[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN113788164B - Space truss connecting device with bidirectional locking function - Google Patents

Space truss connecting device with bidirectional locking function Download PDF

Info

Publication number
CN113788164B
CN113788164B CN202111072365.1A CN202111072365A CN113788164B CN 113788164 B CN113788164 B CN 113788164B CN 202111072365 A CN202111072365 A CN 202111072365A CN 113788164 B CN113788164 B CN 113788164B
Authority
CN
China
Prior art keywords
tenon
crank
groove
rack
hole
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.)
Expired - Fee Related
Application number
CN202111072365.1A
Other languages
Chinese (zh)
Other versions
CN113788164A (en
Inventor
戴野
相朝芳
高延华
张启昊
曲文印
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin University of Science and Technology
Original Assignee
Harbin University of Science and Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Harbin University of Science and Technology filed Critical Harbin University of Science and Technology
Priority to CN202111072365.1A priority Critical patent/CN113788164B/en
Publication of CN113788164A publication Critical patent/CN113788164A/en
Application granted granted Critical
Publication of CN113788164B publication Critical patent/CN113788164B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A40/00Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
    • Y02A40/10Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture
    • Y02A40/25Greenhouse technology, e.g. cooling systems therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Joining Of Building Structures In Genera (AREA)

Abstract

The invention discloses a bidirectional-locking space truss connecting device which comprises a shell, a rotating mechanism and a transmission mechanism, wherein the shell comprises an elastic tenon, a tenon connecting section, a sliding chute, a connecting plate, an opening, a rack groove, a small hole and a semicircular groove, the rotating mechanism comprises a guide rod, a connecting rod, a spring and a crank, and the transmission mechanism comprises a rack, a rotating block and a set screw. The connecting device can simultaneously complete the bidirectional locking of different connected parts at two ends, one end can be connected with the ball head through the tenon, and the other end is connected with the truss rod through the axial joint.

Description

一种双向锁紧的空间桁架连接装置A two-way locking space truss connection device

技术领域technical field

本发明属于桁架结构技术领域,具体涉及一种双向锁紧的空间桁架连接装置。The invention belongs to the technical field of truss structures, and in particular relates to a two-way locking space truss connection device.

背景技术Background technique

随着航天技术的蓬勃发展,以及人类对太空资源探索、开发需求的进一步增加,相应的大型空间结构的规模、在轨操作量级以及任务复杂程度也在急剧增加。由于大型的空间设施难以一次性发射升空,需要分模块发射后再进行在轨组装,因此会产生相应的在轨装配等问题。With the vigorous development of aerospace technology and the further increase of human demand for the exploration and development of space resources, the scale of corresponding large-scale space structures, the magnitude of on-orbit operations, and the complexity of tasks have also increased dramatically. Since large space facilities are difficult to launch at one time, they need to be launched in separate modules and then assembled on-orbit, so there will be problems such as corresponding on-orbit assembly.

目前,应用较多的空间组装方式有宇航员舱外装配以及机械臂组装。由于太空的特殊环境,使得在轨装配任务对航天员的安全会构成极大威胁,因此亟需一种简单高效的桁架结构件,以减少装配时间、提高装配效率、保证装配安全。At present, the most widely used space assembly methods include astronaut extravehicular assembly and robotic arm assembly. Due to the special environment of space, the on-orbit assembly task will pose a great threat to the safety of astronauts. Therefore, a simple and efficient truss structure is urgently needed to reduce assembly time, improve assembly efficiency, and ensure assembly safety.

发明内容SUMMARY OF THE INVENTION

有鉴于此,本发明提供了一种双向锁紧的空间桁架连接装置,目的就是为了解决上述之不足。In view of this, the present invention provides a two-way locking space truss connection device, which aims to solve the above shortcomings.

