CN116654289A - Automatic assembling and adjusting method for star sensor CMOS circuit board target surface - Google Patents
Automatic assembling and adjusting method for star sensor CMOS circuit board target surface Download PDFInfo
- Publication number
- CN116654289A CN116654289A CN202310595871.1A CN202310595871A CN116654289A CN 116654289 A CN116654289 A CN 116654289A CN 202310595871 A CN202310595871 A CN 202310595871A CN 116654289 A CN116654289 A CN 116654289A
- Authority
- CN
- China
- Prior art keywords
- circuit board
- cmos circuit
- assembly
- displacement slide
- star sensor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 82
- 238000005259 measurement Methods 0.000 claims abstract description 32
- 238000001514 detection method Methods 0.000 claims abstract description 22
- 238000012545 processing Methods 0.000 claims abstract description 10
- 238000000227 grinding Methods 0.000 claims abstract description 9
- 238000006073 displacement reaction Methods 0.000 claims description 152
- 238000001179 sorption measurement Methods 0.000 claims description 83
- 239000000463 material Substances 0.000 claims description 32
- 238000003825 pressing Methods 0.000 claims description 32
- 238000009434 installation Methods 0.000 claims description 18
- 230000003287 optical effect Effects 0.000 claims description 13
- 239000000523 sample Substances 0.000 claims description 12
- 125000006850 spacer group Chemical group 0.000 claims description 7
- 238000009826 distribution Methods 0.000 claims description 4
- 238000007689 inspection Methods 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 230000000007 visual effect Effects 0.000 claims description 3
- 238000013461 design Methods 0.000 claims description 2
- 238000012360 testing method Methods 0.000 claims 2
- 238000004364 calculation method Methods 0.000 abstract description 2
- 239000000306 component Substances 0.000 description 12
- 238000010586 diagram Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 238000003384 imaging method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013102 re-test Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/26—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Manufacturing & Machinery (AREA)
- Optical Transform (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
Abstract
Description
技术领域technical field
本发明属于航天器件精密装配技术领域,涉及一种星敏感器CMOS电路板靶面自动装调方法,是一种用于小型化星敏感器星光敏感处理单元中含有靶面的CMOS电路板自动装配和调整的技术。The invention belongs to the technical field of precision assembly of aerospace devices, and relates to a method for automatic assembly and adjustment of a target surface of a CMOS circuit board of a star sensor, which is an automatic assembly method for a CMOS circuit board containing a target surface in a starlight sensitive processing unit of a miniaturized star sensor and tuned techniques.
背景技术Background technique
星敏感器是以星空为工作对象的高精度空间姿态测量装置,用于为航空航天飞行器提供准确的空间方位和基准,其具有姿态确定精度高、数据处理速度快、体积小、质量和功耗大幅度降低等特点。星敏感器主要由小型化结构单元、光学系统单元、星光敏感处理单元三个部分组成,星光敏感处理单元中图像处理器与成像电路焊接后两者统称为CMOS电路板,CMOS电路板是星敏感器的核心组件,靶面即位于CMOS电路板中的指定位置,其制造和装调精度都会对星敏感器性能有着重要影响。因此,星光敏感处理单元中靶面的装调方法对提高星敏感器的姿态测量精度具有重要意义。The star sensor is a high-precision space attitude measurement device with the starry sky as the working object. It is used to provide accurate space orientation and reference for aerospace vehicles. It has high attitude determination accuracy, fast data processing speed, small size, quality and power consumption. Significantly reduced and so on. The star sensor is mainly composed of three parts: a miniaturized structural unit, an optical system unit, and a star-sensitive processing unit. The image processor and the imaging circuit in the star-sensitive processing unit are collectively called a CMOS circuit board after welding. The core component of the star sensor, the target surface is located at the specified position on the CMOS circuit board, and its manufacturing and assembly accuracy will have an important impact on the performance of the star sensor. Therefore, the adjustment method of the target surface in the starlight sensitive processing unit is of great significance to improve the attitude measurement accuracy of the star sensor.
星敏感器中CMOS电路板与星敏感器支架的装调,其精度要求是让靶面相对于星敏感器支架底部基准面的安装倾斜范围小于等于2′,同时要求靶面中像素点矩形的x、y轴相对于基准面边线的安装倾斜范围小于等于1′。目前的装调方法主要是利用专用夹具工装和螺钉、销螺钉等工具的人工装配,如发明专利号CN201810202225.3,陈汀等人发明了一种星载星敏感器高精度高稳定度安装方法,其装调过程是将星敏感器装卡到特制的安装结构上,通过手动拧紧对角安装孔的螺钉并施加要求的力矩保证精度要求,该方法对于力矩的精确施加难以保障,同时对角螺钉的力矩不同易损坏工件。发明专利号CN201811549719.5,翟正一等人发明了一种星敏感器的基准棱镜高效装调系统及装调方法,采用六维调整架和双自准直仪进行装调,该方法的装配过程主要依靠人工装配,对装配过程中的零件调整有一定效果,但需不断进行六个维度的调节,效率较低。在论文《星敏感器成像平面姿态检测方法的研究》中,秦国花设计了一台二维导轨搭配龙门结构的星敏感器成像面姿态检测设备,以底座上的立方镜为参考基准,通过激光位移传感器和相机实现成像面倾斜角检测,采用最小二乘法完成倾斜角的计算,文中设备与方法能实现装配效果的检测但是不涉及具体的零件装配方法,且待检测工件均位于固定底座同一表面上,而本专利装调任务中,CMOS电路板靶面和基准面位于不同平面内,测量难度相对增大。For the assembly and adjustment of the CMOS circuit board and the star sensor bracket in the star sensor, the precision requirement is to make the installation inclination range of the target surface relative to the bottom reference plane of the star sensor bracket less than or equal to 2′, and at the same time require the pixel point rectangle in the target surface to be x , The installation inclination range of the y-axis relative to the edge of the reference plane is less than or equal to 1'. The current assembly and adjustment method mainly uses special fixtures and tools such as screws, pins and screws for manual assembly, such as the invention patent No. CN201810202225.3, Chen Ting and others invented a high-precision and high-stability installation method for satellite-borne star sensors , the installation and adjustment process is to clamp the star sensor to a special installation structure, manually tighten the screws in the diagonal mounting holes and apply the required torque to ensure the accuracy requirements, this method is difficult to guarantee the precise application of torque, and at the same time The torque of the screw is different, which is easy to damage the workpiece. Invention Patent No. CN201811549719.5, Zhai Zhengyi and others invented a high-efficiency assembly and adjustment system and method for the reference prism of the star sensor. The process mainly relies on manual assembly, which has a certain effect on the adjustment of parts during the assembly process, but it needs to continuously adjust six dimensions, and the efficiency is low. In the paper "Research on Attitude Detection Method of Star Sensor Imaging Plane", Qin Guohua designed a star sensor imaging surface attitude detection device with two-dimensional guide rail and gantry structure. The sensor and camera realize the detection of the inclination angle of the imaging surface, and the least square method is used to complete the calculation of the inclination angle. The equipment and method in this paper can realize the detection of the assembly effect but do not involve the specific assembly method of the parts, and the workpieces to be detected are all located on the same surface of the fixed base , but in this patent assembly task, the target surface and the reference surface of the CMOS circuit board are located in different planes, and the measurement difficulty is relatively increased.
综上所述可知,现有的装调方法其装调精度依赖于工人的技术水平、操作习惯、工作经验等,装调精度低、废品率高。针对上述问题,提高工人的操作水平来达到很高的装调精度较难实现,产出投入比很小,并且自动化程度较低,对装调精度的保证很难做到。发明合理可行,方便高效的装调方法并配合自主开发的自动化装调设备,才能满足目前装调效率和装调精度的要求。To sum up, it can be seen that the adjustment accuracy of the existing adjustment methods depends on the technical level, operating habits, work experience, etc. of the workers, and the adjustment accuracy is low and the reject rate is high. In view of the above problems, it is difficult to improve the operation level of workers to achieve high assembly accuracy, the output-to-input ratio is small, and the degree of automation is low, so it is difficult to guarantee the assembly accuracy. Only by inventing a reasonable, feasible, convenient and efficient assembly method and cooperating with the self-developed automatic assembly equipment can the current requirements of assembly efficiency and accuracy be met.
发明内容Contents of the invention
本发明要解决的技术问题是:克服目前CMOS电路板与星敏感器支架装调工艺所带来的精度与效率缺陷,发明一种星敏感器CMOS电路板靶面自动装调方法,可以快速准确地实现CMOS电路板与星敏感器支架的装配调整,提高装调精度和效率。The technical problem to be solved by the present invention is: to overcome the accuracy and efficiency defects brought by the current CMOS circuit board and star sensor bracket assembly process, and to invent an automatic assembly and adjustment method for the star sensor CMOS circuit board target surface, which can be fast and accurate Realize the assembly and adjustment of CMOS circuit board and star sensor bracket accurately, improve the accuracy and efficiency of assembly and adjustment.
