CN102297177A - Pneumatic servo actuator - Google Patents
Pneumatic servo actuator Download PDFInfo
- Publication number
- CN102297177A CN102297177A CN2011101951439A CN201110195143A CN102297177A CN 102297177 A CN102297177 A CN 102297177A CN 2011101951439 A CN2011101951439 A CN 2011101951439A CN 201110195143 A CN201110195143 A CN 201110195143A CN 102297177 A CN102297177 A CN 102297177A
- Authority
- CN
- China
- Prior art keywords
- air
- guide rail
- bellows
- floating guide
- pneumatic servo
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000006073 displacement reaction Methods 0.000 claims abstract description 17
- 239000002184 metal Substances 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 6
- 238000005188 flotation Methods 0.000 claims description 5
- 238000010586 diagram Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
Images
Landscapes
- Actuator (AREA)
Abstract
本发明涉及一种气动伺服执行机构,尤其涉及一种以波纹管作为执行元件同时带有无摩擦气浮导轨的气动伺服执行机构,属于工业自动化仪表与系统技术领域。它包括执行元件、气浮导轨、位移传感器、载物台和机构体;执行元件为波纹管;波纹管是气动伺服执行机构的执行元件,气浮导轨由气浮导轨动子和气浮导轨定子组成;位移传感器由读数头和光栅尺组成;其连接关系为:波纹管一端封死,与气浮导轨动子连接,另一端固定在机构体上,机构体上设有波纹管进气孔;载物台安装在气浮导轨动子上;气浮导轨定子的底端固定在机构体上;当气浮导轨正常工作时,气浮导轨动子无摩擦移动;光栅尺固定在载物台的侧面;读数头固定在机构体的一侧,并与光栅尺相对。
The invention relates to a pneumatic servo actuator, in particular to a pneumatic servo actuator with a bellows as an actuator and a frictionless air-floating guide rail, which belongs to the technical field of industrial automation instruments and systems. It includes actuators, air bearing guide rails, displacement sensors, stages and mechanism bodies; the actuators are bellows; the bellows are the actuators of pneumatic servo actuators, and the air bearing guide rails are composed of air bearing guide rail movers and air bearing guide rail stators The displacement sensor is composed of a reading head and a grating ruler; the connection relationship is as follows: one end of the bellows is sealed and connected with the mover of the air-floating guide rail, and the other end is fixed on the mechanism body, which is provided with a bellows air inlet; The object stage is installed on the mover of the air-floating guide rail; the bottom end of the stator of the air-floating guide rail is fixed on the mechanism body; when the air-floating guide rail is working normally, the mover of the air-floating guide rail moves without friction; the grating ruler is fixed on the side of the loading platform ; The reading head is fixed on one side of the mechanism body and is opposite to the grating ruler.
Description
技术领域 technical field
本发明涉及一种气动伺服执行机构,尤其涉及一种以波纹管作为执行元件同时带有无摩擦气浮导轨的气动伺服执行机构,属于工业自动化仪表与系统技术领域。The invention relates to a pneumatic servo actuator, in particular to a pneumatic servo actuator with a bellows as an actuator and a frictionless air-floating guide rail, which belongs to the technical field of industrial automation instruments and systems.
背景技术 Background technique
气动伺服系统的组成形式同一般伺服系统没有区别,它的各个环节不一定全是气动的,但执行机构一定是气动的。在气动伺服系统中,执行机构一般常采用活塞式气缸,气缸工作时主要靠内腔压力推动活塞运动,但由于气体的可压缩性及传统气缸内部活塞与内筒、杆与端口摩擦力等因素的影响,导致了气动伺服系统的强非线性和低刚度,实现对气动伺服系统的满意控制比较困难,控制精度不高,至今在工业上的应用并不成熟。The composition of the pneumatic servo system is no different from that of the general servo system. Its various links are not necessarily all pneumatic, but the actuator must be pneumatic. In the pneumatic servo system, the actuator generally adopts a piston cylinder. When the cylinder works, it mainly relies on the pressure of the inner cavity to push the piston to move. The impact of the pneumatic servo system has resulted in strong nonlinearity and low stiffness. It is difficult to achieve satisfactory control of the pneumatic servo system, and the control accuracy is not high. So far, the application in industry is not mature.