为解决上述技术问题,本发明提出了一种双向锁紧的空间桁架连接装置,其特征在于,所述双向锁紧的空间桁架连接装置包括:壳体、转动机构、传动机构;所述空间桁架连接装置一端可通过弹性榫头连接球头,所述球头表面设有均匀分布的阶梯状榫头孔,所述阶梯状榫头孔大径与弹性榫头外径尺寸相同,小径与榫头连接段外径尺寸相同,另一端通过轴向接头连接桁架杆,所述轴向接头一端安装有半圆环凸台,凸台上有与插销直径相同的销孔,所述轴向接头另一端为螺纹孔。In order to solve the above technical problems, the present invention proposes a bidirectional locking space truss connection device, which is characterized in that the bidirectional locking space truss connection device includes: a shell, a rotating mechanism, and a transmission mechanism; the space truss One end of the connecting device can be connected to the ball head through an elastic tenon. The surface of the ball head is provided with stepped tenon holes evenly distributed. Similarly, the other end is connected to the truss rod through an axial joint, one end of the axial joint is installed with a semi-circular boss, the boss has a pin hole with the same diameter as the pin, and the other end of the axial joint is a threaded hole.

优选地,所述壳体包括弹性榫头、榫头连接段、滑槽、连接板、开口、齿条槽、小孔、半圆环凹槽;所述壳体一端为弹性榫头,另一端为半圆环凹槽,所述连接板上安装有转动轴,所述连接板与所述壳体外圈接触的部分开设有开口,所述开口用于限制曲柄的转动角度,且其宽度与曲柄的宽度相同,与所述开口相对的壳体另一侧为齿条槽,所述壳体外圈靠近半圆环凹槽一侧开设有小孔,所述半圆环凹槽一侧有细薄挡板。Preferably, the casing includes an elastic tenon, tenon connecting section, chute, connecting plate, opening, rack groove, small hole, and semicircular groove; one end of the casing is an elastic tenon, and the other end is a semicircle a ring groove, a rotating shaft is mounted on the connecting plate, and an opening is formed at the part of the connecting plate in contact with the outer ring of the casing, the opening is used to limit the rotation angle of the crank, and its width is the same as the width of the crank The other side of the casing opposite to the opening is a rack groove, the outer ring of the casing is provided with a small hole on the side close to the semi-circular groove, and the side of the semi-circular groove is provided with a thin baffle.

优选地,所述转动机构包括导杆、连杆、弹簧、曲柄;所述导杆外径与所述榫头连接段内径尺寸与相同,所述导杆一端侧面与所述连杆通过铰链连接,底面与弹簧接触,所述弹簧安装在滑槽内,且一端固定在连接板上,所述连杆另一端通过铰链与曲柄连接,所述曲柄可以通过连杆带动导杆在滑槽内移动从而压缩或释放弹簧,所述曲柄包括曲柄把手、铰链槽、轴心孔、齿轮,所述轴心孔与连接板上的转动轴配合,通过转动曲柄把手使曲柄绕转动轴旋转一定角度从而使顶端的齿轮绕转动轴转动一定角度。Preferably, the rotating mechanism includes a guide rod, a connecting rod, a spring, and a crank; the outer diameter of the guide rod is the same as the inner diameter of the tenon connecting section, and one end side of the guide rod is connected with the connecting rod through a hinge, The bottom surface is in contact with the spring, the spring is installed in the chute, and one end is fixed on the connecting plate, and the other end of the connecting rod is connected with the crank through the hinge, and the crank can drive the guide rod to move in the chute through the connecting rod. Compress or release the spring, the crank includes a crank handle, a hinge slot, a shaft hole, and a gear. The shaft hole is matched with the rotating shaft on the connecting plate. By turning the crank handle, the crank rotates around the rotating shaft at a certain angle so that the top end The gear rotates a certain angle around the axis of rotation.

