CN108535035A - A kind of zero-g hanging test device for cylinder unwrapping mechanism - Google Patents
A kind of zero-g hanging test device for cylinder unwrapping mechanism Download PDFInfo
- Publication number
- CN108535035A CN108535035A CN201810229128.3A CN201810229128A CN108535035A CN 108535035 A CN108535035 A CN 108535035A CN 201810229128 A CN201810229128 A CN 201810229128A CN 108535035 A CN108535035 A CN 108535035A
- Authority
- CN
- China
- Prior art keywords
- guide rail
- fixed
- unfolding
- suspension
- zero
- 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
- 230000007246 mechanism Effects 0.000 title claims abstract description 71
- 239000000725 suspension Substances 0.000 claims abstract description 51
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims 2
- 238000000034 method Methods 0.000 abstract description 12
- 230000008569 process Effects 0.000 abstract description 11
- 230000005484 gravity Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 9
- PCTMTFRHKVHKIS-BMFZQQSSSA-N (1s,3r,4e,6e,8e,10e,12e,14e,16e,18s,19r,20r,21s,25r,27r,30r,31r,33s,35r,37s,38r)-3-[(2r,3s,4s,5s,6r)-4-amino-3,5-dihydroxy-6-methyloxan-2-yl]oxy-19,25,27,30,31,33,35,37-octahydroxy-18,20,21-trimethyl-23-oxo-22,39-dioxabicyclo[33.3.1]nonatriaconta-4,6,8,10 Chemical compound C1C=C2C[C@@H](OS(O)(=O)=O)CC[C@]2(C)[C@@H]2[C@@H]1[C@@H]1CC[C@H]([C@H](C)CCCC(C)C)[C@@]1(C)CC2.O[C@H]1[C@@H](N)[C@H](O)[C@@H](C)O[C@H]1O[C@H]1/C=C/C=C/C=C/C=C/C=C/C=C/C=C/[C@H](C)[C@@H](O)[C@@H](C)[C@H](C)OC(=O)C[C@H](O)C[C@H](O)CC[C@@H](O)[C@H](O)C[C@H](O)C[C@](O)(C[C@H](O)[C@H]2C(O)=O)O[C@H]2C1 PCTMTFRHKVHKIS-BMFZQQSSSA-N 0.000 description 2
- 230000002776 aggregation Effects 0.000 description 1
- 238000004220 aggregation Methods 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M99/00—Subject matter not provided for in other groups of this subclass
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
本发明公开了一种用于柱面展开机构的零重力悬挂试验装置,包括支撑组件、悬挂导轨组件、导轨辅助移动组件。支撑组件用于固定支撑柱面展开机构;悬挂导轨组件包括固定不动的导轨以及可以平移的导轨,导轨上有可沿导轨移动的滑块;悬挂绳一端与展开机构相连,另一端穿过滑轮与配重相连,通过配重的作用消除展开机构自身重力对展开过程的影响;导轨辅助移动组件包括电机和丝杠滑台,在电机的驱动下使得丝杠滑台移动,进而带动悬挂导轨组件中可以平移的导轨移动,保持可平移导轨在展开过程中始终位于展开机构悬挂绳吊挂环的正上方。本发明能够有效的在柱面展开机构展开过程中进行重力卸载,结构简单,可用于柱面展开机构的地面零重力展开试验。
The invention discloses a zero-gravity suspension test device for a cylinder unfolding mechanism, which comprises a support assembly, a suspension guide rail assembly, and a guide rail auxiliary moving assembly. The support assembly is used to fix the support cylinder expansion mechanism; the suspension guide rail assembly includes a fixed guide rail and a translational guide rail, and there is a slider on the guide rail that can move along the guide rail; one end of the suspension rope is connected with the deployment mechanism, and the other end passes through the pulley It is connected with the counterweight, and the influence of the self-gravity of the unfolding mechanism on the unfolding process is eliminated through the function of the counterweight; the guide rail auxiliary moving component includes a motor and a screw slide table, driven by the motor, the screw slide table moves, and then drives the suspension guide rail assembly The guide rail that can be translated in the center moves, and the guide rail that can be translated can be kept directly above the hanging ring of the suspension rope of the unfolding mechanism during the unfolding process. The invention can effectively carry out gravity unloading during the unfolding process of the cylinder unfolding mechanism, has a simple structure, and can be used for the ground zero-gravity unfolding test of the cylinder unfolding mechanism.
Description
技术领域technical field
本发明属于机械技术领域,涉及一种用于柱面展开机构的零重力悬挂试验装置,可用于柱面展开机构的地面零重力展开试验。The invention belongs to the technical field of machinery, and relates to a zero-gravity suspension test device for a cylinder unfolding mechanism, which can be used for the ground zero-gravity deployment test of the cylinder unfolding mechanism.
