[go: up one dir, main page]

CN105387064B - A kind of expansion hinge of quick connection separation - Google Patents

A kind of expansion hinge of quick connection separation Download PDF

Info

Publication number
CN105387064B
CN105387064B CN201510757175.1A CN201510757175A CN105387064B CN 105387064 B CN105387064 B CN 105387064B CN 201510757175 A CN201510757175 A CN 201510757175A CN 105387064 B CN105387064 B CN 105387064B
Authority
CN
China
Prior art keywords
locking
hinge
centre drawer
drawer hinge
swing rod
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.)
Active
Application number
CN201510757175.1A
Other languages
Chinese (zh)
Other versions
CN105387064A (en
Inventor
马静雅
杨巧龙
任守志
王举
梁世杰
闫泽红
魏红丽
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.)
Beijing Institute of Spacecraft System Engineering
Original Assignee
Beijing Institute of Spacecraft System Engineering
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 Beijing Institute of Spacecraft System Engineering filed Critical Beijing Institute of Spacecraft System Engineering
Priority to CN201510757175.1A priority Critical patent/CN105387064B/en
Publication of CN105387064A publication Critical patent/CN105387064A/en
Application granted granted Critical
Publication of CN105387064B publication Critical patent/CN105387064B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00Pivots; Pivotal connections
    • F16C11/04Pivotal connections
    • F16C11/12Pivotal connections incorporating flexible connections, e.g. leaf springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00Pivots; Pivotal connections
    • F16C11/04Pivotal connections
    • F16C11/10Arrangements for locking

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Closing And Opening Devices For Wings, And Checks For Wings (AREA)

Abstract

本发明公开了一种快速连接分离的展开铰链。使用本发明能够实现太阳翼箱板在一定角度范围内展开,并能实现太阳翼的在轨快速连接、分离。本发明包括公铰链组件、母铰链组件和连接分离装置。铰链展开时,铰链收拢状态下涡卷弹簧储存的驱动力通过轴由公铰链传递给母铰链,同时,利用母铰链组件中的平头螺钉与公铰链组件中的圆头螺钉进行展开方向的限位;并在展开末期利用阻尼器减小冲击载荷。太阳翼箱板与套筒处于连接状态时,连接分离装置中的锁定摆杆将母铰链组件中的锁定销轴锁定在连接分离底座上的锁定销轴定位孔中;分离状态时,安装在锁定摆杆上的定位销钉位于锁定摆杆定位槽的锁定端;母铰链组件与连接分离装置分开。

The invention discloses a quick connection and separation unfolding hinge. The use of the invention can realize the deployment of the solar wing box panels within a certain angle range, and can realize the rapid connection and separation of the solar wing on the track. The invention includes a male hinge assembly, a female hinge assembly and a connection and separation device. When the hinge is unfolded, the driving force stored by the volute spring in the folded state of the hinge is transmitted from the male hinge to the female hinge through the shaft. At the same time, the expansion direction is limited by the flat head screw in the female hinge assembly and the round head screw in the male hinge assembly. ; and use the damper to reduce the impact load at the end of deployment. When the sun wing box panel and the sleeve are in the connected state, the locking swing lever in the connecting and separating device locks the locking pin in the female hinge assembly in the locking pin positioning hole on the connecting and separating base; in the separated state, it is installed in the locking The positioning pin on the swing rod is located at the locking end of the positioning groove of the locking swing rod; the female hinge assembly is separated from the connection and separation device.

Description

一种快速连接分离的展开铰链A deployment hinge with quick connection and detachment

技术领域technical field

本发明涉及太阳翼箱板展开及在轨更换技术领域,具体涉及一种快速连接分离的展开铰链。The invention relates to the technical field of solar wing box panel deployment and on-rail replacement, in particular to a deployment hinge for quick connection and separation.

