CN106226012A - A kind of device testing parallel institution tension and compression rigidity - Google Patents
A kind of device testing parallel institution tension and compression rigidity Download PDFInfo
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- 238000007906 compression Methods 0.000 title claims description 13
- 230000006835 compression Effects 0.000 title description 3
- 238000011068 loading method Methods 0.000 claims abstract description 108
- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 238000006073 displacement reaction Methods 0.000 claims abstract description 21
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 43
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- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
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Abstract
本发明公开了一种测试并联机构拉压刚度的装置,包括加载装置框体、蝶形弹簧受载组件、拉压力传感器、力加载杆和拉绳位移传感器。拉绳位移传感器底部与固定于地面的支架固连,拉绳位移传感器的拉绳端与待测的并联机构的动平台顶部连接件固连,力加载杆一端与并联机构动平台顶部连接件固连,力加载杆另一端与拉压力传感器相连,蝶形弹簧受载组件一端与加载装置框体连接,另一端与拉压力传感器相连,加载装置框体固定在设置于地面的支架上。本发明解决了现有技术中输出复合的力/力矩,无法施加某向线性无关的独立载荷,及无法实现加载载荷的连续变化、分级变化等问题。
The invention discloses a device for testing the tensile and compressive stiffness of a parallel mechanism, which comprises a loading device frame body, a disc spring loaded component, a tension and pressure sensor, a force loading rod and a pull rope displacement sensor. The bottom of the pull rope displacement sensor is fixedly connected to the bracket fixed on the ground, the pull rope end of the pull rope displacement sensor is fixedly connected to the top connecting piece of the moving platform of the parallel mechanism to be tested, and one end of the force loading rod is fixed to the top connecting piece of the moving platform of the parallel mechanism. Connected, the other end of the force loading rod is connected with the tension and pressure sensor, one end of the butterfly spring loaded component is connected with the loading device frame, and the other end is connected with the tension and pressure sensor, and the loading device frame is fixed on the support arranged on the ground. The invention solves the problems in the prior art that output compound force/moment, cannot apply linearly independent independent load in a certain direction, and cannot realize continuous change and graded change of loaded load.
Description
技术领域technical field
本发明涉及刚度测试领域,具体涉及一种测试并联机构拉压刚度的装置。The invention relates to the field of stiffness testing, in particular to a device for testing the tension-compression stiffness of a parallel mechanism.
背景技术Background technique
并联机构与串联机构相比具有刚度大、结构稳定、承载能力强、精度高、运动惯量小、实时控制性强等特点。并联机构在各种工业生产、实践活动均有广泛的运用,例如航空航天、精密制造、汽车加工装配、卫生医疗等等许多方面。要掌握并联机构的性能,必须先对该机构的力学特性加以深入分析,而并联机构的刚度是机构力学特性的重要指标。Compared with the series mechanism, the parallel mechanism has the characteristics of large rigidity, stable structure, strong bearing capacity, high precision, small motion inertia, and strong real-time controllability. Parallel mechanisms are widely used in various industrial production and practical activities, such as aerospace, precision manufacturing, automobile processing and assembly, health care and many other aspects. To master the performance of parallel mechanism, it is necessary to analyze the mechanical characteristics of the mechanism in depth, and the stiffness of parallel mechanism is an important index of the mechanical characteristics of the mechanism.
专利号为200510050822.1公开了一种并联六维力传感器标定装置、专利号为200510050834.4公开了一种无级升降式六维力传感器标定装置,二者均使用龙门式框架,通过滑轮无级升降机构可以连续得到绳索与水平面之间的夹角,并采用大减速比减速机对六维力传感器施加载荷。两者的缺点均在于:采用绳索滑轮式机构在施加载荷时易存在方向误差、绳索只可单向输出拉力,不可反向输出压力;输出复合的力/力矩,无法实现个方向独立载荷加载。Patent No. 200510050822.1 discloses a parallel six-dimensional force sensor calibration device. Patent No. 200510050834.4 discloses a stepless lifting six-dimensional force sensor calibration device. The angle between the rope and the horizontal plane is continuously obtained, and a large reduction ratio reducer is used to apply a load to the six-dimensional force sensor. The disadvantages of both are: the rope pulley mechanism is prone to directional error when applying the load, the rope can only output tension in one direction, and cannot output pressure in the opposite direction; output compound force/torque, and cannot realize independent load loading in one direction.
