓之狀態)下,藉由使進給 螺桿544轉動,可使驅動端支撐部530沿著進給螺桿544 而移動。另外,在進給螺桿544之一端(軸承545侧) 設有使進給螺桿544轉動用之手柄542。本實施例中, 如此藉由使驅動端支撐部530移動,可因應測試片s之 尺寸而調整固定端支撐部520與驅動端支擇部53〇之間 隔。 曰 此外,在侧框架532之安裝凸緣537的下部安裝有 編碼器538之皮帶輪538a。安裝凸緣537之外周部537a 亦具有作為皮帶輪之功能’而在編碼器538之皮帶輪 538a與安裝凸緣537之皮帶輪537a上架設無端皮帶 539。編碼器538藉由檢測皮帶輪538a之旋轉角,運算 安裝凸緣537之旋轉數、對安裝凸緣537之初期位置的 旋轉角度及反覆測試時之周期數等’可將其顯示於編碼 益538之顯示部538b。因此,扭力測試機台5〇 1之操作 者可從編碼器538之顯示部538b的顯示内容確認扭力 測試之進展狀況等。 其次’就減速機構536之輸入軸536a與在該輸入軸 上施加扭矩之AC飼服馬達535的配置作說明。第十二 圖係第十一圖之III —III剖面圖。如第十三圖所示,減 速機構536之輸入軸536經由剛性聯結器533而與AC 伺服馬達535之驅動軸535a聯結。因此,藉由驅動Ac 伺服馬達535可在測試片s上施加扭力應力。此外,如 圖所示,AC伺服馬達535經由馬達支撐框架534而固 32 200902971 定於側框架532上。 另外,減速機構536埋入侧框架532上形成之開口 532b中而強固地固定。本實施例中,減速機構536係波 動齒輪減速機構。波動齒輪減速機構具有輸入軸與輪出 軸為同軸的知·徵。因而,本實施例中,旋轉軸A與八匸 伺服馬達535之驅動軸535a成為同軸。由於旋轉軸A 與AC伺服馬達535之驅動軸535a成為同軸,因此成為 扭力測試機台501對包含旋轉軸a之垂直面概略對稱之 形狀。因而,測試機台501之重量平衡佳,於測試時不 易發生振動。此外,波動齒輪減速機構具有齒隙極小之 特徵。因而,藉由在將反覆負載施加於測試片之疲勞測 5式機σ中‘入波動齒輪減速機,可大幅提高疲勞測試之 精確度。就本發明人所瞭解之範圍内,還不存在先前 疲勞測試機台中利用波動齒輪減速機者。 本實施例之剛性聯結器533構成扭力剛性極高,可 以高反應性使施加於AC伺服馬達535之驅動軸53化 扭矩傳達至減速機構536的輸入轴536a。以下,就 聯結器533之構造作說明。第十四圖係顯示剛性聯 533及經由該剛性聯結器533而彼此聯結的ac饲服馬 達535之,動軸535a與減速機構536之輪入車由53 放大剖面圖。 j 如圖所示’剛性聯結器533全體成為中空 圓棒形狀(亦即,階梯形厚度之圓筒) 聯 結器533㊣有1備插入減速機才冓536之輸P入二生3 t …服馬達535之上 之輸入剩部⑽本實施财,機= 33 200902971 之輸入軸遍的直徑比AC飼月良馬達535之驅動轴伽 小,所以輸出側圓筒部533a之外徑比輪入侧圓筒部5饥 之外徑小。 此外,在輸出側圓筒部533&及輸入侧圓筒部5挪 之内側(第十四圖中’輸出_筒部伽之右侧及輸入 侧圓筒部533b之左侧)分別形成有狹窄部533e及5撕 狹窄部533e及迎之直徑分別與減速機構536之輸入 軸遍及AC祠服馬達535之驅動車由他的直徑概略 相等。因而,在狹窄部533e^ 533f之内周面與減速機 構536之輸入轴536a與AC祠服馬達535之驅動轴53允 的外周I乎無間隙的狀恶下’減速機構536之輸入轴 536a與AC伺服馬達535之驅動軸535&收容於狹窄部 533e ' 533f〇 輸出侧開口部533c及輸入側開口部之直徑分 別構成比減速機構536之輸入軸536a及AC伺服馬達 535之驅動軸535a的外徑大。為了將輸出侧開口部533c 及輸入侧開口部533d分別固定於減速機構536之輸入 軸536a及AC伺服馬達535之驅動軸535a,而使用固 定用環630及640。 固定用環630具有:内輪632、外輪634及螺栓636。 内輪632之外周面632a成為直徑朝向AC伺服馬達側 (圖中右侧)而變小的錐形面。此外,内輪632之内周 =632b成為比減速機構536之輸入軸兄如的外徑稍大 私度之圓筒面。在内輪632之減速機構侧(圖中左側) 形j有,大於半徑方向外側的凸緣部032c。凸緣部632c 中设有複數將螺栓636插通於旋轉軸A方向的螺栓孔 632d。外輪634之内周面634a成為直徑朝向AC伺服馬 34 200902971 達側而變小的錐形面。此外,外輪634之外周面634b 成為比輸出側開口部533c之直徑稍小的圓筒面。再者, 外輪634中形成有複數與螺栓630卡合之陰螺紋634c。 將外輪634及内輪632插入輸出侧開口部533c與減速機 構536之輸入軸536a間的間隙,其次藉由螺栓636將内 輪632固定於外輪634,進一步藉由緊固螺栓幻6,而 内輪632之内周面632b強力壓迫減速機構536之輸入 軸536a,外輪634之圓筒面63仆強力壓迫輸出侧開口 =533c。結果,藉由發生之靜摩擦力,減速機構536之 地固定於剛性聯結器533之輸出側圓筒 i螺於&636、^入形成—體。另外,圖中係分別各顯示二 在將二孔幻以及陰螺紋634c’不過,實際上 在將減速機構5 3 6之卓4你A cb , (例如Η)組)。 作為中心的圓周上設有多數個 同樣地,固定用環64〇且 及螺栓646。内輪642之外/面.内輪642、外輪644 機構側而變小的錐形面。此 2a成為直徑朝向減速 成為比AC祠服馬達535卜二輪⑷之内周面· 的圓筒面。在内輪642之下山^ 535a的外徑稍大程度 側之凸緣部642c。在凸緣部^形成有擴大於半徑方向外 插通於旋轉軸A方向的螺^拾42C中設有複數將螺栓646 644a成為直徑朝向減进撼642d。外輪644之内周面 外輪644之外周面側而變小之錐形面。此外, 徑稍小的圓筒面。再者,為比輪入側開口部533d之直 對應之位置形成有複數鱼螺^ 644中,在與螺栓孔642d 將外輪644及内輪642插入、=646卡合之陰螺紋644c。 服馬達535之驅動軸535&雨入側開口部533d與AC伺 a間的間隙,其次藉由螺栓646 35 200902971 = 固定於外輪644,進一步藉由緊固螺栓646, 而内輪642之圓筒面642b強力壓迫人(:伺Further, the support shaft 526 is rotatably supported in the middle by the fixed end side bearing 524. The fixed end side bearing 524 is also strongly fixed to the fixed end support plate 521 by means of bolting, welding, or the like. Next, a description will be given of a mechanism for fixing the fixed end support plate 521 to the lower frame 51A. As shown in Fig. 11, a pair of grooves 511 are formed in the lower frame 5j, and the fixed support plate 521 is fixed to the lower frame 51 by using the grooves 511 and the bolts 5, 12. On the support floor 521, there are seven (ie, 14) insertion holes 521a of the insertion bolts 512 along the respective grooves 511, and all the mounting bolts 512 of the through holes 521a are fixed to the lower frame. 51〇. The mouth and the cutting board are cut and strengthened. Next, the fixed end branch structure is fixed by the bolt 512. The twelfth figure is the eleventh figure: the plate 521 is as shown in the twelfth figure, and the groove 511 is a groove having a wide width of the width of the lower portion 5nb. In addition, 蝉2 邛 511a has a hexagonal hex wrench _&: 丨S19 & 检 形成 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 六角 六角 六角 六角 六角 六角 六角 511 511 511 511 C = The size of the female offender is only slightly smaller than the width of the lower portion 511b. The width of the screw is large, so that the upper portion 511a of the head nut 512 of the bolt 512, the end cutting plate 521 and the groove 511/the bud plate 521 are strongly fixed to the lower frame 510.疋端支30 200902971 Next, the configuration of the driving end support portion 530 will be described. As shown in the tenth figure, the drive end support portion 53A has an 537 for mounting the drive chuck for the test piece s = side chuck 574. A speed reduction mechanism 536 is provided on the surface of the mounting flange 537 opposite to the surface on which the drive 574 is mounted. Specifically, the tray is formed with a mounting flange on the output shaft of the speed reduction mechanism 536. The speed-changing mechanism 536 converts the high-speed, low-torque rotational motion of the input shaft to the low-speed, high-torque of the wheel-out shaft. Rotating motion. The output shaft is disposed (the drive that is transmitted to the test piece s via the flange 537 and the chuck 574) is fixed to the side frame 532 on the drive side of the drive end support portion 53. The side of the drive end side The frame 532 is strongly pressed by the welding end support member 531 of the end support portion 53G. The drive end support plate 531 is fixed to the lower frame 510 by the same fixing means as the fixed end support plate 521. The side frame 'M2 is a plate-shaped member that is substantially perpendicular to the rotation axis A, and a reinforcing rib 532a is formed at a corner portion formed by the side frame 532 and the driving end support plate 531. The rib 532a is also welded to The drive end support plate 531 and the i-quot; side end frame 532 on the drive end side. Therefore, the side frame 532 and the drive end plate 531 are integrated with rigidity back. As described above, the drive end support plate 1 is strongly fixed to the lower frame 510. Therefore, the side frame 532 is visible as a rigid body with the base B. The central portion (between the grooves 511 and 511) of the lower frame 51 is shaped like a hole portion 514. The hollow portion 514 is provided for making The drive end @ ^ ^ 53〇 slides on the lower frame 51 〇 The feed in the A direction has a 'dry machine. As shown in the tenth and eleventh figures, a feed screw 544 extending in a direction parallel to the rotation axis A is provided in the cavity portion 514. Feeding is only 544. Both ends are rotatably supported by a pair of bearings 54s, S46 (thirth figure) 31 200902971. Further, a nut 548 that engages with the feed screw 544 is fixed under the drive end support plate 531. When the driving end support plate 531 is not fixed to the lower frame 510 (that is, the state in which the bolt for fixing the driving end supporting plate 531 is loosened), the driving end supporting portion 530 can be made by rotating the feeding screw 544. Further, it is moved along the feed screw 544. Further, at one end of the feed screw 544 (on the side of the bearing 545), a handle 542 for rotating the feed screw 544 is provided. In this embodiment, the drive end support portion 530 is thus provided. The movement of the fixed end support portion 520 and the drive end support portion 53 is adjusted in accordance with the size of the test piece s. Further, a pulley 538a of the encoder 538 is attached to the lower portion of the mounting flange 537 of the side frame 532. The outer peripheral portion 537a of the mounting flange 537 is also The function of the pulley is set up on the pulley 538a of the encoder 538 and the pulley 537a of the mounting flange 537. The encoder 538 calculates the number of rotations of the mounting flange 537 by detecting the rotation angle of the pulley 538a. The rotation angle of the initial position of the edge 537 and the number of cycles during the repeated test can be displayed on the display portion 538b of the code 538. Therefore, the operator of the torque test machine 5〇1 can be displayed from the display portion of the encoder 538. The display content of 538b confirms the progress of the torque test and the like. Next, the arrangement of the input shaft 536a of the speed reduction mechanism 536 and the AC feeding motor 535 that applies torque to the input shaft will be described. The twelfth figure is a sectional view of the III-III of the eleventh figure. As shown in Fig. 13, the input shaft 536 of the deceleration mechanism 536 is coupled to