CN110077633B - An angle and eccentricity adjustment device and a microgravity roll state simulation system - Google Patents
An angle and eccentricity adjustment device and a microgravity roll state simulation system Download PDFInfo
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- 238000004088 simulation Methods 0.000 title claims abstract description 17
- 230000005486 microgravity Effects 0.000 title claims abstract description 14
- 239000000725 suspension Substances 0.000 claims abstract description 59
- 230000033001 locomotion Effects 0.000 claims description 4
- 238000012360 testing method Methods 0.000 abstract description 15
- 238000012423 maintenance Methods 0.000 abstract description 3
- 238000009987 spinning Methods 0.000 description 56
- 230000007246 mechanism Effects 0.000 description 24
- 230000005540 biological transmission Effects 0.000 description 22
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- 238000000034 method Methods 0.000 description 9
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- 230000005484 gravity Effects 0.000 description 7
- 230000008569 process Effects 0.000 description 7
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- 230000008859 change Effects 0.000 description 6
- 238000005096 rolling process Methods 0.000 description 5
- 238000012795 verification Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
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- 229910000831 Steel Inorganic materials 0.000 description 1
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- 230000021715 photosynthesis, light harvesting Effects 0.000 description 1
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- B64—AIRCRAFT; AVIATION; COSMONAUTICS
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Abstract
本发明提供了一种角度和偏心调整装置及微重力翻滚状态模拟系统,涉及在轨服务与维护技术领域,所述角度和偏心调整装置,其适于吊装悬吊目标并对所述悬吊目标的偏摆角度与偏心位置进行调整;包括:第一目标转接板;第二目标转接板,其相对设置于所述第一目标转接板下侧并与所述悬吊目标固定连接;丝杠,沿其轴线方向水平设置于所述第一目标转接板底部;丝杠螺母座,套设于所述丝杠外侧;所述丝杠螺母座直接或间接与所述第二目标转接板连接,所述丝杠螺母座适于带动所述第二目标转接板与所述第一目标转接板发生相对运动。本发明所述的角度和偏心调整装置可以对悬吊目标的偏摆角度与偏心位置进行调整,满足不同的试验需求。
The invention provides an angle and eccentricity adjustment device and a microgravity roll state simulation system, which relate to the technical field of on-orbit service and maintenance. The angle and eccentricity adjustment device is suitable for hoisting a suspension target and has The yaw angle and eccentric position are adjusted; including: a first target adapter plate; a second target adapter plate, which is relatively disposed on the lower side of the first target adapter plate and is fixedly connected with the suspended target; A lead screw is horizontally arranged at the bottom of the first target adapter plate along its axis direction; a lead screw nut seat is sleeved on the outside of the lead screw; the lead screw nut seat is directly or indirectly rotated with the second target The connecting plate is connected, and the screw nut seat is suitable for driving the second target adapter plate and the first target adapter plate to move relative to each other. The angle and eccentric adjustment device of the present invention can adjust the yaw angle and eccentric position of the suspended target to meet different test requirements.
Description
技术领域technical field
本发明涉及在轨服务与维护技术领域,特别涉及一种角度和偏心调整装置及微重力翻滚状态模拟系统。The invention relates to the technical field of on-orbit service and maintenance, in particular to an angle and eccentricity adjustment device and a microgravity roll state simulation system.
背景技术Background technique
地球静止轨道(GEO)是人类重要的地球轨道资源,在轨资源受轨位限制,极为紧缺。然而随着航天任务的飞速发展,GEO带(GEO±200km)已经堆积了许多不可控的或废弃的卫星,这些卫星导致GEO轨位资源严重浪费。针对在轨失效卫星,在姿态特性方面,由于星体太阳翼和推进剂晃动等能量耗散作用,最终会呈现出翻滚姿态,对其进行在轨捕获是一大难点。为解决这一难点,亟待开展在轨服务与维护相关关键技术攻关;而相关关键技术攻关过程中,由于限于科研成本以及环保等问题,不能直接在太空中进行关键技术验证,通常在工程应用之前,需要先在地面开展大量的验证试验。因此在关键技术在轨验证及应用之前,急需提供一种能够对在轨失效卫星在太空工作环境及目标的真实在轨状态进行模拟的系统,然而,为实现上述目的,首先需要满足地面对悬吊目标自旋状态的模拟,在对悬吊目标自旋状态的模拟过程中,为了更加真实的对在轨状态进行模拟,根据不同的试验需求,有时还需要对悬吊目标的偏摆角度与偏心位置进行调整,因此需要提供这样一种装置使悬吊目标能够进行悬吊状态位姿的调整,以便满足不同的试验需求。Geostationary orbit (GEO) is an important earth orbit resource for mankind, and the in-orbit resource is extremely scarce due to the limitation of orbital position. However, with the rapid development of space missions, the GEO belt (GEO±200km) has accumulated many uncontrollable or abandoned satellites, which lead to a serious waste of GEO orbital space resources. For satellites that fail in orbit, in terms of attitude characteristics, due to the energy dissipation effects of the star's solar wings and propellant swaying, they will eventually show a rolling attitude, and it is a big difficulty to capture them on-orbit. In order to solve this difficulty, it is urgent to carry out key technical research related to on-orbit service and maintenance; and in the process of researching related key technologies, due to the limitations of scientific research costs and environmental protection issues, it is not possible to directly verify key technologies in space, usually before engineering applications. , it is necessary to carry out a large number of verification tests on the ground first. Therefore, before the on-orbit verification and application of key technologies, it is urgent to provide a system capable of simulating the real on-orbit state of the in-orbit satellite working environment and target in space. Simulation of the spin state of the suspended target, in the process of simulating the spin state of the suspended target, in order to simulate the on-orbit state more realistically, according to different test requirements, sometimes the yaw angle of the suspended target needs to be calculated. Therefore, it is necessary to provide such a device so that the suspended target can adjust the posture and posture of the suspended state in order to meet different test requirements.
发明内容SUMMARY OF THE INVENTION
有鉴于此,本发明旨在提出一种手自动一体化起旋装置,以实现空间微重力状态下,对目标进行翻滚姿态的地面模拟。In view of this, the present invention aims to provide a hand-automatic integrated spinning device, so as to realize the ground simulation of the rolling attitude of the target in the state of space microgravity.
为达到上述目的,本发明的技术方案是这样实现的:In order to achieve the above object, the technical scheme of the present invention is achieved in this way:
一种角度和偏心调整装置,其适于对悬吊目标的偏摆角度与偏心位置进行调整;所述角度和偏心调整装置包括:An angle and eccentric adjustment device, which is suitable for adjusting the yaw angle and eccentric position of a suspended target; the angle and eccentric adjustment device includes:
第一目标转接板,其与所述锥形旋转轴固定连接并同步运动;a first target adapter plate, which is fixedly connected with the conical rotating shaft and moves synchronously;
第二目标转接板,其与所述悬吊目标固定连接;a second target adapter plate, which is fixedly connected to the suspended target;
所述第一目标转接板底部设置有丝杠,一丝杠螺母座套设于丝杠外侧,随着丝杠的转动,所述丝杠螺母座前后移动;所述丝杠螺母座带动所述第二目标转接板运动。A lead screw is arranged at the bottom of the first target adapter plate, and a lead screw nut seat is sleeved on the outside of the lead screw. With the rotation of the lead screw, the lead screw nut seat moves back and forth; the lead screw nut seat drives the The second target adapter board moves.