本发明的技术方案如下:Technical scheme of the present invention is as follows:
一种星敏感器CMOS电路板靶面自动装调方法,所采用的装调设备主要由供料模块、测量模块、装调模块和工装锁紧模块组成,其中三个模块的底部均安装在光学平台4上,从左向右依次为测量模块、工装锁紧模块和供料模块,而装调模块则采用龙门结构横架于设备上方,用于实现零件自动锁附功能。A method for automatic installation and adjustment of the target surface of a star sensor CMOS circuit board. The installation and adjustment equipment used is mainly composed of a feeding module, a measurement module, an installation and adjustment module and a tooling locking module. The bottoms of the three modules are all installed on the optical On platform 4, from left to right are the measurement module, tooling locking module and feeding module, while the assembly and adjustment module adopts a gantry structure and is horizontally placed above the equipment to realize the automatic locking function of parts.
所述的测量模块,主要由三轴精密位移滑台5、测头支座a6、组合激光位移测头7、测头支座b8、测量组件支架9和工业相机a10组成。所述测头支座a6和测头支座b8底部安装在测量组件支架9一侧,所述工业相机a10安装在测量组件支架9另一侧,测量组件支架9安装在三轴精密位移滑台5的Z轴上,三轴精密位移滑台5底部安装在光学平台4上,组合激光位移测头7由测头支座a6和测头支座b8前后锁紧,其中,组合激光位移测头7由组合夹具上安装三个小型的分光干涉式位移计构成,三者呈等边三角形形状排布。所述组合激光位移测头7在CMOS电路板1装配后,实现CMOS电路板1的靶面和星敏感器支架3下的基准面平行度的测量功能;所述工业相机a10在CMOS电路板1装配时,实现了CMOS电路板1上的像素点矩形靶面边线和星敏感器支架3基准面边线平行度测量功能;所述三轴精密位移滑台5具有三维直线运动能力,可实现组合激光位移测头7和工业相机a10调整不同的测量位置的功能。The measurement module is mainly composed of a three-axis precision displacement slide table 5, a probe support a6, a combined laser displacement probe 7, a probe support b8, a measurement component bracket 9 and an industrial camera a10. The bottom of the probe support a6 and the probe support b8 are installed on one side of the measuring component bracket 9, the industrial camera a10 is installed on the other side of the measuring component bracket 9, and the measuring component bracket 9 is installed on the three-axis precision displacement slide table On the Z axis of 5, the bottom of the three-axis precision displacement slide table 5 is installed on the optical platform 4, and the combined laser displacement probe 7 is locked front and rear by the probe support a6 and the probe support b8, wherein the combined laser displacement probe 7 consists of three small spectroscopic interferometric displacement meters installed on the combined fixture, and the three are arranged in the shape of an equilateral triangle. After the CMOS circuit board 1 is assembled, the combined laser displacement measuring head 7 realizes the measurement function of the target surface of the CMOS circuit board 1 and the parallelism of the datum plane under the star sensor bracket 3; the industrial camera a10 is mounted on the CMOS circuit board 1 During assembly, the function of measuring the parallelism of the edge of the pixel rectangular target surface on the CMOS circuit board 1 and the edge of the reference plane of the star sensor bracket 3 is realized; the three-axis precision displacement slide table 5 has three-dimensional linear motion capability, and can realize combined laser The displacement probe 7 and the industrial camera a10 can adjust the functions of different measurement positions.
所述的工装锁紧模块,主要由带座轴承33、转轴支座34、转轴35、导杆气缸36、夹具组件底座37、转角气缸38、反光镜39、V型块40、直线精密位移滑台d41、精密转台b42和工装锁紧组件支架43组成。所述工装锁紧组件支架43为U型结构,其中部安装有反光镜39,其一端侧面上安装有带座轴承33,其另一端侧面上安装有精密转台b42,其底部安装在直线精密位移滑台d41上,直线精密位移滑台d41底部安装在光学平台4上;所述夹具组件底座37为L型结构,其一端安装有转轴支座34,转轴35的一端从转轴支座34的开口中穿过并锁紧固定,转轴35的另一端从带座轴承33中穿过并固定;所述夹具组件底座37的另一端安装在精密转台b42的转台面上;所述导杆气缸36安装在夹具组件底座37一端,所述转角气缸38竖直安装在夹具组件底座37中部,所述V型块40安装在夹具组件底座37另一端侧面上。所述反光镜39实现了工业相机a10在侧面自下向上观测CMOS电路板1上像素点矩形靶面和星敏感器支架3基准面的功能;所述L型夹具组件底座37及转轴支座34、转轴35和带座轴承33、精密转台b42等组件,组成类秋千的转动结构,在精密转台b42驱动下,可使夹具组件底座37以及其上的星敏感器支架3零件和转轴支座34、转轴35、导杆气缸36、转角气缸38和V型块40等组件,绕着精密转台b42转轴旋转,在装配和测量时,实现了调整CMOS电路板1、调整垫片2和星敏感器支架3零件姿态的功能;所述V型块40适配星敏感器支架3外轮廓设计,在星敏感器支架3定位夹紧中实现定位的功能;所述导杆气缸36的顶杆可沿着V型块40开口方向伸缩运动,在星敏感器支架3定位夹紧中实现夹紧的功能;所述转角气缸38可绕自身转轴旋转90°后锁紧,实现CMOS电路板1调整装配后,CMOS电路板1的锁紧功能;所述直线精密位移滑台d41可沿单一方向位移,实现其上零件的工作位置调整和装配调整的功能。The tooling locking module is mainly composed of a bearing with seat 33, a rotating shaft support 34, a rotating shaft 35, a guide rod cylinder 36, a fixture assembly base 37, a corner cylinder 38, a reflector 39, a V-shaped block 40, and a linear precision displacement slide. Table d41, precision turntable b42 and tooling locking component bracket 43 are composed. The tooling locking assembly bracket 43 is a U-shaped structure, a reflector 39 is installed in the middle, a bearing with a seat 33 is installed on one end side, a precision turntable b42 is installed on the other end side, and the bottom is installed on a linear precision displacement On the slide table d41, the bottom of the linear precision displacement slide table d41 is installed on the optical table 4; the base 37 of the clamp assembly is an L-shaped structure, and one end of the slide table d41 is equipped with a rotating shaft support 34, and one end of the rotating shaft 35 is connected from the opening of the rotating shaft support 34 The other end of the rotating shaft 35 passes through the bearing 33 and is fixed; the other end of the clamp assembly base 37 is installed on the turntable surface of the precision turntable b42; the guide rod cylinder 36 is installed At one end of the clamp assembly base 37 , the angle cylinder 38 is vertically installed in the middle of the clamp assembly base 37 , and the V-shaped block 40 is installed on the side of the other end of the clamp assembly base 37 . The reflector 39 realizes the function of the industrial camera a10 observing the rectangular target surface of pixels on the CMOS circuit board 1 and the reference plane of the star sensor bracket 3 from the side to the top; the L-shaped clamp assembly base 37 and the rotating shaft support 34 , rotating shaft 35, bearing with seat 33, precision turntable b42 and other components form a swing-like rotating structure. Driven by the precision turntable b42, the fixture assembly base 37 and the star sensor bracket 3 parts and the rotating shaft support 34 on it can be made , rotating shaft 35, guide rod cylinder 36, corner cylinder 38 and V-shaped block 40 and other components rotate around the rotating shaft of precision turntable b42, and realize the adjustment of CMOS circuit board 1, adjustment gasket 2 and star sensor during assembly and measurement The function of the attitude of the bracket 3 parts; the V-shaped block 40 is adapted to the outer contour design of the star sensor bracket 3, and realizes the positioning function in the positioning and clamping of the star sensor bracket 3; the ejector rod of the guide rod cylinder 36 can be moved along the The telescopic movement in the opening direction of the V-shaped block 40 realizes the clamping function in the positioning and clamping of the star sensor bracket 3; the corner cylinder 38 can be locked after rotating 90° around its own rotating shaft, so that the CMOS circuit board 1 can be adjusted and assembled. , the locking function of the CMOS circuit board 1; the linear precision displacement slide table d41 can be displaced in a single direction to realize the function of adjusting the working position and assembly of parts on it.