the drive shaft 535a of the AC servo motor 535 via a rigid coupling 533. Therefore, a torsional stress can be applied to the test piece s by driving the Ac servo motor 535. Further, as shown in the figure, the AC servo motor 535 is fixed to the side frame 532 via the motor support frame 534. Further, the speed reduction mechanism 536 is embedded in the opening 532b formed in the side frame 532 to be firmly fixed. In the present embodiment, the speed reduction mechanism 536 is a wave gear reduction mechanism. The wave gear reduction mechanism has a knowledge that the input shaft and the wheel output shaft are coaxial. Therefore, in the present embodiment, the rotary shaft A and the drive shaft 535a of the gossip servo motor 535 are coaxial. Since the rotation axis A is coaxial with the drive shaft 535a of the AC servo motor 535, the torque test machine 501 has a shape that is substantially symmetrical with respect to the vertical plane including the rotation axis a. Therefore, the weight of the test machine 501 is good, and vibration is not easily generated during the test. Further, the wave gear reduction mechanism has a feature that the backlash is extremely small. Therefore, the accuracy of the fatigue test can be greatly improved by the 'fluctuating gear reducer' in the fatigue tester σ which applies the reverse load to the test piece. To the extent that the inventors are aware, there is no one in the prior fatigue testing machine that utilizes a wave gear reducer. The rigid coupling 533 of the present embodiment constitutes extremely high torque rigidity, and the drive shaft 53 torque applied to the AC servo motor 535 can be transmitted to the input shaft 536a of the speed reduction mechanism 536 with high reactivity. Hereinafter, the configuration of the coupler 533 will be described. Fig. 14 is a cross-sectional view showing the rigid coupling 533 and the ac feeding motor 535 coupled to each other via the rigid coupling 533, and the turning shaft of the moving shaft 535a and the speed reducing mechanism 536 is enlarged. j As shown in the figure, 'the rigid coupling 533 is in the shape of a hollow round bar (that is, a cylinder with a stepped thickness). The coupling 533 has a spare gear inserted into the reducer to enter the second generation 3 t... The input remaining portion (10) above the motor 535 is implemented. The diameter of the input shaft of the machine = 33 200902971 is smaller than the driving shaft of the AC feeding motor 535, so the outer diameter of the output side cylindrical portion 533a is larger than the round side. The outer diameter of the cylindrical portion 5 is small. Further, the output side cylindrical portion 533 & and the input side cylindrical portion 5 are moved inside (the right side of the output_tube portion gamma and the left side of the input side cylindrical portion 533b in the fourteenth drawing) are narrowed, respectively. The diameters of the tearing narrow portions 533e and the welcoming portions 533e and 5, respectively, and the driving shaft of the speed reducing mechanism 536 are substantially equal to the diameter of the driving vehicle of the AC motor 535. Therefore, the inner peripheral surface of the narrow portion 533e^ 533f and the input shaft 536a of the speed reduction mechanism 536 and the outer circumference of the drive shaft 53 of the AC servo motor 535 have no gaps, and the input shaft 536a of the deceleration mechanism 536 is The drive shaft 535 of the AC servo motor 535 is accommodated in the narrow portion 533e' 533f. The output side opening portion 533c and the input side opening portion respectively constitute the outer diameter of the input shaft 536a of the speed reduction mechanism 536 and the drive shaft 535a of the AC servo motor 535. Large diameter. The fixing rings 630 and 640 are used to fix the output side opening 533c and the input side opening 533d to the input shaft 536a of the speed reduction mechanism 536 and the drive shaft 535a of the AC servo motor 535, respectively. The fixing ring 630 has an inner wheel 632, an outer wheel 634, and a bolt 636. The outer circumferential surface 632a of the inner ring 632 has a tapered surface whose diameter is smaller toward the AC servo motor side (the right side in the drawing). Further, the inner circumference of the inner ring 632 = 632b becomes a cylindrical surface slightly larger than the outer diameter of the input shaft of the speed reduction mechanism 536. On the side of the speed reduction mechanism of the inner wheel 632 (left side in the drawing), the shape j is larger than the flange portion 032c on the outer side in the radial direction. A plurality of bolt holes 632d for inserting the bolts 636 into the direction of the rotation axis A are provided in the flange portion 632c. The inner circumferential surface 634a of the outer ring 634 becomes a tapered surface whose diameter is smaller toward the side of the AC servo horse 34 200902971. Further, the outer circumferential surface 634b of the outer ring 634 is a cylindrical surface slightly smaller than the diameter of the output side opening portion 533c. Further, a plurality of female threads 634c that engage with the bolts 630 are formed in the outer wheel 634. The outer wheel 634 and the inner wheel 632 are inserted into the gap between the output side opening 533c and the input shaft 536a of the speed reduction mechanism 536, and then the inner wheel 632 is fixed to the outer wheel 634 by the bolt 636, further by the fastening bolt illusion 6, and the inner wheel 632 The inner peripheral surface 632b strongly presses the input shaft 536a of the speed reduction mechanism 536, and the cylindrical surface 63 of the outer wheel 634 strongly presses the output side opening = 533c. As a result, by the static friction generated, the speed reduction mechanism 536 is fixed to the output side cylinder of the rigid coupling 533, and is formed into a body. In addition, the figure shows that each of the two displays the two-hole phantom and the female thread 634c'. However, in fact, the speed-reducing mechanism 5 3 6 is the fourth you A cb, (for example, Η) group. A plurality of the same, the fixing ring 64 and the bolt 646 are provided on the circumference of the center. The outer wheel 642 is outside/face. The inner wheel 642 and the outer wheel 644 have tapered surfaces on the mechanism side. This 2a is a cylindrical surface whose diameter is reduced toward the inner circumferential surface of the second wheel (4) of the AC servo motor 535. Below the inner wheel 642, the flange 642c on the side of the outer diameter of the mountain 535a is slightly larger. The flange portion 4 is formed with a plurality of screws 42C which are enlarged in the radial direction and inserted in the direction of the rotation axis A. The plurality of bolts 646 644a are formed to have a diameter toward the reduction 撼 642d. The inner peripheral surface of the outer ring 644 has a tapered surface which becomes smaller on the outer peripheral side of the outer ring 644. In addition, the cylindrical surface is slightly smaller in diameter. Further, a female screw 644c is formed in a plurality of fish snails 644 at a position corresponding to the straight portion of the wheel-in opening portion 533d, and the outer ring 644 and the inner wheel 642 are inserted into the bolt hole 642d, and the female screw 644c is engaged. The clearance between the drive shaft 535 & the rain inlet side opening 533d and the AC servo a of the motor 535 is secondarily fixed to the outer wheel 644 by bolts 646 35 200902971 = further by the fastening bolt 646 and the cylindrical surface of the inner wheel 642 642b strongly oppressed people (: servant

^動,535a,外輪644之外周面⑽壓 =開口部533d。肖果藉由發生之靜摩擦力,从祠 入驅動軸加強固地固定於剛性聯結器533之輸 $側圓^遍,兩者形成―體。另外,圖中係分別各 杳不一、,且螺栓646、螺栓孔64^及陰螺紋64讣,不過, =上在將AC飼服馬達535之驅動軸咖的旋轉中心 軸作為中心的圓周上設有多數個(例如1〇組)。^, 535a, outer peripheral surface 644 outer peripheral surface (10) pressure = opening portion 533d. By the static friction that occurs, Xiaoguo is fixedly fixed to the rigid side of the rigid coupling 533 from the driving shaft, and the two form a body. In addition, the drawings are different, and the bolts 646, the bolt holes 64 and the female threads 64 讣, however, on the circumference centering on the central axis of rotation of the drive shaft of the AC feeding motor 535 There are a large number (for example, a group of 1).