优选地,所述传动机构包括齿条、转动块、紧定螺钉;所述齿条两侧开设有与齿条槽尺寸相同的凹槽,并通过卡槽安装在所述壳体上,所述齿条与所述曲柄上的齿轮相啮合,所述转动块一端为环形槽,所述齿条一端镶嵌在环形槽内,所述转动块另一端为直径较小的插销,所述插销可插入到轴向接头的销孔内完成周向固定,防止转动,所述转动块外表面开设有曲面槽,所述曲面槽内安装有紧定螺钉可在曲面槽内滑动。Preferably, the transmission mechanism includes a rack, a rotating block, and a set screw; grooves of the same size as the rack grooves are provided on both sides of the rack, and are installed on the housing through the clamping grooves, and the The rack is meshed with the gear on the crank, one end of the rotating block is an annular groove, one end of the rack is embedded in the annular groove, and the other end of the rotating block is a pin with a smaller diameter, the pin can be inserted The circumferential fixing is completed in the pin hole of the axial joint to prevent rotation. The outer surface of the rotating block is provided with a curved groove, and a set screw is installed in the curved groove to slide in the curved groove.

本发明相对于现有技术取得了以下技术效果:The present invention has achieved the following technical effects with respect to the prior art:

1.该连接装置可以同时完成对两端不同被连接零件的双向锁紧。1. The connecting device can simultaneously complete the two-way locking of different connected parts at both ends.

2.该连接装置通用性强,连接装置两端可以连接不同类型的球头与不同尺寸的桁杆,只需要保证不同球头的榫头孔尺寸一致即可,径向接头的螺纹孔直径也可以根据不同尺寸的桁架而变化。2. The connecting device has strong versatility. Both ends of the connecting device can connect different types of ball heads and truss rods of different sizes. It only needs to ensure that the tenon holes of different ball heads are the same size, and the diameter of the threaded hole of the radial joint can also be Varies according to different sizes of trusses.

3.连接方式简单高效,且可以保证连接刚度,避免脱落。3. The connection method is simple and efficient, and the connection rigidity can be guaranteed to avoid falling off.

4.装配过程简单,不需要用到繁多的安装与固定方式,只需手动拨动曲柄便可实现安装与拆卸,非常适合太空微重力情况下的桁架装配工作。4. The assembly process is simple, and there is no need to use many installation and fixing methods. The installation and disassembly can be realized by manually turning the crank, which is very suitable for the truss assembly work in the microgravity of space.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见的,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the accompanying drawings that are used in the description of the embodiments or the prior art. Obviously, the drawings in the following description are only These are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained from these drawings without creative efforts.

图1为空间桁架连接装置结构示意图;Figure 1 is a schematic structural diagram of a space truss connection device;

图2为壳体剖面结构图;Figure 2 is a cross-sectional structural diagram of the shell;

图3为曲柄三维示意图;Figure 3 is a three-dimensional schematic diagram of a crank;

图4为齿条三维示意图;Figure 4 is a three-dimensional schematic diagram of a rack;

图5为转动块三维示意图;5 is a three-dimensional schematic diagram of a rotating block;

图6为轴向接头结构示意图;Figure 6 is a schematic diagram of the axial joint structure;

图7为球头结构示意图;Figure 7 is a schematic view of the ball head structure;

图8为球头装配示意图;Figure 8 is a schematic diagram of ball head assembly;

图9为空间桁架模块装配示意图;9 is a schematic diagram of the assembly of the space truss module;

在附图中:1、壳体;11、弹性榫头;12、榫头连接段;13、滑槽;14、连接板;15、转动轴;16、开口;17、齿条槽;18、小孔;19、半圆环凹槽;2、转动机构;21、导杆;22、连杆;23、弹簧;24、曲柄;241、曲柄把手;242、铰链槽;243、轴心孔;244、齿轮;3、传动机构;31、齿条;311、凹槽;32、转动块;321、环形槽;322、曲面槽;323、插销;33、紧定螺钉;4、球头;41、榫头孔;5、轴向接头;51、半圆环凸台;52、销孔;53、螺纹孔;6、桁架杆。In the drawings: 1. Housing; 11. Elastic tenon; 12. Tenon connecting section; 13. Chute; 14. Connecting plate; 15. Rotating shaft; 16. Opening; 17. Rack slot; ; 19, semi-circular groove; 2, rotating mechanism; 21, guide rod; 22, connecting rod; 23, spring; 24, crank; 241, crank handle; 242, hinge groove; 243, shaft hole; 244, Gear; 3, Transmission mechanism; 31, Rack; 311, Groove; 32, Rotating block; 321, Annular groove; 322, Curved groove; 323, Latch; 33, Set screw; 4, Ball head; Hole; 5. Axial joint; 51. Half-circle boss; 52. Pin hole; 53. Threaded hole; 6. Truss rod.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