背景技术Background technique

随着航天器种类的不断增加,航天器对太阳翼构型、展开刚度、在轨更换等提出了新的要求。传统太阳翼采用锁钩式或销轴式铰链进行展开固定,其展开角度固定,由于本发明应用的柔性太阳翼箱板体积较大且尺寸链上环节较多,误差积累较大,这种固定展开角度的展开铰链不能消除这种误差,进而造成太阳翼过约束。同时,这种展开铰链固定连接在太阳翼上,不具有在轨更换的能力,一旦太阳翼发生故障或到寿命末期,无法进行更换。With the continuous increase of the types of spacecraft, the spacecraft has put forward new requirements for the configuration of the solar wing, the stiffness of the deployment, and the replacement in orbit. The traditional solar wing adopts lock hook type or pin type hinges for deployment and fixation, and its deployment angle is fixed. Since the flexible solar wing box panel used in the present invention has a large volume and many links in the size chain, the accumulation of errors is relatively large. The deployment hinge at the deployment angle cannot eliminate this error, which in turn causes the sunwing to be over-constrained. At the same time, this deployment hinge is fixedly connected to the solar wing and does not have the ability to be replaced on orbit. Once the solar wing fails or reaches the end of its life, it cannot be replaced.

发明内容Contents of the invention

有鉴于此,本发明提供了一种快速连接分离的展开铰链,能够实现太阳翼箱板在一定角度范围内展开,并能实现太阳翼在轨快速连接、分离。In view of this, the present invention provides a deployment hinge for quick connection and separation, which can realize the deployment of the solar wing box panels within a certain angle range, and can realize the rapid connection and separation of the solar wing on-orbit.

本发明的快速连接分离的展开铰链,包括公铰链组件、母铰链组件和连接分离装置,外围设备为太阳翼套筒和太阳翼箱板;The deployment hinge for quick connection and separation of the present invention includes a male hinge assembly, a female hinge assembly and a connection and separation device, and the peripheral equipment is a solar wing sleeve and a solar wing box panel;

其中,公铰链组件包括公铰链、圆头螺钉、轴、平键和涡卷弹簧;其中,公铰链的一端固定安装在太阳翼套筒上,另一端安装轴;涡卷弹簧的内端安装在轴上,外端固定安装在公铰链上;圆头螺钉安装在公铰链上,且圆头螺钉的轴线与轴的轴线相垂直;平键固定安装在轴上;Among them, the male hinge assembly includes a male hinge, a round head screw, a shaft, a flat key and a scroll spring; wherein, one end of the male hinge is fixedly installed on the sun wing sleeve, and the other end is installed with a shaft; the inner end of the scroll spring is installed on the On the shaft, the outer end is fixedly installed on the male hinge; the round head screw is installed on the male hinge, and the axis of the round head screw is perpendicular to the axis of the shaft; the flat key is fixedly installed on the shaft;

母铰链组件包括母铰链、平头螺钉、方螺母、花键螺母和锁定销轴,其中,母铰链的一端固定安装有锁定销轴,另一端上设有平头螺钉;花键螺母、方螺母分别位于平头螺钉的两端,花键螺母朝向母铰链;The female hinge assembly includes a female hinge, a grub screw, a square nut, a spline nut and a locking pin, wherein, one end of the female hinge is fixedly installed with a locking pin, and the other end is provided with a grub screw; the spline nut and the square nut are respectively located on Both ends of the grub screw with the spline nut towards the female hinge;

连接分离装置包括锁定摆杆、定位锥、扭簧、扭簧转轴、定位销钉和连接分离底座;其中,连接分离底座安装在太阳翼箱板上,并设有锁定销轴定位孔和锁定销轴导向槽;连接分离底座上还设有锁定摆杆定位槽;锁定摆杆定位槽位于锁定销轴导向槽的侧面,且与锁定销轴导向槽相垂直;扭簧转轴固定安装在连接分离底座上;锁定摆杆位于锁定销轴导向槽内,一端套接在扭簧转轴上,另一端安装定位销钉;锁定摆杆定位槽由上自下宽度渐变,其底端为锁定端;定位销钉位于锁定摆杆定位槽内;扭簧一端固定在扭簧转轴上,另一端固定在锁定摆杆上;The connection and separation device includes a locking swing lever, a positioning cone, a torsion spring, a torsion spring shaft, a positioning pin and a connection and separation base; wherein, the connection and separation base is installed on the sun wing box plate, and is provided with a locking pin positioning hole and a locking pin Guide groove; the connecting and separating base is also provided with a locking swing lever positioning groove; the locking swing lever positioning groove is located on the side of the locking pin guide groove, and is perpendicular to the locking pin guiding groove; the torsion spring shaft is fixedly installed on the connecting and separating base ;The lock swing lever is located in the guide groove of the lock pin shaft, one end is sleeved on the torsion spring shaft, and the other end is installed with a positioning pin; the width of the lock swing lever positioning groove gradually changes from top to bottom, and the bottom end is the locking end; In the positioning groove of the pendulum; one end of the torsion spring is fixed on the torsion spring shaft, and the other end is fixed on the locking pendulum;