。因為剛性聯結器533之輸出侧圓筒部533&及輸入侧 圓茼部533b的厚度充分大,所以剛性聯結器實質 地可視為剛體。因此,剛性聯結器533可將作用於AC 伺服馬達535之驅動軸535a的扭矩’以高反應性傳達至 減速機構536。 其次,就本實施例之扭力測試機台5〇1的控制計測 部之構成作說明。第十五圖係本實施例之扭力測試機台 501的控制計測部700之區塊圖。本實施例之扭力測試 機台501可在短時間進行疲勞測試,並可以短周期(每 ~秒鐘數十周期程度)在測試片上施加反覆扭力負載。 扭力測試機台501之控制計測部700具有:設定值 指示單元710、驅動控制單元720及測定單元750。 設定值指示單元710係用於指示如何在測試片Si 施加扭力應力的單元。具體而言,設定值指示單元710 係將安裝凸緣537 (或減速機構536之輸出軸)與初期 位置之角度作為訊號,而輸出至驅動控制單元720的單 元。設定值指示單元710具有:輸入介面712與波形產 生電路714。 36 200902971 輸入介面712係用於連接 二顯:之工作站的介面。扭力測試機Π。;: =工作站’指示如何使下部載台531變位。如=者 :試時’操作者操作工作站,輪入每單位時ίί 之扭力角度,並送訊至輸入介面712。 守間 :片S上施加反覆負載之疲勞測試 = 站,而輸入扭力角度之振幅、頻率及波形 或三角波之波形等),並 人^使用正弦波 ,. 迗汛至輸入介面712。輸入於銓. Since the thickness of the output side cylindrical portion 533 & and the input side rounded portion 533b of the rigid coupling 533 is sufficiently large, the rigid coupling can be substantially regarded as a rigid body. Therefore, the rigid coupling 533 can transmit the torque ' acting on the drive shaft 535a of the AC servo motor 535 to the speed reduction mechanism 536 with high reactivity. Next, the configuration of the control measuring unit of the torque testing machine 5〇1 of the present embodiment will be described. The fifteenth diagram is a block diagram of the control measuring unit 700 of the torque testing machine 501 of the present embodiment. The torque testing machine 501 of the present embodiment can perform the fatigue test in a short time, and can apply a reverse torque load on the test piece in a short cycle (a few tens of cycles per second). The control measurement unit 700 of the torque test machine 501 has a set value instruction unit 710, a drive control unit 720, and a measurement unit 750. The set value indicating unit 710 is a unit for indicating how to apply a torsional stress on the test piece Si. Specifically, the set value instructing unit 710 outputs the angle of the mounting flange 537 (or the output shaft of the speed reducing mechanism 536) to the initial position as a signal, and outputs it to the unit of the drive control unit 720. The set value indicating unit 710 has an input interface 712 and a waveform generating circuit 714. 36 200902971 Input interface 712 is used to connect the interface of the two display: workstation. Torque test machine Π. ;: = Workstation' indicates how to displace the lower stage 531. For example, if the operator is operating the workstation, the torque angle of each unit is rotated and sent to the input interface 712. Guard: The fatigue test of the repeated load on the sheet S = station, and the amplitude, frequency and waveform of the input torque angle, or the waveform of the triangle wave, etc., and the sine wave, 迗汛 to the input interface 712. Enter in 铨

)丨面712之指示傳送至波形產生電路714。 、’J 波形產生電路714解釋從輸入介面71味 2次運算安裝凸緣537與初期位置之角度的變ΐ ^將"达訊至驅動控制單元72〇。另外,進行疲勞測試 4,不僅限於以單一之正弦 ' 率扭轉測試片s,亦可依據==一疋波形、頻 机^入 伙踝從具有各種振幅及頻率之函 ^斤合成的函數扭轉測試片s。如亦可依據乘以頻率不 :綾2波Ϊ函數’扭力角之振幅隨時間變化地使安裝 凸緣537驅動。The indication of facet 712 is passed to waveform generation circuit 714. The 'J waveform generation circuit 714 interprets the change from the input interface 71 to the angle of the mounting flange 537 from the initial position, which will be the same as the drive control unit 72. In addition, the fatigue test 4 is not limited to twisting the test piece s with a single sine' rate, and the test piece can be twisted from a function having a combination of various amplitudes and frequencies according to the == one waveform and the frequency machine. . The mounting flange 537 can also be driven as a function of time, depending on the multiplication by the frequency: 绫2 Ϊ function.

政71= Ϊ緣537之角度作為數位訊號而從波形產生電 =:14輸出。因而,從波形產生電路m賴至驅動控 ^兀720之‘虎’首先輸入D/A轉換器722轉換成 =訊號。轉換成類比訊號之安裝凸緣爪的角度資訊 傳送至放大器724。而後,放大器724將從D/A 才、器722傳送之安裝凸緣537 #角度資訊放大後輸 出。 —如前述,本實施例中,係藉由AC伺服馬達535驅 動安展凸緣537❿進行各種測試。此處,AC伺服馬達 535内藏用於檢測驅動軸535& (第十圖)之轉數的編碼 37 200902971 器,編碼器檢測出之轉數送訊至驅動控制單元720之現 在位置運算電路726。 現在位置運算電路726依據AC伺服馬達535之編 碼器的檢測結果,運算安裝凸緣537之現在角度而輸 出。而後,將放大器724之輸出與現在位置運算電路726 之輸出的差分(亦即相當於安裝凸緣537之目標角度與 現在角度之差的訊號)送訊至電流產生電路728。 電流產生電路728依據收訊之訊號,產生輸出至AC 伺服馬達535之三相電流,並將其輸出至AC伺服馬達 535。結果,驅動AC伺服馬達535使安裝凸緣537之角 度到達目標角度。 藉由驅動安裝凸緣537而施加於測試片S的扭矩大 小,藉由負載傳感器562及用於將負載傳感器562之變 形量作為電訊號而取出的橋接電路756而檢測。檢測出 之扭矩的大小藉由A/D轉換器758轉換成數位訊號, 並經由輸出介面759而送訊至工作站。工作站統計從輸 出介面759送訊之扭矩的大小,產生如將時間轴作為橫 軸,將施加於測試片之扭力應力作為縱軸的圖形而顯 示。 此外,亦可進行將A/D轉換器758之輸出的扭矩 大小傳送至波形產生電路714,因應扭矩而使測試片S 之扭力的行動變化之所謂反饋控制。如安裝凸緣537之 旋轉角度與扭矩並非正比關係,亦即測試片S產生升降 時,可進行擴大扭力角度之振幅等的控制。 藉由使用以上構成之扭力測試機台501,可進行測 試片之靜態破壞測試及疲勞測試等。此處,本實施例中 係使用反應性高,且高扭矩之AC伺服馬達535而扭轉 38 200902971 測試片S。因而’扭力測試機台5〇1可 、 kN· m之扭矩施加於測試片s,此外,亦η敢大達數百 之高頻而將反覆負載施加於測試片s。因、可以數十Ηζ 施例之扭力測試機台5(U時,可在短時^使 勞破壞,且可謀求縮短測試時間。 便測式片疲 此外,採用本實施例之構成時,如 一 用於扭轉測試片S之動力來源的Ac伺 二圖所示, 用於將AC伺服馬達535之驅動軸535二達535,與 速機構536固定於同一板面的侧框架幻2疋轉,速的減 將AC伺服馬達535之驅動軸與 士藉此,可 入軸536a的相對位置高精確度地定 1,構536之輸 輕易且更正確地進行AC伺服馬達535之H。因而,可 減速機構536之輸入軸536a的定心。士軸535a與 成 置 板面上全部配置相對位置需要高精確由f同— :可高精確度地穩定維持已定位之各;件== 如此,採用本實施例之構成時,可使 ,而高精確度地進行AC飼服馬達535 (驅動軸二 及減速機構536之輸入軸536a的定心。因而,因定 差而作^AC伺服馬達535之驅動輛5&及減構 536之輸入轴536a間的彎曲應力較小。通常用於聯结^ 服馬達與減速機構之輸入軸的聯結器,係使用藉由有低 剛性之材料(橡膠等)介入,以緩和彎曲應力而構成的 軟性聯結器。但是,本實施例中,如上述,因為可高精 確度地進行兩軸之定心,所以可使用以剛性高之材料所 形成的剛性聯結器533。因而,可以高反應性使作用於 AC伺服馬達535之驅動軸535a的扭矩傳達至減速機構 39 200902971 536之輸入軸536a。 另外’本實施例中,係藉由剛性聯結器533而聯結 AC伺服馬達535之驅動軸535&與減速機構536之輸入 軸536a 不過,本發明並非限定於上述構成者。亦即’ 亦可取代Π! 聯結n,而使帛本發明第二實施例之半岡 性聯結器’聯結Ac伺服馬達535之驅動軸53Sa與減速 機構536之輪入軸536a而構成。 时一如以^之說明,本發明第一及第二實施例中,係在 早之支撐板(工作台33)上固定伺服馬達、線性導軌 及軸承,此等構件以支撐板作為基準而組合。因而,確 ^構件之精確度容易。此外,因為可使伺服馬達、線 ^執及,相之輯較小,所以可將熱膨脹造成之誤 制在取小限度。此外,因為將從滾珠螺桿至伺服馬 =驅動軸的連接點數量抑制在最小限度,所以,一旦 =¾、地進行進給螺桿與伺服馬達之驅動軸的定心後,維 寺使馬達之驅動軸的旋轉中心與進給螺桿之旋轉中心 精確地(,差數為數十μιη以内)一致的狀態容易。因 ^ ’可、將#由進給螺桿與馬達之轉㈣非直線性聯結 ,心,聯結角)而在旋轉部上發生之彎曲應力抑制為 ϋ此’可以扭力剛性高之剛性聯結11或半剛性聯 給螺桿與馬達之驅動軸,可以高反應性使進 :螺杯^轉驅動。因而’採用本發明之實施例的構成 + ,可現使用進給螺桿機構驅動十字頭,且以高周期 ^反覆負载(應變)正確地施加於職片的通用測試機 口。此外,此種線性驅動器即使對於如在十字頭上固定 式體之狀態下,驅動線性驅動器,而激振供測試體 激振測試機台亦有用。此外,聯結器之聯結部宜具有 200902971 與進給螺桿及伺服馬達之驅動軸相等或其以上之扭力 剛性。 此外,剛性聯結器具有與進給螺桿及伺服馬達之旋 轉軸相等或其以上的剛性之筒狀本體,並分別從其一端 插入進給螺桿,且從另一端插入伺服馬達之驅動軸而與 筒狀本體固定。筒狀本體中,插入進給螺桿及伺服馬達 之驅動軸的内孔之一部分宜成為與進給螺桿及伺服馬 達之驅動轴的圓周面概略無間隙地收容之狹窄部。此 外,宜藉由在剛性聯結器之筒内周面與進給螺桿及前述 馬達之驅動軸的圓周面之間嵌入固定用環,而固定進給 螺桿及馬達之驅動軸與剛性聯結器。如固定用環具有: 外周為錐形面之内輪;内周為對應於内輪之外周的錐形 面之外輪;及在内輪之外周抵接外輪之内周的狀態下, 將内輪及外輪之任何一方向另一方撥壓於其軸方向的 擠壓裝置。如此構成時,可更強固地聯結馬達之驅動軸 與進給螺桿,可以更高之反應性使馬達之驅動軸的扭矩 傳達至進給螺桿。 本發明第一及第二實施例之通用測試機台及線性 驅動器,亦可取代剛性聯結器而使用半剛性聯結器。 藉由以在彎曲方向具有撓曲性,且阻礙傳達在馬達 之驅動軸的延長方向之振動的半剛性聯結器聯結馬達 之驅動軸與進給螺桿,可以高反應性驅動進給螺桿,且 即使有若干軸偏差,仍不致發生極端大之内部輕曲,而 可平滑地驅動,並且可遮斷馬達驅動軸方向之振動。 半剛性聯結器宜具備由樹脂或橡膠形成之黏彈性 元件。此外,半剛性聯結器係構成伺服馬達之驅動軸的 振動衰減率以驅動轴之固有振動數為最大。藉由此種構 41 200902971 成’半剛性聯結器内 π 經由驅動軸而傳送之幸*彈性元件可有效地衰減從馬建 此種振動幾乎不致傳達=向或軸之半徑方向的振動,使 此外’半剛性聯& ‘二 】 外輪;及配置於該具備:屬於剛體元件之1 彈性元件的内輪。分別7之間’而包含彈性元件或勒 在内輪之中心报古、士·在外輪之中心形成有錐形孔,並 穿孔。此外,在㈣之用夕^通^聯結之轴的圓柱狀之貫Politics 71 = The angle of 537 is used as a digital signal to generate electricity from the waveform =: 14 output. Therefore, the "tiger" from the waveform generating circuit m to the drive control 720 is first input to the D/A converter 722 to be converted into a signal. The angle information of the mounting flange claws converted into analog signals is transmitted to the amplifier 724. Then, the amplifier 724 amplifies the mounting flange 537 # angle information transmitted from the D/A 722, and outputs it. - As described above, in the present embodiment, various tests are performed by driving the opening flange 537 by the AC servo motor 535. Here, the AC servo motor 535 has a code 37 200902971 for detecting the number of revolutions of the drive shaft 535 & (the tenth figure), and the encoder detects the number of revolutions sent to the current position operation circuit 726 of the drive control unit 720. . The position calculating circuit 726 now outputs the current angle of the mounting flange 537 based on the detection result of the encoder of the AC servo motor 535. Then, the difference between the output of the amplifier 724 and the output of the current position calculating circuit 726 (i.e., the signal corresponding to the difference between the target angle of the mounting flange 537 and the current angle) is sent to the current generating circuit 728. The current generating circuit 728 generates a three-phase current output to the AC servo motor 535 based on the received signal and outputs it to the AC servo motor 535. As a result, the AC servo motor 535 is driven to bring the angle of the mounting flange 537 to the target angle. The torque applied to the test piece S by driving the mounting flange 537 is detected by the load cell 562 and the bridge circuit 756 for taking out the amount of deformation of the load cell 562 as an electrical signal. The magnitude of the detected torque is converted to a digital signal by A/D converter 758 and sent to the workstation via output interface 759. The workstation counts the magnitude of the torque transmitted from the output interface 759, and produces a pattern in which the time axis is the horizontal axis and the