实施例Example

请参阅图1-7,本发明公开了一种双向锁紧的空间桁架连接装置,包括:壳体1、转动机构2、传动机构3;空间桁架连接装置一端可通过弹性榫头11连接球头4,球头表面设有均匀分布的阶梯状榫头孔41,阶梯状榫头孔42大径与弹性榫头22外径尺寸相同,小径与榫头连接段12外径尺寸相同,另一端通过轴向接头5连接桁架杆6,轴向接头5一端安装有半圆环凸台51,半圆环凸台51上有与插销323直径相同的销孔52,轴向接头5另一端为螺纹孔53。1-7, the present invention discloses a two-way locking space truss connection device, including: a shell 1, a rotating mechanism 2, a transmission mechanism 3; one end of the space truss connection device can be connected to a ball head 4 through an elastic tenon 11 , the surface of the ball head is provided with evenly distributed stepped tenon holes 41, the large diameter of the stepped tenon hole 42 is the same as the outer diameter of the elastic tenon 22, the small diameter is the same as the outer diameter of the tenon connecting section 12, and the other end is connected by the axial joint 5 In the truss rod 6, one end of the axial joint 5 is installed with a semi-circular boss 51, the semi-circular boss 51 has a pin hole 52 with the same diameter as the plug 323, and the other end of the axial joint 5 is a threaded hole 53.

壳体1包括弹性榫头11、榫头连接段12、滑槽13、连接板14、转动轴15、开口16、齿条槽17、小孔18、半圆环凹槽19;壳体1一端为弹性榫头11,另一端为半圆环凹槽19,连接板14上安装有转动轴15,连接板14与壳体1外圈接触的部分开设有开口16,开口用于限制曲柄24的转动角度,且其宽度与曲柄24的宽度相同,与开口16相对的壳体另一侧为齿条槽17,壳体1外圈靠近半圆环凹槽19一侧开设有小孔18,半圆环凹槽19一侧有细薄挡板。The housing 1 includes an elastic tenon 11, a tenon connecting section 12, a chute 13, a connecting plate 14, a rotating shaft 15, an opening 16, a rack groove 17, a small hole 18, and a semi-circular groove 19; one end of the housing 1 is elastic The tenon 11 has a semi-circular groove 19 at the other end, a rotating shaft 15 is installed on the connecting plate 14, and an opening 16 is formed at the part of the connecting plate 14 in contact with the outer ring of the housing 1, and the opening is used to limit the rotation angle of the crank 24, And its width is the same as the width of the crank 24, the other side of the housing opposite to the opening 16 is the rack groove 17, the outer ring of the housing 1 is provided with a small hole 18 on the side close to the semi-circular groove 19, and the semi-circular concave There is a thin baffle on one side of the groove 19.

转动机构2包括导杆21、连杆22、弹簧23、曲柄24;导杆21外径与所述榫头连接段12内径尺寸与相同,导杆21一端侧面与连杆22通过铰链连接,底面与弹簧23接触,弹簧安装在滑槽13内,且一端固定在连接板14上,连杆22另一端通过铰链与曲柄24连接,曲柄24可以通过连杆22带动导杆21在滑槽13内移动从而压缩或释放弹簧23,曲柄24包括曲柄把手241、铰链槽242、轴心孔243、齿轮244,轴心孔243与连接板14上的转动轴15配合,通过转动曲柄把手241使曲柄24绕转动轴15旋转一定角度从而使顶端的齿轮244绕转动轴15转动一定角度。The rotating mechanism 2 includes a guide rod 21, a connecting rod 22, a spring 23, and a crank 24; the outer diameter of the guide rod 21 is the same as the inner diameter of the tenon connecting section 12, and one side of the guide rod 21 is connected with the connecting rod 22 through a hinge, and the bottom surface is connected to the connecting rod 22 through a hinge. The spring 23 contacts, the spring is installed in the chute 13, and one end is fixed on the connecting plate 14, the other end of the connecting rod 22 is connected with the crank 24 through a hinge, and the crank 24 can drive the guide rod 21 to move in the chute 13 through the connecting rod 22 Thereby, the spring 23 is compressed or released, and the crank 24 includes a crank handle 241, a hinge groove 242, an axial hole 243, and a gear 244. The axial hole 243 is matched with the rotating shaft 15 on the connecting plate 14, and the crank handle 241 is rotated to make the crank 24 go around. The rotating shaft 15 rotates at a certain angle so that the top gear 244 rotates around the rotating shaft 15 at a certain angle.

