CN103969845A - Multi-foot heavy-load air-floating supporting device for optical installation and calibration - Google Patents

Multi-foot heavy-load air-floating supporting device for optical installation and calibration Download PDF

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CN103969845A
CN103969845A CN201410187153.1A CN201410187153A CN103969845A CN 103969845 A CN103969845 A CN 103969845A CN 201410187153 A CN201410187153 A CN 201410187153A CN 103969845 A CN103969845 A CN 103969845A
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杨会生
关英俊
姜肖楠
鲍赫
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Changchun Institute of Optics Fine Mechanics and Physics of CAS
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Abstract

一种多足式光学装校用重载气浮支撑装置属于大型精密光学设备的地面装校用微距位移装置领域,该装置包括承载臂、承载臂球头螺柱、球窝轴组件、主承力板和三个气浮支撑组件。该装置通过三个底面共面的小型气浮块均匀地分担了由承载臂球头螺柱传递下来的承重压力,使得主承力板承受的应力得以均匀地分散化,因此充分发挥了小型气浮块加工周期短、易生产、成本低的优势,并克服了单个小型气浮块承载能力有限的缺点。三个小型气浮块的分布充分利用了三点定面的稳定性作用,同时,多个球窝结构的使用也利用了球面定心原理,使得整个重载气浮支撑装置的力学传递路径精确、稳定,完全可以满足空间光学遥感器的地面装调校准需求。

A multi-legged heavy-duty air-floating support device for optical installation and calibration belongs to the field of macro-distance displacement devices for ground installation and calibration of large-scale precision optical equipment. Bearing plate and three air bearing assemblies. The device evenly shares the load-bearing pressure transmitted by the ball stud of the bearing arm through three small air bearing blocks with the same bottom surface, so that the stress on the main load-bearing plate can be evenly dispersed, so the small air bearing is fully utilized. The floating block has the advantages of short processing cycle, easy production and low cost, and overcomes the shortcoming of a single small air floating block with limited carrying capacity. The distribution of the three small air bearing blocks makes full use of the stability of the three-point fixed surface. At the same time, the use of multiple ball-and-socket structures also utilizes the principle of spherical centering, making the mechanical transmission path of the entire heavy-duty air bearing support device accurate. , stable, and can fully meet the ground installation and calibration requirements of space optical remote sensors.

Description

多足式光学装校用重载气浮支撑装置Heavy-duty air-floating support device for multi-legged optical assembly

技术领域technical field

本发明属于大型精密光学设备的地面装校用微距位移装置领域,具体涉及一种多足式光学装校用重载气浮支撑装置。The invention belongs to the field of macro-distance displacement devices for ground installation and calibration of large-scale precision optical equipment, and specifically relates to a multi-legged heavy-duty air-floating support device for optical installation and calibration.

背景技术Background technique

空间光学遥感器属于大型精密光学设备,其在被送入太空之前,需要事先在地面上完成装调和检测校准。现有方法通常采用以直线或圆弧导轨为主体导向机构的大型精密二维转台来固定空间光学遥感器,以便通过大型精密二维转台来实现空间光学遥感器在固定基准面上的微距位移操作。Space optical remote sensors are large-scale precision optical devices, which need to be installed, adjusted, tested and calibrated on the ground before being sent into space. The existing methods usually use a large-scale precision two-dimensional turntable with a linear or arc guide rail as the main guiding mechanism to fix the space optical remote sensor, so that the macro-displacement of the space optical remote sensor on the fixed reference plane can be realized through the large-scale precision two-dimensional turntable operate.