发明内容 Contents of the invention
本发明的目的是为解决气动伺服执行机构在运动过程中存在的摩擦力的问题,提出一种气动伺服执行机构。The object of the present invention is to propose a pneumatic servo actuator to solve the problem of friction existing in the motion process of the pneumatic servo actuator.
为了实现上述目的,本发明是通过以下技术方案来实现的:In order to achieve the above object, the present invention is achieved through the following technical solutions:
一种气动伺服执行机构,它包括执行元件、气浮导轨、位移传感器、载物台和机构体;执行元件为波纹管;波纹管是气动伺服执行机构的执行元件,对气动伺服执行机构提供执行力;气浮导轨由气浮导轨动子和气浮导轨定子组成,用于消除气动伺服执行机构运动过程中的摩擦力;位移传感器由读数头和光栅尺组成,为气动伺服执行机构的位置采集装置,用于对气动伺服执行机构移动位移进行采集和反馈;其连接关系为:波纹管一端封死,与气浮导轨动子连接,另一端固定在机构体上,机构体上设有波纹管进气孔;载物台安装在气浮导轨动子上;气浮导轨定子的底端固定在机构体上;当气浮导轨正常工作时,气浮导轨动子无摩擦移动;光栅尺固定在载物台的侧面;读数头固定在机构体的一侧,并与光栅尺相对;A pneumatic servo actuator, which includes an actuator, an air bearing guide rail, a displacement sensor, a stage, and a mechanism body; the actuator is a bellows; the bellows is the actuator of the pneumatic servo actuator, and provides the actuator for the pneumatic servo actuator. The air-floating guide rail is composed of the air-floating guide rail mover and the air-floating guide rail stator, which is used to eliminate the friction force during the movement of the pneumatic servo actuator; the displacement sensor is composed of a reading head and a grating ruler, which is the position acquisition device of the pneumatic servo actuator , used to collect and feed back the displacement of the pneumatic servo actuator; the connection relationship is: one end of the bellows is sealed, connected with the mover of the air-floating guide rail, and the other end is fixed on the mechanism body, and the bellows is provided on the mechanism body. The air hole; the stage is installed on the mover of the air-floating guide rail; the bottom end of the stator of the air-floating guide rail is fixed on the mechanism body; when the air-floating guide rail works normally, the mover of the air-floating guide rail moves without friction; the grating scale is fixed on the carrier The side of the object stage; the reading head is fixed on one side of the mechanism body and is opposite to the grating ruler;
其工作过程为:打开气源,气体经过过滤器,一路经第一减压阀给气浮导轨定子进气孔通入一定压力的气体和另一路经第二减压阀经进气孔给波纹管通入一定压力的气体,气浮导轨正常工作,波纹管推动气浮导轨动子无摩擦运动,带动安装在气浮导轨动子上的载物台一起运动时,读数头能够读出随载物台一起运动的光栅尺的刻度变化量,该变化量等于载物台的移动距离。Its working process is as follows: open the air source, the gas passes through the filter, one way passes through the first pressure reducing valve to feed a certain pressure gas into the inlet hole of the stator of the air flotation guide rail, and the other way passes through the second pressure reducing valve and through the air inlet hole to feed the corrugated air. A certain pressure of gas is passed through the tube, and the air-floating guide rail works normally. The bellows pushes the mover of the air-floating guide rail to move without friction, and when the stage mounted on the mover of the air-floating guide rail moves together, the reading head can read the The scale change of the grating ruler moving together with the object stage is equal to the moving distance of the stage.