可选的,所述第一目标转接板与所述锥形旋转轴固定连接并同步运动,所述锥形旋转轴被摩擦件带动并与所述摩擦件同轴转动。Optionally, the first target adapter plate is fixedly connected to the conical rotating shaft and moves synchronously, and the conical rotating shaft is driven by the friction member and rotates coaxially with the friction member.
可选的,所述角度和偏心调整装置包括两组丝杠及两组丝杠螺母座;第一组丝杠螺母座与三角板连接且不发生相对转动;第二组丝杠螺母座与连杆通过一根销轴连接且能够发生相对转动;所述三角板以及所述连杆均与所述转接件通过一根销轴连接。Optionally, the angle and eccentricity adjustment device includes two sets of lead screws and two sets of lead screw nut seats; the first set of lead screw nut seats is connected with the triangle plate and does not rotate relative to each other; the second set of lead screw nut seats and connecting rods The triangular plate and the connecting rod are connected with the adapter through a pin and are connected by a pin and can rotate relative to each other.
可选的,所述三角板与所述两块连杆均通过转接件与第二目标转接板连接。Optionally, both the triangular plate and the two connecting rods are connected to the second target adapter plate through an adapter.
可选的,当两组丝杠转动相同角度时,所述第一组丝杠螺母座与所述第二组丝杠螺母座移动相同距离,则所述角度和偏心调整装置带动所述悬吊目标平移,调节悬吊目标的重心。Optionally, when the two sets of lead screws rotate at the same angle, the first set of lead screw nut seats and the second set of lead screw nut seats move the same distance, and the angle and eccentric adjustment device drives the suspension. The target is translated to adjust the center of gravity of the suspended target.
可选的,当两组丝杠转动不同角度时,所述第一组丝杠螺母座与所述第二组丝杠螺母座移动不同距离,则所述连杆同时绕所述第二组丝杠螺母座的销轴和所述转接件的销轴转动,而所述三角板仅能够绕所述转接件的销轴转动,从而使第二目标转接板发生角度a°的偏转,进而调节悬吊目标的角度。Optionally, when the two sets of lead screws are rotated at different angles, the first set of lead screw nut seats and the second set of lead screw nut seats move by different distances, and the connecting rods simultaneously wrap around the second set of leads. The pin of the lever nut seat and the pin of the adapter rotate, while the triangular plate can only rotate around the pin of the adapter, so that the second target adapter plate is deflected by an angle a°, and then Adjust the angle of the hanging target.
可选的,所述第一目标转接板底部固定连接有至少一导轨,所述丝杠螺母座通过滑块与所述导轨相对滑动连接。Optionally, at least one guide rail is fixedly connected to the bottom of the first target adapter plate, and the lead screw nut seat is relatively slidingly connected to the guide rail through a slider.
可选的,所述角度和偏心调整装置还包括一固定盘,所述丝杠沿轴线方向一端与固定盘固定连接,一手轮偏心安装在固定盘上,通过摇动手轮,进而带动固定盘将转矩传递到丝杠上,驱动丝杠转动。Optionally, the angle and eccentric adjustment device further includes a fixed plate, one end of the lead screw is fixedly connected to the fixed plate along the axis direction, and a hand wheel is eccentrically installed on the fixed plate, and by shaking the hand wheel, the fixed plate is further driven to move. The torque is transmitted to the lead screw, which drives the lead screw to rotate.
可选的,所述丝杠通过丝杠支撑端、丝杠固定端与所述第一目标转接板连接。Optionally, the lead screw is connected to the first target adapter board through a lead screw support end and a lead screw fixed end.
相对于现有技术,本发明所述的角度和偏心调整装置具有以下优势:Compared with the prior art, the angle and eccentric adjustment device of the present invention has the following advantages:
本发明提供的角度和偏心调整装置可以对悬吊目标的偏摆角度与偏心位置进行调整,满足不同的试验需求。The angle and eccentric adjustment device provided by the present invention can adjust the yaw angle and eccentric position of the suspended target to meet different test requirements.
本发明的另一目的在于提出一种微重力翻滚状态模拟系统,所述包括如上述所述角度和偏心调整装置。Another object of the present invention is to provide a microgravity roll state simulation system, which includes the angle and eccentricity adjustment devices described above.
所述微重力翻滚状态模拟系统与上述角度和偏心调整装置相对于现有技术所具有的优势相同,在此不再赘述。The microgravity tumbling state simulation system has the same advantages as the above-mentioned angle and eccentricity adjustment device relative to the prior art, which will not be repeated here.
附图说明Description of drawings
构成本发明的一部分的附图用来提供对本发明的进一步理解,本发明的示意性实施例及其说明用于解释本发明,并不构成对本发明的不当限定。在附图中:The accompanying drawings constituting a part of the present invention are used to provide further understanding of the present invention, and the exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation of the present invention. In the attached image:
图1为本发明微重力翻滚状态模拟系统整体结构示意图;1 is a schematic diagram of the overall structure of the microgravity tumbling state simulation system of the present invention;
图2为本发明悬吊起旋机构立体图一;Fig. 2 is a perspective view one of the suspension and swivel mechanism of the present invention;
图3的本发明悬吊起旋机构立体图二;Figure 3 is a perspective view two of the suspension and swivel mechanism of the present invention;
图4为本发明手摇齿轮箱结构示意图;4 is a schematic structural diagram of the hand crank gearbox of the present invention;
图5为本发明起旋组件立体图;5 is a perspective view of the spinning assembly of the present invention;
图6为本发明起旋组件截面图;6 is a cross-sectional view of the spinning assembly of the present invention;
图7为本发明悬吊起旋机构局部结构立体图;Figure 7 is a perspective view of the partial structure of the suspension and swivel mechanism of the present invention;
图8为本发明升降单元立体图;8 is a perspective view of the lifting unit of the present invention;
图9为图7中A处放大图;Fig. 9 is an enlarged view at A place in Fig. 7;
图10为图7中B处放大图;Figure 10 is an enlarged view at B in Figure 7;
图11为本发明制动盘与套筒轴承座结构示意图;Figure 11 is a schematic structural diagram of the brake disc and the sleeve bearing seat of the present invention;
图12为本发明悬吊起旋机构截面图一;Fig. 12 is the sectional view one of the suspension hoisting mechanism of the present invention;
图13为图13中C处放大图;Figure 13 is an enlarged view at C in Figure 13;
图14为本发明摩擦件与锥形旋转轴结构示意图;14 is a schematic structural diagram of the friction member and the conical rotating shaft of the present invention;
图15为本发明柔性悬吊单元示意图;15 is a schematic diagram of the flexible suspension unit of the present invention;
图16为本发明钢丝绳组件截面图;Figure 16 is a sectional view of the wire rope assembly of the present invention;
图17为本发明制动盘非制动状态示意图;17 is a schematic diagram of the non-braking state of the brake disc of the present invention;
图18为本发明制动盘制动状态示意图;18 is a schematic diagram of the braking state of the brake disc of the present invention;
图19为本发明角度和偏心调整装置立体图;Figure 19 is a perspective view of the angle and eccentricity adjustment device of the present invention;
图20为本发明角度和偏心调整装置角度调整示意图一;20 is a schematic diagram 1 of the angle adjustment of the angle and eccentric adjustment device of the present invention;
图21为本发明角度和偏心调整装置角度调整示意图二。Fig. 21 is the second schematic diagram of the angle adjustment of the angle and eccentric adjustment device of the present invention.