然而,随着地面侦查测绘需求的日益提高,空间光学遥感器的体积和重量都越来越大,采用传统的大型精密二维转台实现空间光学遥感器地面装校的方法表现出一些缺点,比如,大型精密二维转台在空间光学遥感器的重压之下进行微距水平运动调整时,会出现爬行现象,导致微距位移定位不精确,分辨率低。同时,为了承载空间光学遥感器的重量,大型精密二维转台需要结构强度更高、体积更大的连续精密导轨,这不但大幅增加了导轨的生产成本和生产周期,也增大了装调难度和可维护性,因此,传统的大型精密二维转台已逐渐无法满足空间光学遥感器的地面装调校准需求。However, with the increasing demand for ground reconnaissance and mapping, the volume and weight of space optical remote sensors are getting larger and larger. The method of using the traditional large-scale precision two-dimensional turntable to realize the ground calibration of space optical remote sensors has some shortcomings, such as , when the large-scale precision two-dimensional turntable is adjusted for macro-distance horizontal movement under the weight of the space optical remote sensor, it will crawl, resulting in inaccurate macro-displacement positioning and low resolution. At the same time, in order to bear the weight of the space optical remote sensor, the large-scale precision two-dimensional turntable needs a continuous precision guide rail with higher structural strength and larger volume, which not only greatly increases the production cost and production cycle of the guide rail, but also increases the difficulty of assembly and adjustment. and maintainability, therefore, the traditional large-scale precision two-dimensional turntable has gradually been unable to meet the ground adjustment and calibration requirements of space optical remote sensors.

另一方面,模块化气浮支撑装置可以实现较高承重载荷下的气浮支撑,辅以微调机构可以实现高精度微距位移调整,但现有的小型气浮块的承载能力有限,而现有的大型气浮块虽然承载能力大,但加工困难,生产周期长,成本高。On the other hand, the modular air-floating support device can realize air-floating support under high load-bearing loads, and the fine-tuning mechanism can realize high-precision micro-distance displacement adjustment, but the carrying capacity of the existing small air-floating blocks is limited, and the current Although some large-scale air-floating blocks have a large carrying capacity, they are difficult to process, have a long production cycle and high cost.

发明内容Contents of the invention

为了解决现有大型精密二维转台已逐渐无法满足空间光学遥感器的地面装调校准需求,同时,现有的小型气浮块的承载能力有限,而现有的大型气浮块虽然承载能力大,但加工困难,生产周期长,成本高的技术问题,本发明提供一种多足式光学装校用重载气浮支撑装置。In order to solve the problem that the existing large-scale precision two-dimensional turntable has gradually been unable to meet the ground adjustment and calibration requirements of space optical remote sensors, and at the same time, the carrying capacity of the existing small Large, but difficult to process, long production cycle, high cost technical problems, the present invention provides a multi-legged optical assembly with a heavy-duty air-floating support device.

本发明解决技术问题所采取的技术方案如下:The technical solution adopted by the present invention to solve the technical problems is as follows:

多足式光学装调用重载气浮支撑装置,其特征在于,该装置包括承载臂、承载臂球头螺柱、球窝轴组件、主承力板和三个气浮支撑组件,球窝轴组件包括承载臂球窝轴、第一防脱盖和连接轴承,气浮支撑组件包括紧固垫、球头小轴、第二防脱盖和气浮块;所述承载臂球头螺柱的上端是螺杆,下端设有球头,承载臂球头螺柱的上端螺杆与承载臂上的螺孔螺纹连接,承载臂球头螺柱的球头与承载臂球窝轴形成第一球面副;The heavy-duty air bearing support device for multi-legged optical installation is characterized in that the device includes a bearing arm, a bearing arm ball stud, a ball and socket shaft assembly, a main bearing plate and three air bearing support assemblies, the ball and socket shaft The assembly includes the bearing arm ball shaft, the first anti-off cover and the connecting bearing, and the air bearing assembly includes the fastening pad, the small shaft of the ball joint, the second anti-off cover and the air bearing block; the upper end of the bearing arm ball stud It is a screw with a ball head at the lower end, and the upper end screw of the ball stud of the load arm is threadedly connected with the screw hole on the load arm, and the ball head of the ball stud of the load arm and the ball socket shaft of the load arm form a first spherical pair;