背景技术Background technique
随着航天事业的发展,航天器结构趋于大型化,但又受到运载火箭几何空间的限制,展开机构应运而生;柱面展开机构由于其较好的信号汇聚能力,得到了广泛的关注和应用。柱面展开机构投入使用前,需要在地面进行展开试验;而由于机构在轨运行时处于失重状态,因此地面展开试验也必须模拟在轨环境的零重力状态。地面展开试验装置需要根据展开机构的结构特点、展开运动轨迹等进行设计。现有的地面零重力试验装置,主要是针对展开轨迹为一条直线的展开机构,少数针对二维平面展开的试验装置,移动的悬挂导轨也会给机构展开增添额外阻力,降低重力卸载效果。With the development of the aerospace industry, the structure of the spacecraft tends to be larger, but due to the limitation of the geometric space of the launch vehicle, the deployment mechanism emerges as the times require; the cylindrical deployment mechanism has received extensive attention and attention due to its better signal aggregation ability application. Before the cylindrical deployment mechanism is put into use, a deployment test needs to be carried out on the ground; and since the mechanism is in a state of weightlessness during orbital operation, the ground deployment test must also simulate the zero-gravity state of the orbital environment. The ground deployment test device needs to be designed according to the structural characteristics of the deployment mechanism and the deployment trajectory. The existing zero-gravity test devices on the ground are mainly for the deployment mechanism whose deployment trajectory is a straight line, and a few of the test devices are for two-dimensional plane deployment. The moving suspension guide rail will also add additional resistance to the mechanism deployment and reduce the gravity unloading effect.
发明内容Contents of the invention
本发明的目的是为了解决上述问题,提出一种用于柱面展开机构的零重力悬挂试验装置,能够用于柱面展开机构在地面重力环境下模拟在轨的零重力状态,用于展开试验。The purpose of the present invention is to solve the above problems, and propose a zero-gravity suspension test device for a cylindrical deployment mechanism, which can be used for the cylindrical deployment mechanism to simulate the zero-gravity state on the track under the ground gravity environment, and is used for the deployment test. .
一种用于柱面展开机构的零重力悬挂试验装置,包括支撑组件、悬挂导轨组件、导轨辅助移动组件。A zero-gravity suspension test device for a cylinder unfolding mechanism, comprising a support assembly, a suspension guide rail assembly, and a guide rail auxiliary moving assembly.
所述支撑组件包括框架、支撑导轨、固定支撑座、移动支撑座。框架由型材连接而成,整体呈长方体形;支撑导轨固定安装于框架侧面的一个横梁上,固定支撑座固定安装于支撑导轨上,固定支撑座与框架上方用于安装固定长导轨的横梁位于同一垂直平面内;移动支撑座安装于支撑导轨上,可沿导轨移动;固定支撑座和移动支撑座结构完全一样,支撑座两侧安装有轴承座,柱面展开机构最外侧关节连接处的转轴分别与固定支撑座和移动支撑座上的轴承座相连;移动支撑座沿导轨往复移动即可实现柱面展开机构的展开和收拢;在固定支撑座、移动支撑座与展开机构的连接约束下,与固定支撑座位于同一列上的展开机构关节在展开过程中始终位于同一垂直面内;同样的,与移动支撑座位于同一列上的展开机构关节在展开过程中也始终位于同一垂直面内。The support assembly includes a frame, a support guide rail, a fixed support seat, and a mobile support seat. The frame is connected by profiles, and the whole is in the shape of a cuboid; the support guide rail is fixedly installed on a beam on the side of the frame, the fixed support base is fixedly installed on the support guide rail, and the fixed support base and the beam used to install and fix the long guide rail above the frame are located at the same In the vertical plane; the mobile support seat is installed on the support guide rail and can move along the guide rail; the structure of the fixed support seat and the mobile support seat are exactly the same, bearing seats are installed on both sides of the support seat, and the rotating shafts at the outermost joint connection of the cylindrical surface expansion mechanism are respectively It is connected with the bearing seat on the fixed support seat and the mobile support seat; the mobile support seat can move back and forth along the guide rail to realize the unfolding and folding of the cylindrical surface deployment mechanism; under the connection constraints of the fixed support seat, the mobile support seat and the deployment mechanism, the The joints of the deployment mechanism with the fixed support seats on the same row are always located in the same vertical plane during the deployment process; similarly, the joints of the deployment mechanism with the mobile support seats on the same row are also always located in the same vertical plane during the deployment process.