收拢状态时,涡卷弹簧为压缩状态;平键的外端与母铰链连接;In the retracted state, the scroll spring is in a compressed state; the outer end of the flat key is connected to the female hinge;

展开状态时,母铰链组件中的平头螺钉与公铰链组件中的圆头螺钉同轴且接触;In the unfolded state, the grub screw in the female hinge assembly is coaxial and in contact with the round head screw in the male hinge assembly;

连接状态时,连接分离装置中的锁定摆杆将母铰链组件中的锁定销轴锁定在连接分离底座上的锁定销轴定位孔中;In the connected state, the locking swing lever in the connecting and separating device locks the locking pin in the female hinge assembly in the locking pin positioning hole on the connecting and separating base;

分离状态时,安装在锁定摆杆上的定位销钉位于锁定摆杆定位槽的锁定端;母铰链组件与连接分离装置分开。In the separated state, the positioning pin installed on the locking swing rod is located at the locking end of the positioning groove of the locking swing rod; the female hinge assembly is separated from the connection and separation device.

进一步地,涡卷弹簧的上端面上设有粘性阻尼器,粘性阻尼器的外壳与公铰链固定安装。Further, a viscous damper is provided on the upper end surface of the scroll spring, and the shell of the viscous damper is fixedly installed with the male hinge.

进一步地,所述方螺母与平头螺钉之间存在间隙。Further, there is a gap between the square nut and the grub screw.

进一步地,连接分离底座与母铰链相接触的端面上设有定位锥,母铰链对应位置上设有锥孔。Furthermore, a positioning cone is provided on the end surface of the connection and separation base that contacts the female hinge, and a taper hole is provided at the corresponding position of the female hinge.

进一步地,锁定摆杆的下端面设有凸台。Further, a boss is provided on the lower end surface of the locking swing rod.

有益效果:Beneficial effect:

本发明采用纯机械的方法实现了铰链的展开与快速连接、分离功能,减小使用电机等方式带来的航天器资源的紧张;采用锁定摆杆的连接方式,锁定后利用锁定摆杆的摆杆曲线使锁定轴的脱出力在锁定摆杆的自锁圆内,将脱出力转化为自锁力,提供可靠的刚性连接。本发明脱离和锁定方式简单,航天员仅需将新装置推入指定位置,无需再使用工具操作,紧固螺钉等方式固定连接,减少航天员在太空中操作的难度和时间,从而极大程度降低了航天员出舱活动的成本和风险。The invention adopts a purely mechanical method to realize the unfolding, fast connection and separation functions of the hinge, and reduces the tension of spacecraft resources caused by the use of motors and other methods; the connection mode of the locking pendulum is adopted, and the pendulum of the locking pendulum is used after locking. The rod curve makes the disengagement force of the locking shaft within the self-locking circle of the locking swing rod, which converts the disengagement force into a self-locking force, providing a reliable rigid connection. The invention has a simple disengagement and locking method, and the astronauts only need to push the new device into the designated position, without using tools to operate, fastening screws and other methods to fix the connection, reducing the difficulty and time of astronauts operating in space, thereby greatly The cost and risk of astronauts' extravehicular activities are reduced.

附图说明Description of drawings

图1为本发明在太阳翼展开状态时的主视图。Fig. 1 is the front view of the present invention when the solar wings are deployed.