所述的装调模块,主要由型材支架11、直线精密位移滑台a12、滑台支架16、装调模组和锁付模组组成;所述滑台支架16为U型结构,其两端分别安装有装调模组和锁付模组,其中部安装在直线精密位移滑台a12上,直线精密位移滑台a12底部安装在型材支架11上,型材支架11底部安装在光学平台4上。所述装调模组主要由工业相机b13、装调组件支架14、直线精密位移滑台b15、精密转台a26、圆柱式力传感器27和零件吸附头28组成。所述零件吸附头28顶部安装在圆柱式力传感器27底部,圆柱式力传感器27顶部安装在精密转台a26底部的转台面上,精密转台a26顶部安装在装调组件支架14底部的安装面上,工业相机b13安装在装调组件支架14上,装调组件支架14侧面安装在直线精密位移滑台b15的台面上,直线精密位移滑台b15安装在滑台支架16侧面上。所述锁付模组主要由滑台气缸17、锁付气缸18、锁付组件底座19、直线导轨20、电动螺丝刀21、电动螺丝刀支架22和螺丝吸附头23组成。所述电动螺丝刀21安装在电动螺丝刀支架22上,电动螺丝刀支架22为L型结构,其侧面安装在直线导轨20上,直线导轨20底部安装在锁付组件底座19上,锁付组件底座19为L型结构,其侧面安装在滑台气缸17台面上,滑台气缸17底部安装在滑台支架16侧面上,所述锁付气缸18固定安装在锁付组件底座19上,其顶杆与电动螺丝刀支架22相连接安装,所述螺丝吸附头23安装在锁付组件底座19的底部。所述直线精密位移滑台a12、直线精密位移滑台b15和直线精密位移滑台d41组合形成零件拾取装配的三维运动结构;所述直线精密位移滑台a12、滑台气缸17和直线精密位移滑台d41组合形成螺丝吸附取料和零件锁付过程的三维运动结构;所述精密转台a26可驱动零件吸附头28上吸附的零件绕转轴旋转,即实现调整CMOS电路板1上的像素点矩形靶面边线和星敏感器支架3基准面边线平行度的功能;所述工业相机b13实现待装配零件位置识别的功能;所述圆柱式力传感器27实时反馈装配过程中零件吸附头28与零件之间的接触力,既避免接触不充分导致零件拾取失败,也避免过大的接触力损伤零件及设备;所述锁付模组可实现螺丝吸附和零件锁付功能,其中,锁付气缸18实现驱动电动螺丝刀支架22及其上电动螺丝刀21上下往复锁付运动的功能,直线导轨20实现对电动螺丝刀支架22及其上电动螺丝刀21上下往复运动的导向功能,螺丝吸附头23实现螺丝供料器24提供的螺丝吸附取料功能。The assembly and adjustment module is mainly composed of a profile bracket 11, a linear precision displacement slide a12, a slide table support 16, an assembly and adjustment module and a locking module; the slide table support 16 is a U-shaped structure, and its two ends The adjustment module and the locking module are respectively installed, the middle part of which is installed on the linear precision displacement slide a12, the bottom of the linear precision displacement slide a12 is installed on the profile support 11, and the bottom of the profile support 11 is installed on the optical table 4. The assembly and adjustment module is mainly composed of an industrial camera b13, an assembly assembly bracket 14, a linear precision displacement slide b15, a precision turntable a26, a cylindrical force sensor 27 and a part adsorption head 28. The top of the part adsorption head 28 is installed on the bottom of the cylindrical force sensor 27, the top of the cylindrical force sensor 27 is installed on the turntable surface at the bottom of the precision turntable a26, and the top of the precision turntable a26 is installed on the mounting surface at the bottom of the assembly bracket 14, The industrial camera b13 is installed on the adjustment component bracket 14, the side of the adjustment component bracket 14 is installed on the table top of the linear precision displacement slide b15, and the linear precision displacement slide b15 is installed on the side of the slide bracket 16. The locking module is mainly composed of a sliding table cylinder 17, a locking cylinder 18, a locking assembly base 19, a linear guide rail 20, an electric screwdriver 21, an electric screwdriver bracket 22 and a screw suction head 23. The electric screwdriver 21 is installed on the electric screwdriver support 22, the electric screwdriver support 22 is an L-shaped structure, its side is installed on the linear guide rail 20, and the bottom of the linear guide rail 20 is installed on the lock assembly base 19, and the lock assembly base 19 is L-shaped structure, its side is installed on the slide table cylinder 17 table, the bottom of the slide table cylinder 17 is installed on the side of the slide table bracket 16, the lock pay cylinder 18 is fixedly installed on the lock pay assembly base 19, its ejector rod and electric The screwdriver brackets 22 are connected and installed, and the screw suction head 23 is installed on the bottom of the base 19 of the locking assembly. The linear precision displacement slide a12, the linear precision displacement slide b15 and the linear precision displacement slide d41 are combined to form a three-dimensional motion structure for picking and assembling parts; the linear precision displacement slide a12, the slide cylinder 17 and the linear precision displacement slide The table d41 is combined to form a three-dimensional motion structure of the process of screw adsorption and retrieving and parts lock and pay; the precision turntable a26 can drive the parts adsorbed on the part adsorption head 28 to rotate around the rotation axis, that is, to realize the adjustment of the pixel point rectangular target on the CMOS circuit board 1 The function of parallelism between the surface edge and the star sensor bracket 3 reference surface edge; the industrial camera b13 realizes the function of identifying the position of the parts to be assembled; the cylindrical force sensor 27 provides real-time feedback between the part suction head 28 and the part during the assembly process. The contact force can not only avoid the failure of picking up parts due to insufficient contact, but also avoid damage to parts and equipment due to excessive contact force; the locking module can realize the functions of screw adsorption and parts locking, wherein the locking cylinder 18 realizes the driving The electric screwdriver bracket 22 and its upper electric screwdriver 21 have the function of reciprocating up and down movement, the linear guide rail 20 realizes the guiding function of the electric screwdriver bracket 22 and its upper electric screwdriver 21 up and down reciprocating movement, and the screw suction head 23 realizes the screw feeder 24 The provided screw adsorption and reclaiming function.
所述的供料模块主要由螺丝供料器24、螺丝供料器底座25、料盘29、压块30、直线精密位移滑台c31和供料组件底座32组成。所述螺丝供料器24底部安装在螺丝供料器底座25上,螺丝供料器底座25底部安装在光学平台4上;所述料盘29底部安装在直线精密位移滑台c31上,直线精密位移滑台c31底部安装在供料组件底座32上,供料组件底座32底部安装在光学平台4上;所述压块30放置在料盘上固定区域。所述螺丝供料器24实现螺丝的供料功能;所述料盘29适配CMOS电路板1、调整垫片2和压块30上的孔位,设计有凸台形状的限位结构,使得三个调整垫片2放置在料盘29上直接呈三角形分布,使得调整垫片2和压块30放置在料盘29的平面上被限位结构限制,不产生过大的转动,便于零件吸附头28的吸附拾取;所述压块30底部涂覆有缓冲材料,CMOS电路板1安装后,由装调模块拾取压块30并压装在CMOS电路板1上,再由转角气缸38压紧压块30,避免转角气缸38直接压紧在CMOS电路板1上损伤零件,并且由于CMOS电路板1与星敏感器支架3之间最终需要螺丝锁紧,所以压块30压紧CMOS电路板1后,对应CMOS电路板1上的螺孔位置设计有开口结构,保证压紧状态下不影响螺丝锁付。The feeding module is mainly composed of a screw feeder 24 , a screw feeder base 25 , a tray 29 , a pressing block 30 , a linear precision displacement slide table c31 and a feeding assembly base 32 . The bottom of the screw feeder 24 is installed on the screw feeder base 25, and the bottom of the screw feeder base 25 is installed on the optical platform 4; the bottom of the material tray 29 is installed on the linear precision displacement slide table c31, and the linear precision The bottom of the displacement slide c31 is installed on the base 32 of the feeding assembly, and the bottom of the base 32 of the feeding assembly is installed on the optical table 4; the pressing block 30 is placed on a fixed area on the tray. The screw feeder 24 realizes the feeding function of the screw; the feed tray 29 is adapted to the holes on the CMOS circuit board 1, the adjustment gasket 2 and the pressure block 30, and is designed with a boss-shaped stop structure, so that The three adjusting shims 2 are placed directly on the tray 29 in a triangular distribution, so that the adjusting shims 2 and the briquetting block 30 are placed on the plane of the feeding tray 29 and are limited by the limit structure, without excessive rotation, which is convenient for parts adsorption Adsorption and picking of the head 28; the bottom of the press block 30 is coated with a buffer material. After the CMOS circuit board 1 is installed, the press block 30 is picked up by the assembly module and pressed on the CMOS circuit board 1, and then compressed by the corner cylinder 38 The pressing block 30 prevents the corner cylinder 38 from directly pressing on the CMOS circuit board 1 to damage the parts, and since the CMOS circuit board 1 and the star sensor bracket 3 need to be screwed and locked eventually, the pressing block 30 presses the CMOS circuit board 1 Finally, an opening structure is designed corresponding to the position of the screw hole on the CMOS circuit board 1, so as to ensure that the screw lock is not affected under the pressed state.