所述悬挂导轨组件包括固定长导轨、固定短导轨、连接滑块、移动长导轨、滑块、滑轮、悬挂绳、配重。固定长导轨固定安装于框架上方的纵向横梁上;固定短导轨共有两根,分别固定安装于框架上方的横向横梁上;两根固定短导轨上分别安装有一个可沿导轨移动的连接滑块,移动长导轨与这两个连接滑块相连,可以沿着短导轨方向移动;固定长导轨和移动长导轨上分别安装有七个可沿导轨移动的滑块,每个滑块上安装有滑轮;悬挂绳一端与柱面展开机构上的悬挂环相连;悬挂环与右连杆、左连杆通过转动副相连,右连杆、左连杆分别与对应的右关节、左关节通过转动副相连,右连杆、左连杆长度相等,其与关节连接处距离关节转轴距离相等,因此可以保证悬挂环始终位于两个关节的角平分面上;悬挂绳另一端绕过滑轮与配重相连,配重质量与对应悬挂绳吊挂柱面展开机构部分的重量相等。The suspension guide rail assembly includes a fixed long guide rail, a fixed short guide rail, a connecting slide block, a moving long guide rail, a slide block, a pulley, a suspension rope, and a counterweight. The fixed long guide rail is fixedly installed on the longitudinal beam above the frame; there are two fixed short guide rails, which are respectively fixedly installed on the transverse beam above the frame; the two fixed short guide rails are respectively installed with a connecting slider that can move along the guide rail. The moving long guide rail is connected with the two connecting sliders and can move along the direction of the short guide rail; the fixed long guide rail and the moving long guide rail are respectively equipped with seven sliders that can move along the guide rails, and each slider is equipped with a pulley; One end of the suspension rope is connected with the suspension ring on the cylinder unfolding mechanism; the suspension ring is connected with the right connecting rod and the left connecting rod through a rotating pair, and the right connecting rod and the left connecting rod are respectively connected with the corresponding right joint and left joint through a rotating pair. The length of the right link and the left link are equal, and the distance between the joint connection and the joint rotation axis is equal, so that the suspension ring can always be located on the angle bisector of the two joints; the other end of the suspension rope is connected to the counterweight around the pulley, The heavy mass is equal to the weight of the corresponding suspension rope hanging cylinder expansion mechanism part.
所述导轨辅助移动组件包括底座、丝杠、滑台、电机、连接块。底座两端分别固定安装于框架顶部;丝杠两端通过轴承安装于底座上,与电机通过联轴器相连;滑台安装于丝杠上,连接块一端与滑台相连,另一端与移动长导轨相连,通过电机的驱动带动滑台移动,进而可以带动移动长导轨运动。The guide rail auxiliary moving assembly includes a base, a lead screw, a slide table, a motor, and a connecting block. The two ends of the base are respectively fixed on the top of the frame; the two ends of the lead screw are installed on the base through bearings, and connected with the motor through a coupling; The guide rails are connected, and the drive of the motor drives the sliding table to move, and then can drive the moving long guide rail to move.
所述零重力悬挂试验装置不仅适用于由两列构成的柱面展开机构,还可以用于横向扩展后的具有n列的柱面展开机构。每一列展开机构悬挂环正上方对应一根长导轨,第一列对应的导轨为固定长导轨,与框架固定相连;第2列到第n列对应的移动长导轨通过滑台与丝杠相连;各组件中的丝杠通过齿轮系与电机相连,各齿轮转速比为1,即可将电机转动传递到各个丝杠上;第i列对应的丝杠螺距与第2列对应的丝杠螺距之比为(i-1),也就是第i列对应的移动长导轨移动速度为第2列对应的移动长导轨移动速度的(i-1)倍;由此即可实现通过一个电机的驱动,使得展开机构展开过程中各个移动长导轨始终位于对应的悬挂环的正上方。The zero-gravity suspension test device is not only suitable for a cylinder unfolding mechanism composed of two columns, but also for a cylinder expanding mechanism with n columns after lateral expansion. There is a long guide rail directly above the suspension ring of the expansion mechanism in each row, and the guide rail corresponding to the first row is a fixed long guide rail, which is fixedly connected with the frame; the mobile long guide rails corresponding to the second row to the nth row are connected to the lead screw through a slide table; The lead screws in each component are connected to the motor through a gear train, and the speed ratio of each gear is 1, so that the rotation of the motor can be transmitted to each lead screw; The ratio is (i-1), that is, the moving speed of the moving long guide rail corresponding to the i-th column is (i-1) times the moving speed of the moving long guide rail corresponding to the second column; thus, it can be driven by a motor, So that each moving long guide rail is always located directly above the corresponding suspension ring during the unfolding process of the unfolding mechanism.