图2为本发明在太阳翼展开状态时的A-A剖视图。Fig. 2 is an A-A sectional view of the present invention when the solar wings are deployed.

图3为本发明在太阳翼展开状态时的B-B剖视图。Fig. 3 is a B-B sectional view of the present invention when the solar wings are deployed.

图4为本发明在太阳翼展开状态时的轴侧图。Fig. 4 is a perspective view of the present invention when the solar wings are deployed.

图5为本发明连接分离装置结构示意图。Fig. 5 is a schematic structural diagram of the connection and separation device of the present invention.

其中,1-公铰链,2-弹簧安装柱,3-涡卷弹簧,4-阻尼器连接花键,5-阻尼器安装法兰,6-母铰链,7-锁定销轴,8-连接分离底座,9-轴,10-弹簧安装柱螺钉,11-平键,12-圆头螺钉,13-平头螺钉,14-方螺母,15-花键螺母,16-右扭簧,17-右锁定摆杆,18-右定位销钉,19-垫片,20-左定位锥,21-左定位销钉,22-左锁定摆杆,23-左扭簧,24-扭簧转轴,25-右定位锥。Among them, 1-male hinge, 2-spring mounting post, 3-volume spring, 4-damper connection spline, 5-damper mounting flange, 6-female hinge, 7-lock pin, 8-connection separation Base, 9-shaft, 10-spring mounting column screw, 11-flat key, 12-round head screw, 13-flat head screw, 14-square nut, 15-spline nut, 16-right torsion spring, 17-right lock Swing rod, 18-right positioning pin, 19-spacer, 20-left positioning cone, 21-left positioning pin, 22-left locking swing rod, 23-left torsion spring, 24-torsion spring shaft, 25-right positioning cone .

具体实施方式detailed description

下面结合附图并举实施例,对本发明进行详细描述。The present invention will be described in detail below with reference to the accompanying drawings and examples.

本发明提供了一种快速连接分离的展开铰链,如图2所示,包括公铰链组件、母铰链组件和连接分离装置,其中,公铰链组件安装在太阳翼套筒上,连接分离装置安装在太阳翼箱板上,母铰链组件安装在连接分离装置上,母铰链组件和公铰链组件配合安装。The present invention provides a deployment hinge for quick connection and separation, as shown in Figure 2, including a male hinge assembly, a female hinge assembly and a connection and separation device, wherein the male hinge assembly is installed on the solar wing sleeve, and the connection and separation device is installed on On the sun wing box panel, the female hinge assembly is installed on the connection and separation device, and the female hinge assembly and the male hinge assembly are installed in cooperation.

如图1所示,公铰链组件由公铰链1、弹簧安装柱2、涡卷弹簧3、阻尼器连接花键4、阻尼器安装法兰5、轴9、弹簧安装柱螺钉10、平键11、圆头螺钉12组成。其中,公铰链1的一端固定安装在太阳翼套筒上,轴9通过轴承垂直安装在公铰链1的另一端,涡卷弹簧3的内端安装在轴9上,外端固定安装在弹簧安装柱2上,弹簧安装柱2通过弹簧安装柱螺钉10安装在公铰链1上,阻尼器连接花键4安装在轴9上,位于涡卷弹簧3的上方,粘性阻尼器安装在阻尼器连接花键4上,其外壳安装在阻尼器安装法兰5上,圆头螺钉12安装在公铰链1上,位于轴9的后方,圆头螺钉12的轴线与轴9的轴线相垂直;平键11固定安装在轴9上,其外端与母铰链6连接,轴9上平键11与母铰链6实现铰链驱动力的传递。铰链展开时,铰链收拢状态下涡卷弹簧储存的驱动力通过轴9由公铰链1传递给母铰链6,驱动铰链展开,采用阻尼器减小展开末期铰链的冲击载荷,避免过大冲击对箱板的损坏。As shown in Figure 1, the male hinge assembly consists of a male hinge 1, a spring mounting column 2, a scroll spring 3, a damper connecting spline 4, a damper mounting flange 5, a shaft 9, a spring mounting column screw 10, and a flat key 11 , 12 round head screws. Among them, one end of the male hinge 1 is fixedly installed on the solar wing sleeve, the shaft 9 is vertically installed on the other end of the male hinge 1 through a bearing, the inner end of the scroll spring 3 is installed on the shaft 9, and the outer end is fixedly installed on the spring. On the column 2, the spring mounting column 2 is installed on the male hinge 1 through the spring mounting column screw 10, the damper connecting spline 4 is installed on the shaft 9 above the scroll spring 3, and the viscous damper is installed on the damper connecting spline On the key 4, its shell is installed on the damper mounting flange 5, the round head screw 12 is installed on the male hinge 1, located behind the shaft 9, the axis of the round head screw 12 is perpendicular to the axis of the shaft 9; the flat key 11 It is fixedly installed on the shaft 9, and its outer end is connected with the female hinge 6, and the flat key 11 on the shaft 9 and the female hinge 6 realize the transmission of the hinge driving force. When the hinge is unfolded, the driving force stored by the scroll spring in the folded state of the hinge is transmitted from the male hinge 1 to the female hinge 6 through the shaft 9, driving the hinge to unfold, and the damper is used to reduce the impact load of the hinge at the end of unfolding to avoid excessive impact on the box board damage.