torsional stress applied to the test piece is plotted on the vertical axis. Further, a so-called feedback control for transmitting the torque of the output of the A/D converter 758 to the waveform generating circuit 714 and changing the torque of the test piece S in response to the torque may be performed. If the rotation angle of the mounting flange 537 is not proportional to the torque, that is, when the test piece S is lifted and lowered, the amplitude of the torsion angle can be controlled. By using the above-described torque testing machine 501, it is possible to perform static breaking test, fatigue test, and the like of the test piece. Here, in the present embodiment, the AC servo motor 535 having high reactivity and high torque is used to twist the 38 200902971 test piece S. Therefore, the torque of the torque testing machine 5 〇 1 and kN· m is applied to the test piece s, and η dares to reach a high frequency of several hundreds to apply a reverse load to the test piece s. Therefore, it is possible to use dozens of torque test machines 5 of the example (U can break the work in a short time, and can shorten the test time.) The test piece is fatigued, and when the configuration of the embodiment is used, The Ac servo diagram for the power source for twisting the test piece S is used to rotate the drive shaft 535 of the AC servo motor 535 to 535, and the side frame fixed to the same plate surface as the speed mechanism 536 is tweeted. By subtracting the drive shaft of the AC servo motor 535, the relative position of the input shaft 536a is accurately set to 1, and the transmission of the structure 536 easily and more accurately performs the H of the AC servo motor 535. Thus, the speed can be reduced. The centering of the input shaft 536a of the mechanism 536. The relative position of the shaft 535a and the forming plate surface needs to be highly accurate by f-: the high-precision and stable maintaining of each position; the piece == In the configuration of the embodiment, the centering of the AC feeding motor 535 (the driving shaft 2 and the input shaft 536a of the speed reducing mechanism 536 can be performed with high precision. Therefore, the driving of the AC servo motor 535 is caused by the difference. The bending stress between the 5& and the input shaft 536a of the subtractive structure 536 is small. A coupler generally used for coupling an input shaft of a motor and a speed reduction mechanism is a soft coupler constructed by interposing a material having low rigidity (rubber or the like) to relieve bending stress. However, in this embodiment As described above, since the centering of the two shafts can be performed with high precision, the rigid coupling 533 formed of a material having high rigidity can be used. Therefore, the driving shaft 535a acting on the AC servo motor 535 can be made highly reactive. The torque is transmitted to the input shaft 536a of the speed reduction mechanism 39 200902971 536. In the present embodiment, the drive shaft 535 & of the AC servo motor 535 and the input shaft 536 of the speed reduction mechanism 536 are coupled by the rigid coupling 533. The invention is not limited to the above-described constituents, that is, 'can also be replaced by Π!, and the semi-coupling coupler of the second embodiment of the present invention is coupled to the drive shaft 53Sa of the Ac servo motor 535 and the wheel of the speed reduction mechanism 536. The first shaft and the second embodiment of the present invention fix the servo motor, the linear guide rail and the bearing on the early support plate (the work table 33). These components are combined with the support plate as a reference. Therefore, the accuracy of the component is easy. In addition, since the servo motor, the wire can be held, and the phase is smaller, the thermal expansion can be misused. In addition, since the number of connection points from the ball screw to the servo horse = drive shaft is kept to a minimum, once the centering of the drive shaft of the feed screw and the servo motor is performed, the temple is made. It is easy to accurately match the center of rotation of the drive shaft of the motor with the center of rotation of the feed screw (the difference is within several tens of μm). Because of the non-linearity of the feed screw and the motor (4) The bending stress occurring on the rotating portion is suppressed by the coupling, the heart, and the coupling angle. Therefore, the rigid coupling 11 or the semi-rigid coupling screw and the motor drive shaft can be highly reactive. ^ Turn to drive. Thus, with the configuration + of the embodiment of the present invention, the feed screw mechanism can be used to drive the crosshead, and the load (strain) is applied to the general test machine of the job at a high cycle. In addition, such a linear actuator drives a linear actuator even in the state of a fixed body such as a crosshead, and excitation is also useful for the test body excitation tester. In addition, the coupling portion of the coupler preferably has a torque of 200902971 equal to or greater than the drive shaft of the feed screw and the servo motor. In addition, the rigid coupling has a rigid cylindrical body equal to or above the rotation axis of the feed screw and the servo motor, and is inserted into the feed screw from one end thereof, and the drive shaft of the servo motor is inserted into the cylinder from the other end. The body is fixed. In the cylindrical body, one of the inner holes into which the feed screw and the drive shaft of the servo motor are inserted is preferably a narrow portion that is accommodated substantially without a gap with the circumferential surface of the feed screw and the drive shaft of the servo motor. Further, it is preferable to fix the feed shaft of the feed screw and the motor and the rigid coupling by inserting a fixing ring between the inner circumferential surface of the cylindrical body of the rigid coupling and the circumferential surface of the feed screw and the drive shaft of the motor. For example, the fixing ring has: an inner wheel whose outer circumference is a tapered surface; an inner circumference which is a tapered outer surface corresponding to the outer circumference of the inner wheel; and a state in which the outer circumference of the outer wheel abuts the inner circumference of the outer wheel, and any one of the inner wheel and the outer wheel The other side of the direction is pressed against the extrusion device in its axial direction. According to this configuration, the drive shaft of the motor and the feed screw can be more strongly coupled, and the torque of the drive shaft of the motor can be transmitted to the feed screw with higher reactivity. The universal test machine and the linear actuator of the first and second embodiments of the present invention can also use a semi-rigid coupling instead of the rigid coupling. By feeding the drive shaft and the feed screw of the motor with a semi-rigid coupling that has flexibility in the bending direction and hinders vibration in the direction of extension of the drive shaft of the motor, the feed screw can be driven with high reactivity, even if There are a number of axis deviations that still do not cause extreme large internal soft curvatures, but can be driven smoothly and can block vibrations in the direction of the motor drive shaft. The semi-rigid coupling should preferably have a viscoelastic element formed of resin or rubber. Further, the semi-rigid coupling constitutes the vibration damping rate of the drive shaft of the servo motor to maximize the natural vibration number of the drive shaft. With this configuration 41 200902971 into the 'semi-rigid coupling π through the drive shaft to transmit the * elastic element can effectively attenuate the vibration from the horse to the vibration of the horse or the axis of the shaft, so that 'Semi-rigid joint & 'two outer wheel; and an inner wheel provided with one elastic element belonging to a rigid body element. Between the 7's respectively, the elastic element is included or the center of the inner wheel is reported, and the tapered hole is formed in the center of the outer wheel and perforated. In addition, in the (4) of the use of the evening, the axis of the joint of the cylindrical column