本发明的优点在于:The advantages of the present invention are:
(1)本发明针对一种柱面展开机构开发了一套地面零重力悬挂试验装置,可以用于模拟在轨的零重力状态进行展开试验,并且可适用于横向扩展后的柱面展开机构,结构简单;(1) The present invention develops a set of ground zero-gravity suspension test device for a cylindrical surface deployment mechanism, which can be used to simulate the zero-gravity state on the track for deployment tests, and can be applied to the cylindrical surface deployment mechanism after lateral expansion, Simple structure;
(2)本发明可移动悬挂导轨可以保证用于卸载重力的配重始终位于展开机构悬挂环的正上方;(2) The movable suspension guide rail of the present invention can ensure that the counterweight for unloading gravity is always located directly above the suspension ring of the deployment mechanism;
(3)本发明导轨辅助移动组件可用于驱动可移动导轨移动,避免给展开机构增添额外的展开阻力。(3) The guide rail auxiliary moving assembly of the present invention can be used to drive the movable guide rail to move, avoiding adding extra deployment resistance to the deployment mechanism.
附图说明Description of drawings
图1为本发明一种用于柱面展开机构的零重力悬挂试验装置整体示意图;Fig. 1 is an overall schematic diagram of a zero-gravity suspension test device for a cylindrical unfolding mechanism of the present invention;
图2为本发明支撑组件示意图;Fig. 2 is a schematic diagram of the support assembly of the present invention;
图3为本发明支撑组件局部放大示意图;Fig. 3 is a partially enlarged schematic view of the support assembly of the present invention;
图4为本发明柱面展开机构示意图;Fig. 4 is a schematic diagram of the cylinder unfolding mechanism of the present invention;
图5为本发明悬挂组件示意图;Fig. 5 is a schematic diagram of the suspension assembly of the present invention;
图6为本发明悬挂环示意图;Fig. 6 is a schematic diagram of the suspension ring of the present invention;
图7为本发明导轨辅助移动组件示意图;Fig. 7 is a schematic diagram of the guide rail auxiliary moving assembly of the present invention;
图8为本发明适用于n列展开机构的悬挂试验装置示意图;Fig. 8 is a schematic diagram of the suspension test device applicable to the n-column deployment mechanism of the present invention;
图中:In the picture:
1-支撑组件 2-悬挂组件 3-导轨辅助移动组件1-Support component 2-Suspension component 3-Rail auxiliary moving component
101-框架 102-支撑导轨 103-固定支撑座101-frame 102-support rail 103-fixed support seat
104-移动支撑座 105-轴承座 106-转轴104-mobile support seat 105-bearing seat 106-rotating shaft
201-固定长导轨 202-固定短导轨 203-连接滑块201-Fix the long guide rail 202-Fix the short guide rail 203-Connect the slider
204-移动长导轨 205-滑块 206-滑轮204-moving long guide rail 205-slider 206-pulley
207-悬挂绳 208-悬挂环 209-右连杆207-suspension rope 208-suspension ring 209-right link
210-左连杆 211-右关节 212-左关节210-left link 211-right joint 212-left joint
213-配重 301-底座 302-丝杠213-counterweight 301-base 302-lead screw
303-滑台 304-电机 305-连接块303-slide 304-motor 305-connection block
具体实施方式Detailed ways
下面将结合附图和实施例对本发明作进一步的详细说明。The present invention will be further described in detail with reference to the accompanying drawings and embodiments.
申请号2017107554079公开了一种基于Bennett机构的同步展收圆柱面天线,其中,公开了一种柱面展开机构,本发明的零重力悬挂试验装置可以应用在此可展机构上。如图4所示,该展开机构展开过程中,A、B、C、D四点始终共面;关节M1、M2、M3、M4、M5、M6在平面ABCD上的投影始终位于直线AB上;关节N1、N2、N3、N4、N5、N6的轨迹在平面ABCD上的投影可以分解成两部分,一部分为始终沿着直线CD的移动,另一部分为沿着AC方向的移动。根据上述关节的运动轨迹即可确定展开机构的悬挂位置及方式,一条导轨固定位于关节M1、M2、M3、M4、M5、M6正上方,另一条导轨位于关节N1、N2、N3、N4、N5、N6的正上方,并且可以跟随关节一起平移。Application No. 2017107554079 discloses a synchronously deployable cylindrical antenna based on a Bennett mechanism, in which a cylindrical deployable mechanism is disclosed, and the zero-gravity suspension test device of the present invention can be applied to this deployable mechanism. As shown in Figure 4, during the deployment process of the deployment mechanism, the four points A, B, C, and D are always coplanar; the projections of the joints M 1 , M 2 , M 3 , M 4 , M 5 , and M 6 on the plane ABCD is always on the straight line AB; the projection of the trajectories of the joints N 1 , N 2 , N 3 , N 4 , N 5 , and N 6 on the plane ABCD can be decomposed into two parts, one part is always moving along the straight line CD, and the other part is is the movement along the AC direction. The suspension position and mode of the unfolding mechanism can be determined according to the movement trajectories of the above joints. One guide rail is fixed directly above the joints M 1 , M 2 , M 3 , M 4 , M 5 , and M 6 , and the other guide rail is located directly above the joints N 1 , It is directly above N 2 , N 3 , N 4 , N 5 , and N 6 , and can translate along with the joints.