母铰链组件由母铰链6、平头螺钉13、方螺母14、花键螺母15、锁定销轴7等组成。其中,母铰链6的一端安装在连接分离装置上,另一端设有平头螺钉13,花键螺母15、方螺母14分别位于平头螺钉13的两端,花键螺母15朝向母铰链6,通过拧紧方螺母14、花键螺母15使得平头螺钉13固定母铰链6上。铰链展开状态下,平头螺钉13与公铰链组件中的圆头螺钉12同轴且接触,提供展开方向的限位。可通过调节方螺母14与平头螺钉13之间的间隙,调节平头螺钉和公铰链圆头螺钉的接触角度,即调节展开铰链的展开角度,从而实现铰链展开角度在85°~95°范围内的调节,进而能够适用于柔性太阳翼装配过程中的误差;锁定销轴7固定安装在母铰链上,与连接分离装置的锁定销轴定位孔相配合。The female hinge assembly is composed of a female hinge 6, flat head screws 13, square nuts 14, spline nuts 15, locking pins 7 and the like. Wherein, one end of the female hinge 6 is installed on the connection and separation device, and the other end is provided with a grub screw 13, and the spline nut 15 and the square nut 14 are respectively located at the two ends of the grub screw 13, and the spline nut 15 faces the female hinge 6, and by tightening The square nut 14 and the spline nut 15 make the grub screw 13 fixed on the female hinge 6 . When the hinge is unfolded, the flat-head screw 13 is coaxial and in contact with the round-head screw 12 in the male hinge assembly, providing a limit in the unfolding direction. By adjusting the gap between the square nut 14 and the flat-head screw 13, the contact angle between the flat-head screw and the round-head screw of the male hinge can be adjusted, that is, the unfolding angle of the unfolding hinge can be adjusted, so that the unfolding angle of the hinge can be within the range of 85° to 95°. The adjustment can be applied to the error in the assembly process of the flexible solar wing; the locking pin shaft 7 is fixedly installed on the female hinge, and cooperates with the locking pin shaft positioning hole of the connecting and separating device.