;;:rr一内周=端 穿孔中插入進給螺桿及伺服馬達之驅動轴丄 形面抵接-對外輪之錐㈣*㈣之錐 ,it Λ 稭由以螺栓彼此固 疋°亥f卜輪並經由内輪而聯結其轴。藉由如此椹 成,可以極簡單之構成實現以高反應性傳達 動的半剛性聯結器。藉此,實現振動雜 3孔 >、且反應性南之線性驅動器。 此外$ 了構成在支撐板上^有插通進給螺桿之開 口部,在開口部中固定可旋轉地支撐進給螺桿的轴承之 外輪。如此構成時,因為軸承、線性導軌及伺服馬達形 成一體,所以可維持更精確地使馬達之驅動軸的旋轉中 心與進給螺桿之旋轉中心一致的狀態。 此時’轴承係正面組合形之組合角滾珠轴承而構成 時,於測試時,可以轴承支樓施加於進給螺桿之推力方 向的大負載’且可旋轉地支撐進給螺桿。 此外,亦可為進給螺桿係滾珠螺桿,且螺母係滾珠 螺桿用之螺母而構成’亦即十字頭以滾珠螺桿機構而驅 動之構成。如此構成時,可以小齒隙使十字頭高速來回 運動,而使負載之反覆速度更加高速。 42 200902971 二=構=有線性導執之固定部與可移動部的 動之移動塊,移動塊具有:包圍執道之凹部;^移動 塊之移動方向而形成於該凹部的溝 部之溝形成閉路地與溝之前述移動方向兩端;;:rr one inner circumference = the end of the perforation inserted into the feed screw and the servo motor's drive shaft 抵-shaped surface abutment - the outer wheel cone (four) * (four) cone, it Λ straw by the bolts to each other The wheel is coupled to its shaft via the inner wheel. By doing so, it is extremely simple to construct a semi-rigid coupling that transmits with high reactivity. Thereby, a vibrational three-hole > and a reactive south linear actuator are realized. Further, the opening portion of the feed screw is formed on the support plate, and the outer wheel of the bearing rotatably supporting the feed screw is fixed in the opening portion. According to this configuration, since the bearing, the linear guide, and the servo motor are integrally formed, it is possible to maintain a state in which the center of rotation of the drive shaft of the motor and the center of rotation of the feed screw are more accurately matched. In this case, when the bearing is combined with the combined angular ball bearing, the bearing can be applied to the large load in the thrust direction of the feed screw and the feed screw can be rotatably supported. Further, it may be configured such that the screw-type ball screw is fed and the nut is a nut for the ball screw, that is, the crosshead is driven by the ball screw mechanism. When constructed in this way, the crosshead can be moved back and forth at high speed with a small backlash, and the speed of the load can be made higher. 42 200902971 Two = structure = moving block with fixed guide and movable part of linear guide, moving block has: concave part surrounding the obstruction; ^ moving direction of moving block and groove formed in the groove of the concave part forms closed circuit Both ends of the moving direction of the ground and the groove

出路徑路中循環’並且位於溝内時與前:執道 抵接之稷數雜。再者,須構成移動塊中形成有四個上 述閉路,該四_路中’兩個閉路之配置於各個溝的滚 珠具有對線性導軌之逕向方向概略為±45度之接觸角, 其他兩個閉路之配置於各個溝的滾珠具有對線性導軌 之反逕向方向概略為±45度之接觸角。 使用如此構成之線性導軌時,即使在測試片上施加 大負載時’進給螺桿機構之螺母不致搖晃,可平滑地沿 著線性導軌移動。 ,外斤本發明苐三實施例之扭力測試機台,在固定 於框架之第一支撐構件(驅動端側之側框架532)上固 定有祠服馬達與減逮機構。 =此本發明之構成中,單一構件之第一支撐構件 上固定舰馬達與減速機構兩者’此等構件係以第一支 樓構件作為鱗心合。因而,確保各構件之精確度容 易。此外,因為可使伺服馬達與減速機構間之距離較 小,所以可將熱膨服造成之誤差抑制在最小限度。此 外,因為將從飼服馬達之驅動軸至減速機構之輸入軸的 連接占”量抑制在最小限度,所以一旦精密地進行伺服 馬達之驅練與滅速機構之輸人軸的定讀,維持使馬 達之驅動轴的旋轉中^與進給螺桿之旋轉巾心精確地 (誤差為數十μηι以内)一致的狀態容易。因而,可使 43 200902971 藉由減速機構之輸八軸與馬達 結(偏心及聯結角)旋 ^的非直線性 小。因可以具有高扭力剛性彎曲應力極 聯結器聯結減速機構 帅聯結ϋ或半剛性 ,吏減速機構之輪入轴旋轉:之:動轴’可以高 周期將扭力倉速機構扭轉測試片,: 驅 ,減速機構之輸入軸與前述飼:的f力測試機台^ 裔之聯結部’宜具有與減迷機構之*入^驅_的聯結 動軸相等或其以上的扭力剛性。〗由及伺服馬達之 此外,宜進—步具有固定於框架上 (固定端側之側框架522),第二 支撐構件 ,《臂梁狀咖定支撐於前:’藉由 把持部固定於前述框架上。該構成中了3構件’第二 念撐構件之間固定用於計測作 々在軸部與第二 持部之轴部的固定端側軸承裝置。讀地支撐第二把 此外,減速機構宜係波動齒輪減球 構及行星#輪機狀其他減賴構@ #。蜗輪機 減速機構反覆扭轉測試片時之齒=所因為=輪 5=二勞^。1齒輪減速機構 件而固疋,错此以南剛性而與第—切構件一體化。 【圖式簡單說明】 视圖第一圖係本發明第—實施例之通用測試機台的前 第二圖係本發明第-實施例之通用剩試機台的可 44 200902971 移動部及其周圍的縱剖面圖。 的剛 的工 第三圖係本發明第一實施例之通用測試 性聯結及其周圍的縱剖面圖。 第四圖係本發明第一實施例之通用測試機台 作台之貫穿孔附近之縱剖面圖。 σ ,五圖係在本發明第一實施例之通用測試機台 二在垂直於執道之長軸方向的—面切斷移動塊 的剖面圖。 <When the path is looped in the path and is located in the ditch, it is mixed with the front: the obstruction. Furthermore, four closed circuits are formed in the moving block, and the balls disposed in the respective grooves of the two closed paths have a contact angle of ±45 degrees to the radial direction of the linear guide, and the other two The balls disposed in each of the closed channels have a contact angle of ±45 degrees to the reverse radial direction of the linear guide. When the linear guide thus constructed is used, even if a large load is applied to the test piece, the nut of the feed screw mechanism does not wobble and smoothly moves along the linear guide. In the torque testing machine of the third embodiment of the present invention, the squatting motor and the slamming mechanism are fixed to the first supporting member (the side frame 532 on the driving end side) fixed to the frame. = In the constitution of the present invention, both the fixed ship motor and the speed reduction mechanism are attached to the first support member of the single member. These members are centered on the first branch member. Thus, it is ensured that the accuracy of each component is easy. In addition, since the distance between the servo motor and the speed reduction mechanism can be made small, the error caused by the thermal expansion can be minimized. In addition, since the amount of connection from the drive shaft of the feeding motor to the input shaft of the speed reduction mechanism is minimized, once the servo motor is accurately drilled and the input shaft of the deceleration mechanism is fixed, the maintenance is maintained. It is easy to make the rotation of the drive shaft of the motor coincide with the rotation of the feed screw accurately (within an error of several tens of μηι). Therefore, 43 200902971 can be connected to the eight-axis and the motor by the speed reduction mechanism ( Eccentricity and coupling angle) The non-linearity of the screw is small. Because it can have high torsion rigidity, the bending stress is extremely coupled to the deceleration mechanism, and the semi-rigid, the rotation of the wheel of the 吏 reduction mechanism: the moving shaft can be high The cycle will twist the test mechanism with the torque mechanism, and the input shaft of the drive and the speed reduction mechanism and the above-mentioned feeding force test unit of the f-force test machine should have a coupling axis with the deflation mechanism. Torque rigidity equal to or above. In addition to the servo motor, the step is to be fixed to the frame (the side frame 522 on the fixed end side), the second support member, "the beam is supported by the arm : 'The fixing portion is fixed to the frame. In this configuration, the fixed member-side bearing device for measuring the shaft portion of the shaft portion and the second holding portion is fixed between the two members. Reading the ground support second, in addition, the speed reduction mechanism should be the wave gear reduction ball structure and the planetary # turbine-like other depreciation structure @ #. The turbine speed reduction mechanism repeatedly twists the test piece when the tooth = because = wheel 5 = two labor ^ 1 The gear reducer member is fixed, and the south is rigid and integrated with the first-cut member. [Schematic description] The first view of the first embodiment of the present invention is the first test machine of the present invention. 2 is a longitudinal cross-sectional view of the movable portion of the universal residual test machine of the first embodiment of the present invention and its surroundings. The third working view of the first embodiment of the present invention is a universal test coupling of the first embodiment of the present invention. The fourth drawing is a longitudinal sectional view of the vicinity of the through hole of the universal testing machine of the first embodiment of the present invention. σ , the fifth drawing is the universal testing machine 2 of the first embodiment of the present invention. Cut off the plane in the direction perpendicular to the long axis of the road . FIG sectional block <

第六圖係第五圖之I—!剖面圖。 第七圖係本發明第一實施例之通用測試機台的 制計測部之區塊圖。 二 、第八圖係顯示將本發明第一實施例之線性驅動器 適用於激振測試機台的一例。 第九圖係本發明第二實施例之通用測試機台的半 剛性聯結器及其周圍之縱剖面圖。 第十圖係本發明第三實施例之扭力測試機台的 視圖。 第十一圖係本發明第三實施例之扭力測試機台的 俯視圖。 第十二圖係第十一圖之II 一 II剖面圖。 第十三圖係第十一圖之III — III剖面圖。 第十四圖係本發明第三實施例之扭力測試機台的 剛性聯結器及其周圍的縱剖面圖。 第十五圖係本發明第三實施例之扭力測試機台的 控制計測部之區塊圖。 【主要元件符號說明】 45 200902971 1 通用測試機台 10 機台框架部 10, 機台框架部 11 腳部 11a 上面 lib 内側側面 12 導桿 13 頂部 13a 貫穿孔 20 固定部 21 上部載台 21a 貫穿孔 21b 螺栓孔 21c 螺栓 22 進給螺桿 23a 螺母 24a 逕向滾珠軸承 24b 軸承支撐部 25 馬達 25a 驅動軸 26 齒輪盒 26a 輸出轴 26b 主動皮帶輪 27 無端皮帶 28 附件 30 可移動部 31 下部載台 31a 滾珠絲槓用螺母 31b 十字頭 33 工作台 33a 側面 33b 下面 33c 上面 33d 貫穿孔 33e 陰螺紋 34 剛性聯結器 34a 上部圓筒部 34b 下部圓筒部 34B 筒狀本體 34c 上部開口部 34d 下部開口部 34e 狹窄部 34f 狹窄部 35 AC伺服馬達 35a 驅動軸 36 滚珠螺桿 36a 螺桿部 36b 軸部 36c 陽螺紋 37 馬達支撐框架 40 線性導執 42 導引框 42a 側壁 42b 上部壁面 46 200902971 42c 開口部 144 外輪 44 軌道 144a 内周面 44a 溝 144b 圓筒面 44a, 溝 144c 陰螺紋 46 移動塊 146 螺栓 46a 溝 150 軸承部 46a, 溝 151 組合角滚珠軸承 46b 滾珠 151a 角滾珠軸承 46c 退出路徑 151b 角滚珠軸承 46d U字形路徑 152 第一轴承安裝構件 130 固定用環 152a 凸緣部 132 内輪 152b 貫穿孔 132a 外周面 153 第二軸承安裝構件 132b 内周面 153a 貫穿孔 132c 凸緣部 153b 盲板 132d 螺栓孔 154 第一套環 134 外輪 155 第二套環 134a 内周面 156 螺母 134b 外周面 157a 油封 134c 陰螺紋 157b 油封 136 螺栓 158a 螺栓 140 固定用環 158b 螺栓 142 内輪 159 襯塾 142a 外周面 200 控制計測部 142b 内周面 210 設定值指不单元 142c 凸緣部 212 輸入介面 142d 螺栓孔 214 波形產生電路 47 200902971 220 驅動控制單元 511b 下部 222 D/A轉換器 512 螺栓 224 放大器 512a 六角子L 226 現在位置運算電路 513 螺母 228 電流產生電路 514 空洞部 254 負載傳感器 520 固定端支撐部 256 橋接電路 521 固定端支撐板 258 A/D轉換器 521a 貫穿孔 259 輸出介面 522 固定端側之側框架 300 半剛性聯結器 522a 補強用之肋條 320 外輪 524 固定端侧軸承 340 外輪 526 支撐軸 322 内側面 527 安裝凸緣 342 内側面 530 驅動端支撐部 360 内輪 531 驅動端支撐板 360a 凸緣部 532 驅動端側之侧框架 362a 圓孔 532a 補強用之肋條 362b 圓孔 532b 開口 364 外側面 533 剛性聯結器 