本发明是一种用于柱面展开机构的零重力悬挂试验装置,包括支撑组件1、悬挂导轨组件2、导轨辅助移动组件3,如图1所示。The present invention is a zero-gravity suspension test device for a cylinder unfolding mechanism, including a support assembly 1, a suspension guide rail assembly 2, and a guide rail auxiliary moving assembly 3, as shown in FIG. 1 .
所述支撑组件1包括框架101、支撑导轨102、固定支撑座103、移动支撑座104,如图2所示。框架101由型材连接而成,整体呈长方体形;支撑导轨102固定安装于框架101侧面的一个横梁上,固定支撑座103固定安装于支撑导轨上,不能移动,固定支撑座103与框架101上方用于安装固定长导轨201的横梁位于同一垂直平面内;移动支撑座104安装于支撑导轨上,可沿导轨移动;固定支撑座103和移动支撑座104结构完全一样,支撑座两侧安装有轴承座105,柱面展开机构最外侧关节连接处的转轴106分别与固定支撑座103和移动支撑座104上的轴承座105相连,如图3所示;移动支撑座104沿导轨往复移动即可实现柱面展开机构的展开和收拢。在固定支撑座103、移动支撑座104与展开机构的连接约束下,与固定支撑座103位于同一列上的展开机构关节A、M1、M2、M3、M4、M5、M6、B在展开过程中始终位于同一垂直面内;同样的,与移动支撑座104位于同一列上的展开机构关节C、N1、N2、N3、N4、N5、N6、D在展开过程中也始终位于同一垂直面内。The support assembly 1 includes a frame 101 , a support rail 102 , a fixed support base 103 , and a movable support base 104 , as shown in FIG. 2 . The frame 101 is connected by profiles and is in the shape of a cuboid as a whole; the support guide rail 102 is fixedly installed on a beam on the side of the frame 101, and the fixed support seat 103 is fixedly installed on the support guide rail and cannot be moved. The beam on which the fixed long guide rail 201 is installed is located in the same vertical plane; the mobile support base 104 is installed on the support guide rail and can move along the guide rail; the fixed support base 103 and the mobile support base 104 have exactly the same structure, and bearing seats are installed on both sides of the support base 105, the rotating shaft 106 at the outermost joint joint of the cylinder unfolding mechanism is connected to the bearing seat 105 on the fixed support seat 103 and the mobile support seat 104 respectively, as shown in Figure 3; the mobile support seat 104 can move back and forth along the guide rail to realize the column The unfolding and retracting of the surface unfolding mechanism. Under the constraints of the connection between the fixed support base 103, the mobile support base 104 and the deployment mechanism, the joints A, M 1 , M 2 , M 3 , M 4 , M 5 , M 6 of the deployment mechanism located on the same row as the fixed support base 103 , B are always located in the same vertical plane during the unfolding process; similarly, joints C, N 1 , N 2 , N 3 , N 4 , N 5 , N 6 , D It is also always in the same vertical plane during unfolding.