在整个装调过程中,完成CMOS电路板1靶面与星敏感器支架3基准面的平行度检测后,需要比对其是否满足精度要求,如若满足安装倾斜范围要求,可以继续进行下一步装配过程;如若不满足安装倾斜范围要求,则要立刻停止装配,依据算法计算出调整垫片所需的研磨量,待研磨加工完成以新的调整垫片重新检测平行度直至合格后完成整个装调流程。因此,以平行度检测过程为分界点,将该星敏感器CMOS电路板靶面自动装调方法划分为三道工序,分别是装配工序、检验工序、锁附工序,具体步骤如下:During the entire assembly and adjustment process, after completing the parallelism detection of the target surface of the CMOS circuit board 1 and the reference surface of the star sensor bracket 3, it is necessary to compare whether it meets the accuracy requirements. If the installation tilt range requirements are met, the next step of assembly can be continued process; if the installation tilt range requirements are not met, the assembly must be stopped immediately, and the grinding amount required for the adjustment gasket is calculated according to the algorithm. After the grinding process is completed, a new adjustment gasket is used to re-test the parallelism until it is qualified, and the entire assembly and adjustment is completed. process. Therefore, taking the parallelism detection process as the demarcation point, the automatic assembly and adjustment method of the target surface of the star sensor CMOS circuit board is divided into three processes, which are the assembly process, the inspection process, and the locking process. The specific steps are as follows:
第一步,零件上料:装配前,由人工将星敏感器支架3放置在工装锁紧模块的V型块40上定位,由导杆气缸36的推杆将星敏感器支架3夹紧在V型块40中;再将压块30和待装配零件CMOS电路板1和调整垫片2放置在带有限位结构的料盘29上,完成上料。其中,料盘29对应于CMOS电路板1、调整垫片2和压块30上的孔位,设计有凸台形状的限位结构,使得三个调整垫片2放置在料盘29上直接呈三角形分布,使得调整垫片2和压块30放置在料盘29的平面上被限位结构限制,不产生过大的转动,便于零件吸附头28的吸附拾取。The first step, parts loading: before assembly, the star sensor bracket 3 is manually placed on the V-shaped block 40 of the tooling locking module for positioning, and the star sensor bracket 3 is clamped by the push rod of the guide rod cylinder 36. In the V-shaped block 40 ; place the pressing block 30 , the parts to be assembled, the CMOS circuit board 1 and the adjusting spacer 2 on the charging tray 29 with a position-limiting structure, and complete the loading. Wherein, the material tray 29 corresponds to the hole position on the CMOS circuit board 1, the adjustment gasket 2 and the pressure block 30, and is designed with a boss-shaped stop structure, so that the three adjustment gaskets 2 are placed on the material tray 29 directly to form a The triangular distribution makes the adjustment gasket 2 and the pressure block 30 placed on the plane of the material tray 29 limited by the limit structure, without excessive rotation, which is convenient for the adsorption and picking of the part adsorption head 28.
第二步,调整垫片2装配:上料完成后,进行调整垫片2装配。装调模块在直线精密位移滑台a12驱动下运动至调整垫片2吸附拾取工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台c31组合形成二维平面运动,调整零件吸附头28与调整垫片2之间的相对位置,由精密转台a26调整零件吸附头28与调整垫片2之间的相对姿态,对准后,由直线精密位移滑台b15驱动零件吸附头28向下运动,对调整垫片2进行吸附取料,取料成功后,由直线精密位移滑台b15驱动零件吸附头28带动其上调整垫片2向上运动,完成调整垫片2取料。其中,零件吸附头28与调整垫片2接触取料时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备;三个调整垫片2相互之间的位置,已在上料时由料盘29上呈三角形分布的凸台形状结构进行限位,实现零件吸附头28单次吸附拾取三个调整垫片2,提高装配效率。取料完成后,装调模块在直线精密位移滑台a12驱动下运动至调整垫片2装配调整工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台d41组合形成二维平面运动,调整零件吸附头28上吸附的调整垫片2与星敏感器支架3上装配孔位之间的相对位置,由精密转台a26调整零件吸附头28上吸附的调整垫片2与星敏感器支架3上安装孔位之间的相对姿态,对准后,由直线精密位移滑台b15驱动零件吸附头28上吸附的调整垫片2向下运动,将调整垫片2装配在星敏感器支架3的装配孔位上,装配完成后,由直线精密位移滑台b15驱动零件吸附头28向上运动恢复初始位置,完成调整垫片2装配。其中,零件吸附头28上吸附的调整垫片2与星敏感器支架3上装配孔位装配时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备。The second step, the assembly of the adjusting gasket 2: after the loading is completed, the adjusting gasket 2 is assembled. The assembly and adjustment module is driven by the linear precision displacement slide a12 to move to the position where the adjustment gasket 2 is absorbed and picked up. With the assistance of the industrial camera b13, the combination of the linear precision displacement slide a12 and the linear precision displacement slide c31 forms a two-dimensional plane Movement, adjust the relative position between the parts adsorption head 28 and the adjustment gasket 2, adjust the relative posture between the parts adsorption head 28 and the adjustment gasket 2 by the precision turntable a26, after alignment, it is driven by the linear precision displacement slide b15 The parts suction head 28 moves downwards to absorb and take out the adjustment gasket 2. After the material is taken successfully, the parts adsorption head 28 is driven by the linear precision displacement slide b15 to drive the adjustment gasket 2 to move upwards, and the adjustment gasket 2 is completed. Reclaimer. Among them, the mutual contact force between the parts adsorption head 28 and the adjustment gasket 2 when contacting and picking up materials is fed back in real time by the cylindrical force sensor 27 to ensure a suitable contact force without damaging the parts and equipment; The position of the position has been limited by the triangularly distributed boss shape structure on the material tray 29 during loading, so that the part adsorption head 28 can pick up three adjusting gaskets 2 in a single adsorption, and the assembly efficiency is improved. After the material retrieving is completed, the assembly and adjustment module is driven by the linear precision displacement slide a12 to move to the assembly and adjustment working position of the adjustment gasket 2. With the assistance of the industrial camera b13, the linear precision displacement slide a12 and the linear precision displacement slide d41 Combined to form a two-dimensional plane movement, adjust the relative position between the adjusting gasket 2 adsorbed on the part adsorption head 28 and the assembly hole position on the star sensor bracket 3, and adjust the adjusting gasket adsorbed on the part adsorption head 28 by the precision turntable a26 2 and the mounting hole on the star sensor bracket 3, after alignment, the adjusting gasket 2 adsorbed on the part adsorption head 28 is driven by the linear precision displacement slide b15 to move downward, and the adjusting gasket 2 is assembled At the assembly hole position of the star sensor bracket 3, after the assembly is completed, the linear precision displacement slide table b15 drives the part adsorption head 28 to move upward to restore the initial position, and the assembly of the adjusting gasket 2 is completed. Among them, the mutual contact force between the adjusting gasket 2 adsorbed on the part adsorption head 28 and the assembly hole position on the star sensor bracket 3 is fed back in real time by the cylindrical force sensor 27 to ensure an appropriate contact force without damaging parts and equipment .