中国专利CN101936797A公开了一种六维力传感器标定装置及其标定方法,采用更换不同重量砝码加载的方式对六维力传感器进行加载,砝码加载无法实现加载载荷连续变化,此装置同样只可施加复合的力/力矩。Chinese patent CN101936797A discloses a six-dimensional force sensor calibration device and its calibration method. The six-dimensional force sensor is loaded by replacing weights with different weights. Loading the weights cannot achieve continuous changes in the loading load. This device can only Apply compound forces/torques.
中国专利CN103604561A公开了一种六维力/力矩传感器标定装置及其标定方法,采用滑轮、钢丝绳、砝码加载,设计回转台以标定传感器多方向,其缺点砝码加载无法实现加载载荷连续变化。Chinese patent CN103604561A discloses a six-dimensional force/torque sensor calibration device and its calibration method. Pulleys, wire ropes, and weights are used to load, and a turntable is designed to calibrate the sensor in multiple directions. The disadvantage is that weight loading cannot realize continuous change of loading load.
以上专利共同缺点为均需要设计相应的工作台,若针对大尺寸的六维力传感器标定则成本较高。The common disadvantage of the above patents is that a corresponding workbench needs to be designed, and the cost of calibration for a large-sized six-dimensional force sensor is relatively high.
发明内容Contents of the invention
本发明的目的在于提供一种测试并联机构扭转刚度的装置,解决了现有技术中输出复合的力/力矩,无法施加某向线性无关的独立载荷;采用砝码加载加载,无法实现加载载荷的连续变化、分级变化等问题。The purpose of the present invention is to provide a device for testing the torsional stiffness of a parallel mechanism, which solves the problem of outputting compound force/moment in the prior art, and cannot apply a linearly independent independent load in a certain direction; loading with weights cannot realize the problem of loading Continuous change, graded change, etc.
实现本发明目的的技术解决方案为:一种测试并联机构拉压刚度的装置,包括加载装置框体、蝶形弹簧受载组件、拉压力传感器、力加载杆和拉绳位移传感器;其中,拉绳位移传感器底部与固定于地面的支架固连,拉绳位移传感器的拉绳端与待测的并联机构的动平台顶部的连接件固连,力加载杆一端与并联机构动平台顶部的连接件固连,力加载杆另一端与拉压力传感器相连,蝶形弹簧受载组件一端与加载装置框体连接,另一端与拉压力传感器相连,加载装置框体固定在设置于地面的支架上。蝶形弹簧受载组件、拉压力传感器、力加载杆和拉绳位移传感器的拉绳四者共轴线。The technical solution to realize the object of the present invention is: a device for testing the tension-compression stiffness of a parallel mechanism, including a loading device frame, a butterfly spring loaded assembly, a tension pressure sensor, a force loading rod and a stay rope displacement sensor; The bottom of the rope displacement sensor is fixedly connected to the bracket fixed on the ground, the rope end of the pull rope displacement sensor is fixedly connected to the connecting piece on the top of the moving platform of the parallel mechanism to be tested, and the end of the force loading rod is connected to the connecting piece on the top of the moving platform of the parallel mechanism Fixed connection, the other end of the force loading rod is connected to the tension and pressure sensor, one end of the butterfly spring loaded component is connected to the loading device frame, and the other end is connected to the tension and pressure sensor, and the loading device frame is fixed on the support set on the ground. The belleville spring loaded assembly, the tension pressure sensor, the force loading rod and the stay rope of the stay rope displacement sensor are coaxial.
所述加载装置框体为立方体,其中任意两个平行的侧面无侧板,所述无侧板的侧面的四个角上焊接三角连接板,增加加载装置框体的整体刚度,加载装置框体四周均设有若干个安装孔位。The frame of the loading device is a cube, wherein any two parallel sides have no side plates, and the four corners of the sides without side plates are welded with triangular connecting plates to increase the overall rigidity of the frame of the loading device, and the frame of the loading device There are a number of installation holes all around.