366 外側面 533a 輸出側圓筒部 324 螺栓孔 533b 輸入側圓筒部 368 螺栓孔 533c 輸出側開口部 382 螺栓 533d 輸入側開口部 501 扭力測試機台 533e 狹窄部 510 下部框架 533f 狹窄部 511 一對溝 535 AC伺服馬達 511a 上部 535a 驅動軸 48 200902971 536 減速機構 640 固定用環 536a 輸入軸 642 内輪 537 安裝凸緣 642a 外周面 537a 外周部 642b 内周面 538 編碼器 642c 凸緣部 538a 皮帶輪 642d 螺栓孔 538b 顯示部 644 外輪 539 無端皮帶 644a 内周面 544 進給螺桿 644b 外周面 545 軸承 644c 陰螺紋 546 軸承 646 螺栓 548 螺母 700 控制計測部 562 負載傳感器 710 設定值指不早元 572 卡盤 712 輸入介面 574 卡盤 714 波形產生電路 572a 爪 720 驅動控制單元 574a 爪 722 D/A轉換器 630 固定用環 724 放大器 632 内輪 726 現在位置運算電路 632a 外周面 728 電流產生電路 632b 内周面 750 測定單元 632c 凸緣部 756 橋接電路 634 外輪 758 A/D轉換器 634a 内周面 759 輸出介面 634b 外周面 B 基座 634c 陰螺紋 C 汽車 636 螺栓 s 測試片 49The sixth figure is the I-! section view of the fifth figure. The seventh drawing is a block diagram of the measuring unit of the universal testing machine of the first embodiment of the present invention. Second and eighth figures show an example in which the linear actuator of the first embodiment of the present invention is applied to an excitation test machine. The ninth drawing is a longitudinal sectional view of a semi-rigid coupling of a universal testing machine according to a second embodiment of the present invention. The tenth drawing is a view of a torque testing machine of a third embodiment of the present invention. The eleventh drawing is a plan view of a torque testing machine of a third embodiment of the present invention. Figure 12 is a cross-sectional view of the II-II of the eleventh figure. The thirteenth picture is a sectional view of the III-III of the eleventh figure. Fig. 14 is a longitudinal sectional view showing the rigid coupling of the torque testing machine of the third embodiment of the present invention and its surroundings. Fig. 15 is a block diagram showing a control measuring unit of the torque testing machine of the third embodiment of the present invention. [Main component symbol description] 45 200902971 1 Universal test machine 10 Machine frame part 10, machine frame part 11 Foot part 11a Upper surface lib Inner side surface 12 Guide rod 13 Top portion 13a Through hole 20 Fixing portion 21 Upper stage 21a Through hole 21b Bolt hole 21c Bolt 22 Feed screw 23a Nut 24a Radial ball bearing 24b Bearing support 25 Motor 25a Drive shaft 26 Gear box 26a Output shaft 26b Drive pulley 27 Endless belt 28 Attachment 30 Movable part 31 Lower stage 31a Ball wire Bar nut 31b Crosshead 33 Table 33a Side 33b Lower 33c Upper 33d Through hole 33e Female thread 34 Rigid coupling 34a Upper cylindrical portion 34b Lower cylindrical portion 34B Cylindrical body 34c Upper opening 34d Lower opening 34e Narrow portion 34f narrow portion 35 AC servo motor 35a drive shaft 36 ball screw 36a screw portion 36b shaft portion 36c male thread 37 motor support frame 40 linear guide 42 guide frame 42a side wall 42b upper wall surface 46 200902971 42c opening portion 144 outer wheel 44 inner rail 144a Circumference 44a groove 144b Cylindrical surface 44a, groove 144c female thread 46 moving block 146 bolt 46a groove 150 bearing portion 46a, groove 151 combined angular ball bearing 46b ball 151a angular ball bearing 46c exit path 151b angular ball bearing 46d U-shaped path 152 first bearing mounting member 130 Fixing ring 152a Flange portion 132 Inner wheel 152b Through hole 132a Outer peripheral surface 153 Second bearing mounting member 132b Inner peripheral surface 153a Through hole 132c Flange portion 153b Blind plate 132d Bolt hole 154 First ring 134 Outer wheel 155 Second ring 134a inner peripheral surface 156 nut 134b outer peripheral surface 157a oil seal 134c female thread 157b oil seal 136 bolt 158a bolt 140 fixing ring 158b bolt 142 inner wheel 159 lining 142a outer peripheral surface 200 control measuring portion 142b inner peripheral surface 210 set value indicating unit 142c convex Edge 212 Input Interface 142d Bolt Hole 214 Waveform Generation Circuit 47 200902971 220 Drive Control Unit 511b Lower 222 D/A Converter 512 Bolt 224 Amplifier 512a Hexagon L 226 Current Position Operation Circuit 513 Nut 228 Current Generation Circuit 514 Cavity 254 Load Sensor 520 fixed end Bracing portion 256 Bridge circuit 521 Fixed end support plate 258 A/D converter 521a Through hole 259 Output interface 522 Fixed end side side frame 300 Semi-rigid coupling 522a Reinforcement rib 320 Outer wheel 524 Fixed end side bearing 340 Outer wheel 526 Support Shaft 322 Inner side 527 Mounting flange 342 Inner side 530 Drive end support 360 Inner wheel 531 Drive end support plate 360a Flange portion 532 Drive side side frame 362a Round hole 532a Reinforcement rib 362b Round hole 532b Opening 364 Outer side 533 Rigid coupling 366 Outer side 533a Output side cylindrical portion 324 Bolt hole 533b Input side cylindrical portion 368 Bolt hole 533c Output side opening portion 382 Bolt 533d Input side opening portion 501 Torque test machine 533e Narrow portion 510 Lower frame 533f Narrow 511 a pair of grooves 535 AC servo motor 511a upper 535a drive shaft 48 200902971 536 speed reduction mechanism 640 fixing ring 536a input shaft 642 inner wheel 537 mounting flange 642a outer peripheral surface 537a outer peripheral portion 642b inner peripheral surface 538 encoder 642c flange portion 538a Pulley 642d bolt hole 538b display part 644 outer wheel 539 Endless belt 644a Inner circumferential surface 544 Feed screw 644b Outer circumferential surface 545 Bearing 644c Female thread 546 Bearing 646 Bolt 548 Nut 700 Control measuring unit 562 Load sensor 710 Setting value is not early 572 Chuck 712 Input interface 574 Chuck 714 Waveform Generation circuit 572a Claw 720 Drive control unit 574a Claw 722 D/A converter 630 Fixing ring 724 Amplifier 632 Inner wheel 726 Current position operation circuit 632a Outer peripheral surface 728 Current generation circuit 632b Inner peripheral surface 750 Measurement unit 632c Flange portion 756 Bridge circuit 634 outer wheel 758 A/D converter 634a inner circumferential surface 759 output interface 634b outer circumferential surface B pedestal 634c female thread C car 636 bolt s test piece 49

Claims (1)

200902971 十、申請專利範圍: 1. 一種通用測試機台,具有: 伺服馬達,其係使驅動軸來回旋轉運動; 進給螺桿; 聯結器,其係聯結前述進給螺桿與前述伺服馬達 之驅動轴; 螺母,其係與前述進給螺桿卡合; 線性導軌,其係將前述螺母之移動方向僅限制於 前述進給螺桿之轴方向; 固定部,其係抵接或固定測試片之一端; 十字頭,其係抵接或固定測試片之另一端,固定 於前述螺母,而與前述螺母一起移動;及 支撐板,其固定有前述伺服馬達及前述線性導 軌。 2. 如申請專利範圍第1項之通用測試機台,其中前述聯 結器之聯結部具有與前述進給螺桿及前述伺服馬達 之驅動軸相等或其以上的扭力剛性。 3. 如申請專利範圍第2項之通用測試機台,其中前述聯 結器係剛性聯結器。 4. 如申請專利範圍第3項之通用測試機台,其中前述剛 性聯結器具有筒狀本體,其具有與前述進給螺桿及前 述伺服馬達之驅動軸相等或其以上的扭力剛性,且分 別從其一端插入前述進給螺桿,從另一端插入前述伺 服馬達之驅動轴,而與該筒狀本體固定。 5. 如申請專利範圍第4項之通用測試機台,其中前述筒 狀本體中,插入前述進給螺桿及前述伺服馬達之驅動 軸的内孔之一部分,成為與前述進給螺桿及前述伺服 50 200902971 馬達之驅動軸的圓周面概略無間隙地收容的狹窄部。 6. 如申請專利範圍第4項之通用測試機台,其中藉由在 前述筒狀本體之内孔的内周面與前述進給螺桿及前 述伺服馬達之驅動轴的圓周面之間嵌入固定用環,而 固定該進給螺桿及該伺服馬達之驅動軸與前述剛性 聯結器。 7. 如申請專利範圍第6項之通用測試機台, 其中前述固定用環具有; 内輪,其外周成為錐形面; 外輪,其内周成為對應於前述内輪之外周的錐形 面;及 擠壓裝置,其係在使前述内輪之外周抵接前述外 輪之内周的狀態下,將該内輪及外輪中之任何一方向 另一方播壓於其轴方向。 8. 如申請專利範圍第2項之通用測試機台,其中前述聯 結器係構成在彎曲方向具有撓曲性,且阻礙傳達前述 伺服馬達之驅動軸的延長方向之振動的半剛性聯結 器。 9. 如申請專利範圍第8項之通用測試機台,其中前述半 剛性聯結器包含黏彈性元件。 10. 如申請專利範圍第9項之通用測試機台,其中前述黏 彈性元件之至少一部分以樹脂而形成。 11. 如申請專利範圍第9項之通用測試機台,其中前述黏 彈性元件之至少一部分以橡膠而形成。 12. 如申請專利範圍第8項之通用測試機台,其中前述半 剛性聯結器係構成在前述伺服馬達之驅動軸方向的 振動衰減率,在該驅動轴之固有振動數中為最大。 51 200902971 13. 如申請專利範圍第8項之通用測試機台,其中前述半 剛性聯結器具有: 一對外輪,其係在中心貫穿地形成了錐形孔的剛 體元件;及 彈性元件或黏彈性元件之内輪,其係配置於前述 一對外輪之間,形成用於通過聯結於中心之軸的圓柱 狀之貫穿孔,在外周之軸方向兩端形成有可分別與前 述一對外輪之錐形孔的内周卡合的錐形面; 在前述内輪之貫穿孔中插入前述進給螺桿及前 述伺服馬達之驅動軸,使前述内輪之錐形面抵接前述 一對外輪之錐形孔的内周,藉由以螺栓彼此固定前述 一對外輪,經由内輪而聯結其軸。 14. 如申請專利範圍第1項之通用測試機台,其中在前述 支撐板上設有插通前述進給螺桿之開口部,前述開口 部中固定有可旋轉地支撐前述進給螺桿之軸承的外 輪,前述轴承具有角滾珠轴承。 15. 如申請專利範圍第14項之通用測試機台,其中前述 軸承具有使一對角滾珠轴承之正面相對而組合的正 面組合型之組合角滾珠軸承。 16. 如申請專利範圍第1項之通用測試機台,其中前述進 給螺桿係滾珠螺桿,前述螺母係滾珠螺桿用之螺母。 17. 如申請專利範圍第1項之通用測試機台,其中前述支 撐板係一片金屬板,或是藉由焊接而將複數金屬板一 體化。 18. 如申請專利範圍第1項之通用測試機台,其中前述支 撐板焊接於前述通用測試機台之腳部。 19. 如申請專利範圍第1項之通用測試機台,其中前述線 52 200902971 性導軌具有:固定於前述固定部之第一部,與固定於 前述螺母之第二部,前述第一部與第二部之一方具有 軌道,且另一方與前述軌道卡合,且具有可沿著該軌 道而移動之移動塊,前述移動塊具有: 凹部,其係包圍前述軌道; 溝,其係在前述凹部中,沿著前述移動塊之移動 方向而形成; 退出路徑,其係形成於前述移動塊之内部,與前 述溝形成閉路地連繫前述溝之前述移動方向兩端;及 複數滚珠,其係在前述閉路中循環,並且位於前 述溝内時與前述軌道抵接。 20. 如申請專利範圍第19項之通用測試機台,其中在前 述移動塊中形成有四個前述閉路,前述四個閉路中, 兩個閉路之配置於各個溝的滾珠具有對線性導軌之 逕向方向概略為±45度之接觸角,其他兩個閉路之配 置於各個溝的滚珠具有對前述線性導軌之反逕向方 向概略為±45度之接觸角。 21. 如申請專利範圍第1項之通用測試機台,其中進一步 具有固定於前述腳部之至少一支固定部用導軸,前述 固定部藉由夾住前述固定部用導轴,而固定於前述固 定部用導軸,在前述固定部未夾住前述固定部用導軸 之狀態下,前述固定部可沿著前述固定部用導轴而移 動。 22. 如申請專利範圍第21項之通用測試機台,其中進一 步具有固定部驅動裝置,其係用於在前述固定部未夾 住前述固定部用導軸之狀態下,使前述固定部沿著前 述固定部用導軸而移動。 53 200902971 23. 如申請專利範圍第22項之通用測試機台,其中前述 固定部驅動裝置藉由進給螺桿機構而使前述固定部 移動。 24. —種線性驅動器,其具有: 伺服馬達; 進給螺桿; 聯結器,其係聯結前述進給螺桿與前述伺服馬達 之驅動軸; 螺母,其係與前述進給螺桿卡合; 線性導軌,其係將前述螺母之移動方向僅限制在 前述進給螺桿之軸方向;及 支撐板,其係固定有前述伺服馬達及前述線性導 執。 25. 如申請專利範圍第24項之線性驅動器,其中前述聯 結器之聯結部具有與前述進給螺桿及前述伺服馬達 之驅動轴相等或其以上之扭力剛性。 26. 如申請專利範圍第25項之線性驅動器,其中前述聯 結器係剛性聯結器。 27. 如申請專利範圍第26項之線性驅動器,其中前述剛 性聯結器具有筒狀本體,其具有與前述進給螺桿及前 述伺服馬達之驅動軸相等或其以上的扭力剛性,且分 別從其一端插入前述進給螺桿,從另一端插入前述伺 服馬達之驅動軸,而與該筒狀本體固定。 28. 如申請專利範圍第27項之線性驅動器,其中前述筒 狀本體中,插入前述進給螺桿及前述伺服馬達之驅動 軸的内孔之一部分,成為與前述進給螺桿及前述伺服 馬達之驅動軸的圓周面概略無間隙地收容的狹窄部。 