附图标记说明:Description of reference numbers:
11-桁架,12-电气箱,13-桁架连接板,9-悬吊目标;11-truss, 12-electrical box, 13-truss connecting plate, 9-suspension target;
2-手动组件;21-手摇齿轮箱,22-起旋齿轮箱,23-制动齿轮箱,24-制动第一万向联轴器,25-起旋第一万向联轴器,26-制动第二万向联轴器,27-起旋第二万向联轴器;211-第一手轮,212-第二手轮,213-第一锥齿,214-第二锥齿,215-第三锥齿,216-第四锥齿,221-第五锥齿,222-第六锥齿,421-第七锥齿,422-第八锥齿;2-Manual components; 21-hand gear box, 22-starting gear box, 23-braking gear box, 24-braking the first universal joint, 25-starting the first universal joint, 26-brake the second universal joint, 27-spin the second universal joint; 211-first hand wheel, 212-second hand wheel, 213-first bevel tooth, 214-second cone Teeth, 215-third bevel tooth, 216-fourth bevel tooth, 221-fifth bevel tooth, 222-sixth bevel tooth, 421-seventh bevel tooth, 422-eighth bevel tooth;
3-欠驱动装置;31-制动电机,32-制动传动部,33-升降部,35-锥形旋转轴;331-升降底座,332-升降滑轨,333-双向丝杠,334-正向丝杠螺母座,335-反向丝杠螺母座,336-轴承座升降杆,337-制动盘升降杆,338-丝杠固定座;341-安装板,342-制动盘,3421-制动器,343-套筒轴承座,344-制动盘导向杆,345-轴承座导向杆,346-直线轴承,347-导向件,348-限位锥形块,351-第一摩擦面,352-压紧部,353-第三轴承;3-Under drive device; 31-Brake motor, 32-Brake transmission part, 33-Lifting part, 35-Conical rotating shaft; 331-Lifting base, 332-Lifting slide rail, 333-Two-way screw, 334- Forward screw nut seat, 335-reverse screw nut seat, 336-bearing seat lifting rod, 337-brake disc lifting rod, 338-screw fixing seat; 341-installation plate, 342-brake disc, 3421 -brake, 343-sleeve bearing seat, 344-brake disc guide rod, 345-bearing seat guide rod, 346-linear bearing, 347-guide piece, 348-limiting cone block, 351-first friction surface, 352-pressing part, 353-third bearing;
4-电动起旋组件;41-起旋电机,42-起旋传动部,43-起旋转动部,44-起旋伸缩部,45-摩擦件;411-联轴器,423-齿轮驱动轴,424-第一超越离合器,425-第二超越离合器,431-起旋轴承座,432-上部套筒,433-第一轴承,434-第二轴承,441-伸缩套筒,442-连接键,451-第一摩擦面;4-Electric winking assembly; 41- Spinning motor, 42- Spinning transmission part, 43- Spinning moving part, 44- Spinning telescopic part, 45- Friction part; 411- Coupling, 423- Gear drive shaft , 424-first overrunning clutch, 425-second overrunning clutch, 431-spin bearing seat, 432-upper sleeve, 433-first bearing, 434-second bearing, 441-telescopic sleeve, 442-connection key , 451 - the first friction surface;
5-角度和偏心调整装置;51-第一目标转接板,52-第二目标转接板,53-手摇部,54-丝杠部,55-连杆部;531-手轮,532-固定盘;541-丝杠,542-丝杠螺母座,543-丝杠支撑端,544-丝杠固定端,545-导轨,546-滑块;551-销轴,552-连杆,553-转接件,554-三角板,555-销轴锁紧件;5-angle and eccentric adjustment device; 51-first target adapter plate, 52-second target adapter plate, 53-hand crank part, 54-screw part, 55-connecting rod part; 531-handwheel, 532 -Fixed plate; 541-screw, 542-screw nut seat, 543-screw support end, 544-screw fixed end, 545-guide rail, 546-slider; 551-pin, 552-connecting rod, 553 - Adapter, 554-triangle plate, 555-pin lock;
6-柔性悬吊单元,611-钢丝绳,612-钢丝绳焊接半球,613-钢丝绳上部固定件,614-钢丝绳套筒,615-拉力传感器,616-圆螺母座,617-球螺母;620-钢丝绳板,621-力传感器模块,631-光栅,632-光电传感器,633-测速模块。6-Flexible Suspension Unit, 611-Wire Rope, 612-Wire Rope Welding Hemisphere, 613-Wire Rope Upper Fixing, 614-Wire Rope Sleeve, 615-Tension Sensor, 616-Round Nut Seat, 617-Ball Nut; 620-Wire Rope Plate , 621-force sensor module, 631-grating, 632-photoelectric sensor, 633-speed module.
具体实施方式Detailed ways
需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。另外,在本申请的实施例中所提到的所有方向或位置关系(例如“上”、“下”、“前”、“后”、“左”、“右”)均为基于附图的位置关系,仅为了便于理解本申请和简化描述,而不是暗示所指的装置或元件必须具有的特定的方位,不能理解为对本申请的限制。It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict. In addition, all directions or positional relationships (such as "up", "down", "front", "rear", "left", "right") mentioned in the embodiments of the present application are based on the drawings The positional relationship is only for the purpose of facilitating the understanding of the present application and simplifying the description, rather than implying a specific orientation that the indicated device or element must have, and should not be construed as a limitation on the present application.
本发明旨在保护一种角度和偏心调整装置,所述角度和偏心调整装置作为悬吊起旋机构的组成部分,能够对悬吊目标的偏摆角度与偏心位置进行调整,满足不同的试验需求;为便于更清楚的对所述角度和偏心调整装置进行描述,且使本发明构成完整的技术方案,以下将对悬吊起旋机构整体技术方案进行描述,并在描述过程中,着重对所述角度和偏心调整装置的具体实现形式进行描述。The present invention aims to protect an angle and eccentricity adjustment device, which, as a component of a suspension hoisting mechanism, can adjust the yaw angle and eccentric position of a suspension target to meet different test requirements ; In order to describe the angle and the eccentric adjustment device more clearly, and to make the present invention constitute a complete technical solution, the following will describe the overall technical solution of the suspension and swivel mechanism, and in the description process, focus on all The specific implementation form of the above-mentioned angle and eccentric adjustment device will be described.
下面将参考附图并结合具体技术方案来详细说明本发明。The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with specific technical solutions.
本发明提出的悬吊起旋机构,能够实现空间微重力状态下,对目标进行翻滚姿态的地面模拟,从而在地面试验的基础上,验证空间任务方案的合理性和技术可行性。The suspension and swivel mechanism proposed by the invention can realize ground simulation of the target's rolling attitude under the state of microgravity in space, so as to verify the rationality and technical feasibility of the space mission scheme on the basis of ground tests.
一种悬吊起旋机构,结合图1-图3所示,其包括:A suspension hoisting mechanism, as shown in Fig. 1-Fig. 3, includes:
手自动一体化起旋装置,其适于使悬吊目标9绕自旋轴产生自旋;A hand-automatic integrated spinning device, which is suitable for making the suspended target 9 spin around the spin axis;
刚柔约束转换装置,其适于使悬吊机构与悬吊目标之间在刚性约束和柔性约束之间切换;A rigid-flexible constraint conversion device, which is suitable for switching between a suspension mechanism and a suspension target between rigid constraints and flexible constraints;
角度和偏心调整装置5,其适于对悬吊目标9的偏摆角度与偏心位置进行调整。The angle and
所述悬吊起旋机构通过桁架连接板13安装设置于桁架11上,并与电气箱12进行电连接,以实现对所述悬吊起旋机构的操作控制。The suspending and hoisting mechanism is installed on the
所述桁架连接板13通过四个双螺母安装于桁架11的支撑螺杆上,可利用螺母调节桁架连接板13至水平位置,从而调整整个机构的主体部分的安装水平度。The
[手自动一体化起旋装置][Hand-automatic integrated spinning device]
所述手自动一体化起旋装置,其适于使悬吊目标9绕自旋轴产生自旋;包括:用于提供起旋驱动力的手动起旋组件和/或起旋电机41;适于在所述起旋驱动力的带动下将转矩转变为绕自身轴线转动运动的起旋转动部43;直接或间接与所述起旋转动部43连接的摩擦件45。The hand-automatic integrated spinning device is suitable for making the suspended target 9 spin around the spin axis; including: a manual spinning assembly and/or a spinning
作为具体的实现形式,结合图4-图6所示,所述手自动一体化起旋装置包括:手动起旋组件,电动起旋组件4;所述手自动一体化起旋装置采用手自动一体化起旋形式,能够在手动起旋与电动起旋两种驱动方式之间切换。As a specific implementation form, with reference to Figures 4-6, the hand-automatic integrated winking device includes: a manual winking assembly and an electric winking assembly 4; the hand-automatic integrated winking device adopts a manual automatic winking It can switch between two driving modes, manual and electric.
所述手动起旋组件具体包括:依次连接的手摇齿轮箱21、起旋第一万向联轴器25、起旋齿轮箱22、起旋第二万向联轴器27。The manual spinning assembly specifically includes: a hand cranked
其中,作为本发明的具体实现形式,所述手摇齿轮箱21包括:第一手轮211、第一锥齿213、第二锥齿214;其中,第一手轮211、第一锥齿213、第二锥齿214依次连接,用于对起旋动作进行手动控制;所述起旋齿轮箱22包括啮合连接的第五锥齿221与第六锥齿222;Wherein, as a specific implementation form of the present invention, the hand crank
所述第二锥齿214与所述起旋第一万向联轴器25第一端固定连接,所述起旋第一万向联轴器25第二端与所述第五锥齿221固定连接,所述第六锥齿222与所述起旋第二万向联轴器27第一端固定连接。The
所述第一锥齿213与所述第二锥齿214啮合将传动力进行第一次变向,所述第五锥齿221与所述第六锥齿222啮合将传动力进行第二次变向;从而将所述第一手轮211上作用的手摇力进行传递。The
额外的,所述手摇齿轮箱21还包括:依次连接的第二手轮212、第三锥齿215、第四锥齿216,用于对制动动作进行手动控制;将用于起旋动作与制动动作的结构部件设置于同一个手摇齿轮箱21内,能够方便操作人员进行控制,在手动试验阶段,能够快速的在起旋与制动之间进行调节切换。较佳的,手动驱动方式主要由手动组件2进行操控,所述手动组件2进一步包括手动起旋组件与手动制动组件,将手动起旋组件与手动制动组件放置在一起,结构紧凑,便于操作人员控制。In addition, the
所述手动起旋组件的具体工作形式描述如下:摇动第一手轮211,所述第一手轮211与第一锥齿213连接,传递转矩;所述第一锥齿213与第二锥齿214啮合,将传动力进行第一次变向;第二锥齿214通过所述起旋第一万向联轴器25与第五锥齿221相连,传递转矩;所述第五锥齿221与所述第六锥齿222啮合,将传动力进行第二次变向;所述第六锥齿222与所述起旋第二万向联轴器27第一端固定连接,继续通过所述起旋第二万向联轴器27将转矩进行传递。The specific working form of the manual spinning assembly is described as follows: shake the
所述电动起旋组件4包括:The electric spinning assembly 4 includes:
起旋电机41,起旋传动部42,起旋转动部43,起旋伸缩部44,摩擦件45;Spinning
所述起旋电机41适于对所述电动起旋组件4的起旋传动部42提供电动驱动力;The spinning
所述起旋传动部42适于传递驱动力,具体的,所述起旋传动部42包括啮合连接的第七锥齿421与第八锥齿422;所述起旋第二万向联轴器27的第二端通过第一超越离合器424与所述第七锥齿421连接,进而在手动模式下,将所述起旋第二万向联轴器27的转矩传递给所述第七锥齿421;所述第七锥齿421与所述第八锥齿422啮合,将传动力进行第三次变向。The spin-up
所述起旋传动部42还包括一联轴器411,所述联轴器411第一端与所述起旋电机41的输出轴连接,所述联轴器411第二端与齿轮驱动轴423连接,所述第八锥齿422套设在所述齿轮驱动轴423上,所述第八锥齿422与所述齿轮驱动轴423同步且同轴转动,所述齿轮驱动轴423通过第二超越离合器425与所述起旋转动部43连接,具体的,所述齿轮驱动轴423通过第二超越离合器425与所述起旋转动部43的上部套筒432连接。The spinning
所述手自动一体化起旋装置采用手自动一体化起旋形式,能够在手动起旋与电动起旋两种驱动方式之间切换。所述手动起旋组件适于将手摇齿轮箱21上作用的手摇力传递至起旋传动部42,同时,所述起旋电机41也适于将转矩传递至起旋传动部42。通过设置第一超越离合器424与第二超越离合器425,使手动起旋与电动起旋互不干涉;在手动起旋状态下,第一超越离合器424与所述起旋第二万向联轴器27联接,将转矩经由所述第七锥齿421与所述第八锥齿422传递给上部套筒432;在电动起旋状态下,第一超越离合器424与所述起旋第二万向联轴器27脱开,所述第七锥齿421空转,起旋电机41上的转矩经由联轴器411、齿轮驱动轴423传递至上部套筒432。The manual-automatic integrated spinning device adopts the manual-automatic integrated spinning form, and can switch between two driving modes of manual spinning and electric spinning. The manual spin-up assembly is suitable for transmitting the hand crank force acting on the hand crank
所述起旋转动部43适于在外部驱动力的带动下,将转矩转变为上部套筒432绕自身轴线的转动运动。所述起旋转动部43包括:上部套筒432,所述上部套筒432设置于起旋轴承座431内,且所述上部套筒432与所述起旋轴承座431之间设置有转动轴承,使所述上部套筒432能够在驱动力的带动下,在所述起旋轴承座431内转动;较佳的,作为具体的实现形式,所述转动轴承包括第一轴承433与第二轴承434,所述第一轴承433与第二轴承434分别设置于所述上部套筒432的两端,便于使所述上部套筒432平稳转动。The starting and
所述起旋伸缩部44包括伸缩套筒441,所述伸缩套筒441通过连接键442与所述上部套筒432滑动连接,所述伸缩套筒441与所述上部套筒432同轴设置,使所述伸缩套筒441能够与所述上部套筒432沿轴线方向相对滑动,同时,所述伸缩套筒441能够跟随所述上部套筒432同轴转动。The spinning
所述伸缩套筒441远离所述上部套筒432一端端部固定连接有所述摩擦件45,所述摩擦件45与所述伸缩套筒441同轴设置,同步转动,在所述伸缩套筒441带动下,所述摩擦件45的第一摩擦面451绕轴线转动,进而与后续部件产生相对转动的摩擦力。The
所述手自动一体化起旋装置的具体工作形式描述如下:通过手动起旋组件或所述起旋电机41提供转矩,将转矩经由联轴器411、齿轮驱动轴423传递至上部套筒432;所述上部套筒432在所述起旋轴承座431内绕自身轴线转动,进而所述上部套筒432带动所述伸缩套筒441,所述伸缩套筒441进一步带动所述摩擦件45绕轴转动;同时,所述伸缩套筒441能够带动所述摩擦件45沿轴线方向伸缩。The specific working form of the manual-automatic integrated spinning device is described as follows: torque is provided by the manual spinning assembly or the spinning
本发明提供的所述悬吊起旋机构,同时具有手动与电机两种驱动方式,配置离合器,两种驱动方式互不干涉,一次装配完成后可在手动驱动与电机驱动间任意切换,不用重新更改硬件,不必重新调试。可根据试验需要、试验成熟度及试验安全性等自由选择驱动方式。The suspension hoisting mechanism provided by the present invention has two driving modes, manual and motor, and is equipped with a clutch. The two driving modes do not interfere with each other. Change hardware without re-commissioning. The drive mode can be freely selected according to the test needs, test maturity and test safety.