所述蝶形弹簧受载组件包括加载螺杆、铜制螺母孔盘、蝶形弹簧锁紧盖、蝶形弹簧安装壳体、铜制加载圆柱、销、手轮、铜套法兰、第一蝶形弹簧组、第二蝶形弹簧组和两根导向杆,加载装置框体与拉压力传感器同侧的侧板外壁固连铜制螺母孔盘,两根导向杆分别穿过铜制螺母孔盘和加载装置框体,蝶形弹簧安装壳体一端固连有蝶形弹簧锁紧盖,蝶形弹簧锁紧盖固定在加载装置框体外侧的导向杆上,随导向杆滑动,蝶形弹簧安装壳体内依次设置第一蝶形弹簧组、铜制加载圆柱和第二蝶形弹簧组,其中第一蝶形弹簧组紧靠蝶形弹簧锁紧盖,加载螺杆一端依次穿过铜制螺母孔盘中心通孔、加载装置框体、蝶形弹簧锁紧盖、第一蝶形弹簧组和铜制加载圆柱,铜制加载圆柱抵住第二蝶形弹簧组,加载螺杆另一端穿过与设有铜制螺母孔盘平行的加载装置框体的侧壁,所述端部设有手轮,且另一端与侧壁内侧的连接处设有铜套法兰;铜制加载圆柱和加载螺杆通过销固连。The butterfly spring loaded assembly includes a loading screw, a copper nut hole plate, a butterfly spring locking cover, a butterfly spring mounting shell, a copper loading cylinder, a pin, a hand wheel, a copper sleeve flange, a first butterfly The outer wall of the side plate on the same side as the loading device frame and the tension pressure sensor is fixedly connected to the copper nut hole plate, and the two guide rods pass through the copper nut hole plate respectively. And the frame of the loading device, one end of the butterfly spring installation shell is fixedly connected with a butterfly spring locking cover, the butterfly spring locking cover is fixed on the guide rod outside the loading device frame, slides with the guide rod, and the butterfly spring is installed The first butterfly spring group, the copper loading cylinder and the second butterfly spring group are arranged in sequence in the housing, wherein the first butterfly spring group is close to the butterfly spring locking cover, and one end of the loading screw passes through the copper nut hole plate in turn Central through hole, loading device frame, butterfly spring locking cover, first butterfly spring group and copper loading cylinder, copper loading cylinder resists the second butterfly spring group, the other end of the loading screw passes through and is equipped with The side wall of the loading device frame parallel to the copper nut hole plate, the end is provided with a hand wheel, and the connection between the other end and the inner side of the side wall is provided with a copper sleeve flange; the copper loading cylinder and the loading screw pass through the pin Solid connection.
所述铜制螺母孔盘中心通孔为螺纹孔,对应的加载螺杆中段设有螺纹。The central through hole of the copper nut hole plate is a threaded hole, and the middle section of the corresponding loading screw is provided with threads.
本发明与现有技术相比,其显著优点在于:Compared with the prior art, the present invention has significant advantages in that:
(1)装置的结构简单紧凑、制作成本低。(1) The structure of the device is simple and compact, and the manufacturing cost is low.
(2)加载装置框体四周上设有若干个安装孔位,便于调节整个装置的安装高度与加载方向,以适应各类尺寸与形状并联机构,通用性强。(2) There are several installation holes around the frame of the loading device, which is convenient for adjusting the installation height and loading direction of the whole device, so as to adapt to parallel mechanisms of various sizes and shapes, and has strong versatility.
(3)蝶形弹簧组受载变形,以提供螺纹进给所需位移量,由于载荷随螺纹进给量线性变化,因此可以通过手轮转动控制载荷线性变化。手轮转动过程中,结合拉压力传感器可以控制载荷连续加载、分级加载,以保证施加载荷的精度。(3) The belleville spring group is deformed under load to provide the displacement required for thread feed. Since the load changes linearly with the thread feed, the linear change of load can be controlled by turning the hand wheel. During the rotation of the handwheel, combined with tension and pressure sensors, the load can be controlled continuously and step by step to ensure the accuracy of the applied load.