54 200902971 29. 如申請專利範圍第27項之線性驅動器,其中藉由在 前述筒狀本體之内孔的内周面與前述進給螺桿及前 述伺服馬達之驅動轴的圓周面之間嵌入固定用環,而 固定該進給螺桿及該伺服馬達之驅動軸與前述剛性 聯結器。 30. 如申請專利範圍第27項之線性驅動器,其中前述固 定用環具有: 内輪,其外周成為錐形面; 外輪,其内周成為對應於前述内輪之外周的錐形 面;及 播壓裝置,其係在使前述内輪之外周抵接前述外 輪之内周的狀態下,將該内輪及外輪中之任何一方向 另一方擠壓於其轴方向。 31. 如申請專利範圍第25項之線性驅動器,其中前述聯 結器係構成在彎曲方向具有撓曲性,且阻礙傳達前述 馬達之驅動軸的延長方向之振動的半剛性聯結器。 32. 如申請專利範圍第31項之線性驅動器,其中前述半 剛性聯結器包含黏彈性元件。 33. 如申請專利範圍第32項之線性驅動器,其中前述黏 彈性元件之至少一部分以樹脂而形成。 34. 如申請專利範圍第32項之線性驅動器,其中前述黏 彈性元件之至少一部分以橡膠而形成。 35. 如申請專利範圍第31項之線性驅動器,其中前述半 剛性聯結器係構成在前述馬達之驅動轴方向的振動 衰減率,在該驅動軸之固有振動數中為最大。 36. 如申請專利範圍第31項之線性驅動器,其中前述半 剛性聯結器具有: 55 200902971 一對外輪,其係在中心貫穿地形成了錐形孔的剛 體元件;及 彈性元件或黏彈性元件之内輪,其係配置於前述 一對外輪之間,形成用於通過聯結於中心之軸的圓柱 狀之貫穿孔,在外周之兩端形成有可分別與前述一對 外輪之錐形孔的内周卡合的錐形部; 在前述内輪之貫穿孔中插入前述進給螺桿及前 述伺服馬達之驅動軸,使前述内輪之錐形面抵接前述 一對外輪之錐形孔的内周,藉由以螺栓彼此固定前述 一對外輪,經由内輪而聯結其軸。 37. 如申請專利範圍第24項之線性驅動器,其中在前述 支撐板上設有插通前述進給螺桿之開口部,前述開口 部中固定有可旋轉地支撐前述進給螺桿之轴承的外 輪,前述轴承具有角滾珠轴承。 38. 如申請專利範圍第37項之線性驅動器,其中前述軸 承具有使一對角滾珠軸承之正面相對而組合的正面 組合型之組合角滾珠轴承。 39. 如申請專利範圍第24項之線性驅動器,其中前述進 給螺桿係滚珠螺桿,前述螺母係滚珠螺桿用之螺母。 40. 如申請專利範圍第24項之線性驅動器,其中前述支 撐板係一片金屬板,或是藉由焊接而將複數金屬板一 體化。 41. 如申請專利範圍第24項之線性驅動器,其中前述線 性導執具有:固定於前述固定部之第一部,與固定於 前述螺母之第二部,前述第一部與第二部之一方具有 執道,且另一方與前述軌道卡合,且具有可沿著該軌 道而移動之移動塊,前述移動塊具有: 56 200902971 凹部,其係包圍前述軌道; 溝,其係在前述凹部中,沿著前述移動塊之移動 方向而形成; 退出路徑,其係形成於前述移動塊之内部,與前 述溝形成閉路地連繫前述溝之前述移動方向兩端;及 複數滾珠,其係在前述閉路中循環,並且位於前 述溝内時與前述執道抵接。 42. 如申請專利範圍第41項之線性驅動器,其中在前述 移動塊中形成有四個前述閉路,前述四個閉路中,二 個閉路之配置於各個溝的滾珠具有對前述線性導軌 之逕向方向概略為士45度之接觸角,其他二個閉路之 配置於各個溝的滾珠具有對前述線性導軌之反逕向 方向概略為±45度之接觸角。 43. —種扭力測試機台,其具有: 框架,其係固定於機台之基座上; 伺服馬達; 減速機構; 聯結器,其係聯結前述減速機構之輸入轴與前述 伺服馬達之驅動轴; 第一把持部,其係固定於前述減速機構之輸出軸 上,而把持測試片之一端; 第二把持部,其係固定於前述框架上,而把持該 測試片之另一端;及 第一支撐構件,其係固定於前述框架上,並且固 定前述伺服馬達及前述減速機構。 44. 如申請專利範圍第43項之扭力測試機台,其中前述 聯結器之聯結部具有與前述減速機構之輸入軸及前 57 200902971 述伺服馬達之驅動軸相等或其以上的扭力剛性。 45. 如申請專利範圍第40項之扭力測試機台,其中前述 聯結器係剛性聯結器。 46. 如申請專利範圍第44項之扭力測試機台,其中前述 聯結器係構成在彎曲方向具有撓曲性,且阻礙傳達前 述馬達之驅動轴的延長方向之振動的半剛性聯結器。 47. 如申請專利範圍第43項之扭力測試機台,其中進一 步具有第二支撐構件,其係固定於前述框架上; 前述第二把持部具有軸部; 藉由將前述軸部懸臂梁狀地固定支撐於前述第 二支撐構件,而將前述第二把持部固定於前述框架 上。 48. 如申請專利範圍第47項之扭力測試機台,其中進一 步具有固定端側軸承裝置,其係固定於前述框架上, 且可旋轉地支撐前述第二把持部之軸部。 49. 如申請專利範圍第43項之扭力測試機台,其中在前 述軸部與前述第二支撐構件之間固定有用於計測作 用於該測試片之扭矩的負載傳感器。 50. 如申請專利範圍第43項之扭力測試機台,其中前述 減速機構係波動齒輪減速機構。 51. 如申請專利範圍第45項之扭力測試機台,其中前述 波動齒輪減速機構埋入前述第一支撐構件而固定。 58200902971 X. Patent application scope: 1. A universal testing machine having: a servo motor that rotates the drive shaft back and forth; a feed screw; a coupling that couples the feed screw to the drive shaft of the servo motor a nut that engages with the feed screw; a linear guide that limits the direction of movement of the nut to only the axial direction of the feed screw; and a fixed portion that abuts or fixes one end of the test piece; The head is abutting or fixing the other end of the test piece, fixed to the nut and moving together with the nut; and a support plate to which the servo motor and the linear guide are fixed. 2. The universal testing machine of claim 1, wherein the coupling portion of the coupling has a torsional rigidity equal to or greater than a driving axis of the feed screw and the servo motor. 3. A universal test machine as claimed in claim 2, wherein the aforementioned coupling is a rigid coupling. 4. The universal testing machine of claim 3, wherein the rigid coupling has a cylindrical body having a torsional rigidity equal to or greater than a driving axis of the feed screw and the servo motor, and respectively One end of the feed screw is inserted into the feed screw, and the drive shaft of the servo motor is inserted from the other end to be fixed to the cylindrical body. 5. The universal testing machine of claim 4, wherein a part of the inner hole of the feed screw and the drive shaft of the servo motor is inserted into the cylindrical body to be the same as the feed screw and the servo 50 200902971 The narrow surface of the peripheral surface of the drive shaft of the motor is roughly received without gaps. 6. The universal test machine of claim 4, wherein the inner peripheral surface of the inner hole of the cylindrical body is fitted and fixed between the feed screw and the circumferential surface of the drive shaft of the servo motor a ring, and the feed screw and the drive shaft of the servo motor are fixed to the rigid coupling. 7. The universal testing machine of claim 6, wherein the fixing ring has; the inner wheel has a tapered surface; the outer wheel has an inner circumference which becomes a tapered surface corresponding to the outer circumference of the inner wheel; and The pressing device presses one of the inner and outer wheels in the axial direction in a state in which the outer circumference of the inner ring abuts against the inner circumference of the outer ring. 8. The universal test machine of claim 2, wherein the coupler constitutes a semi-rigid coupler having flexibility in a bending direction and obstructing vibration in a direction in which the drive shaft of the servo motor is extended. 9. The universal testing machine of claim 8 wherein said semi-rigid coupling comprises a viscoelastic element. 10. The universal testing machine of claim 9, wherein at least a portion of the aforementioned viscoelastic member is formed of a resin. 11. The universal testing machine of claim 9, wherein at least a portion of the aforementioned viscoelastic member is formed of rubber. 12. The universal test machine of claim 8, wherein the semi-rigid coupling constitutes a vibration damping rate in a direction of a drive shaft of the servo motor, and is maximum in a natural vibration number of the drive shaft. 51 200902971 13. The universal testing machine of claim 8 wherein said semi-rigid coupling has: an outer wheel that is a rigid body member that is formed with a tapered hole in the center; and an elastic element or viscoelasticity The inner wheel of the component is disposed between the outer wheel and the cylindrical through hole formed by the shaft coupled to the center, and is formed at each end of the outer circumferential direction to be tapered with the outer wheel Inserting a tapered surface of the inner circumference of the hole; inserting the feed screw and the drive shaft of the servo motor into the through hole of the inner wheel such that the tapered surface of the inner wheel abuts the tapered hole of the outer wheel In the circumferential direction, the shaft is coupled via the inner wheel by fixing the aforementioned outer wheel to each other with bolts. 14. The universal testing machine of claim 1, wherein the support plate is provided with an opening through which the feed screw is inserted, and the opening is fixed with a bearing rotatably supporting the feed screw. The outer wheel, the aforementioned bearing has an angular ball bearing. 15. The universal test machine of claim 14, wherein the aforementioned bearing has a combination face type ball bearing of a face combination type in which the front faces of the pair of angular ball bearings are opposed to each other. 16. The universal testing machine of claim 1, wherein the feed screw is a ball screw, and the nut is a nut for a ball screw. 17. The universal test machine of claim 1, wherein the support plate is a metal plate or a plurality of metal plates are integrated by welding. 18. The universal test machine of claim 1, wherein the support plate is welded to the foot of the universal test machine. 19. The universal testing machine of claim 1, wherein the wire 52 200902971 rail has: a first portion fixed to the fixing portion, and a second portion fixed to the nut, the first portion and the first portion One of the two parts has a track, and the other side is engaged with the track, and has a moving block movable along the track, the moving block has: a recess that surrounds the track; a groove that is in the recess Forming along the moving direction of the moving block; the exiting path is formed inside the moving block, and the groove is formed in a closed circuit to connect the two ends of the groove in the moving direction; and the plurality of balls are in the foregoing It circulates in a closed circuit and abuts the aforementioned track when it is located in the groove. 20. The universal testing machine of claim 19, wherein four of the aforementioned closed circuits are formed in the moving block, and wherein the two closed circuits are disposed in the respective grooves and have a diameter on the linear guide. The direction of the contact is generally a contact angle of ±45 degrees, and the balls of the other two closed paths disposed in the respective grooves have a contact angle of ±45 degrees to the reverse radial direction of the linear guide. 21. The universal testing machine of claim 1, further comprising at least one guide shaft for fixing the leg portion, wherein the fixing portion is fixed to the fixing portion by a guide shaft In the guide shaft for the fixing portion, the fixing portion is movable along the guide shaft for the fixing portion in a state where the fixing portion is not sandwiched by the fixing portion. 