传动机构3包括齿条31、转动块32、紧定螺钉33;所述齿条31两侧开设有与齿条槽17尺寸相同的凹槽311,并通过卡槽安装在壳体1上,齿条31与曲柄24上的齿轮244相啮合,转动块32一端为环形槽321,齿条31一端镶嵌在环形槽321内,转动块32另一端为直径较小的插销323,插销323可插入到轴向接头5的销孔52内完成周向固定,防止转动,转动块32外表面开设有曲面槽322,曲面槽322内安装有紧定螺钉33可在槽内滑动。The transmission mechanism 3 includes a rack 31, a rotating block 32, and a set screw 33; the two sides of the rack 31 are provided with grooves 311 of the same size as the rack groove 17, and are installed on the casing 1 through the card groove. The bar 31 meshes with the gear 244 on the crank 24. One end of the rotating block 32 is an annular groove 321. The pin hole 52 of the axial joint 5 is circumferentially fixed to prevent rotation. The outer surface of the rotating block 32 is provided with a curved groove 322, and a set screw 33 is installed in the curved groove 322 to slide in the groove.

本发明具体工作过程如下:The concrete working process of the present invention is as follows:

进行空间桁架装配时,拨动曲柄把手241使曲柄24绕转动轴15转动一定角度,曲柄24一端通过连杆22带动导杆21在滑槽13内水平移动,此时,导杆21脱离榫头连接段12进入滑槽13内,弹簧23受到挤压,同时,曲柄24另一端在齿轮244带动下使与之相啮合的齿条31移动至最左端,由于齿条31一端镶嵌在环形槽321内,同时受到紧定螺钉33的限制,使得齿条31的水平移动带动转动块32进行水平方向的移动和沿环形槽方向的转动,此时转动块32另一端的插销323脱离出轴向接头5的插孔52,参见图1所示位置,可进行接头装配工作,由于榫头连接段12是弹性材料,可将弹性榫头11插入球头4的榫头孔41内,另一端将轴向接头5插入连接装置壳体1并旋转180度与细薄挡板接触,完成装配工作。When the space truss is assembled, the crank handle 241 is toggled to make the crank 24 rotate at a certain angle around the rotation axis 15. One end of the crank 24 drives the guide rod 21 to move horizontally in the chute 13 through the connecting rod 22. At this time, the guide rod 21 is disconnected from the tenon connection. The segment 12 enters the chute 13, the spring 23 is squeezed, and at the same time, the other end of the crank 24 is driven by the gear 244 to move the rack 31 engaged with it to the leftmost end, because one end of the rack 31 is embedded in the annular groove 321. At the same time, it is restricted by the set screw 33, so that the horizontal movement of the rack 31 drives the rotating block 32 to move in the horizontal direction and rotate in the direction of the annular groove. 1, the joint assembly can be performed. Since the tenon connecting section 12 is an elastic material, the elastic tenon 11 can be inserted into the tenon hole 41 of the ball head 4, and the axial joint 5 can be inserted into the other end. Connect the device housing 1 and rotate 180 degrees to contact with the thin baffle to complete the assembly work.