(4)手轮正转反转均可输出载荷,既可以输出拉力也可以输出压力。通过手轮的正转反转可以方便地地完成加载与卸载的过程,操作简单,性能可靠。(4) The load can be output both in forward and reverse rotation of the hand wheel, and it can output both tension and pressure. The process of loading and unloading can be conveniently completed through the forward and reverse rotation of the hand wheel, with simple operation and reliable performance.
(5)可以输出沿某一方向线性无关的独立载荷。(5) Independent loads that are linearly independent along a certain direction can be output.
附图说明Description of drawings
图1为本发明测量并联机构拉压刚度的装置的立体结构示意图。Fig. 1 is a three-dimensional structural schematic diagram of the device for measuring the tension-compression stiffness of a parallel mechanism according to the present invention.
图2为本发明测量并联机构拉压刚度的装置的主视图。Fig. 2 is a front view of the device for measuring the tension-compression stiffness of a parallel mechanism according to the present invention.
图3为本发明测量并联机构拉压刚度的装置的局部剖视图。Fig. 3 is a partial cross-sectional view of the device for measuring the tension-compression stiffness of a parallel mechanism according to the present invention.
具体实施方式detailed description
下面结合附图对发明作进一步说明。The invention will be further described below in conjunction with the accompanying drawings.
结合图1至图3,一种测试并联机构拉压刚度的装置,包括加载装置框体1、蝶形弹簧受载组件2、拉压力传感器3、力加载杆4和拉绳位移传感器6。其中,拉绳位移传感器6底部通过螺钉固定于地面的支架固连,拉绳位移传感器6的拉绳端与待测的并联机构5的动平台顶部的连接件固连,力加载杆4一端与并联机构5动平台顶部的连接件固连,力加载杆4另一端通过螺纹与拉压力传感器3相连,蝶形弹簧受载组件2一端与加载装置框体1连接,另一端通过法兰盘与拉压力传感器3相连,加载装置框体1固定在设置于地面的支架上;蝶形弹簧受载组件2、拉压力传感器3、力加载杆4和拉绳位移传感器6的拉绳四者共轴线。1 to 3 , a device for testing the tension-compression stiffness of a parallel mechanism includes a loading device frame 1 , a butterfly spring loaded assembly 2 , a tension-pressure sensor 3 , a force loading rod 4 and a rope displacement sensor 6 . Wherein, the bottom of the stay rope displacement sensor 6 is fixedly connected with the bracket fixed on the ground by screws, the stay rope end of the stay rope displacement sensor 6 is fixedly connected with the connector at the top of the moving platform of the parallel mechanism 5 to be measured, and one end of the force loading rod 4 is connected with The connecting piece on the top of the parallel mechanism 5 moving platform is fixedly connected, the other end of the force loading rod 4 is connected with the tension pressure sensor 3 through a thread, one end of the butterfly spring loaded component 2 is connected with the loading device frame 1, and the other end is connected with the loading device frame 1 through a flange plate. The tension and pressure sensors 3 are connected, and the loading device frame body 1 is fixed on the support arranged on the ground; the butterfly spring loaded component 2, the tension pressure sensor 3, the force loading rod 4 and the stay rope of the stay rope displacement sensor 6 are coaxial .
所述加载装置框体1共六个平面,其中两个平行的面无侧板,其余四个面焊接为一个立方体,所述无侧板的面的四个角上均焊接三角连接板,增加加载装置框体1的整体刚度,加载装置框体1四周均设有若干个安装孔位,便于调节整个测量装置的安装高度与加载方向,以适应各类尺寸与形状并联机构。The loading device frame body 1 has six planes in total, two of which are parallel without side plates, and the remaining four sides are welded into a cube, and triangular connecting plates are welded on the four corners of the faces without side plates, increasing The overall rigidity of the loading device frame 1 is provided with several mounting holes around the loading device frame 1, which is convenient for adjusting the installation height and loading direction of the entire measuring device, so as to adapt to parallel mechanisms of various sizes and shapes.