第三步,CMOS电路板1装配:调整垫片2装配完成后,进行CMOS电路板1装配。装调模块在直线精密位移滑台a12驱动下运动至CMOS电路板1吸附拾取工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台c31组合形成二维平面运动,调整零件吸附头28与CMOS电路板1之间的相对位置,由精密转台a26调整零件吸附头28与CMOS电路板1之间的相对姿态,对准后,由直线精密位移滑台b15驱动零件吸附头28向下运动,对CMOS电路板1进行吸附取料,取料成功后,由直线精密位移滑台b15驱动零件吸附头28带动其上CMOS电路板1向上运动,完成CMOS电路板1取料。其中,零件吸附头28与CMOS电路板1接触取料时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备。取料完成后,装调模块在直线精密位移滑台a12驱动下运动至CMOS电路板1装配调整工作位置,在工业相机a10和工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台d41组合形成二维平面运动,调整零件吸附头28上吸附的CMOS电路板1与星敏感器支架3上装配孔位之间的相对位置,由精密转台a26调整零件吸附头28上吸附的CMOS电路板1的像素点矩形靶面边线和星敏感器支架3基准面边线的平行度;其中,工业相机a10在侧面,通过反光镜39自下而上地观测CMOS电路板1的像素点矩形靶面边线和星敏感器支架3基准面边线,辅助精密转台a26进行边线平行度的姿态调整,工业相机b13在顶部,自上而下观测星敏感器支架3上装配孔位,辅助直线精密位移滑台a12和直线精密位移滑台d41进行CMOS电路板1和星敏感器支架3之间的位置调整;位置姿态调整完成后,由直线精密位移滑台b15驱动零件吸附头28上吸附的CMOS电路板1向下运动,将CMOS电路板1叠装在调整垫片2上,装配完成后,由直线精密位移滑台b15驱动零件吸附头28向上运动恢复初始位置,完成CMOS电路板1装配。其中,零件吸附头28上吸附的CMOS电路板1与调整垫片2装配时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备。The third step, CMOS circuit board 1 assembly: after the adjustment spacer 2 is assembled, the CMOS circuit board 1 is assembled. The assembly module is driven by the linear precision displacement slide a12 to move to the adsorption and picking position of the CMOS circuit board 1. With the assistance of the industrial camera b13, the combination of the linear precision displacement slide a12 and the linear precision displacement slide c31 forms a two-dimensional plane Movement, to adjust the relative position between the parts suction head 28 and the CMOS circuit board 1, the relative posture between the parts suction head 28 and the CMOS circuit board 1 is adjusted by the precision turntable a26, after alignment, it is driven by the linear precision displacement slide b15 The parts suction head 28 moves downward to absorb and take out the CMOS circuit board 1. After the material is taken successfully, the linear precision displacement slide b15 drives the parts suction head 28 to drive the CMOS circuit board 1 to move upwards to complete the CMOS circuit board 1. Reclaimer. Wherein, the mutual contact force between the part adsorption head 28 and the CMOS circuit board 1 is fed back in real time by the cylindrical force sensor 27 to ensure proper contact force without damaging parts and equipment. After the material retrieving is completed, the assembly and adjustment module moves to the CMOS circuit board 1 assembly and adjustment working position driven by the linear precision displacement slide a12. With the assistance of the industrial camera a10 and the industrial camera b13, the linear precision displacement slide a12 and the linear precision The displacement slide table d41 is combined to form a two-dimensional plane movement to adjust the relative position between the CMOS circuit board 1 adsorbed on the part adsorption head 28 and the assembly hole position on the star sensor bracket 3, and the precision turntable a26 is used to adjust the adsorption on the part adsorption head 28 The parallelism between the pixel point rectangular target surface edge of the CMOS circuit board 1 and the star sensor bracket 3 reference plane edge; wherein, the industrial camera a10 is on the side, and observes the pixel points of the CMOS circuit board 1 from bottom to top through the mirror 39 The sideline of the rectangular target surface and the sideline of the reference plane of the star sensor bracket 3, the auxiliary precision turntable a26 is used to adjust the attitude of the sideline parallelism, the industrial camera b13 is on the top, and the assembly hole position on the star sensor bracket 3 is observed from top to bottom, and the auxiliary line is precise The displacement slide table a12 and the linear precision displacement slide table d41 adjust the position between the CMOS circuit board 1 and the star sensor bracket 3; after the position and attitude adjustment is completed, the linear precision displacement slide table b15 drives the CMOS adsorbed on the part adsorption head 28 The circuit board 1 moves downward, and the CMOS circuit board 1 is stacked on the adjusting gasket 2. After the assembly is completed, the linear precision displacement slide table b15 drives the part suction head 28 to move upward to restore the initial position, and the assembly of the CMOS circuit board 1 is completed. Wherein, the mutual contact force between the CMOS circuit board 1 adsorbed on the part suction head 28 and the adjusting gasket 2 during assembly is fed back in real time by the cylindrical force sensor 27 to ensure proper contact force without damaging parts and equipment.
第四步,CMOS电路板1和调整垫片2压紧:CMOS电路板1装配完成后,需要由转角气缸38压紧固定,为保护零件不受损伤,采用压块30作为中间缓冲零件。装调模块在直线精密位移滑台a12驱动下运动至压块30吸附拾取工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台c31组合形成二维平面运动,调整零件吸附头28与压块30之间的相对位置,由精密转台a26调整零件吸附头28与压块30之间的相对姿态,对准后,由直线精密位移滑台b15驱动零件吸附头28向下运动,对压块30进行吸附取料,取料成功后,由直线精密位移滑台b15驱动零件吸附头28带动其上压块30向上运动,完成压块30取料。其中,零件吸附头28与压块30接触取料时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备。取料完成后,装调模块在直线精密位移滑台a12驱动下运动至压块30装配调整工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台d41组合形成二维平面运动,调整零件吸附头28上吸附的压块30与CMOS电路板1之间的相对位置,由精密转台a26调整零件吸附头28上吸附的压块30与CMOS电路板1之间的相对姿态,对准后,由直线精密位移滑台b15驱动零件吸附头28上吸附的压块30向下运动,将压块30叠装在CMOS电路板1上,装配完成后,由直线精密位移滑台b15驱动零件吸附头28向上运动恢复初始位置,完成压块30装配。其中,零件吸附头28上吸附的压块30与CMOS电路板1叠装时的相互接触力,由圆柱式力传感器27实时反馈,保证合适的接触力,不损伤零件和设备。压块30装配完成后,转角气缸38旋转90°再下压,其压杆直接作用在压块30上,将压块30压紧在CMOS电路板1上,间接将CMOS电路板1压紧在调整垫片2上,再将调整垫片2间接压紧在星敏感器支架3上,完成所有零件的压紧。其中,压块30下表面涂覆有缓冲材料,使得压紧力均匀分布在CMOS电路板1的背面上,避免损伤CMOS电路板1。至此为装配工序。The fourth step is to compress the CMOS circuit board 1 and the adjusting spacer 2: after the CMOS circuit board 1 is assembled, it needs to be compressed and fixed by the corner cylinder 38. In order to protect the parts from damage, the pressure block 30 is used as the intermediate buffer part. The assembly and adjustment module is driven by the linear precision displacement slide a12 to move to the pick-up position of the pressure block 30. With the assistance of the industrial camera b13, the combination of the linear precision displacement slide a12 and the linear precision displacement slide c31 forms a two-dimensional plane movement , adjust the relative position between the parts adsorption head 28 and the pressing block 30, adjust the relative posture between the parts adsorption head 28 and the pressing block 30 by the precision turntable a26, after alignment, drive the parts adsorption head by the linear precision displacement slide b15 28 moves downwards to absorb and reclaim the briquetting block 30. After the material retrieving is successful, the linear precision displacement slide b15 drives the part adsorption head 28 to drive the upper briquetting block 30 to move upwards to complete the retrieving of the briquetting block 30. Among them, the mutual contact force between the part suction head 28 and the pressing block 30 is fed back in real time by the cylindrical force sensor 27 to ensure proper contact force without damaging parts and equipment. After the retrieving is completed, the assembly and adjustment module moves to the assembly and adjustment working position of the pressure block 30 under the drive of the linear precision displacement slide a12. With the assistance of the industrial camera b13, the linear precision displacement slide a12 and the linear precision displacement slide d41 are combined Form a two-dimensional plane movement, adjust the relative position between the pressure block 30 adsorbed on the part adsorption head 28 and the CMOS circuit board 1, and adjust the distance between the pressure block 30 adsorbed on the part adsorption head 28 and the CMOS circuit board 1 by the precision turntable a26 After alignment, the pressure block 30 adsorbed on the part adsorption head 28 is driven by the linear precision displacement slide b15 to move downward, and the pressure block 30 is stacked on the CMOS circuit board 1. After the assembly is completed, the linear precision The displacement slide b15 drives the part adsorption head 28 to move upwards to restore the initial position, and completes the assembly of the pressing block 30 . Among them, the mutual contact force between the pressure block 30 adsorbed on the part suction head 28 and the CMOS circuit board 1 is fed back in real time by the cylindrical force sensor 27 to ensure proper contact force without damaging parts and equipment. After the briquetting block 30 is assembled, the corner cylinder 38 rotates 90° and then presses down, and its pressing rod directly acts on the briquetting block 30, pressing the briquetting block 30 on the CMOS circuit board 1, and indirectly pressing the CMOS circuit board 1 on the CMOS circuit board 1. Adjust the gasket 2, and then press the adjusting gasket 2 indirectly on the star sensor bracket 3 to complete the compression of all parts. Wherein, the lower surface of the pressure block 30 is coated with a buffer material, so that the pressing force is evenly distributed on the back of the CMOS circuit board 1 to avoid damage to the CMOS circuit board 1 . This is the assembly process.