连接分离装置由左定位锥20、左锁定摆杆22、左扭簧23、扭簧转轴24、左定位销钉21、右定位锥25、右锁定摆杆17、右扭簧16、右定位销钉18、连接分离底座8等组成。连接分离底座8安装在太阳翼箱板上,连接分离底座8上设有锁定销轴定位孔与锁定销轴导向槽,左、右锁定摆杆22、17位于锁定销轴导向槽内,其一端套接在扭簧转轴24上,另一端上安装左、右定位销钉21、18;左、右扭簧23、16一端固定在扭簧转轴24上,另一端固定在左、右锁定摆杆22、17上;左、右扭簧23、16之间设有垫片19;扭簧转轴24固定安装在连接分离底座8上;左、右锁定摆杆连动,并在左、右扭簧23、16的作用下处于锁定状态,即将母铰链组件的锁定销轴7卡在定位孔内,锁定销轴脱离连接分离底座8方向的力,在左右锁定摆杆的自锁圆范围内,不会发生连接分离装置的意外脱离状况。连接分离底座8还设有2个宽度渐变的锁定摆杆定位槽,锁定摆杆定位槽分别位于锁定销轴导向槽的两侧,且锁定摆杆定位槽与锁定销轴导向槽相垂直,其底端为锁定端;左定位销钉21一端固联在左锁定摆杆22上,另一端安装在连接分离底座8左侧的锁定摆杆定位槽内;右定位销钉18一端固联在右锁定摆杆17上,另一端安装在连接分离底座8右侧的锁定摆杆定位槽内。左、右定位销钉与锁定摆杆定位槽配合,当锁定摆杆上的定位销钉运动到锁定摆杆定位槽的锁定端时自动锁紧,左、右锁定摆杆处于解锁状态,实现母铰链组件的锁定销轴7与连接分离底座8的分离。即,当需要太阳翼箱板和套筒分离时,通过工装使左锁定摆杆22、右锁定摆杆17移动到分离极限位置(即左定位销钉21、右定位销钉18运动到锁定摆杆定位槽的锁定端)。此时,锁定摆杆上的定位销钉将在摩擦力的作用下静止在的锁定摆杆定位槽内,防止摆杆在扭簧的作用下摆回至锁定位置。航天员可直接将旧箱板推离。The connection and separation device consists of left positioning cone 20, left locking fork 22, left torsion spring 23, torsion spring rotating shaft 24, left positioning pin 21, right positioning cone 25, right locking fork 17, right torsion spring 16, right positioning pin 18 , connection and separation of the base 8 and other components. The connection and separation base 8 is installed on the sun wing box plate, and the connection and separation base 8 is provided with a locking pin positioning hole and a locking pin guide groove. Socketed on the torsion spring rotating shaft 24, left and right positioning pins 21,18 are installed on the other end; left and right torsion springs 23,16 one ends are fixed on the torsion spring rotating shaft 24, and the other end is fixed on the left and right locking fork 22 , 17; Gasket 19 is provided between left and right torsion springs 23,16; Torsion spring rotating shaft 24 is fixedly installed on the connection separation base 8; , 16 is in the locked state, that is, the locking pin shaft 7 of the female hinge assembly is stuck in the positioning hole, and the locking pin shaft is separated from the force in the direction of the separation base 8, within the self-locking circle range of the left and right locking swing rods, it will not An accidental disengagement of the connection-detachment device has occurred. The connection and separation base 8 is also provided with two locking swing bar positioning grooves with gradually changing widths. The locking swing bar positioning slots are respectively located on both sides of the locking pin shaft guide groove, and the locking swing bar positioning grooves are perpendicular to the locking pin shaft guide groove. The bottom end is the locking end; one end of the left positioning pin 21 is fixedly connected on the left locking swing rod 22, and the other end is installed in the locking swing rod positioning groove on the left side of the connection and separation base 8; one end of the right positioning pin 18 is fixedly connected on the right locking swing rod. On the bar 17, the other end is installed in the locking fork locating groove that connects the separation base 8 right sides. The left and right positioning pins cooperate with the positioning groove of the locking swing rod. When the positioning pin on the locking swing rod moves to the locking end of the locking swing rod positioning groove, it is automatically locked. The left and right locking swing rods are in the unlocked state, realizing the female hinge assembly. The locking pin shaft 7 is separated from the connection and separation base 8. That is, when the solar wing box panel and the sleeve are required to be separated, the left locking swing link 22 and the right locking swing link 17 are moved to the separation limit position by the tooling (that is, the left positioning pin 21 and the right positioning pin 18 are moved to the locking swing link positioning locking end of the groove). At this moment, the positioning pin on the locking fork will be static in the locking fork positioning groove under the effect of friction force, preventing the fork from swinging back to the locked position under the action of the torsion spring. Astronauts can simply push the old box panels away.