所述蝶形弹簧受载组件2包括加载螺杆2-1、铜制螺母孔盘2-3、蝶形弹簧锁紧盖2-4、蝶形弹簧安装壳体2-5、铜制加载圆柱2-6、销2-7、手轮2-9、铜套法兰2-10、第一蝶形弹簧组2-8、第二蝶形弹簧组2-11和两根导向杆2-2。加载装置框体1与拉压力传感器3同侧的侧板外壁上通过螺栓固连铜制螺母孔盘2-3,铜制螺母孔盘2-3中心设有螺纹通孔,以螺纹通孔为中心对称分布两个导向孔,两根导向杆2-2分别穿过铜制螺母孔盘2-3的导向孔和加载装置框体1的侧壁,蝶形弹簧安装壳体2-5一端通过螺纹连接有蝶形弹簧锁紧盖2-4,并通过紧定螺钉固定止旋,蝶形弹簧锁紧盖2-4通过螺纹固定在加载装置框体1外侧的导向杆2-2上,随导向杆2-2滑动,蝶形弹簧安装壳体2-5内依次设置第一蝶形弹簧组2-8、铜制加载圆柱2-6和第二蝶形弹簧组2-11,其中第一蝶形弹簧组2-8紧靠蝶形弹簧锁紧盖2-4,加载螺杆2-1一端依次穿过铜制螺母孔盘2-3中心通孔、加载装置框体1、蝶形弹簧锁紧盖2-4、第一蝶形弹簧组2-8和铜制加载圆柱2-6,铜制加载圆柱2-6抵住第二蝶形弹簧组2-11,加载螺杆2-1另一端穿过与设有铜制螺母孔盘2-3平行的加载装置框体1的侧壁,所述端部设有手轮2-9,且另一端与侧壁内侧的连接处设有铜套法兰2-10;铜制加载圆柱2-6和加载螺杆2-1通过销2-7固连,使载荷通过铜制加载圆柱2-6作用于两个蝶形弹簧组。The butterfly spring loaded assembly 2 includes a loading screw 2-1, a copper nut hole plate 2-3, a butterfly spring locking cover 2-4, a butterfly spring mounting shell 2-5, and a copper loading cylinder 2 -6, pin 2-7, hand wheel 2-9, copper sleeve flange 2-10, the first butterfly spring group 2-8, the second butterfly spring group 2-11 and two guide rods 2-2. The outer wall of the side plate on the same side of the loading device frame body 1 and the tension pressure sensor 3 is fixedly connected to the copper nut hole plate 2-3 by bolts, and the center of the copper nut hole plate 2-3 is provided with a threaded through hole, with the threaded through hole as the Two guide holes are symmetrically distributed in the center, two guide rods 2-2 pass through the guide holes of the copper nut hole plate 2-3 and the side wall of the loading device frame 1 respectively, and one end of the butterfly spring installation shell 2-5 passes through The butterfly spring locking cover 2-4 is threadedly connected, and the rotation is fixed by the set screw, and the butterfly spring locking cover 2-4 is fixed on the guide rod 2-2 on the outside of the loading device frame body 1 by threads. The guide rod 2-2 slides, and the first butterfly spring group 2-8, the copper loading cylinder 2-6 and the second butterfly spring group 2-11 are arranged successively in the butterfly spring installation housing 2-5, wherein the first The butterfly spring group 2-8 is close to the butterfly spring locking cover 2-4, one end of the loading screw 2-1 passes through the center through hole of the copper nut hole plate 2-3, the loading device frame 1, and the butterfly spring lock Tight cover 2-4, first butterfly spring group 2-8 and copper loading cylinder 2-6, copper loading cylinder 2-6 against the second butterfly spring group 2-11, the other end of loading screw rod 2-1 Pass through the side wall of the loading device frame 1 parallel to the copper nut hole plate 2-3, the end is provided with a hand wheel 2-9, and the other end is provided with a copper sleeve at the connection with the inner side of the side wall Flange 2-10; copper loading cylinder 2-6 and loading screw rod 2-1 are fixedly connected by pin 2-7, so that the load acts on two butterfly spring groups through copper loading cylinder 2-6.