第五步,CMOS电路板1靶面和星敏感器支架3基准面平行度检测:CMOS电路板1和调整垫片2压紧在星敏感器3上后,测量CMOS电路板1靶面和星敏感器支架3基准面平行度。工装锁紧模块在直线精密位移滑台d41驱动下运动至CMOS电路板1靶面和星敏感器支架3基准面平行度检测工作位置,由精密转台b42驱动调整V型块40以及其上已经被转角气缸38夹紧的CMOS电路板1、调整垫片2和星敏感器支架3装配体的姿态,使得CMOS电路板1靶面和星敏感器支架3标准面朝向组合激光位移测头7,由三轴精密位移滑台5驱动组合激光位移测头7移动,分别测量CMOS电路板1靶面和星敏感器支架3标准面,并将数据传输给工控机,计算两平面之间的平行度,CMOS电路板1靶面和星敏感器支架3基准面平行度检测完成后,由精密转台b42驱动调整V型块40以及其上已经被转角气缸38夹紧的CMOS电路板1、调整垫片2和星敏感器支架3装配体的姿态,使得CMOS电路板1靶面和星敏感器支架3标准面恢复竖直向下的状态。若CMOS电路板1靶面和星敏感器支架3基准面平行度检测合格,则进行螺丝锁付流程;若CMOS电路板1靶面和星敏感器支架3基准面平行度检测不合格则计算三个调整垫片2的调整量并记录反馈给操作人员,再由装调模块将压块30、CMOS电路板1和调整垫片2进行下料,具体步骤与装配工序步骤相反,由操作人员取走调整垫片2研磨加工,加工后再重新装配调整测量。装配过程停止的该阶段,设备可继续对另一组新的零件进行平行度测量,避免耗时无效等待,同时可达到批量测量的效果。至此为检验工序。The fifth step is to measure the parallelism between the target surface of CMOS circuit board 1 and the reference plane of star sensor bracket 3: after CMOS circuit board 1 and adjusting gasket 2 are pressed on star sensor 3, measure the target surface of CMOS circuit board 1 and the star sensor bracket. Parallelism of the reference plane of the sensor bracket 3. The tooling locking module is driven by the linear precision displacement slide table d41 to move to the working position for detecting the parallelism of the target surface of the CMOS circuit board 1 and the reference plane of the star sensor bracket 3, and the V-shaped block 40 and its upper part have been adjusted by the precision turntable b42. The attitude of the CMOS circuit board 1 clamped by the corner cylinder 38, the adjustment gasket 2 and the star sensor bracket 3 assembly makes the target surface of the CMOS circuit board 1 and the standard surface of the star sensor bracket 3 face the combined laser displacement measuring head 7, by The three-axis precision displacement slide table 5 drives the combined laser displacement measuring head 7 to move, respectively measure the target surface of the CMOS circuit board 1 and the standard surface of the star sensor bracket 3, and transmit the data to the industrial computer to calculate the parallelism between the two planes. After the parallelism detection of the target surface of the CMOS circuit board 1 and the reference plane of the star sensor support 3 is completed, the precision turntable b42 drives and adjusts the V-shaped block 40 and the CMOS circuit board 1 and the adjustment gasket 2 clamped by the corner cylinder 38 on it. The posture of the assembly with the star sensor bracket 3 makes the target surface of the CMOS circuit board 1 and the standard surface of the star sensor bracket 3 return to a vertically downward state. If the parallelism detection of the target surface of CMOS circuit board 1 and the reference plane of star sensor bracket 3 is qualified, the screw lock payment process is performed; if the parallelism detection of the target surface of CMOS circuit board 1 and the reference plane of star sensor bracket 3 is unqualified, then three The adjustment amount of each adjusting gasket 2 is recorded and fed back to the operator, and then the assembly and adjustment module is used to unload the pressing block 30, the CMOS circuit board 1 and the adjusting gasket 2. Grind and process the adjustment shim 2, and then reassemble and adjust the measurement after processing. At this stage when the assembly process is stopped, the equipment can continue to measure the parallelism of another set of new parts, avoiding time-consuming and invalid waiting, and at the same time achieving the effect of batch measurement. This is the inspection process.
第六步,若满足精度要求,进行CMOS电路板1锁付:CMOS电路板1靶面和星敏感器支架3基准面平行度检测合格后,进行CMOS电路板1锁付。工装锁紧模块在直线精密位移滑台d41驱动下运动至CMOS电路板1锁付工作位置,锁付模组在直线精密位移滑台a12驱动下运动至螺丝供料器24上的吸附取料位置,由滑台气缸17驱动锁付模组中的螺丝吸附头23向下运动,对螺丝进行吸附取料,取料成功后,由滑台气缸17驱动螺丝吸附头23及其上吸附的螺丝向上运动,完成螺丝的吸附取料。其中,螺丝每次吸附拾取的位置固定,已提前将螺丝供料器24的螺丝出料口调整对准,锁付模组在直线精密位移滑台a12驱动下每次移动至同一位置进行吸附取料即可,无需视觉定位反馈。螺丝吸附取料完成后,锁付模组在直线精密位移滑台a12驱动下运动至CMOS电路板1锁付工作位置,在工业相机b13的辅助下,由直线精密位移滑台a12和直线精密位移滑台d41组合形成二维平面运动,调整锁付模组中螺丝吸附头23与星敏感器支架3上装配孔位之间的相对位置,对准后,由滑台气缸17驱动螺丝吸附头23及其上吸附的螺丝向下运动,再由锁付气缸18的顶杆推动电动螺丝刀支架22及其上安装的电动螺丝刀21在直线导轨20的导向下向下运动,将螺丝顶出螺丝吸附头23,将CMOS电路板1和调整垫片2锁紧在星敏感器支架3上,再依次完成剩下两个螺丝的拾取锁付,完成CMOS电路板1锁付,最后设备各模块复位,由操作人员取下锁紧后的CMOS电路板1、调整垫片2和星敏感器支架3装配体,完成装配;Step 6: If the accuracy requirements are met, perform CMOS circuit board 1 locking: After the parallelism of the target surface of CMOS circuit board 1 and the reference plane of star sensor bracket 3 is qualified, perform CMOS circuit board 1 locking. The tooling locking module moves to the locking position of CMOS circuit board 1 under the drive of the linear precision displacement slide d41, and the locking module moves to the adsorption and retrieving position on the screw feeder 24 under the drive of the linear precision displacement slide a12 , the screw adsorption head 23 in the lock payment module is driven by the slide cylinder 17 to move downward, and the screw is adsorbed and picked up. Movement to complete the adsorption and retrieving of the screw. Among them, the position of the screw is fixed for each adsorption and pickup, and the screw outlet of the screw feeder 24 has been adjusted and aligned in advance, and the locking module is driven by the linear precision displacement slide a12 to move to the same position each time for adsorption and pickup. materials without visual positioning feedback. After the screw is absorbed and picked up, the locking module moves to the CMOS circuit board 1 locking position driven by the linear precision displacement slide a12. With the assistance of the industrial camera b13, the linear precision displacement slide a12 and the linear precision displacement The slide table d41 is combined to form a two-dimensional plane movement, adjust the relative position between the screw suction head 23 in the locking module and the assembly hole on the star sensor bracket 3, after alignment, the slide table cylinder 17 drives the screw suction head 23 And the screw adsorbed on it moves downward, and then the push rod of the locking cylinder 18 pushes the electric screwdriver bracket 22 and the electric screwdriver 21 installed on it to move downward under the guidance of the linear guide rail 20, and the screw is pushed out of the screw adsorption head 23. Lock the CMOS circuit board 1 and the adjusting spacer 2 on the star sensor bracket 3, and then complete the picking and locking of the remaining two screws in sequence, complete the locking and payment of the CMOS circuit board 1, and finally reset each module of the device, by The operator removes the locked CMOS circuit board 1, adjusting gasket 2 and star sensor bracket 3 assembly to complete the assembly;
若不满足精度要求,调整垫片2研磨加工完成后,重复零件上料、调整垫片2装配、CMOS电路板1装配、CMOS电路板1和调整垫片2压紧、CMOS电路板1靶面和星敏感器支架3基准面平行度检测过程,检测后若仍不满足精度要求,计算调整量,下料重新研磨加工,直至检测结果为满足安装倾斜范围要求,进行CMOS电路板1锁付,完成整个装调流程。至此为锁附工序。If the accuracy requirements are not met, after the grinding of the adjustment gasket 2 is completed, repeat the parts loading, the assembly of the adjustment gasket 2, the assembly of the CMOS circuit board 1, the compression of the CMOS circuit board 1 and the adjustment gasket 2, and the target surface of the CMOS circuit board 1. Hexing sensor bracket 3 reference plane parallelism detection process, if the accuracy requirements are still not met after the detection, the adjustment amount is calculated, the material is cut and re-grinded, and the CMOS circuit board 1 is locked until the detection result meets the installation tilt range requirements. Complete the entire assembly process. So far it is the locking process.