22. The universal testing machine of claim 21, further comprising a fixing portion driving device for causing the fixing portion to be along a state in which the fixing portion does not sandwich the guiding portion for the fixing portion The fixed portion is moved by a guide shaft. 53 200902971 23. The universal test machine of claim 22, wherein the fixed portion driving device moves the fixed portion by a feed screw mechanism. 24. A linear actuator having: a servo motor; a feed screw; a coupler coupling the feed screw to a drive shaft of the servo motor; a nut engaged with the feed screw; a linear guide, The movement direction of the nut is limited only to the axial direction of the feed screw; and the support plate is fixed with the servo motor and the linear guide. 25. The linear actuator of claim 24, wherein the coupling portion of the coupler has a torsional rigidity equal to or greater than a drive shaft of the feed screw and the servo motor. 26. The linear actuator of claim 25, wherein the coupler is a rigid coupler. 27. The linear actuator of claim 26, wherein the rigid coupling has a cylindrical body having a torsional rigidity equal to or greater than a drive shaft of the feed screw and the servo motor, and one end thereof respectively The feed screw is inserted, and the drive shaft of the servo motor is inserted from the other end to be fixed to the cylindrical body. 28. The linear actuator of claim 27, wherein a portion of the inner hole of the feed screw and the drive shaft of the servo motor is inserted into the cylindrical body to be driven by the feed screw and the servo motor. A narrow portion of the circumferential surface of the shaft that is accommodated substantially without a gap. The linear actuator according to claim 27, wherein the inner peripheral surface of the inner hole of the cylindrical body is fitted and fixed between the feed screw and the circumferential surface of the drive shaft of the servo motor. a ring, and the feed screw and the drive shaft of the servo motor are fixed to the rigid coupling. 30. The linear actuator of claim 27, wherein the fixing ring has: an inner wheel whose outer circumference is a tapered surface; an outer wheel whose inner circumference is a tapered surface corresponding to an outer circumference of the inner wheel; and a pressure spreading device In a state in which the outer circumference of the inner ring abuts against the inner circumference of the outer ring, one of the inner wheel and the outer wheel is pressed in the axial direction. 31. The linear actuator of claim 25, wherein the coupler constitutes a semi-rigid coupler having flexibility in a bending direction and obstructing vibration in a direction in which the drive shaft of the motor is extended. 32. The linear actuator of claim 31, wherein the semi-rigid coupling comprises a viscoelastic element. 33. The linear actuator of claim 32, wherein at least a portion of the aforementioned viscoelastic member is formed of a resin. 34. The linear actuator of claim 32, wherein at least a portion of the aforementioned viscoelastic member is formed of rubber. 35. The linear actuator of claim 31, wherein the semi-rigid coupling constitutes a vibration damping rate in a direction of a drive axis of the motor, and is maximum in a natural vibration number of the drive shaft. 36. The linear actuator of claim 31, wherein the semi-rigid coupling has: 55 200902971 an outer wheel that is a rigid body member that is formed with a tapered hole at a center; and an elastic member or a viscoelastic member The inner wheel is disposed between the outer wheel and defines a cylindrical through hole for connecting to the shaft of the center, and inner circumferences of the tapered hole respectively formed by the outer wheel are formed at both ends of the outer circumference Engaging the tapered portion; inserting the feed screw and the drive shaft of the servo motor into the through hole of the inner wheel such that the tapered surface of the inner wheel abuts against the inner circumference of the tapered hole of the outer wheel The aforementioned outer wheel is fixed to each other by bolts, and the shaft is coupled via the inner wheel. 37. The linear actuator of claim 24, wherein the support plate is provided with an opening through which the feed screw is inserted, and an outer wheel rotatably supporting a bearing of the feed screw is fixed in the opening. The aforementioned bearings have angular ball bearings. 38. The linear actuator of claim 37, wherein the aforementioned bearing has a combined front type combined angular ball bearing that combines the front faces of the pair of angular ball bearings. 39. The linear actuator of claim 24, wherein the feed screw is a ball screw, and the nut is a nut for a ball screw. 40. The linear actuator of claim 24, wherein the support plate is a metal plate or a plurality of metal plates are integrated by welding. The linear actuator of claim 24, wherein the linear guide has: a first portion fixed to the fixing portion, and a second portion fixed to the nut, one of the first portion and the second portion The other side is engaged with the aforementioned track and has a moving block movable along the track. The moving block has: 56 200902971 a recess that surrounds the track; a groove that is in the recess, Forming along the moving direction of the moving block; the exiting path is formed inside the moving block, and the groove is formed in a closed circuit to connect the two ends of the groove in the moving direction; and the plurality of balls are in the closed circuit It circulates and abuts the aforementioned way when it is located in the groove. 42. The linear actuator of claim 41, wherein four of the aforementioned closed circuits are formed in the moving block, and two of the four closed circuits are disposed in a radial direction of the linear guide. The direction is roughly a contact angle of 45 degrees, and the other two closed paths of the balls disposed in the respective grooves have a contact angle of ±45 degrees to the reverse radial direction of the linear guide. 43. A torque testing machine having: a frame fixed to a base of the machine; a servo motor; a speed reducing mechanism; and a coupling coupling the input shaft of the speed reducing mechanism and the driving shaft of the servo motor a first gripping portion fixed to an output shaft of the speed reducing mechanism and holding one end of the test piece; a second gripping portion fixed to the frame and holding the other end of the test piece; and the first A support member fixed to the frame and fixed to the servo motor and the speed reduction mechanism. 44. The torque testing machine of claim 43, wherein the coupling portion of the coupling has a torque rigidity equal to or greater than an input shaft of the speed reduction mechanism and a drive shaft of the servo motor. 45. The torque testing machine of claim 40, wherein the coupling is a rigid coupling. 46. The torque testing machine of claim 44, wherein the coupling constitutes a semi-rigid coupling that is flexible in a bending direction and that hinders vibration in an extending direction of a drive shaft of the motor. 47. The torque testing machine of claim 43, further comprising a second supporting member fixed to the frame; the second holding portion having a shaft portion; wherein the shaft portion is cantilevered The second support member is fixedly supported to the second support member, and the second grip portion is fixed to the frame. 48. The torque testing machine of claim 47, further comprising a fixed end side bearing device fixed to the frame and rotatably supporting the shaft portion of the second holding portion. 49. The torque testing machine of claim 43, wherein a load sensor for measuring a torque applied to the test piece is fixed between the shaft portion and the second support member. 50. The torque testing machine of claim 43, wherein the speed reducing mechanism is a wave gear reduction mechanism. 51. The torque testing machine of claim 45, wherein the wave gear reduction mechanism is fixed by embedding the first support member. 58
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TWI504892B (en) 2015-10-21
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CN101680828B (en) 2012-06-20
KR101223548B1 (en) 2013-01-18
CN102645384B (en) 2016-05-04
CN101680828A (en) 2010-03-24
TW201413243A (en) 2014-04-01
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KR20120005555A (en) 2012-01-16
KR20090127169A (en) 2009-12-09

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