所述悬挂导轨组件2包括固定长导轨201、固定短导轨202、连接滑块203、移动长导轨204、滑块205、滑轮206、悬挂绳207和配重213,如图5所示。固定长导轨201固定安装于框架101上方的纵向横梁上,并且和固定支撑座103位于同一平面内;固定短导轨202共有两根,分别固定安装于框架101上方的横向横梁上;两根固定短导轨202上分别安装有一个可沿导轨移动的连接滑块203,移动长导轨204与这两个连接滑块203相连,可以沿着短导轨202方向移动;固定长导轨201和移动长导轨204上分别安装有七个可沿导轨移动的滑块205,每个滑块205上安装有滑轮206;悬挂绳207一端与柱面展开机构上的悬挂环208相连;如图6所示,悬挂环208与右连杆209、左连杆210通过转动副相连,右连杆209、左连杆210分别与对应的右关节211、左关节212通过转动副相连,右连杆209、左连杆210长度相等,其与关节连接处距离关节转轴距离相等,因此可以保证悬挂环208始终位于两个关节的角平分面上;悬挂绳207另一端绕过滑轮206与配重213相连,配重213质量与对应悬挂绳207吊挂柱面展开机构部分的重量相等。在展开机构展开过程中,各关节会上下移动,与之相连的配重也会随之上下移动,并且二者移动距离相同,也就是二者的重力势能始终保持不变,即可消除重力对展开过程的影响。The suspension guide rail assembly 2 includes a fixed long guide rail 201, a fixed short guide rail 202, a connecting slider 203, a moving long guide rail 204, a slider 205, a pulley 206, a suspension rope 207 and a counterweight 213, as shown in FIG. 5 . The fixed long guide rail 201 is fixedly installed on the longitudinal beam above the frame 101, and is located in the same plane as the fixed support seat 103; there are two fixed short guide rails 202, which are respectively fixedly installed on the transverse beam above the frame 101; A connection slider 203 movable along the guide rails is respectively installed on the guide rails 202, and the moving long guide rail 204 is connected with the two connection sliders 203, and can move along the direction of the short guide rails 202; Seven slide blocks 205 movable along the guide rails are installed respectively, and a pulley 206 is installed on each slide block 205; one end of the suspension rope 207 links to each other with the suspension ring 208 on the cylinder unfolding mechanism; as shown in Figure 6, the suspension ring 208 Connect with the right connecting rod 209 and the left connecting rod 210 through a rotating pair, the right connecting rod 209 and the left connecting rod 210 are respectively connected with the corresponding right joint 211 and left joint 212 through a rotating pair, the length of the right connecting rod 209 and the left connecting rod 210 Equal, it is equated with the distance of the joint rotating shaft from the joint joint, so it can be ensured that the suspension ring 208 is always on the angle bisector of the two joints; Corresponding suspension rope 207 suspends the weight of cylindrical surface unfolding mechanism part equal. During the unfolding process of the unfolding mechanism, each joint will move up and down, and the counterweight connected to it will also move up and down, and the moving distance of the two is the same, that is, the gravitational potential energy of the two remains unchanged, which can eliminate the gravitational impact. The effect of the unfolding process.
所述导轨辅助移动组件3包括底座301、丝杠302、滑台303、电机304、连接块305,如图7所示。底座301两端分别固定安装于框架101顶部;丝杠302两端通过轴承安装于底座301上,与电机304通过联轴器相连;滑台303安装于丝杠302上,在电机304的驱动下丝杠302转动,并带动滑台303沿丝杠302方向移动;连接块305一端与滑台303相连,另一端与移动长导轨204相连,滑台303移动即可可以带动移动长导轨204运动。通过电机304可以控制移动长导轨204的移动速度,即可使得展开过程中移动长导轨204始终位于关节N1、N2、N3、N4、N5、N6的正上方。移动长导轨204运动所需能量来自导轨辅助移动组件3的电机304,不会对展开机构造成额外的运动阻力。The guide rail auxiliary moving assembly 3 includes a base 301 , a lead screw 302 , a slide table 303 , a motor 304 , and a connecting block 305 , as shown in FIG. 7 . The two ends of the base 301 are fixedly installed on the top of the frame 101 respectively; the two ends of the screw 302 are installed on the base 301 through bearings, and are connected with the motor 304 through a coupling; The leading screw 302 rotates and drives the slide table 303 to move along the lead screw 302 direction; one end of the connecting block 305 is connected with the slide table 303, and the other end is connected with the moving long guide rail 204, and the moving slide table 303 can drive the moving long guide rail 204 to move. The moving speed of the long moving guide rail 204 can be controlled by the motor 304 , so that the long moving guide rail 204 is always located directly above the joints N 1 , N 2 , N 3 , N 4 , N 5 , and N 6 during deployment. The energy required for moving the long guide rail 204 comes from the motor 304 of the guide rail auxiliary moving assembly 3, which will not cause additional motion resistance to the unfolding mechanism.