接头装配完成后,松开曲柄24,由于弹簧23弹力作用会使导杆21在弹力作用下弹回榫头连接段12,参见图8所示的位置,此时,连接装置壳体1一端的导杆21在弹簧23推力作用下进入弹性连接段12,保证了壳体1与球头4之间的连接安全性,提高连接刚度,另一端通过曲柄24上端齿轮244的带动使转动快32末端的插销323可以旋转着向靠近径向接头5的一端移动,并进入径向接头5的插孔52内,完成周向固定,防止转动,半圆环凸台51保证了连接装置在轴向的连接可靠性,插销323保证了连接装置周向连接的可靠性。After the joint assembly is completed, loosen the crank 24, the guide rod 21 will spring back to the tenon connecting section 12 due to the elastic force of the spring 23, see the position shown in FIG. The rod 21 enters the elastic connecting section 12 under the thrust of the spring 23, which ensures the safety of the connection between the housing 1 and the ball head 4 and improves the connection rigidity. The plug 323 can rotate and move toward the end close to the radial joint 5, and enter the insertion hole 52 of the radial joint 5 to complete the circumferential fixation and prevent rotation. The semi-circular boss 51 ensures the connection of the connecting device in the axial direction. Reliability, the plug 323 ensures the reliability of the circumferential connection of the connecting device.

最终通过桁架杆6将多个接头装配件连接起来形成完整的空间桁架模块,参见图9。Finally, a plurality of joint assemblies are connected by truss rods 6 to form a complete space truss module, see FIG. 9 .

以上所述,仅是本发明较佳实施例而已,并非对本发明的技术范围作任何限制,故凡是依据本发明的技术实质对以上实施例所作的任何细微修改、等同变化与修饰,均仍属于本发明技术方案的范围内。The above are only preferred embodiments of the present invention, and do not limit the technical scope of the present invention. Therefore, any minor modifications, equivalent changes and modifications made to the above embodiments according to the technical essence of the present invention are still within the scope of the present invention. within the scope of the technical solution of the present invention.

Claims (2)

1. A bi-directionally locking space truss attachment apparatus, comprising: the space truss connecting device comprises a shell, a rotating mechanism and a transmission mechanism, wherein one end of the space truss connecting device can be connected with a ball head through an elastic tenon, the surface of the ball head is provided with step-shaped tenon holes which are uniformly distributed, the major diameter of each step-shaped tenon hole is the same as the outer diameter of the elastic tenon, the minor diameter of each step-shaped tenon hole is the same as the outer diameter of a tenon connecting section, the other end of each step-shaped tenon hole is connected with a truss rod through an axial joint, one end of each axial joint is provided with a semicircular boss, each boss is provided with a pin hole with the same diameter as a pin, and the other end of each axial joint is a threaded hole;
the rotating mechanism comprises a guide rod, a connecting rod, a spring and a crank, the outer diameter of the guide rod is the same as the inner diameter of the tenon connecting section, one end of the guide rod is connected with the connecting rod through a hinge, the bottom surface of the guide rod is in contact with the spring, the spring is installed in the chute, one end of the spring is fixed on the connecting plate, the other end of the connecting rod is connected with the crank through a hinge, the crank can drive the guide rod to move in the chute through the connecting rod so as to compress or release the spring, the crank comprises a crank handle, a hinge groove, a shaft center hole and a gear, the shaft center hole is matched with a rotating shaft on the connecting plate, and the crank is rotated for a certain angle around the rotating shaft by rotating the crank handle so as to rotate the gear at the top end for a certain angle around the rotating shaft;
drive mechanism includes rack, turning block, holding screw, the recess the same with rack groove size is seted up to the rack both sides, and installs through the draw-in groove on the casing, the rack with epaxial gear mesh mutually, turning block one end is the ring channel, rack one end is inlayed in the ring channel, the turning block other end is the less bolt of diameter, the bolt can be inserted and accomplish circumference fixed in axial joint's the pinhole, prevents to rotate, the curved surface groove has been seted up to the turning block surface, the holding screw is installed to the curved surface inslot and can be slided in the curved surface inslot.
2. The space truss connecting device with the bidirectional locking function as claimed in claim 1, wherein the housing comprises an elastic tenon, a tenon connecting section, a sliding groove, a connecting plate, an opening, a rack groove, a small hole and a semicircular groove, one end of the housing is the elastic tenon, the other end of the housing is the semicircular groove, a rotating shaft is mounted on the connecting plate, the connecting plate is provided with the opening in contact with the outer ring of the housing, the opening is used for limiting the rotation angle of the crank and has the width the same as that of the crank, the other side of the housing opposite to the opening is the rack groove, the outer ring of the housing is provided with the small hole on one side close to the semicircular groove, and a thin baffle is arranged on one side of the semicircular groove.
CN202111072365.1A 2021-09-14 2021-09-14 Space truss connecting device with bidirectional locking function Expired - Fee Related CN113788164B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111072365.1A CN113788164B (en) 2021-09-14 2021-09-14 Space truss connecting device with bidirectional locking function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111072365.1A CN113788164B (en) 2021-09-14 2021-09-14 Space truss connecting device with bidirectional locking function