本发明提供的所述悬吊起旋机构,起旋转速可控,使用初期可采用手动驱动保证安全,确保无安全隐患后改为电机驱动,可自行控制转速与转矩,安全隐患小。The suspension hoisting mechanism provided by the present invention has a controllable start-up rotation speed, can be manually driven to ensure safety at the initial stage of use, and then changed to motor-driven after ensuring that there is no safety hazard, and can control the rotational speed and torque by itself, with little safety hazard.
[刚柔约束转换装置][rigid-flexible constraint conversion device]
结合图7-图14所示,所述刚柔约束转换装置适于使悬吊机构与悬吊目标之间在刚性约束和柔性约束之间切换;在起旋过程中,所述悬吊机构与悬吊目标之间为刚性约束约束,在所述悬吊目标处于稳定的翻滚状态后,所述刚柔约束转换装置使所述悬吊机构与悬吊目标之间转变为柔性约束。7-14, the rigid-flexible constraint conversion device is suitable for switching between the suspension mechanism and the suspension target between rigid constraints and flexible constraints; during the spinning process, the suspension mechanism and The suspension targets are rigid constraints, and after the suspension targets are in a stable rolling state, the rigid-flexible constraint conversion device converts the suspension mechanism and the suspension targets into flexible constraints.
所述刚柔约束转换装置包括:被动驱动单元、欠驱动装置3和柔性悬吊单元6;所述被动驱动单元适于在所述手自动一体化起旋装置的驱动下,进行被动动作,并将作用力传递给悬吊目标9;所述欠驱动装置3适于在悬吊目标9达到预定转速后,将手自动一体化起旋装置进行脱离,并适于对处于翻滚状态的悬吊目标9进行制动;所述柔性悬吊单元6适于对所述悬吊目标9进行柔性约束。The rigid-flexible constraint conversion device includes: a passive driving unit, an under-actuated device 3 and a flexible suspension unit 6; The acting force is transmitted to the suspension target 9; the underactuated device 3 is suitable for disengaging the hand-integrated spinning device after the suspension target 9 reaches a predetermined rotation speed, and is suitable for the suspension target in a rolling state 9 for braking; the flexible suspension unit 6 is adapted to flexibly restrain the suspension target 9 .
作为本发明的具体实现形式,所述被动驱动单元包括锥形旋转轴35,所述锥形旋转轴35与所述摩擦件45相对设置,较佳的,在本发明中,所述锥形旋转轴35与所述摩擦件45同轴设置;在起旋状态下,所述锥形旋转轴35的第二摩擦面351与所述摩擦件45的第一摩擦面451相贴合,所述摩擦件45利用摩擦力带动所述锥形旋转轴35,使所述锥形旋转轴35与所述摩擦件45同轴转动。As a specific implementation form of the present invention, the passive drive unit includes a conical
[欠驱动装置][underactuated device]
所述欠驱动装置3包括:安装板341,制动电机31,制动传动部32,升降部33;The under-actuated device 3 includes: a mounting
所述安装板341与所述桁架连接板13固定连接;The mounting
所述制动传动部32用于传递所述制动电机31或手动制动组件所施加的转矩;所述手动制动组件适于将施加在第二手轮212上的转矩传递至所述制动传动部32上,用于对制动动作进行手动控制;所述手动制动组件包括依次连接的第二手轮212、第三锥齿215、第四锥齿216、制动第一万向联轴器24、制动齿轮箱23、制动第二万向联轴器26;所述手动制动组件与所述手动起旋组件结构形式相同,在此不再赘述。进一步的,所述制动传动部32与所述起旋传动部42结构形式相同,均采用手自动一体化制动形式,并通过超越离合器在手动制动与电动制动两种驱动方式之间切换,在此不再赘述;The
所述升降部33包括:升降底座331,所述升降底座331与所述安装板341共同固定设置于所述桁架连接板13上;升降滑轨332,所述升降滑轨332固定设置于所述升降底座331上;双向丝杠333,所述双向丝杠一半为左旋、一半为右旋,所述双向丝杠333接受所述制动传动部32传递过来的扭矩绕自身轴线转动;丝杠固定座338,所述丝杠固定座338固定设置于所述升降底座331上,且所述双向丝杠333贯穿设置于所述丝杠固定座338内,所述丝杠固定座338与所述双向丝杠333之间设置有轴承,所述丝杠固定座338适于对所述双向丝杠333进行径向限位;正向丝杠螺母座334,套设于所述双向丝杠333上半部分,并在所述双向丝杠333的带动下,沿所述升降滑轨332滑动;反向丝杠螺母座335,套设于所述双向丝杠333下半部分,并在所述双向丝杠333的带动下,沿所述升降滑轨332滑动;轴承座升降杆336,与所述正向丝杠螺母座334固定连接,并跟随所述正向丝杠螺母座334运动;制动盘升降杆337,与所述反向丝杠螺母座335固定连接,并跟随所述反向丝杠螺母座335运动。The lifting portion 33 includes: a lifting
所述欠驱动装置3还包括:The underactuated device 3 further includes:
制动盘342,所述制动盘升降杆337通过制动盘升降杆法兰与所述制动盘342固定连接,所述制动盘342在所述制动盘升降杆337带动下同步运动;The
至少一个制动盘导向杆344,所述制动盘导向杆344一端与所述制动盘342固定连接,所述制动盘导向杆344通过直线轴承346与所述安装板341滑动连接,在所述制动盘342运动时,所述制动盘升降杆337为所述制动盘342提供驱动力,所述制动盘导向杆344为所述制动盘342进行导向;At least one brake
套筒轴承座343,所述轴承座升降杆336通过轴承座升降杆法兰与所述套筒轴承座343固定连接,所述套筒轴承座343在所述轴承座升降杆336带动下同步运动;所述套筒轴承座343套设于所述伸缩套筒441外部,并通过轴承与所述伸缩套筒441转动连接,且所述套筒轴承座343与所述伸缩套筒441同轴设置,同时,所述套筒轴承座343能够带动所述伸缩套筒441沿轴线方向上下运动,进而带动所述摩擦件45沿轴线方向上下运动;