所述主承力板是正三棱柱结构,其上端面的旋转中心设有中心凹槽,其三棱柱上端面正三角形的每个顶角分别设有一个顶角通孔,所述承载臂球窝轴通过连接轴承与主承力板的中心凹槽连接;所述第一防脱盖设有带内螺纹的中心孔,该中心孔的直径小于承载臂球头螺柱的球头直径,第一防脱盖与主承力板的上端面固连;The main load-bearing plate is a regular triangular prism structure, the center of rotation of its upper end surface is provided with a central groove, and each vertex of an equilateral triangle on the upper end surface of the triangular prism is respectively provided with a vertex through hole, and the bearing arm ball socket The shaft is connected to the central groove of the main bearing plate through the connecting bearing; the first anti-off cover is provided with a central hole with an internal thread, and the diameter of the central hole is smaller than the ball head diameter of the bearing arm ball stud, the first The anti-off cover is fixedly connected with the upper end surface of the main bearing plate;

所述三个气浮支撑组件的球头小轴分别穿过主承力板的一个顶角通孔,球头小轴的上端通过紧固垫与主承力板固连,紧固垫通过螺栓与主承力板的上端面固连;气浮块的上端面设有球窝,第二防脱盖的中心孔直径小于球头小轴的球头直径,第二防脱盖通过螺栓与气浮块的上端面固连,球头小轴的下端球头与气浮块的球窝形成第二球面副。The small shafts of the ball joints of the three air bearing components pass through a corner through hole of the main bearing plate respectively, the upper ends of the small shafts of the ball joints are fixedly connected with the main bearing plate through fastening pads, and the fastening pads pass through bolts It is fixedly connected with the upper end surface of the main bearing plate; the upper end surface of the air floating block is provided with a ball socket, the diameter of the center hole of the second anti-off cover is smaller than the diameter of the ball head of the small shaft of the ball head, and the second anti-off cover is connected with the air through bolts. The upper end surface of the floating block is fixedly connected, and the ball head at the lower end of the small shaft of the ball head and the ball socket of the air floating block form a second spherical pair.

本发明的有益效果是:该多足式光学装校用重载气浮支撑装置通过三个底面共面的小型气浮块均匀地分担了由承载臂球头螺柱传递下来的承重压力,使得主承力板承受的应力得以均匀地分散化,因此充分发挥了小型气浮块加工周期短、易生产、成本低的优势,并克服了单个小型气浮块承载能力有限的缺点。三个小型气浮块的分布充分利用了三点定面的稳定性作用,同时,多个球窝结构的使用也利用了球面定心原理,使得整个重载气浮支撑装置的力学传递路径精确、稳定,完全可以满足空间光学遥感器的地面装调校准需求。The beneficial effect of the present invention is that: the multi-legged heavy-duty air-floating support device for optical installation and correction evenly shares the load-bearing pressure transmitted by the ball stud of the load-bearing arm through three small air-floating blocks whose bottom surfaces are coplanar, so that The stress borne by the main load-bearing plate can be evenly dispersed, so the advantages of short processing period, easy production and low cost of the small air-floating block are fully utilized, and the shortcoming of the limited carrying capacity of a single small air-floating block is overcome. The distribution of the three small air bearing blocks makes full use of the stability of the three-point fixed surface. At the same time, the use of multiple ball-and-socket structures also utilizes the principle of spherical centering, making the mechanical transmission path of the entire heavy-duty air bearing support device accurate. , stable, and can fully meet the ground adjustment and calibration requirements of space optical remote sensors.

附图说明Description of drawings

图1是本发明多足式光学装校用重载气浮支撑装置的立体图;Fig. 1 is the perspective view of the heavy-duty air-floating support device for multi-legged optical installation and calibration of the present invention;

图2是图1侧视轴向局部剖视图。Fig. 2 is a side axial partial sectional view of Fig. 1 .