所述纹管优选金属材质。The bellows is preferably made of metal.
所述第一减压阀给气浮导轨定子进气孔通入的气体压力为0.3~0.6Mpa;第二减压阀经进气孔给波纹管通入的气体压力为0~1.0Mpa。The gas pressure that the first pressure reducing valve feeds into the inlet hole of the stator of the air flotation guide rail is 0.3-0.6Mpa; the gas pressure that the second pressure reducing valve feeds into the bellows through the air inlet hole is 0-1.0Mpa.
有益效果Beneficial effect
本发明对比现有技术,具有以下优点:Compared with the prior art, the present invention has the following advantages:
1、通过将波纹管安装在载物台的一端,使得气动伺服执行机构在运动过程中不受摩擦力等非线性因素的影响;并且波纹管输出位移和输入压力成线性关系,容易控制。1. By installing the bellows at one end of the stage, the pneumatic servo actuator will not be affected by non-linear factors such as friction during the movement; and the output displacement of the bellows has a linear relationship with the input pressure, which is easy to control.
2、气浮导轨通过外部输入的压力气体在气浮导轨定子和动子之间形成一层气膜,使气浮导轨动子可以无摩擦、无振动的平滑运动,从而使气动伺服执行机构获得较高的运动精度和定位精度。2. The air-floating guide rail forms a layer of air film between the stator and the mover of the air-floating guide rail through the pressure gas input from the outside, so that the mover of the air-floating guide rail can move smoothly without friction and vibration, so that the pneumatic servo actuator can obtain High motion accuracy and positioning accuracy.
附图说明 Description of drawings
图1为本发明所述气动伺服执行机构的整体结构图;Fig. 1 is the overall structural diagram of the pneumatic servo actuator of the present invention;
图2为本发明所述气动伺服执行机构的剖视结构图;Fig. 2 is a sectional structure diagram of the pneumatic servo actuator of the present invention;
图3为本发明所述气浮导轨结构图;Fig. 3 is a structural diagram of the air-floating guide rail of the present invention;
图4为本发明所述气动伺服执行机构的气动回路图;Fig. 4 is a pneumatic circuit diagram of the pneumatic servo actuator of the present invention;
图5为本发明所述气动伺服执行机构中直流电压和光栅尺的连接图;Fig. 5 is a connection diagram of a DC voltage and a grating ruler in the pneumatic servo actuator of the present invention;
图中,1-金属波纹管、2-进气孔、3-气浮导轨动子、4-气浮导轨定子、5-气浮导轨定子进气孔、6-光栅尺、7-读数头、8-机构体、9-载物台、10-过滤器、11-气源、12-第一减压阀、13-第二减压阀、14-直流电源。In the figure, 1-metal bellows, 2-intake hole, 3-air-floating guide rail mover, 4-air-floating guide rail stator, 5-air-floating guide rail stator air inlet, 6-grating ruler, 7-reading head, 8-mechanism body, 9-stage, 10-filter, 11-air source, 12-first pressure reducing valve, 13-second pressure reducing valve, 14-DC power supply.