Publications (2)

Publication Number Publication Date
CN113788164A CN113788164A (en) 2021-12-14
CN113788164B true CN113788164B (en) 2022-09-02

Family

ID=79183271

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111072365.1A Expired - Fee Related CN113788164B (en) 2021-09-14 2021-09-14 Space truss connecting device with bidirectional locking function

Country Status (1)

Country Link
CN (1) CN113788164B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0137429A2 (en) * 1983-10-10 1985-04-17 Beer, Manfred, Dipl.-Ing. Assembling knot for a three-dimensional framework, and three-dimensional framework comprising such a knot
US4692054A (en) * 1985-08-26 1987-09-08 Northwest Design Products, Inc. Connector system for structural framework
JPH02283598A (en) * 1989-04-24 1990-11-21 Kawasaki Heavy Ind Ltd Expanding truss structure and hinge mechanism with expansive force
US5310273A (en) * 1991-07-09 1994-05-10 Yamaha Hatsudoki Kabushiki Kaisha Joint for truss structure
JPH0719403U (en) * 1993-07-29 1995-04-07 松尾建設株式会社 Space truss joint device
JP2000179051A (en) * 1998-12-14 2000-06-27 Sumitomo Jukikai Chutan Kk Joint and shaft combination for space truss
CN207596295U (en) * 2017-12-07 2018-07-10 杭州西奥电梯有限公司 A kind of staircase and girder intermediate strutting device
CN109264028A (en) * 2018-09-05 2019-01-25 北华大学 A kind of club truss element based on memorial alloy

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2104529A1 (en) * 1971-02-01 1972-08-10 Gebrüder Mylaeus, 5970 Plettenberg Kit for creating spatial frameworks
US4637193A (en) * 1984-03-16 1987-01-20 Interlock Structures International, Inc. Connecting apparatus
US4684156A (en) * 1986-07-30 1987-08-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Preloaded space structural coupling joint
US4763459A (en) * 1987-04-01 1988-08-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Collet lock joint for space station truss
DE3866022D1 (en) * 1987-05-19 1991-12-12 Astro Aerospace Corp CONNECTING DEVICE FOR RODS OF A DEVELOPABLE CONSTRUCTION.
NZ224675A (en) * 1987-05-26 1991-08-27 Syma Intercontinental Sa Connecting element for scaffolding rod end
US5186567A (en) * 1992-01-15 1993-02-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Quick-connect fasteners for assembling devices in space
US5439310A (en) * 1993-05-25 1995-08-08 The United States Of America As Represented By United States National Aeronautics And Space Administration Connector systems for structures
JPH08121433A (en) * 1994-10-20 1996-05-14 Fujitsu Ltd Locking mechanism for connecting truss members
US5771742A (en) * 1995-09-11 1998-06-30 Tini Alloy Company Release device for retaining pin
JP3349952B2 (en) * 1998-04-30 2002-11-25 株式会社ティー・エス・ケー Truss joint structure
US10024050B2 (en) * 2011-12-07 2018-07-17 Cpi Technologies, Llc Solar panel truss deployable from moving carrier
CN109057005B (en) * 2018-09-14 2019-05-21 北华大学 Space truss connecting rod with locking function and the fixture for installing the connecting rod
CN109015616B (en) * 2018-09-28 2023-11-24 哈尔滨理工大学 Space cell robot based on rack and pinion transmission
CN110697090B (en) * 2019-09-04 2022-09-02 上海宇航系统工程研究所 Rapid assembly method suitable for assembling space truss structure
CN111959826A (en) * 2020-08-12 2020-11-20 南京林业大学 A space truss structure connector with fast on-orbit assembly function

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0137429A2 (en) * 1983-10-10 1985-04-17 Beer, Manfred, Dipl.-Ing. Assembling knot for a three-dimensional framework, and three-dimensional framework comprising such a knot
US4692054A (en) * 1985-08-26 1987-09-08 Northwest Design Products, Inc. Connector system for structural framework
JPH02283598A (en) * 1989-04-24 1990-11-21 Kawasaki Heavy Ind Ltd Expanding truss structure and hinge mechanism with expansive force
US5310273A (en) * 1991-07-09 1994-05-10 Yamaha Hatsudoki Kabushiki Kaisha Joint for truss structure
JPH0719403U (en) * 1993-07-29 1995-04-07 松尾建設株式会社 Space truss joint device
JP2000179051A (en) * 1998-12-14 2000-06-27 Sumitomo Jukikai Chutan Kk Joint and shaft combination for space truss
CN207596295U (en) * 2017-12-07 2018-07-10 杭州西奥电梯有限公司 A kind of staircase and girder intermediate strutting device
CN109264028A (en) * 2018-09-05 2019-01-25 北华大学 A kind of club truss element based on memorial alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
空间太阳能电站大型体状可展桁架机构研究;刘海婷;《中国优秀硕士学位论文全文数据库工程科技II辑》;20200215(第2期);全文 *

Also Published As

Publication number Publication date
CN113788164A (en) 2021-12-14

Similar Documents

Publication Publication Date Title
CN105729498B (en) Modularization cotton rope drives non-individual body mechanical arm
CN103625656B (en) A kind of Small-size spacecraft butt-joint mechanism
CN205363898U (en) Open -ended modularity arm
CN103341863A (en) End effector capable of achieving space manipulator self crawling and load operation
CN101693472B (en) Repeatable locking device for magnetically suspended flywheel
JPS5890492A (en) Robot arm device with split ball type wrist manipulator
WO2019126919A1 (en) Three-degree-of-freedom parallel mechanism
CN113788164B (en) Space truss connecting device with bidirectional locking function
CN113353294B (en) Non-firer star arrow locking and releasing device based on polygonal synchronous limiting mechanism
CN110666774A (en) A three-degree-of-freedom rope-driven joint module based on parallel mechanism
JPS6323504B2 (en)
CN102390548A (en) Space robot orbit tool replacing device
CN111268042A (en) Floating structure connecting device
CN108258473A (en) A kind of isomorphism formula rapid replacing interface based on cooperation robot
CN204976638U (en) Snakelike net robot of climbing
CN107336221A (en) A kind of Novel two-freedom-degree parallel robot in apery elbow joint
CN105058373B (en) A Compliant Docking Device for Robotic Arm Based on Double Hooke Hinge Mechanism
CN111923032B (en) A Modular Reconfigurable Orthogonal Joint Chain Robot
CN113865821A (en) Ball head connection simulation assembly and wind load test device for bundled rocket scaling model
CN109747867B (en) Vector adjustment mechanism for electric thruster
CN108791967B (en) Controllable step-by-step unlocking device applied to spacecraft
CN103358325A (en) Orbit tool changer based on grooved wheel mechanism
CN110238786B (en) Mechanical device capable of disassembling and assembling screws at multiple angles
CN108858166A (en) A kind of robot modularized turning joint adapting to lunar surface environment
TWM632226U (en) Powered torque wrench with support mechanism

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20220902

CF01 Termination of patent right due to non-payment of annual fee