具体实施方式Detailed ways

下面结合附图对本发明做进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings.

如图1至图2所示,多足式光学装校用重载气浮支撑装置包括承载臂1、承载臂球头螺柱2、球窝轴组件3、主承力板4和三个气浮支撑组件5,球窝轴组件3包括承载臂球窝轴3-1、第一防脱盖3-2和连接轴承3-3,气浮支撑组件5包括紧固垫5-1、球头小轴5-2、第二防脱盖5-3和气浮块5-4。As shown in Figures 1 to 2, the heavy-duty air bearing support device for multi-legged optical assembly includes a bearing arm 1, a bearing arm ball stud 2, a ball-and-socket shaft assembly 3, a main bearing plate 4 and three air bearings. The floating support assembly 5, the ball shaft assembly 3 includes the bearing arm ball shaft 3-1, the first anti-off cover 3-2 and the connecting bearing 3-3, the air bearing assembly 5 includes the fastening pad 5-1, the ball head Small shaft 5-2, the second anti-off cover 5-3 and air floating block 5-4.

所述承载臂球头螺柱2的上端是螺杆,下端设有球头;承载臂球头螺柱2的上端螺杆与承载臂1上的螺孔螺纹连接,承载臂球头螺柱2的球头与承载臂球窝轴3-1形成第一球面副。The upper end of the bearing arm ball stud 2 is a screw, and the lower end is provided with a ball head; the upper end screw of the bearing arm ball stud 2 is threadedly connected with the screw hole on the bearing arm 1, and the ball of the bearing arm ball stud 2 The head and the bearing arm ball and socket shaft 3-1 form a first spherical pair.

所述主承力板4是正三棱柱结构,其上端面的旋转中心设有中心凹槽,其三棱柱上端面正三角形的每个顶角分别设有一个顶角通孔,所述承载臂球窝轴3-1通过连接轴承3-3与主承力板4的中心凹槽连接;所述第一防脱盖3-2设有带内螺纹的中心孔,该中心孔的直径小于承载臂球头螺柱2的球头直径,第一防脱盖3-2与主承力板4的上端面固连。The main bearing plate 4 is a regular triangular prism structure, the center of rotation of its upper end surface is provided with a central groove, and each vertex of an equilateral triangle on the upper end surface of the triangular prism is respectively provided with a vertex through hole, and the bearing arm ball The socket shaft 3-1 is connected to the central groove of the main bearing plate 4 through the connecting bearing 3-3; the first anti-off cover 3-2 is provided with a central hole with an internal thread, and the diameter of the central hole is smaller than that of the bearing arm The ball head diameter of the ball stud 2, the first anti-off cover 3-2 is fixedly connected with the upper end surface of the main bearing plate 4.

组装时,先将承载臂球头螺柱2的球头放入承载臂球窝轴3-1,以形成第一球面副,再通过带内螺纹的中心孔将第一防脱盖3-2沿承载臂球头螺柱2螺杆的顶端旋至空刀槽的位置,然后再承载臂球头螺柱2的上端螺杆与承载臂1上的螺孔螺纹连接,最后,用螺栓将第一防脱盖3-2的外沿与承力板4的上端面固连。这样,在整个设备起吊和转运的过程中,由于空刀槽对第一防脱盖3-2的限位作用,使得第一防脱盖3-2无法轴向运动,在第一防脱盖3-2的阻挡下,承载臂球头螺柱2的球头也就不会从承载臂球窝轴3-1中滑脱。When assembling, put the ball head of the bearing arm ball stud 2 into the bearing arm ball socket shaft 3-1 to form the first spherical pair, and then put the first anti-off cover 3-2 through the center hole with internal thread Screw along the top of the ball stud 2 of the load arm to the position of the empty knife groove, and then screw the upper end of the ball stud 2 of the load arm to the screw hole on the load arm 1, and finally, use bolts to screw the first anti The outer edge of the cover 3-2 is fixedly connected with the upper end surface of the bearing plate 4. Like this, in the process of whole equipment hoisting and transshipment, due to the position-limiting effect of the empty sipes to the first anti-off cover 3-2, the first anti-off cover 3-2 cannot move axially. Under the blocking of 3-2, the ball head of the bearing arm ball stud 2 will not slip off from the bearing arm ball socket shaft 3-1.

所述三个气浮支撑组件5均为小型气浮块,每一个气浮支撑组件5的球头小轴5-2分别穿过主承力板4的一个顶角通孔,球头小轴5-2的上端通过紧固垫5-1与主承力板4固连,紧固垫5-1通过螺栓与主承力板4的上端面固连;气浮块5-4的上端面设有球窝,第二防脱盖5-3的中心孔直径小于球头小轴5-2的球头直径,第二防脱盖5-3通过螺栓与气浮块5-4的上端面固连,球头小轴5-2的下端球头与气浮块5-4的球窝形成第二球面副。第二防脱盖5-3的功能与第一防脱盖3-2类似,其能够在整个设备起吊和转运的过程中防止球头小轴5-2从气浮块5-4上端面的球窝中滑脱。The three air bearing components 5 are all small air bearing blocks, and the small ball shaft 5-2 of each air bearing component 5 passes through a corner through hole of the main force plate 4 respectively, and the small shaft of the ball The upper end of 5-2 is fixedly connected with the main bearing plate 4 through the fastening pad 5-1, and the fastening pad 5-1 is fixedly connected with the upper end surface of the main bearing plate 4 through bolts; the upper end surface of the air floating block 5-4 A ball socket is provided, the diameter of the central hole of the second anti-off cover 5-3 is smaller than the diameter of the ball head of the small shaft 5-2 of the ball head, and the second anti-off cover 5-3 passes through the bolt and the upper end surface of the air floating block 5-4 Fixedly connected, the ball socket of the lower end ball head of the small shaft 5-2 of the ball head and the ball socket of the air floating block 5-4 forms the second spherical pair. The function of the second anti-off cover 5-3 is similar to that of the first anti-off cover 3-2, which can prevent the small shaft 5-2 of the ball joint from being lifted from the upper end surface of the air bearing block 5-4 during the lifting and transfer of the whole equipment. Slip in ball socket.

具体应用本发明的多足式光学装校用重载气浮支撑装置时,首先将所述装置放置在高精度平台6上,并用气源给每个气浮块5-4通气,在气压作用下,每个气浮块5-4与其自身下方的高精度平台6之间都会形成一层气膜,从而使气浮块5-4浮起,同时产生一个正比于气压的气浮力F,气浮力F集中作用在该球头小轴5-2与气浮块5-4的球窝所形成的第二球面副上。三个气浮支撑组件5呈120°均匀分布,由三点共面的原理可知,三个第二球面副唯一的确定主承力板4以及承载臂球窝轴3-1的位置,并将每一个气浮块5-4的气浮力F集中作用到承载臂球窝轴3-1上,合力为3F。When specifically applying the heavy-duty air-floating support device for multi-legged optical assembly and calibration of the present invention, first the device is placed on the high-precision platform 6, and each air-floating block 5-4 is ventilated with an air source. Next, a layer of air film will be formed between each air buoyancy block 5-4 and the high-precision platform 6 below itself, so that the air buoyancy block 5-4 is floated, and an air buoyancy force F proportional to the air pressure is generated at the same time. The buoyancy force F concentrates on the second spherical pair formed by the small shaft 5-2 of the ball head and the ball socket of the air floating block 5-4. The three air bearing support components 5 are evenly distributed at 120°. According to the principle of three-point coplanarity, the three second spherical pairs uniquely determine the positions of the main bearing plate 4 and the bearing arm ball shaft 3-1, and The air buoyancy force F of each air buoyancy block 5-4 concentrates on the bearing arm ball shaft 3-1, and the resultant force is 3F.