所述零重力悬挂试验装置不仅用于由两列构成的柱面展开机构,还可以用于横向扩展后的具有多列的柱面展开机构,如图8所示为具有n列的柱面展开机构俯视示意图以及对应的上方导轨辅助移动组件示意图。每一列展开机构悬挂环正上方对应一根长导轨,第一列对应的导轨为固定长导轨201,与框架101固定相连;第2列到第n列对应的移动长导轨通过滑台与丝杠相连;各组件中的丝杠通过齿轮系与电机304相连,各齿轮转速比为1,即可将电机转动传递到各个丝杠上;第i列对应的丝杠螺距与第2列对应的丝杠螺距之比为(i-1),也就是第i列对应的移动长导轨移动速度为第2列对应的移动长导轨移动速度的(i-1)倍;由此即可实现通过一个电机的驱动,使得展开机构展开过程中各个移动长导轨始终位于对应的悬挂环的正上方。The zero-gravity suspension test device is not only used for the cylinder expansion mechanism composed of two rows, but also can be used for the cylinder expansion mechanism with multiple columns after lateral expansion, as shown in Figure 8. Schematic diagram of the top view of the mechanism and the corresponding schematic diagram of the auxiliary moving components of the upper guide rail. Each row of expansion mechanism suspension rings corresponds to a long guide rail directly above, and the guide rail corresponding to the first row is a fixed long guide rail 201, which is fixedly connected with the frame 101; The lead screws in each assembly are connected to the motor 304 through a gear train, and the speed ratio of each gear is 1, so that the rotation of the motor can be transmitted to each lead screw; the lead screw pitch corresponding to the i column is the same as the screw pitch corresponding to the second column The ratio of the pitch of the bar is (i-1), that is, the moving speed of the moving long guide rail corresponding to the i-th column is (i-1) times the moving speed of the moving long guide rail corresponding to the second column; thus, it can be realized by a motor The drive makes each moving long guide rail always be located directly above the corresponding suspension ring during the unfolding process of the unfolding mechanism.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810229128.3A CN108535035B (en) | 2018-03-20 | 2018-03-20 | A Zero Gravity Suspension Test Device for Cylinder Unfolding Mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810229128.3A CN108535035B (en) | 2018-03-20 | 2018-03-20 | A Zero Gravity Suspension Test Device for Cylinder Unfolding Mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108535035A true CN108535035A (en) | 2018-09-14 |
CN108535035B CN108535035B (en) | 2020-04-14 |
Family
ID=63484916
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810229128.3A Active CN108535035B (en) | 2018-03-20 | 2018-03-20 | A Zero Gravity Suspension Test Device for Cylinder Unfolding Mechanism |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108535035B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110304550A (en) * | 2019-07-15 | 2019-10-08 | 西安工业大学 | An active suspension device and suspension method for an antenna structure |
CN110827611A (en) * | 2019-11-29 | 2020-02-21 | 桂林电子科技大学 | A comprehensive experimental platform for unmanned aerial vehicles with adjustable degrees of freedom and simulating the external environment |
CN112061432A (en) * | 2020-09-25 | 2020-12-11 | 西安电子科技大学 | Parabolic cylinder antenna low-gravity unfolding test bed based on curved guide rail |
CN113212815A (en) * | 2021-05-31 | 2021-08-06 | 长光卫星技术有限公司 | Ground unfolding device suitable for solar wings in different structural forms |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3599976B2 (en) * | 1997-10-28 | 2004-12-08 | 三菱電機株式会社 | Exercise test equipment |
CN102145755A (en) * | 2010-02-10 | 2011-08-10 | 上海卫星工程研究所 | Zero-gravity suspension type deployment test device |
CN104318828A (en) * | 2014-10-10 | 2015-01-28 | 北京卫星制造厂 | Zero-gravity experiment system for spatial multi-dimensional unfolding mechanism |
CN205060041U (en) * | 2015-09-24 | 2016-03-02 | 天津航天机电设备研究所 | Battery battle array zero -g expandes two -way drive arrangement |
CN106909074A (en) * | 2015-11-30 | 2017-06-30 | 欧姆龙株式会社 | Control device |
CN206552285U (en) * | 2017-03-09 | 2017-10-13 | 西安汾阳钢结构有限公司 | A kind of radial suspension arrangement of multilayer |
CN107579332A (en) * | 2017-08-29 | 2018-01-12 | 北京航空航天大学 | A Synchronously Expandable Cylindrical Antenna Based on Bennett Mechanism |
CN206969006U (en) * | 2017-06-26 | 2018-02-06 | 西安汾阳钢结构有限公司 | A kind of zero-gravity suspension type deployment test device |
-
2018
- 2018-03-20 CN CN201810229128.3A patent/CN108535035B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3599976B2 (en) * | 1997-10-28 | 2004-12-08 | 三菱電機株式会社 | Exercise test equipment |
CN102145755A (en) * | 2010-02-10 | 2011-08-10 | 上海卫星工程研究所 | Zero-gravity suspension type deployment test device |
CN104318828A (en) * | 2014-10-10 | 2015-01-28 | 北京卫星制造厂 | Zero-gravity experiment system for spatial multi-dimensional unfolding mechanism |
CN205060041U (en) * | 2015-09-24 | 2016-03-02 | 天津航天机电设备研究所 | Battery battle array zero -g expandes two -way drive arrangement |