具体实施方式 Detailed ways
下面结合附图和实施例对本发明做进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
本实施例中的一种气动伺服执行机构,其结构组成如图1所示,包括金属波纹管1、气浮导轨动子3、气浮导轨定子4、光栅尺6、读数头7、机构体8、载物台9。其中,金属波纹管1的一端中央设有进气孔2。气浮导轨动子3和气浮导轨定子4组成气浮导轨,气浮导轨定子一侧设有进气孔5。A pneumatic servo actuator in this embodiment has a structural composition as shown in Figure 1, including a
上述组成部件的连接关系为:The connection relationship of the above components is as follows:
金属波纹管1一端封死,并与气浮导轨动子3连接,设有进气孔2的一端固定在机构体8上。载物台9安装在气浮导轨动子3上。气浮导轨定子4固定连接在机构体8上。气浮导轨动子3穿过气浮导轨定子4;One end of the
读数头7和光栅尺6组成位移传感器,光栅尺6固定在载物台9的侧面。读数头7固定在机构体8的一侧,并与光栅尺6相对,直流电源14给读数头7提供工作电压14;The
当气动伺服执行机构工作时,气源11产生供气压力经过气体过滤器10,一路经第二减压阀13通过波纹管1的进气孔2给金属波纹管供气;另一路经第一减压阀12通过气浮导轨定子上4的进气孔6给气浮导轨供气。When the pneumatic servo actuator is working, the air supply pressure generated by the
优选的,金属波纹管1工作的压力为0.5Mpa可调压力,气浮导轨的工作压力为0.4MPa,位移传感器的工作电压为5V。Preferably, the working pressure of the
打开气源11,气体经过过滤器10,经第一减压阀12给气浮导轨提供0.4MPa的压力,气浮导轨正常工作,气浮导轨动子3可以无摩擦运动。Turn on the
同时,气源11经第二减压阀13给金属波纹管1的进气孔2提供0.5MPa的可调压力,直流电源14为位移传感器读数头7提供5V的工作电压。金属波纹管1内腔承受气压时会伸长,并带动气浮导轨动子3及安装在气浮导轨动子3上的载物台5一起运动,读数头7读出随载物台9一起运动的位移传感器光栅尺6刻度的变化量,即载物台9移动的距离为1.797mm。At the same time, the
调节第二减压阀13,改变输入金属波纹管1的压力在0~0.8Mpa的范围内变化,可以得到位移传感器测得的相应的位移量。By adjusting the second decompression valve 13 and changing the pressure input to the
通过上述过程,金属波纹管1将输入的压力变为位移输出,输入压力和输出位移呈线性关系,如图5所示。由此可见,在这一过程中,完全避免了非线性因素的扰动。Through the above process, the
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201110195143 CN102297177B (en) | 2011-07-13 | 2011-07-13 | Pneumatic servo actuator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201110195143 CN102297177B (en) | 2011-07-13 | 2011-07-13 | Pneumatic servo actuator |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102297177A true CN102297177A (en) | 2011-12-28 |
CN102297177B CN102297177B (en) | 2013-10-30 |
Family
ID=45357790
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201110195143 Expired - Fee Related CN102297177B (en) | 2011-07-13 | 2011-07-13 | Pneumatic servo actuator |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102297177B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110076734A (en) * | 2019-05-20 | 2019-08-02 | 青岛理工大学 | Pneumatic bellows drive ultra-precise two-dimensional positioning platform |
CN110174047A (en) * | 2018-10-25 | 2019-08-27 | 山东理工大学 | A kind of back pressure type U-tube gas electric transducer |
CN111120149A (en) * | 2019-12-13 | 2020-05-08 | 内蒙航天动力机械测试所 | Servo actuator stroke detection device |
CN111895917A (en) * | 2020-08-19 | 2020-11-06 | 中国科学院力学研究所 | A method for detecting deformation of high-enthalpy gas medium compensator |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5347914A (en) * | 1991-10-21 | 1994-09-20 | Matsushita Electric Industrial Co., Ltd. | Traverse apparatus |
DE202005014215U1 (en) * | 2005-09-09 | 2006-03-09 | Morawski, Jerzy Henryk | Linear guide for transmitting of transverse forces for standard cylinders of all types has slide unit detachably connected to piston rod of standard cylinder by means of driver-angle piece |
CN101275594A (en) * | 2007-03-31 | 2008-10-01 | 费斯托合资公司 | Fluid power arrangement |
CN101290021A (en) * | 2008-06-10 | 2008-10-22 | 胡书彬 | Bellows power cylinder |
-
2011
- 2011-07-13 CN CN 201110195143 patent/CN102297177B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5347914A (en) * | 1991-10-21 | 1994-09-20 | Matsushita Electric Industrial Co., Ltd. | Traverse apparatus |
DE202005014215U1 (en) * | 2005-09-09 | 2006-03-09 | Morawski, Jerzy Henryk | Linear guide for transmitting of transverse forces for standard cylinders of all types has slide unit detachably connected to piston rod of standard cylinder by means of driver-angle piece |
CN101275594A (en) * | 2007-03-31 | 2008-10-01 | 费斯托合资公司 | Fluid power arrangement |
CN101290021A (en) * | 2008-06-10 | 2008-10-22 | 胡书彬 | Bellows power cylinder |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110174047A (en) * | 2018-10-25 | 2019-08-27 | 山东理工大学 | A kind of back pressure type U-tube gas electric transducer |
CN110076734A (en) * | 2019-05-20 | 2019-08-02 | 青岛理工大学 | Pneumatic bellows drive ultra-precise two-dimensional positioning platform |
CN111120149A (en) * | 2019-12-13 | 2020-05-08 | 内蒙航天动力机械测试所 | Servo actuator stroke detection device |
CN111895917A (en) * | 2020-08-19 | 2020-11-06 | 中国科学院力学研究所 | A method for detecting deformation of high-enthalpy gas medium compensator |
CN111895917B (en) * | 2020-08-19 | 2021-08-31 | 中国科学院力学研究所 | A method for detecting deformation of high-enthalpy gas medium compensator |
Also Published As
Publication number | Publication date |
---|---|
CN102297177B (en) | 2013-10-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103170845B (en) | Accuracy compensation method of coaxial macro-micro composite linear motion platform device | |
CN102297177B (en) | Pneumatic servo actuator | |
CN110434835A (en) | A kind of macro micro- precisely locating platform device of two degrees of freedom and control method | |
JP3825737B2 (en) | Precision positioning device and processing machine using the same | |
CN102543217A (en) | Macro-micro driven bidimensional integrated micro positioning platform | |
CN107622786B (en) | Two-stage piezoelectric driving micro-nano positioning platform | |
CN205064770U (en) | Grand little two actuation transmission platform | |
CN101556933A (en) | Motion-decoupling XY-direction precise locating platform | |
CN110439958B (en) | Planar two-degree-of-freedom micro-disturbance flexible active vibration isolation device and method | |
CN106896851A (en) | It is a kind of to rotate and the mobile double-flexibility beam control device and method for directly driving | |
CN108555322B (en) | An experimental method for comprehensive performance testing of lathe feed system | |
CN106430088A (en) | Large-stroke six-degree-of-freedom magnetic-suspension magnetically-driven nano positioning platform | |
CN106594070B (en) | Sub-nano-scale precision drive workbench based on flexible structure | |
CN204349758U (en) | A kind of grand micro-positioning table | |
Kawashima et al. | Development of coarse/fine dual stage using pneumatically driven bellows actuator and cylinder with air bearings | |
CN109296895B (en) | X-Z long-stroke high-speed scanning device | |
CN102069201A (en) | Two-degree-of-freedom dynamic error counteracting device for free-form surface ultra-precision turning | |
CN205166401U (en) | Parallelly connected X -Y workstation | |
CN108227487A (en) | Friction Compensation Auto-disturbance-rejection Control and motion platform are switched based on prediction model | |
CN202155740U (en) | Numerically controlled quick precision feeder | |
CN212311409U (en) | Gantry machine tool with high-pressure counterweight component | |
CN103062285B (en) | Coplane air floatation orthogonal decoupling and flexible membrane angle decoupling zero-stiffness vibration isolator | |
CN211117334U (en) | Planar two-degree-of-freedom micro-disturbance flexible active vibration isolation device | |
CN209578822U (en) | Coupled Rigid-flexible platform and motion platform with frictional rigidity switching device | |
CN107240422B (en) | A kind of Pneumatic precision positioning mechanism of piezoelectric micromotor bit shift compensation |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131030 Termination date: 20160713 |