所述球头螺柱与球窝轴为球面副连接,所述球窝轴与主承力板为转动副连接,当气浮块5-4的气源关闭后,气浮块5-4与高精度平台6之间气膜消失,在重力作用下,三个气浮支撑组件5与高精度平台6贴合。在承载臂球头螺柱2与主承力板4呈任何角度时,承载臂1依然可以通过转动螺纹实现沿承载臂球头螺柱2的轴线上下运动或沿该轴线转动,由此可知多足式光学装调用重载气浮支撑装置可以实现承载臂多自由度运动。The ball stud and the ball shaft are connected by a spherical pair, and the ball shaft and the main bearing plate are connected by a rotating pair. When the air source of the air floating block 5-4 is closed, the air floating block 5-4 and the The air film between the high-precision platforms 6 disappears, and the three air-floating support components 5 are attached to the high-precision platforms 6 under the action of gravity. When the bearing arm ball stud 2 is at any angle with the main bearing plate 4, the bearing arm 1 can still move up and down along the axis of the bearing arm ball stud 2 or rotate along the axis by rotating the screw thread. The foot-type optical device uses a heavy-duty air-floating support device to realize the multi-degree-of-freedom movement of the carrying arm.

该多足式光学装校用重载气浮支撑装置通过三个底面共面的小型气浮块均匀地分担了由承载臂球头螺柱传递下来的承重压力,使得主承力板承受的应力得以均匀地分散化,因此充分发挥了小型气浮块加工周期短、易生产、成本低的优势,并克服了单个小型气浮块承载能力有限的缺点。三个小型气浮块的分布充分利用了三点定面的稳定性作用,同时,多个球窝结构的使用也利用了球面定心原理,使得整个重载气浮支撑装置的力学传递路径精确、稳定,完全可以满足空间光学遥感器的地面装调校准需求。The heavy-duty air bearing support device for multi-legged optical assembly evenly shares the load-bearing pressure transmitted by the ball stud of the bearing arm through three small air bearing blocks with the same bottom surface, so that the stress on the main load-bearing plate It can be dispersed evenly, so the advantages of short processing cycle, easy production and low cost of the small-sized air-floating block are fully utilized, and the shortcoming of the limited carrying capacity of a single small-sized air-floating block is overcome. The distribution of the three small air bearing blocks makes full use of the stability of the three-point fixed surface. At the same time, the use of multiple ball-and-socket structures also utilizes the principle of spherical centering, making the mechanical transmission path of the entire heavy-duty air bearing support device accurate. , stable, and can fully meet the ground adjustment and calibration requirements of space optical remote sensors.

Claims (1)

1.多足式光学装调用重载气浮支撑装置,其特征在于,该装置包括承载臂(1)、承载臂球头螺柱(2)、球窝轴组件(3)、主承力板(4)和三个气浮支撑组件(5),球窝轴组件(3)包括承载臂球窝轴(3-1)、第一防脱盖(3-2)和连接轴承(3-3),气浮支撑组件(5)包括紧固垫(5-1)、球头小轴(5-2)、第二防脱盖(5-3)和气浮块(5-4);所述承载臂球头螺柱(2)的上端是螺杆,下端设有球头,承载臂球头螺柱(2)的上端螺杆与承载臂(1)上的螺孔螺纹连接,承载臂球头螺柱(2)的球头与承载臂球窝轴(3-1)形成第一球面副;1. The heavy-duty air bearing support device for multi-legged optical installation, which is characterized in that the device includes a bearing arm (1), a bearing arm ball stud (2), a ball-and-socket shaft assembly (3), and a main bearing plate (4) and three air bearing assemblies (5), the ball shaft assembly (3) includes the bearing arm ball shaft (3-1), the first anti-off cover (3-2) and the connecting bearing (3-3 ), the air bearing assembly (5) includes a fastening pad (5-1), a small ball shaft (5-2), a second anti-off cover (5-3) and an air bearing block (5-4); the The upper end of the bearing arm ball stud (2) is a screw, and the lower end is provided with a ball head. The upper end screw of the bearing arm ball stud (2) is threadedly connected with the screw hole on the bearing arm (1), and the bearing arm ball screw The ball head of the column (2) and the bearing arm ball socket shaft (3-1) form a first spherical pair; 所述主承力板(4)是正三棱柱结构,其上端面的旋转中心设有中心凹槽,其三棱柱上端面正三角形的每个顶角分别设有一个顶角通孔,所述承载臂球窝轴(3-1)通过连接轴承(3-3)与主承力板(4)的中心凹槽连接;所述第一防脱盖(3-2)设有带内螺纹的中心孔,该中心孔的直径小于承载臂球头螺柱(2)的球头直径,第一防脱盖(3-2)与主承力板(4)的上端面固连;The main bearing plate (4) is a regular triangular prism structure, the center of rotation of its upper end surface is provided with a central groove, and each vertex of an equilateral triangle on the upper end surface of the triangular prism is provided with a vertex through hole respectively. The arm ball socket shaft (3-1) is connected with the central groove of the main bearing plate (4) through the connecting bearing (3-3); the first anti-off cover (3-2) is provided with a central Hole, the diameter of this central hole is less than the diameter of the ball head of the bearing arm ball stud (2), and the first anti-off cover (3-2) is fixedly connected with the upper end surface of the main bearing plate (4); 所述三个气浮支撑组件(5)的球头小轴(5-2)分别穿过主承力板(4)的一个顶角通孔,球头小轴(5-2)的上端通过紧固垫(5-1)与主承力板(4)固连,紧固垫(5-1)通过螺栓与主承力板(4)的上端面固连;气浮块(5-4)的上端面设有球窝,第二防脱盖(5-3)的中心孔直径小于球头小轴(5-2)的球头直径,第二防脱盖(5-3)通过螺栓与气浮块(5-4)的上端面固连,球头小轴(5-2)的下端球头与气浮块(5-4)的球窝形成第二球面副。The small ball shafts (5-2) of the three air bearing assemblies (5) respectively pass through a top angle through hole of the main bearing plate (4), and the upper ends of the small ball shafts (5-2) pass through The fastening pad (5-1) is fixedly connected with the main bearing plate (4), and the fastening pad (5-1) is fixedly connected with the upper end surface of the main bearing plate (4) by bolts; the air floating block (5-4 ) is provided with a ball socket, the diameter of the center hole of the second anti-off cover (5-3) is smaller than the diameter of the ball head of the small shaft of the ball head (5-2), and the second anti-off cover (5-3) passes through the bolt It is fixedly connected with the upper end surface of the air floating block (5-4), and the ball socket at the lower end of the small shaft of the ball head (5-2) and the ball socket of the air floating block (5-4) form the second spherical pair.
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CN106143955A (en) * 2016-07-11 2016-11-23 上海卫星装备研究所 A kind of heavy load high-precise synchronization support system for three-axis air-bearing table
CN113967924A (en) * 2021-10-28 2022-01-25 郑州轻工业大学 Test and analysis platform for self-adaptive compliance characteristics of thin-walled fragile parts manipulators

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CN106143955A (en) * 2016-07-11 2016-11-23 上海卫星装备研究所 A kind of heavy load high-precise synchronization support system for three-axis air-bearing table
CN113967924A (en) * 2021-10-28 2022-01-25 郑州轻工业大学 Test and analysis platform for self-adaptive compliance characteristics of thin-walled fragile parts manipulators
CN113967924B (en) * 2021-10-28 2024-02-09 郑州轻工业大学 Self-adaptive compliance characteristic test analysis platform for thin-wall fragile part operation manipulator

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