至少一轴承座导向杆345,所述轴承座导向杆345一端与所述套筒轴承座343固定连接,所述轴承座导向杆345通过直线轴承346与所述安装板341滑动连接,在所述套筒轴承座343运动时,所述轴承座升降杆336为所述套筒轴承座343提供驱动力,所述轴承座导向杆345为所述套筒轴承座343进行导向;At least one bearing
所述制动盘342底部还设置有至少一个制动器3421。At least one
所述欠驱动装置3具体动作形式如下:通过所述制动电机31或手动制动组件所施加的转矩,带动所述制动传动部32动作,进而将将转矩传递给所述双向丝杠333,当双向丝杠333正转时,双向丝杠333带动正向丝杠螺母座334向上运动,正向丝杠螺母座334带动轴承座升降杆336向上运动,进而,轴承座升降杆336带动套筒轴承座343向上运动,使所述伸缩套筒441向上运动,从而使所述摩擦件45向上运动并与所述锥形旋转轴35脱开;此时,双向丝杠333正转同步带动反向丝杠螺母座335向下运动,反向丝杠螺母座335带动制动盘升降杆337向下运动,制动盘升降杆337进一步带动所述制动盘342向下运动,当所述制动盘342下降到一定高度时,所述制动盘342上的制动器3421将对第一目标转接板51进行制动,从而使悬吊目标9停止转动。The specific action form of the underactuated device 3 is as follows: through the torque applied by the
同理,当双向丝杠5反转时,双向丝杠333带动正向丝杠螺母座334向下运动,并依次带动正向丝杠螺母座334、轴承座升降杆336、套筒轴承座343、伸缩套筒441、摩擦件45向下运动,进而使所述摩擦件45与所述锥形旋转轴35贴合;此时,双向丝杠333同步带动反向丝杠螺母座335向上运动,并依次带动制动盘升降杆337、制动盘342、制动器3421向上运动,进而使制动器3421与第一目标转接板51脱开。Similarly, when the two-
较佳的,结合图17-图18所示,其中,图18为制动盘制动状态示意图,制动盘升降杆337带动所述制动盘342向下运动,当所述制动盘342下降到一定高度时,所述制动盘342上的制动器3421将对第一目标转接板51进行制动,从而使悬吊目标9停止转动。Preferably, with reference to FIGS. 17-18 , in which, FIG. 18 is a schematic diagram of the braking state of the brake disc. The brake
较佳的,作为本发明的具体实现形式,所述起旋轴承座431固定设置于所述安装板341上方,所述上部套筒432设置于起旋轴承座431内并贯穿所述安装板341,所述上部套筒432能够相对所述安装板341转动。Preferably, as a specific implementation form of the present invention, the
较佳的,所述制动传动部32的输出轴通过联轴器与双向丝杠333连接,所述联轴器上开设有螺纹孔,通过拧入顶丝进行防松。Preferably, the output shaft of the
较佳的,使用双向丝杠代替了两根丝杠,在保证行程的同时使结构简单。Preferably, a bidirectional lead screw is used instead of two lead screws, so that the structure is simple while ensuring the stroke.
较佳的,双向丝杠一端安装于丝杠固定座338、一端套有轴承后装于升降底座331底端,节约空间与成本。Preferably, one end of the bidirectional lead screw is mounted on the lead
较佳的,丝杠螺母座上打孔,同时侧面切槽,将轴承座升降杆/制动盘升降杆装入孔内后使用螺钉拧紧防松。Preferably, holes are drilled on the screw nut seat, and at the same time the side is notched, and the bearing seat lifting rod/brake disc lifting rod is installed into the hole and then tightened with screws to prevent loosening.
较佳的,制动盘导向杆344、轴承座导向杆345分别设置三组,能够防止目标产生偏摆。Preferably, three groups of the brake
较佳的,制动盘导向杆344、轴承座导向杆345均安装于直线轴承中,保证升降时的流畅度。Preferably, the
[柔性悬吊单元][Flexible Suspension Unit]
结合图15-图16所示,所述柔性悬吊单元6包括:钢丝绳611,所述钢丝绳611上端与钢丝绳焊接半球612固定连接,钢丝绳焊接半球612设置于钢丝绳上部固定件613内;所述钢丝绳611下端与钢丝绳套筒614一端固定连接,所述钢丝绳套筒614另一端与拉力传感器615螺纹连接,所述拉力传感器615通过球螺母617与圆螺母座616固定连接,所述圆螺母座616固定连接于钢丝绳板620上,从而使钢丝绳611对所述钢丝绳板620进行柔性悬吊。15-16, the flexible suspension unit 6 includes: a
较佳的,钢丝绳上部固定件613固定连接于所述起旋轴承座431下方,即所述钢丝绳上部固定件613与所述安装板341、所述桁架连接板13均为相对固定设置,从而使所述钢丝绳板620与所述安装板341、所述桁架连接板13均为相对固定设置。Preferably, the wire rope
较佳的,所述钢丝绳611与钢丝绳套筒614焊接连接,钢丝绳套筒614攻外螺纹,且加工了4条缝隙,所述钢丝绳套筒614可被抱紧,所述钢丝绳套筒614侧面为矩形,方便装夹。Preferably, the
作为本发明的具体实现形式,在试验初期,所述摩擦件45带动所述锥形旋转轴35转动,进而使所述悬吊目标9进行旋转,当所述悬吊目标9到达预期的稳定转速后,所述摩擦件45向上运动,解除刚性约束,起旋电机41不再提供动力,使得悬吊目标9自由旋转,仅由钢丝绳611承受重力,模拟载荷失重状态,此时转为柔性约束。As a specific implementation form of the present invention, in the early stage of the test, the
较佳的,所述锥形旋转轴35与钢丝绳板620之间通过第三轴承353滑动连接;所述锥形旋转轴35底部与第一目标转接板51固定连接,所述钢丝绳板620与所述第一目标转接板51能够相对转动;柔性悬吊单元6在悬吊状态下,对所述锥形旋转轴35进行柔性约束,此时,所述锥形旋转轴35能够与钢丝绳板620发生相对转动,从而使锥形旋转轴35带动第一目标转接板51转动,进而带动悬吊目标9转动。Preferably, the conical
较佳的,所述拉力传感器615与力传感器模块621电连接,便于监测拉力数据;所述钢丝绳板620底部还设置有光电传感器632,所述第一目标转接板51上还设置有光栅631,所述锥形旋转轴35转动,带动第一目标转接板51转动,进而带动光栅631转动,从而使光栅631与光电传感器632发生相对转动,所述光电传感器632与测速模块633电连接,从而监测转速数据。Preferably, the
所述刚柔约束转换装置还包括:导向限位单元,所述导向限位单元适于限制所述被动驱动单元的偏摆幅度。The rigid-flexible constraint conversion device further includes: a guide limiting unit, which is adapted to limit the yaw amplitude of the passive driving unit.
具体的,所述导向限位单元包括一导向件347,所述导向件347套设于所述摩擦件45内部,并通过轴承与所述摩擦件45相对转动连接,所述导向件347能够跟随所述摩擦件45沿轴线方向上下运动,所述导向件347贯穿所述锥形旋转轴35,所述导向件347能够在柔性约束状态下,对所述锥形旋转轴35进行偏摆幅度的限位;所述导向限位单元还包括限位锥形块348,所述限位锥形块348设置于导向件347远离所述摩擦件45的一端端部,所述限位锥形块348沿径向方向尺寸大于所述锥形旋转轴35的最小内径,能够防止所述锥形旋转轴35沿上下方向运动超出限制,避免所述轴承座导向杆345从所述安装板341内滑脱。Specifically, the guiding and limiting unit includes a guiding
本发明提供的所述悬吊起旋机构具备制动功能,使用过程中可随时根据需要对悬吊目标制动,并增加了旋转限位锥形块可限制目标的偏摆幅度,增加安全性。The suspension hoisting mechanism provided by the present invention has a braking function, which can brake the suspended target at any time as required during use, and the rotation limit cone block is added to limit the deflection range of the target, thereby increasing the safety. .
较佳的,所述柔性悬吊单元6安装于与轴承外圈相连的钢丝绳板620上部,因此,所述柔性悬吊单元6可以保持竖直状态而不参与旋转。Preferably, the flexible suspension unit 6 is installed on the upper part of the
较佳的,所述柔性悬吊单元6下端连接拉力传感器,可实时测量钢丝绳承受重量,使操作者更加了解试验状态,利于试验分析;Preferably, the lower end of the flexible suspension unit 6 is connected with a tension sensor, which can measure the bearing weight of the steel wire rope in real time, so that the operator can better understand the test state, which is conducive to the test analysis;
较佳的,锥形旋转轴35采用类似摩擦轮结构。Preferably, the conical
本发明提供的悬吊起旋机构,在悬吊目标达到指定转速前为刚性约束,达到指定转速后,刚性约束脱开,仅由钢丝绳承受重力,模拟微重力状态;任意切换对悬吊目标的刚性约束和柔性约束状态,从而实现对在轨故障卫星某一种可能存在的姿态翻滚状态的地面模拟。The suspension hoisting mechanism provided by the present invention is rigidly constrained before the suspension target reaches the specified rotational speed. After reaching the specified rotational speed, the rigid constraint is disengaged, and only the wire rope bears the gravity, simulating a microgravity state; Rigid constraint and flexible constraint state, so as to realize the ground simulation of a possible attitude rollover state of a faulty satellite in orbit.
[角度和偏心调整装置][Angle and eccentric adjustment device]
结合图19所示,角度和偏心调整装置5,其适于对悬吊目标9的偏摆角度与偏心位置进行调整。所述角度和偏心调整装置5包括:第一目标转接板51、第二目标转接板52、手摇部53、丝杠部54、连杆部55;Referring to FIG. 19 , the angle and
所述第一目标转接板51固定设置于所述角度和偏心调整装置的顶端并构造为基准板,作为本发明的具体实现形式,所述第一目标转接板51与所述锥形旋转轴35固定连接并同步运动;The first
所述第二目标转接板52相对设置于所述第一目标转接板51下侧并与所述悬吊目标9固定连接;The second
所述第一目标转接板51底部设置有丝杠541,具体的,所述丝杠541沿其轴线方向水平设置于所述第一目标转接板51底部;A
所述角度和偏心调整装置还包括:至少一丝杠支撑端543、至少一丝杠固定端544;所述丝杠支撑端543与所述丝杠固定端544成对设置,并分别设置于所述丝杠541沿轴线方向的两端;所述丝杠541通过丝杠支撑端543、丝杠固定端544与所述第一目标转接板51连接,所述丝杠支撑端543与所述丝杠固定端544固定安装于所述第一目标转接板51下部,所述丝杠支撑端543与所述丝杠541沿轴线方向第一端之间通过轴承连接;所述丝杠固定端544与所述丝杠541沿轴线方向第二端之间通过轴承连接;所述丝杠支撑端543与所述丝杠固定端544对所述丝杠541进行悬吊并对丝杠541的绕轴运动进行导向,使调节过程更加顺畅;The angle and eccentricity adjustment device further includes: at least one
所述偏摆角度与偏心位置还包括至少一固定盘532,所述丝杠541沿轴线方向一端与固定盘532固定连接,手轮531偏心安装在固定盘532上,通过摇动手轮531,进而带动固定盘532将转矩传递到丝杠541上,驱动丝杠541转动;The yaw angle and eccentric position also include at least one
一丝杠螺母座542套设于丝杠541外侧,随着丝杠541的转动,所述丝杠螺母座542沿水平方向移动;所述丝杠螺母座542直接或间接与所述第二目标转接板52连接,所述丝杠螺母座542适于带动所述第二目标转接板52与所述第一目标转接板51发生相对运动。A lead
所述第一目标转接板51底部固定连接有至少一导轨545,所述丝杠螺母座542通过滑块546与所述导轨545相对滑动连接,所述滑块546安装于所述导轨545之上,对所述丝杠螺母座542的运动起到导向作用;At least one
所述角度和偏心调整装置5共包括两组丝杠541,及对应的两组丝杠支撑端543、丝杠固定端544、丝杠螺母座542;The angle and
其中,第一组丝杠螺母座上连接至少一块三角板554,所述三角板554与第一组丝杠螺母座通过至少两个固定轴连接且不发生相对转动;第二组丝杠螺母座上连接至少一块连杆552;所述连杆552与第二组丝杠螺母座通过一根销轴551连接且能够发生相对转动;作为本发明的具体实现形式,第一组丝杠螺母座542上连接两块三角板554,第二组丝杠螺母座542上连接两块连杆552;Among them, at least one
所述三角板554与所述两块连杆552均通过转接件553与第二目标转接板52连接,所述第二目标转接板52与所述悬吊目标固定连接。The
所述第一组丝杠螺母座与所述三角板554固定连接,较佳的,所述第一组丝杠螺母座与所述三角板554通过至少两个固定轴固定,使所述第一组丝杠螺母座与所述三角板554不能够发生相对转动;The first group of screw nut seats and the
所述第二组丝杠螺母座与连杆552通过一根销轴551连接,所述第二组丝杠螺母座与连杆552能够发生相对转动;The second group of screw nut seats and the connecting
所述三角板554以及所述连杆552均与所述转接件553通过一根销轴551转动连接;所述三角板554以及所述连杆552均能够与所述转接件553发生相对转动;The
所述第一组丝杠螺母座与所述第二组丝杠螺母座在两组丝杠转动相同角度时移动相同距离,使所述角度和偏心调整装置带动所述悬吊目标9平移;The first set of lead screw nut seats and the second set of lead screw nut seats move the same distance when the two sets of lead screws rotate at the same angle, so that the angle and eccentric adjustment device drives the suspension target 9 to translate;
所述第一组丝杠螺母座与所述第二组丝杠螺母座在两组丝杠转动不同角度时移动不同距离,使所述连杆552同时绕所述第二组丝杠螺母座的销轴和所述转接件553的销轴转动,而所述三角板554仅能够绕所述转接件553的销轴转动,进而带动第二目标转接板52发生角度a°的偏转。The first set of lead screw nut seats and the second set of lead screw nut seats move by different distances when the two sets of lead screws rotate at different angles, so that the connecting
结合图20-图21所示,通过旋转手轮531,带动丝杠541转动,当两根丝杠转动相同角度时,即所述第一组丝杠螺母座与所述第二组丝杠螺母座移动相同距离,则所述角度和偏心调整装置带动所述悬吊目标9平移,可以调节悬吊目标9的重心;20-21, by rotating the
当两根丝杠转动不同角度时,所述第一组丝杠螺母座与所述第二组丝杠螺母座移动不同距离,则所述连杆552同时绕所述第二组丝杠螺母座的销轴和所述转接件553的销轴转动,而所述三角板554仅能够绕所述转接件553的销轴转动,从而使第二目标转接板52发生角度a°的偏转,进而调节悬吊目标9的角度。When the two lead screws rotate at different angles, the first set of lead screw nut seats and the second set of lead screw nut seats move by different distances, and the connecting
较佳的,本实施例中,所述固定盘532与所述丝杠固定端544转动连接;Preferably, in this embodiment, the fixing
较佳的,所述固定盘532上还设置有孔,并且与之相连的丝杠固定端上攻螺纹孔,当悬吊目标9调节到目标位置或重心后,通过所述孔将所述固定盘532与所述丝杠固定端544固定,使丝杠541固定在目标位置或重心;通过在手轮531处增加固定板,调节到目标角度或重心后可保持该状态;Preferably, the fixing
较佳的,所述销轴551通过销轴锁紧件555进行锁紧,避免悬吊目标在转动过程中产生偏移;Preferably, the
较佳的,所述销轴551外套有铜套,降低转动的摩擦力。Preferably, the
较佳的,所述角度和偏心调整装置使用滑块546与导轨545进行导向,保证丝杠螺母座移动时的流畅度。Preferably, the angle and eccentricity adjustment device is guided by the
较佳的,转接件553为U型转接件,避免悬臂梁结构,加大结构强度。Preferably, the
在一可选实施例中,对转接件内的销轴一端安装销轴锁紧件,并且留有余量,使用螺钉连接时利用摩擦力对销轴进行固定。In an optional embodiment, a pin shaft locking member is installed on one end of the pin shaft in the adapter with a margin, and friction force is used to fix the pin shaft when screwing is used.
本发明提供的所述悬吊起旋机构,可通过调节手柄调节悬吊目标的偏摆角度与重心位置,满足不同的实验需求;调节方法简单方便,只需摇动手轮,不用拆装机构;丝杠部54具有导向,使调节过程更加顺畅;The suspension hoisting mechanism provided by the present invention can adjust the yaw angle and the position of the center of gravity of the suspension target by adjusting the handle, so as to meet different experimental requirements; The screw part 54 has a guide, which makes the adjustment process smoother;
本发明提供的悬吊起旋机构采用手自动一体化欠驱动设计,具备起旋、刚柔约束转换、制动、悬吊位姿调整等多种功能;起旋转速可控,并具备制动功能,操作简单,安全可靠;同时具有手动与电机两种驱动方式,通过配置离合器使两种驱动方式互不干涉;The suspension hoisting mechanism provided by the present invention adopts a hand-automatic integrated under-drive design, and has various functions such as hoisting, rigid-flexible constraint conversion, braking, and suspension posture adjustment; the hoisting speed is controllable, and it has braking Function, simple operation, safety and reliability; at the same time, it has two driving modes, manual and motor, and the two driving modes do not interfere with each other by configuring the clutch;
本发明提供的悬吊起旋机构既可实现悬吊目标绕自旋轴产生自旋,又可实现悬吊目标自旋轴产生摆动,并任意切换对悬吊目标的刚性约束和柔性约束状态,从而实现对在轨故障卫星某一种可能存在的姿态翻滚状态的地面模拟。The suspension-spinning mechanism provided by the present invention can not only realize the suspension target to generate spin around the spin axis, but also realize the suspension target's spin axis to swing, and arbitrarily switch the rigid constraint and flexible constraint states on the suspension target, In this way, the ground simulation of a possible state of attitude rollover of a faulty satellite in orbit can be realized.
一种微重力翻滚状态模拟系统,所述微重力翻滚状态模拟系统采用上述所述的悬吊起旋机构,所述悬吊起旋机构通过桁架连接板13安装设置于桁架11上,并与电气箱12进行电连接,以实现对所述悬吊起旋机构的操作控制。A microgravity tumbling state simulation system, the microgravity tumbling state simulation system adopts the above-mentioned suspension and swivel mechanism. The
作为空间任务实施的地面验证关键部分,地面试验的目标是验证空间任务方案的合理性和技术可行性,而其成功与否在很大程度上取决于所采用的验证方法对其空间任务实施过程特征是否是真实的反映,因此,本发明提供的微重力翻滚状态模拟系统对空间目标在轨状态的地面模拟具有非常重要的工程意义。As a key part of the ground verification of space mission implementation, the goal of ground test is to verify the rationality and technical feasibility of the space mission scheme, and its success depends largely on the verification method used to implement its space mission process. Whether the feature is a real reflection, therefore, the microgravity roll state simulation system provided by the present invention has very important engineering significance for the ground simulation of the space target on-orbit state.
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the scope of the present invention. within the scope of protection.
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008133187A1 (en) * | 2007-04-19 | 2008-11-06 | Kokusai Keisokuki Kabushiki Kaisha | General-purpose test device, linear actuator, and twist test device |
CN106081173A (en) * | 2016-07-19 | 2016-11-09 | 哈尔滨工业大学 | Three-dimensional actively suspension spacecraft microgravity analog |
CN206696086U (en) * | 2016-12-08 | 2017-12-01 | 吉林大学 | Eccentric load stretch bending in-situ testing device under temperature match curing conditions |
CN107758506A (en) * | 2016-08-19 | 2018-03-06 | 中石化重型起重运输工程有限责任公司 | Spliced operating platform |
CN108761855A (en) * | 2018-05-04 | 2018-11-06 | 芜湖良匠机械制造有限公司 | A kind of apparatus for correcting for position of glass substrate correction |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008133187A1 (en) * | 2007-04-19 | 2008-11-06 | Kokusai Keisokuki Kabushiki Kaisha | General-purpose test device, linear actuator, and twist test device |
CN106081173A (en) * | 2016-07-19 | 2016-11-09 | 哈尔滨工业大学 | Three-dimensional actively suspension spacecraft microgravity analog |
CN107758506A (en) * | 2016-08-19 | 2018-03-06 | 中石化重型起重运输工程有限责任公司 | Spliced operating platform |
CN206696086U (en) * | 2016-12-08 | 2017-12-01 | 吉林大学 | Eccentric load stretch bending in-situ testing device under temperature match curing conditions |
CN108761855A (en) * | 2018-05-04 | 2018-11-06 | 芜湖良匠机械制造有限公司 | A kind of apparatus for correcting for position of glass substrate correction |
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