加载螺杆2-1由于受载过程中蝶形弹簧组总变形量不大,因此加载螺杆2-1仅需在铜制螺母孔盘2-3的中心螺纹孔附近加工一段螺纹,其余为光杆。加载螺杆2-1在铜制螺母孔盘2-3的螺纹孔中运动,螺纹进给减速比大,使手轮2-9力降低并输出较大的载荷。Loading screw 2-1 is because the total deformation of the butterfly spring group is not large during the loading process, so loading screw 2-1 only needs to process a section of thread near the central threaded hole of copper nut hole plate 2-3, and the rest are polished rods. The loading screw 2-1 moves in the threaded hole of the copper nut hole plate 2-3, and the thread feed reduction ratio is large, so that the force of the hand wheel 2-9 is reduced and a larger load is output.
导向杆2-2限制了蝶形弹簧受载组件2整体绕加载螺杆2-1轴线的旋转,保留了蝶形弹簧受载组件2整体可沿加载螺杆2-1的轴线移动,保证加载载荷仍可沿加载螺杆2-1轴向方向传递。两个蝶形弹簧组受载变形提供了螺纹进给所需位移量与手轮2-9所需转动量,手轮2-9正转反转均可输出载荷,铜制加载圆柱2-6通过压缩第一蝶形弹簧组2-8以施加压力,通过压缩第二蝶形弹簧组2-11以施加拉力。The guide rod 2-2 limits the rotation of the Belleville spring loaded assembly 2 as a whole around the axis of the loading screw 2-1, retaining the movement of the Belleville spring loaded assembly 2 as a whole along the axis of the loading screw 2-1, ensuring that the loaded load remains It can be transmitted along the axial direction of the loading screw 2-1. The deformation of the two butterfly spring groups under load provides the displacement required for thread feed and the required rotation of the handwheel 2-9. The handwheel 2-9 can output load in both forward and reverse rotations. The copper loading cylinder 2-6 Compression is applied by compressing the first Belleville spring set 2-8, and tension is applied by compressing the second Belleville spring set 2-11.
拉压力传感器3选用上海高灵传感系统工程有限公司生产的GLBLY轮辐拉压力传感器,中心配有螺纹孔,四周配有若干连接孔位。蝶形弹簧组受载变形,且载荷随螺纹进给量线性变化,因此载荷随手轮2-9转动量线性变化。以某一方向转动手轮2-9进行加载,结合拉压力传感器3,可以控制载荷连续变化、分级变化,以保证施加载荷的精度,手轮2-9以反方向转动即可完成卸载,同时获取拉压载荷F。The tension pressure sensor 3 is the GLBLY wheel spoke tension pressure sensor produced by Shanghai Gaoling Sensing System Engineering Co., Ltd., with a threaded hole in the center and several connection holes around it. The Belleville spring group is deformed under load, and the load changes linearly with the thread feed, so the load changes linearly with the rotation of the handwheel 2-9. Turn the handwheel 2-9 in a certain direction to load, combined with the tension and pressure sensor 3, the load can be controlled continuously and in stages to ensure the accuracy of the applied load, and the unloading can be completed by turning the handwheel 2-9 in the opposite direction, and at the same time Obtain the tension and compression load F.
力加载杆4可根据实际使用情形选用合适的长度,以增强通用性,并输出沿其轴线向的独立载荷。拉绳位移传感器6能够获取并联机构5在载荷作用下的位移变化量x,则拉压刚度为:The force loading rod 4 can be selected with an appropriate length according to the actual use situation, so as to enhance the versatility, and output an independent load along its axial direction. The rope displacement sensor 6 can obtain the displacement change x of the parallel mechanism 5 under the load, then the tensile and compressive stiffness is:
将并联机构5的定平台与地面固定,测试装置按照所需测试方向进行设置,转动手轮2-9进行加载,结合拉压力传感器3控制加载载荷逐级变化,即输出载荷从零到满量程分为10~12次加载。在完成加载后手轮2-9反转以完成卸载,同样地控制输出载荷从满量程到零分成10~12次加载。为保证测量精度,重复多次加载卸载过程。加载过程中通过拉绳位移传感器6实时获取并联机构5在载荷作用下的位移变化量,结合数据分析并联机构5该方向的向拉压刚度KF。Fix the fixed platform of the parallel mechanism 5 to the ground, set the test device according to the required test direction, turn the hand wheel 2-9 to load, and combine the tension and pressure sensor 3 to control the loading load to change step by step, that is, the output load is from zero to full scale Divided into 10 to 12 loads. After the loading is completed, the hand wheel 2-9 is reversed to complete the unloading, and the same control output load is divided into 10-12 loadings from full scale to zero. In order to ensure the measurement accuracy, the loading and unloading process was repeated several times. During the loading process, the displacement change of the parallel mechanism 5 under the load is obtained in real time through the rope displacement sensor 6, and the tensile and compressive stiffness K F of the parallel mechanism 5 in this direction is analyzed in combination with the data.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100222A (en) * | 2018-07-24 | 2018-12-28 | 大连理工大学 | A kind of clip rigidity automatic calibration device and its application method |