本发明具有以下有益效果:The present invention has the following beneficial effects:
a.除开始装配前需人工上料,装调过程可有程序实现自动化控制,提高装配效率并避免人工装配产生的误差;a. In addition to manual loading before assembly, the assembly and adjustment process can be automatically controlled by a program to improve assembly efficiency and avoid errors caused by manual assembly;
b.装调过程可视,且靶面调整及孔位对准可由视觉技术反馈,精密位移滑台配合精密转台动作实现自动调整及对准功能;b. The installation and adjustment process is visible, and the target surface adjustment and hole position alignment can be fed back by visual technology, and the precision displacement slide table cooperates with the precision turntable to realize automatic adjustment and alignment functions;
c.既可一次性完成整个装调流程,也可在等待研磨加工时进行批量测量,具有双重作用。c. It can not only complete the whole assembly process at one time, but also perform batch measurement while waiting for the grinding process, which has dual functions.
附图说明Description of drawings
图1(a)和图1(b)为星敏感器零件的分解和整体示意图;Figure 1(a) and Figure 1(b) are the decomposition and overall schematic diagram of the star sensor parts;
图2为装调设备正面总体示意图;Figure 2 is an overall schematic diagram of the front of the installation and adjustment equipment;
图3为装调设备背面总体示意图;Figure 3 is an overall schematic diagram of the back of the assembly and adjustment equipment;
图4为测量模块示意图;Fig. 4 is a schematic diagram of the measurement module;
图5为工装锁紧模块示意图;Figure 5 is a schematic diagram of the tooling locking module;
图6为装调模块示意图。Figure 6 is a schematic diagram of the assembly and adjustment module.
图中:1CMOS电路板;2调整垫片;3星敏感器支架;4光学平台;5三轴精密位移滑台;6测头支座a;7组合激光位移测头;8测头支座b;9测量组件支架;10工业相机a;11型材支架;12直线精密位移滑台a;13工业相机b;14装调组件支架;15直线精密位移滑台b;16滑台支架;17滑台气缸;18锁付气缸;19锁付组件底座;20直线导轨;21电动螺丝刀;22电动螺丝刀支架;23螺丝吸附头;24螺丝供料器;25螺丝供料器底座;26精密转台a;27圆柱式力传感器;28零件吸附头;29料盘;30压块;31直线精密位移滑台c;32供料组件底座;33带座轴承;34转轴支座;35转轴;36导杆气缸;37夹具组件底座;38转角气缸;39反光镜;40V型块;41直线精密位移滑台d;42精密转台b;43工装锁紧组件支架。In the figure: 1CMOS circuit board; 2Adjusting gasket; 3Star sensor bracket; 4Optical platform; ;9 measurement component bracket; 10 industrial camera a; 11 profile bracket; 12 linear precision displacement slide a; 13 industrial camera b; Cylinder; 18 lock cylinder; 19 lock component base; 20 linear guide rail; 21 electric screwdriver; 22 electric screwdriver bracket; 23 screw suction head; 24 screw feeder; 25 screw feeder base; 26 precision turntable a; 27 Cylindrical force sensor; 28 parts adsorption head; 29 material tray; 30 press block; 31 linear precision displacement slide table c; 32 feeding component base; 33 bearing with seat; 34 rotating shaft support; 35 rotating shaft; 37 fixture assembly base; 38 corner cylinder; 39 mirror; 40V block; 41 linear precision displacement slide table d; 42 precision turntable b;
具体实施方式Detailed ways
下面结合附图和具体实施例对本发明进行详细说明。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
星敏感器零件的结构如图1(a)和图1(b)所示,本发明方法所采用的装调设备具体如图2、图3、图4、图5和图6所示。The structure of the star sensor parts is shown in Figure 1(a) and Figure 1(b), and the assembly and adjustment equipment used in the method of the present invention is specifically shown in Figure 2, Figure 3, Figure 4, Figure 5 and Figure 6.
装配前,先将零件星敏感器支架3通过V型块40和导杆气缸36装卡在工装锁紧模块上;料盘29水平安装在直线精密位移滑台c31上,将CMOS电路板1和调整垫片2放置在料盘29上,并具有一定的预限位,完成待装配零件的上料。Before assembly, the part star sensor bracket 3 is mounted and clamped on the tooling locking module through the V-shaped block 40 and the guide rod cylinder 36; the material tray 29 is horizontally installed on the linear precision displacement slide table c31, and the CMOS circuit board 1 and The adjusting gasket 2 is placed on the material tray 29 with a certain pre-limit position to complete the loading of the parts to be assembled.
待装配零件的位置姿态通过工业相机b13所获取,以实现直线精密位移滑台a12带动零件吸附头28精准运动至取料位置,直线精密位移滑台a12与零件吸附头28在工业相机b13的反馈下分两次完成对三个调整垫片2和CMOS电路板1的自动精确吸附取料(CMOS电路板1需放置在调整垫片2上方,先一次性拾取三个调整垫片2)。零件拾取完成后,在装配调整垫片2时,直线精密位移滑台a12、c31和精密转台a26在工业相机b13的反馈下调整零件的位置姿态,以保证三个调整垫片2精准地放入星敏感器支架3预设的孔位中;在装配CMOS电路板1时,由工业相机a10经由45°的反光镜39自下而上地观测星敏感器支架3底部基准面边线和CMOS电路板1中的靶面边线,再由精密转台a26旋转调整靶面姿态,以达到靶面中像素点矩形的x、y轴相对于基准面边线的安装倾斜范围要求,同时还要保证CMOS电路板1上的安装孔位对准,避免影响后续锁附过程,待调整完成后,进行装配。The position and posture of the parts to be assembled are acquired by the industrial camera b13, so as to realize the linear precision displacement slide table a12 to drive the part adsorption head 28 to move accurately to the pick-up position, and the feedback of the linear precision displacement slide table a12 and the part adsorption head 28 on the industrial camera b13 The automatic and accurate adsorption and retrieving of the three adjusting pads 2 and the CMOS circuit board 1 is completed twice in two steps (the CMOS circuit board 1 needs to be placed above the adjusting pad 2, and the three adjusting pads 2 are first picked up at one time). After the parts are picked up, when the adjustment shims 2 are assembled, the linear precision displacement slides a12, c31 and the precision turntable a26 adjust the position and posture of the parts under the feedback of the industrial camera b13, so as to ensure that the three adjustment shims 2 are placed accurately In the preset hole position of the star sensor bracket 3; when assembling the CMOS circuit board 1, the industrial camera a10 observes the edge of the bottom reference plane of the star sensor bracket 3 and the CMOS circuit board from bottom to top through the 45° mirror 39 The edge of the target surface in 1 is rotated by the precision turntable a26 to adjust the attitude of the target surface, so as to meet the installation tilt range requirements of the x and y axes of the pixel point rectangle in the target surface relative to the edge of the reference surface, and at the same time ensure that the CMOS circuit board 1 Align the installation holes on the upper part to avoid affecting the subsequent locking process. After the adjustment is completed, assemble it.
调整垫片2和CMOS电路板1装配完成后,不可直接进行螺丝锁附,需检测CMOS电路板1靶面和星敏感器支架3基准面的平行度是否满足精度要求,故采用转角气缸38作用在压块30上的方式保持装配体当前的状态,并通过精密转台b42配合组合激光位移测头7完成对基准面与靶面的测量。具体过程如下:直线精密位移滑台a12带动零件吸附头28运动至取料位置,吸取压块30并叠装在CMOS电路板1之上,其中压块30上与螺孔相对应的位置开槽口,便于螺丝锁付,叠装时的压力由圆柱式力传感器27测量,力信号通过控制回路传至工控机,实现闭环控制;转角气缸38作用在压块30上,将CMOS电路板1压紧,保证后续动作不影响装配精度且减少零件损伤。精密转台b42驱动V型块40上的星敏感器装配体旋转90°,将基准面与靶面朝向测量模块,组合激光位移测头7在三轴精密位移滑台5运动下完成对基准面与靶面的测量,由算法计算靶面与基准面之间的平行度。After the assembly of the adjusting gasket 2 and the CMOS circuit board 1 is completed, screw locking cannot be performed directly. It is necessary to check whether the parallelism between the target surface of the CMOS circuit board 1 and the reference plane of the star sensor bracket 3 meets the accuracy requirements, so the corner cylinder 38 is used The way on the pressure block 30 maintains the current state of the assembly, and the measurement of the reference plane and the target plane is completed through the combination of the precision turntable b42 and the combined laser displacement measuring head 7 . The specific process is as follows: the linear precision displacement slide table a12 drives the part adsorption head 28 to move to the pick-up position, absorbs the pressing block 30 and stacks it on the CMOS circuit board 1, wherein the position corresponding to the screw hole on the pressing block 30 is slotted The pressure is measured by the cylindrical force sensor 27 during stacking, and the force signal is transmitted to the industrial computer through the control circuit to realize closed-loop control; the corner cylinder 38 acts on the pressing block 30 to press the CMOS circuit board 1 Tight, to ensure that subsequent actions do not affect assembly accuracy and reduce damage to parts. The precision turntable b42 drives the star sensor assembly on the V-shaped block 40 to rotate 90°, and the reference plane and the target surface face the measurement module, and the combined laser displacement measuring head 7 completes the alignment between the reference plane and the target surface under the movement of the three-axis precision displacement slide table 5. For the measurement of the target surface, the algorithm calculates the parallelism between the target surface and the reference plane.