CN106909074A (en) * | 2015-11-30 | 2017-06-30 | 欧姆龙株式会社 | Control device |
CN206552285U (en) * | 2017-03-09 | 2017-10-13 | 西安汾阳钢结构有限公司 | A kind of radial suspension arrangement of multilayer |
CN206969006U (en) * | 2017-06-26 | 2018-02-06 | 西安汾阳钢结构有限公司 | A kind of zero-gravity suspension type deployment test device |
CN107579332A (en) * | 2017-08-29 | 2018-01-12 | 北京航空航天大学 | A Synchronously Expandable Cylindrical Antenna Based on Bennett Mechanism |
Non-Patent Citations (2)
Title |
---|
DING XILUN: "DESIGN AND TEST ANALYSIS OF A SOLAR ARRAY ROOT HINGE DRIVE ASSEMBLY", 《CHINESE JOURNAL OF MECHANICAL ENGINEERING》 * |
杨佳鑫: "基于Bennett机构柱面拟合可展机构设计及分析", 《深空探测学报》 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110304550A (en) * | 2019-07-15 | 2019-10-08 | 西安工业大学 | An active suspension device and suspension method for an antenna structure |
CN110827611A (en) * | 2019-11-29 | 2020-02-21 | 桂林电子科技大学 | A comprehensive experimental platform for unmanned aerial vehicles with adjustable degrees of freedom and simulating the external environment |
CN110827611B (en) * | 2019-11-29 | 2021-10-29 | 桂林电子科技大学 | A comprehensive experimental platform for unmanned aerial vehicles with adjustable degrees of freedom and simulating the external environment |
CN112061432A (en) * | 2020-09-25 | 2020-12-11 | 西安电子科技大学 | Parabolic cylinder antenna low-gravity unfolding test bed based on curved guide rail |
CN112061432B (en) * | 2020-09-25 | 2022-02-25 | 西安电子科技大学 | A low-gravity deployment test bench for parabolic cylindrical antennas based on curved guide rails |
CN113212815A (en) * | 2021-05-31 | 2021-08-06 | 长光卫星技术有限公司 | Ground unfolding device suitable for solar wings in different structural forms |
Also Published As
Publication number | Publication date |
---|---|
CN108535035B (en) | 2020-04-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108535035A (en) | A kind of zero-g hanging test device for cylinder unwrapping mechanism | |
WO2021068960A1 (en) | Experimental system and method capable of simulating gear transmission non-inertial system environment | |
CN106124157B (en) | A kind of space mechanism in six degree of freedom for the experiment of hypersonic wind tunnel Multi-bodies Separation | |
CN108382616B (en) | Suspension gravity compensation device based on magnetic suspension follow-up | |
CN103192999A (en) | Ground zero-gravity test device for small-space one-dimension extension mechanism | |
CN108248885B (en) | Method for improving structural stability of unmanned aerial vehicle in aerial photography process | |
CN107757955A (en) | Multi-joint space mechanism gravity unloading device | |
CN206114269U (en) | Windscreen performance testing device between rail train carriage | |
CN106078698A (en) | A kind of multi-freedom parallel connection follower mechanism and driving method thereof | |
CN109540198B (en) | A ground test equipment for a parabolic antenna unfolding a reflector | |
CN205642793U (en) | A embedded device of high rigidity for separation of hypersonic wind tunnel multi -body is experimental | |
CN113460338B (en) | Multifunctional antenna gravity unloading device | |
CN108275287A (en) | Multi-rotor aerocraft aerodynamic interference and ground effect integrated experiment device and method | |
CN113911408B (en) | A solar wing deployment mechanism, system and method of use for simulating gravity unloading | |
CN104964829A (en) | KC test stand driving loading device and method and application thereof | |
CN106872137B (en) | High maneuvering wind tunnel test device based on pitch heave interaction | |
CN109848907A (en) | A kind of large-scale workpiece flexible docking device based on air bag | |
CN114476148A (en) | Satellite-borne flat plate type antenna gravity unloading device and method | |
CN106504631A (en) | Twelve degrees of freedom full physical simulation device for spacecraft based on levitation technology | |
CN110207939A (en) | A kind of real-time test mechanism for changing model mean angle of attack | |
CN103879569B (en) | Oscillating block slider reciprocating solar wing assisting overturn mechanism | |
CN106872138B (en) | Based on the captive trajectory testing device being laid out in second level course three outer four | |
CN102680229A (en) | Test platform for testing reliability of traction drive systems of frame-suspended bogies of high speed train | |
CN110637511B (en) | Follow-up mechanism for balancing influence of space expansion and gravity of multidimensional movement mechanism | |
CN111551340A (en) | Pneumatic force measuring and adjusting device for free jet wind tunnel test model |
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 | ||
GR01 | Patent grant | ||
GR01 | Patent grant |