| CN112683517A (en) * | 2021-01-13 | 2021-04-20 | 中南大学 | Testing system for static rigidity of photoelectron packaging flexible parallel platform |
| CN112729648A (en) * | 2020-12-30 | 2021-04-30 | 慈兴集团有限公司 | Ball friction torque testing device |
| CN115265903A (en) * | 2022-08-02 | 2022-11-01 | 柳州五菱新能源汽车有限公司 | Device and method for calibrating tension and compression bidirectional loading of steering pull rod |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1739238A1 (en) * | 1990-08-06 | 1992-06-07 | Университет дружбы народов им.Патриса Лумумбы | Arrangement for determining rigidity characteristics of flexible supports of dynamometers |
| CN1439869A (en) * | 2002-02-22 | 2003-09-03 | 李贵涛 | Virtual mechanical axis material test systems |
| CN1727861A (en) * | 2005-07-22 | 2006-02-01 | 浙江大学 | Parallel six-dimensional force sensor calibration device |
| CN101571441A (en) * | 2008-05-01 | 2009-11-04 | 中国科学院合肥物质科学研究院 | Six-dimension force sensor calibration device with medium measurement range |
| CN103616128A (en) * | 2013-12-09 | 2014-03-05 | 中国航天空气动力技术研究院 | Six-dimension force sensor calibration device and loading unit thereof |
| CN103926039A (en) * | 2014-04-30 | 2014-07-16 | 中国航天空气动力技术研究院 | Electromechanical type force source device allowing bi-directional loading |
-
2016
- 2016-07-12 CN CN201610550203.7A patent/CN106226012B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1739238A1 (en) * | 1990-08-06 | 1992-06-07 | Университет дружбы народов им.Патриса Лумумбы | Arrangement for determining rigidity characteristics of flexible supports of dynamometers |
| CN1439869A (en) * | 2002-02-22 | 2003-09-03 | 李贵涛 | Virtual mechanical axis material test systems |
| CN1727861A (en) * | 2005-07-22 | 2006-02-01 | 浙江大学 | Parallel six-dimensional force sensor calibration device |
| CN101571441A (en) * | 2008-05-01 | 2009-11-04 | 中国科学院合肥物质科学研究院 | Six-dimension force sensor calibration device with medium measurement range |
| CN103616128A (en) * | 2013-12-09 | 2014-03-05 | 中国航天空气动力技术研究院 | Six-dimension force sensor calibration device and loading unit thereof |
| CN103926039A (en) * | 2014-04-30 | 2014-07-16 | 中国航天空气动力技术研究院 | Electromechanical type force source device allowing bi-directional loading |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100222A (en) * | 2018-07-24 | 2018-12-28 | 大连理工大学 | A kind of clip rigidity automatic calibration device and its application method |
| CN109100222B (en) * | 2018-07-24 | 2020-05-19 | 大连理工大学 | A kind of clamp stiffness automatic calibration device and its use method |
| CN112729648A (en) * | 2020-12-30 | 2021-04-30 | 慈兴集团有限公司 | Ball friction torque testing device |
| CN112683517A (en) * | 2021-01-13 | 2021-04-20 | 中南大学 | Testing system for static rigidity of photoelectron packaging flexible parallel platform |
| CN115265903A (en) * | 2022-08-02 | 2022-11-01 | 柳州五菱新能源汽车有限公司 | Device and method for calibrating tension and compression bidirectional loading of steering pull rod |
| CN115265903B (en) * | 2022-08-02 | 2025-08-01 | 柳州五菱新能源汽车有限公司 | Bidirectional loading calibration device and calibration method for pull and press of steering pull rod |
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