平行度检测完成后,若满足精度要求则进行螺丝锁付流程;若不满足精度要求则计算三个调整垫片2的调整量并记录反馈给操作人员,再由装调模块先后将压块30、CMOS电路板1和调整垫片2进行下料,由操作人员取走调整垫片2研磨加工,加工后再重新装配调整测量。装配过程停止的该阶段,设备可继续对另一组新的零件进行平行度测量,避免耗时无效等待,同时可达到批量测量的效果。After the parallelism detection is completed, if the accuracy requirements are met, the screw locking process will be carried out; if the accuracy requirements are not met, the adjustments of the three adjusting shims 2 will be calculated and recorded and fed back to the operator, and then the assembly and adjustment module will successively place the pressing blocks 30 , The CMOS circuit board 1 and the adjusting gasket 2 are unloaded, and the adjusting gasket 2 is taken away by the operator for grinding and processing, and then reassembled for adjustment and measurement after processing. At this stage when the assembly process is stopped, the equipment can continue to measure the parallelism of another set of new parts, avoiding time-consuming and invalid waiting, and at the same time achieving the effect of batch measurement.
满足精度要求,直接继续进行CMOS电路板1锁付,精密转台b42将星敏感器装配体旋转90°使得CMOS电路板1靶面和星敏感器支架3标准面恢复竖直向下的状态,直线精密位移滑台d41带动星敏感器装配体运动到锁付位置;由直线精密位移滑台a12驱动锁付模组运动到吸附取料位置,滑台气缸17驱动锁付模组中的螺丝吸附头23向下运动,真空吸附取料,其中,由螺丝供料器24实现螺丝自动供料;再由直线精密位移滑台a12和滑台气缸17驱动锁付模组运动至锁付工作位置,电动螺丝刀21在锁付气缸18驱动下,将螺丝锁付在星敏感器装配体上,重复三次将CMOS电路板1锁紧;由直线精密位移滑台d41驱动装配体退出到下料位置,转角气缸38和导杆气缸36松预紧,操作人员取料,完成装配。Satisfy the precision requirement, continue to lock the CMOS circuit board 1 directly, the precision turntable b42 rotates the star sensor assembly 90° so that the target surface of the CMOS circuit board 1 and the standard surface of the star sensor bracket 3 return to the vertical downward state, straight line The precision displacement slide d41 drives the star sensor assembly to move to the locking position; the linear precision displacement slide a12 drives the lock module to move to the adsorption and retrieving position, and the slide cylinder 17 drives the screw adsorption head in the lock module 23 moves downwards, and vacuum absorbs and picks up materials. Among them, the screw feeder 24 realizes automatic screw feeding; then the linear precision displacement slide a12 and the slide cylinder 17 drive the locking module to move to the locking working position. Driven by the locking cylinder 18, the screwdriver 21 locks the screw on the star sensor assembly, repeats three times to lock the CMOS circuit board 1; the linear precision displacement slide table d41 drives the assembly back to the blanking position, and the corner cylinder 38 and guide rod cylinder 36 are loose and pre-tightened, and the operator takes the material and completes the assembly.
不满足精度要求,需等待调整垫片2研磨加工完成后,重复零件上料、调整垫片2装配、CMOS电路板1装配、CMOS电路板1和调整垫片2压紧、CMOS电路板1靶面和星敏感器支架3基准面平行度检测过程,检测后若仍不满足精度要求,计算调整量,下料重新研磨加工,直至检测结果为满足安装倾斜范围要求,进行CMOS电路板1锁付,完成整个装调流程。If the accuracy requirements are not met, it is necessary to wait for the grinding of the adjusting gasket 2 to be completed, then repeat the parts loading, the assembly of the adjusting gasket 2, the assembly of the CMOS circuit board 1, the pressing of the CMOS circuit board 1 and the adjusting gasket 2, and the target of the CMOS circuit board 1 The parallelism detection process of the surface and the star sensor bracket 3 reference plane, if the accuracy requirements are still not met after the detection, the adjustment amount is calculated, the material is cut and re-grinded, and the CMOS circuit board 1 is locked until the detection result meets the installation tilt range requirements. , to complete the entire assembly process.
本发明是一种用于航天器件星敏感器CMOS电路板靶面自动装调方法。本发明不仅仅局限于对星敏感器零件的自动装配,通过对部分装调流程的修改即可增强该方法的适应性,其它规格零件的装配调整仍可以使用此装调方法。The invention relates to an automatic assembly and adjustment method for a target surface of a CMOS circuit board of a star sensor of an aerospace device. The present invention is not limited to the automatic assembly of star sensor parts, the adaptability of the method can be enhanced by modifying part of the assembly and adjustment process, and the assembly and adjustment of parts of other specifications can still use this assembly and adjustment method.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202310595871.1A CN116654289A (en) | 2023-05-25 | 2023-05-25 | Automatic assembling and adjusting method for star sensor CMOS circuit board target surface |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202310595871.1A CN116654289A (en) | 2023-05-25 | 2023-05-25 | Automatic assembling and adjusting method for star sensor CMOS circuit board target surface |
Publications (1)
Publication Number | Publication Date |
---|---|
CN116654289A true CN116654289A (en) | 2023-08-29 |
Family
ID=87714636
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202310595871.1A Pending CN116654289A (en) | 2023-05-25 | 2023-05-25 | Automatic assembling and adjusting method for star sensor CMOS circuit board target surface |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN116654289A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN119526010A (en) * | 2025-01-21 | 2025-02-28 | 常州市泽涛机械制造有限公司 | An assembly device for producing universal couplings |
-
2023
- 2023-05-25 CN CN202310595871.1A patent/CN116654289A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN119526010A (en) * | 2025-01-21 | 2025-02-28 | 常州市泽涛机械制造有限公司 | An assembly device for producing universal couplings |
CN119526010B (en) * | 2025-01-21 | 2025-04-11 | 常州市泽涛机械制造有限公司 | Assembly quality is used in universal joint production |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP7688713B2 (en) | Dispensing mounting device for workpieces | |
CN106002285B (en) | A kind of automatic assembly line of saucepan | |
CN108594494A (en) | One kind detecting assembly line automatically without FPC liquid crystal displays | |
CN110582171B (en) | Automatic chip mounting device and automatic chip mounting method | |
CN102706889B (en) | Visual detection equipment with convenient loading and unloading of material tray | |
CN108663836B (en) | Liquid crystal display panel detection and positioning device | |
CN206302516U (en) | Dual camera calibration equipment | |
CN105137131A (en) | Automatic fine tuning positioning FPC board detection device | |
CN215704235U (en) | Feeding mechanism and cutting detection equipment | |
CN109896283A (en) | A kind of glass bracket installation detecting device | |
CN116654289A (en) | Automatic assembling and adjusting method for star sensor CMOS circuit board target surface | |
CN107378438A (en) | Camera lens mold train assembling machine | |
CN115452058A (en) | Automatic detection mechanism for micro components | |
CN112289242A (en) | Display panel detection device | |
CN115625506A (en) | An assembly device and method for tiny parts integrating glue dispensing and locking | |
CN112595498B (en) | Optical property detection system for light emission of laser bars and single tubes of laser bars | |
CN213580726U (en) | Automatic optical inspection blanking machine of AOI | |
CN212432070U (en) | Flatness detector | |
CN211401101U (en) | High-precision 3D contour modeling equipment | |
CN116690177A (en) | Automatic assembling and adjusting equipment for star sensor CMOS circuit board target surface | |
CN216781213U (en) | Full-automatic numerical control machine tool | |
CN214538037U (en) | Detection device | |
CN114082679B (en) | Full-automatic resistance tester | |
CN114273161A (en) | Sensor dispensing and assembling integrated machine | |
CN114265167A (en) | Surface mounting machine with accurate surface mounting |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |