CN104743144A - Variable-cross-section spiral winding type gas-filled capturing manipulator - Google Patents
Variable-cross-section spiral winding type gas-filled capturing manipulator Download PDFInfo
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- CN104743144A CN104743144A CN201510139311.0A CN201510139311A CN104743144A CN 104743144 A CN104743144 A CN 104743144A CN 201510139311 A CN201510139311 A CN 201510139311A CN 104743144 A CN104743144 A CN 104743144A
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- 238000004804 winding Methods 0.000 title 1
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 230000007423 decrease Effects 0.000 claims abstract description 9
- 239000000463 material Substances 0.000 claims description 16
- 239000002131 composite material Substances 0.000 claims description 5
- 229920005549 butyl rubber Polymers 0.000 claims description 3
- 229920001971 elastomer Polymers 0.000 claims description 3
- 125000003118 aryl group Chemical group 0.000 claims description 2
- 238000005485 electric heating Methods 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims 1
- 230000007246 mechanism Effects 0.000 abstract description 10
- 238000005516 engineering process Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 6
- 210000000078 claw Anatomy 0.000 description 2
- 229920006231 aramid fiber Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
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Abstract
一种变截面螺旋缠绕式充气抓捕手,属于航天技术领域,解决了现有的空间目标抓捕机构存在的问题,它包含一根螺旋形的充气管,充气管的螺旋半径由后端至前端递减,充气管的横截面半径由后端至前端递减;充气管的管壁由内到外依次为气密层、承力层、加热层和防滑层;在充气管的外侧面设置有卷簧,卷簧的自由卷曲方向与充气管的螺旋方向相反,本发明用于抓捕空间大尺寸非合作目标。
A variable cross-section helically wound inflatable catcher belongs to the field of aerospace technology and solves the problems existing in the existing space target catch mechanism. The front end decreases, and the cross-sectional radius of the inflatable tube decreases from the rear end to the front end; the tube wall of the inflatable tube is an airtight layer, a load-bearing layer, a heating layer and an anti-skid layer from the inside to the outside; Spring, the free coiling direction of the coil spring is opposite to the helical direction of the inflatable tube, and the invention is used to capture large-sized non-cooperative targets in space.
Description
技术领域 technical field
本发明属于航天技术领域,具体涉及一种变截面螺旋缠绕式充气抓捕手。 The invention belongs to the field of aerospace technology, and in particular relates to a helically wound inflatable catcher with variable cross-section.
背景技术 Background technique
对空间目标(包括合作目标和非合作目标)进行在轨操作和服务需要有抓捕机构完成目标的在轨抓捕、释放及相对固定等操作;现有的空间目标抓捕机构主要采用机械式手爪机构,可用于实现空间合作目标的抓捕。但利用机械式手爪抓捕机构进行非合作目标的抓捕,包括未安装合作抓持机构的己方飞行器、己方装置合作部件发生故障或失效卫星、对方航天器、空间大尺寸碎片等,则将大量增加抓捕机构的尺寸和关节数量,增大了抓捕机构及其控制系统的复杂程度、整体质量和操作难度,降低了系统的可靠性,增加了制造和发射成本,而且容易对目标造成损伤。 The on-orbit operation and service of space targets (including cooperative targets and non-cooperative targets) requires a capture mechanism to complete the on-orbit capture, release, and relative fixation of the target; the existing space target capture mechanisms mainly use mechanical The claw mechanism can be used to realize the capture of space cooperation targets. However, if the mechanical claw capture mechanism is used to capture non-cooperative targets, including one's own aircraft that is not equipped with a cooperative grasping mechanism, a malfunctioning or invalid satellite of one's own device's cooperative components, the opponent's spacecraft, and large-scale debris in space, etc., it will A large increase in the size and number of joints of the capture mechanism increases the complexity, overall quality and operational difficulty of the capture mechanism and its control system, reduces the reliability of the system, increases the cost of manufacturing and launching, and is easy to cause damage to the target. damage.
发明内容 Contents of the invention
本发明的目的是为了解决现有的空间目标抓捕机构存在的上述问题,提供了一种变截面螺旋缠绕式充气抓捕手,其技术方案如下: The object of the present invention is to solve the above-mentioned problems existing in the existing space target capture mechanism, and to provide a variable cross-section helically wound inflatable capture hand, whose technical scheme is as follows:
一种变截面螺旋缠绕式充气抓捕手,它包含一根螺旋形的充气管,充气管的螺旋半径由后端至前端递减,充气管的横截面半径由后端至前端递减;充气管的管壁由内到外依次为气密层、承力层、加热层和防滑层,气密层材料为丁基橡胶薄膜材料,保证抓捕手内充气压力的稳定性;承力层材料为芳纶纤维复合材料,是承担抓捕手充气压力的主要结构;加热层为电热丝,保证抓捕手在空间低温条件下结构内部气压的稳定性及材料性能;防滑层采用防滑橡胶材料,直接与目标接触的材料层,用来增大目标体与抓捕手间接触面的摩擦力,可防止目标滑脱,可以仅在充气管的内侧面设置防滑层,减小整体质量;在充气管的外侧面设置有卷簧,卷簧的自由卷曲方向与充气管的螺旋方向相反。 A variable-section helically wound inflatable catcher, which includes a helical inflatable tube, the helical radius of the inflatable tube decreases from the rear end to the front end, and the cross-sectional radius of the inflatable tube decreases from the rear end to the front end; the inflatable tube The pipe wall is composed of airtight layer, load-bearing layer, heating layer and anti-skid layer from inside to outside. The material of the air-tight layer is butyl rubber film material to ensure the stability of the inflation pressure in the catcher; the material of the load-bearing layer is aromatic The nylon fiber composite material is the main structure that bears the inflation pressure of the catcher; the heating layer is an electric heating wire to ensure the stability of the air pressure inside the structure and the material performance of the catcher under the condition of low temperature in space; the anti-slip layer is made of non-slip rubber material, The material layer in contact with the target is used to increase the friction of the contact surface between the target body and the catcher, which can prevent the target from slipping, and an anti-skid layer can be set only on the inner side of the inflatable tube to reduce the overall quality; on the outside of the inflatable tube A coil spring is arranged on the side, and the free coiling direction of the coil spring is opposite to the helical direction of the inflatable tube.
本发明的有益效果为:可对较大尺寸的非合作目标进行抓捕;不需配合安装在目标体上的抓持机构;抓捕形式灵活;可从多个部位上进行目标的抓捕,抓捕过程可靠;对于目标的形状及尺寸有极大的适应能力;抓捕目标后抓捕手在充气压力作用下具有足够刚度,且抓捕手采用变截面结构,进一步增大抓捕手刚度,从而使得抓捕手与被抓目标间形成硬连接,便于对目标进行移动、固定等操作;通过充气和放气控制抓捕过程,控制方式简单可靠;发射体积小、重量轻;充气抓捕手可自动卷曲折叠,可实现目标的释放和多次抓捕;抓捕手采用柔性复合材料,不会对目标造成损伤。 The beneficial effects of the present invention are: it is possible to capture large-sized non-cooperative targets; it does not need to cooperate with the grasping mechanism installed on the target body; the capture form is flexible; the target can be captured from multiple positions, The capture process is reliable; it has great adaptability to the shape and size of the target; after capturing the target, the catcher has sufficient rigidity under the action of inflation pressure, and the catcher adopts a variable cross-section structure to further increase the rigidity of the catcher , so that a hard connection is formed between the catcher and the caught target, which is convenient for moving and fixing the target; the capture process is controlled by inflating and deflated, and the control method is simple and reliable; the launch volume is small and light; the inflatable capture The hand can be curled and folded automatically, which can realize the release of the target and multiple captures; the capture hand is made of flexible composite materials, which will not cause damage to the target.
附图说明:Description of drawings:
图1是本发明的结构示意图; Fig. 1 is a structural representation of the present invention;
图2是充气管的横截面示意图; Fig. 2 is a schematic cross-sectional view of an inflatable tube;
图3是抓捕过程示意图。 Figure 3 is a schematic diagram of the capture process.
具体实施方式:Detailed ways:
参照图1、图2和图3,一种变截面螺旋缠绕式充气抓捕手,它包含一根螺旋形的充气管1,充气管1的螺旋半径由后端至前端递减,充气管1的横截面半径由后端至前端递减;充气管1的管壁由内到外依次为气密层1-1、承力层1-2、加热层1-3和防滑层1-4,气密层1-1材料为丁基橡胶薄膜材料,保证抓捕手内充气压力的稳定性;承力层1-2材料为芳纶纤维复合材料,是承担抓捕手充气压力的主要结构;加热层1-3为电热丝,保证抓捕手在空间低温条件下结构内部气压的稳定性及材料性能;防滑层1-4采用防滑橡胶材料,直接与目标接触的材料层,用来增大目标体与抓捕手间接触面的摩擦力,可防止目标滑脱,可以仅在充气管1的内侧面设置防滑层1-4,减小整体质量;在充气管1的外侧面设置有卷簧2,卷簧2的自由卷曲方向与充气管1的螺旋方向相反。 Referring to Fig. 1, Fig. 2 and Fig. 3, a variable cross-section helically wound inflatable catcher includes a helical inflatable tube 1, the spiral radius of the inflatable tube 1 decreases from the rear end to the front end, and the inflatable tube 1 The cross-sectional radius decreases from the rear end to the front end; the tube wall of the inflatable tube 1 is an airtight layer 1-1, a load-bearing layer 1-2, a heating layer 1-3 and an anti-slip layer 1-4 from the inside to the outside, and the airtight The material of layer 1-1 is butyl rubber film material, which ensures the stability of the inflation pressure in the catcher; the material of load-bearing layer 1-2 is aramid fiber composite material, which is the main structure that bears the inflation pressure of the catcher; the heating layer 1-3 are heating wires to ensure the stability and material performance of the internal air pressure of the catcher under the condition of low temperature in space; the anti-slip layer 1-4 is made of anti-slip rubber material, and the material layer directly in contact with the target is used to increase the size of the target. The friction force between the contact surface with the catcher can prevent the target from slipping, and the anti-skid layer 1-4 can be set only on the inner side of the inflatable tube 1 to reduce the overall quality; the outer side of the inflatable tube 1 is provided with a coil spring 2, The free coiling direction of the coil spring 2 is opposite to the helical direction of the inflatable tube 1 .
充气管1的前端直接压扁粘接封闭,呈扁端头结构,使充气管1泄气后更容易在卷簧2的驱动下卷曲。 The front end of the inflatable tube 1 is directly flattened and sealed by bonding, and has a flat end structure, so that the inflatable tube 1 is more likely to be curled under the drive of the coil spring 2 after the gas is deflated.
在充气管1的后端设置有气嘴。 An air nozzle is arranged at the rear end of the inflation pipe 1 .
使用方法及原理:将充气管1后端与飞行器的机械伸缩臂连接,气嘴与充放气设备连接,加热层1-3与加热控制电路连接,充气管1采用柔性复合材料制造,在无充气压力状态下,卷簧2驱动充气管1卷曲折叠;对目标进行抓捕时,利用充放气设备对充气管1进行充气,充气压力驱动充气管1逐渐螺旋式展开对目标进行缠绕抓捕,由于充气管1的螺旋半径由后端至前端递减,所以抓捕目标的外形尺寸在充气管1的前端螺旋半径和后端螺旋半径之间的范围内均可以被牢固缠绕;需要释放目标时,对充气抓捕手进行放气,在卷簧2的作用下,带动充气管1卷曲回缩,将目标释放。 Method of use and principle: connect the rear end of the inflatable tube 1 with the mechanical telescopic arm of the aircraft, connect the air nozzle with the inflation and deflation equipment, connect the heating layers 1-3 with the heating control circuit, and the inflatable tube 1 is made of flexible composite materials. In the state of inflation pressure, the coil spring 2 drives the inflation tube 1 to curl and fold; when capturing the target, use the inflation and deflation equipment to inflate the inflation tube 1, and the inflation pressure drives the inflation tube 1 to spirally expand gradually to wrap and capture the target , since the helical radius of the inflatable tube 1 decreases from the rear end to the front end, the external dimensions of the captured target can be firmly wound within the range between the front end helical radius and the rear end helical radius of the inflatable tube 1; when the target needs to be released , the inflatable catcher is deflated, and under the action of the coil spring 2, the inflatable tube 1 is driven to curl and retract, and the target is released.
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109732586A (en) * | 2019-01-18 | 2019-05-10 | 哈尔滨工业大学 | A multi-stage growth soft robot |
CN110615124A (en) * | 2019-09-29 | 2019-12-27 | 南京航空航天大学 | Wound form space capture device |
CN113696172A (en) * | 2021-09-08 | 2021-11-26 | 哈尔滨工业大学 | Inflatable grasper capable of rigidizing |
CN114083541A (en) * | 2021-12-07 | 2022-02-25 | 哈尔滨工业大学 | A soft-body robot grasping device with visual feedback |
CN114211488A (en) * | 2021-12-07 | 2022-03-22 | 哈尔滨工业大学 | Flexible robot control method based on fuzzy control algorithm |
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CN101913270A (en) * | 2010-07-23 | 2010-12-15 | 哈尔滨工业大学 | A foldable-deployable shape memory support tube and its preparation method |
CN203954673U (en) * | 2014-05-30 | 2014-11-26 | 万文山 | A kind of formula toy whistle that stucks out one's tongue |
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2015
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Patent Citations (4)
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US4815782A (en) * | 1986-12-08 | 1989-03-28 | United Technologies Corporation | Grappling device |
CN1672914A (en) * | 2005-04-08 | 2005-09-28 | 哈尔滨工业大学 | Composite thermosetting film for inflated spatial expanded structure and its making and rigidizing process |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109732586A (en) * | 2019-01-18 | 2019-05-10 | 哈尔滨工业大学 | A multi-stage growth soft robot |
CN110615124A (en) * | 2019-09-29 | 2019-12-27 | 南京航空航天大学 | Wound form space capture device |
CN110615124B (en) * | 2019-09-29 | 2022-05-03 | 南京航空航天大学 | Wound form space capture device |
CN113696172A (en) * | 2021-09-08 | 2021-11-26 | 哈尔滨工业大学 | Inflatable grasper capable of rigidizing |
CN114083541A (en) * | 2021-12-07 | 2022-02-25 | 哈尔滨工业大学 | A soft-body robot grasping device with visual feedback |
CN114211488A (en) * | 2021-12-07 | 2022-03-22 | 哈尔滨工业大学 | Flexible robot control method based on fuzzy control algorithm |
CN114211488B (en) * | 2021-12-07 | 2024-03-01 | 哈尔滨工业大学 | Flexible robot control method based on fuzzy control algorithm |
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Application publication date: 20150701 |