在连接分离底座上与母铰链相接触的端面上设置的定位锥20、25,与母铰链对应位置上设置的锥孔相配合,从而实现连接分离装置与母铰链之间的扭转方向的快速、精准定位。The positioning cones 20, 25 arranged on the end faces of the connection and separation base in contact with the female hinge are matched with the taper holes provided on the corresponding positions of the female hinge, so as to realize the fast, fast and accurate torsion between the connection and separation device and the female hinge. precise positioning.

更换时,新的箱板上也配有相同结构的连接分离装置。其左锁定摆杆22、右锁定摆杆17处于未锁定状态。当航天员将母铰链组件的锁定销轴7推入至连接分离装置并锁定的过程中,连接分离装置首先在左定位锥20、右定位锥25的作用下,定位到正确位置。在推入过程中,母铰链3上的锁定销轴7会沿左锁定摆杆22、右锁定摆杆17的斜面滑动,将左锁定摆杆22、右锁定摆杆17推离未锁定位置,此时左定位销钉21、右定位销钉18可在锁定摆杆定位槽中自由滑动,不与锁定摆杆定位槽发生摩擦。当锁定销轴7进入锁定销轴定位孔后,左锁定摆杆22、右锁定摆杆17在扭簧的作用下有回转到未锁定状态的趋势,将锁定销轴7卡在锁定销轴定位孔内。此时,左锁定摆杆22、右锁定摆杆17和锁定销轴7处于自锁状态,锁定销轴7无法从连接分离装置中脱出。从而实现了太阳翼箱板的刚性快速连接功能。When replacing, the new box plate is also equipped with a connection and separation device with the same structure. Its left locking fork 22, right locking fork 17 are in unlocked state. When the astronaut pushes the locking pin 7 of the female hinge assembly into the connection and separation device and locks it, the connection and separation device is first positioned to the correct position under the action of the left positioning cone 20 and the right positioning cone 25 . During the push-in process, the locking pin 7 on the female hinge 3 will slide along the slopes of the left locking swing bar 22 and the right locking swing bar 17, pushing the left locking swing bar 22 and the right locking swing bar 17 away from the unlocked position, At this moment, the left positioning pin 21 and the right positioning pin 18 can slide freely in the positioning groove of the locking fork, without friction with the positioning groove of the locking fork. After the locking pin 7 enters the locking pin positioning hole, the left locking fork 22 and the right locking fork 17 have a tendency to turn to the unlocked state under the action of the torsion spring, and the locking pin 7 is stuck in the locking pin for positioning. inside the hole. At this moment, the left lock swing bar 22, the right lock swing bar 17 and the lock pin shaft 7 are in a self-locking state, and the lock pin shaft 7 cannot escape from the connection and separation device. Thereby, the rigid fast connection function of the solar wing box panel is realized.

其中,还可以在锁定摆杆的底部设置一个凸台,从而可以通过使用与凸台形状相配合的支杆工装,利用支点效应快速方便地实现锁定摆杆的解锁。Wherein, a boss can also be provided at the bottom of the locking swing lever, so that the unlocking of the locking swing lever can be realized quickly and conveniently by using the fulcrum effect by using the pole tooling matched with the shape of the boss.

本发明中铰链展开驱动元件为涡卷弹簧3,属于一种平面涡卷弹簧,也可以采用其他弹簧如圆柱扭转弹簧、恒力矩弹簧等作为展开驱动元件。The hinge unfolding driving element in the present invention is a scroll spring 3, which belongs to a plane scroll spring, and other springs such as cylindrical torsion springs, constant moment springs, etc. can also be used as the unfolding driving element.

综上所述,以上仅为本发明的较佳实施例而已,并非用于限定本发明的保护范围。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。To sum up, the above are only preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the protection scope of the present invention.

Claims (5)

1. a kind of expansion hinge of quick connection separation, including:Centre drawer hinge bracket component, centre drawer hinge component and connection separator, its In, centre drawer hinge bracket component includes centre drawer hinge bracket (1), axle (9) and scroll spring (3), wherein, centre drawer hinge bracket (1) one end installation axle (9);Whirlpool The inner of coil spring (3) is arranged on axle (9), and outer end is fixedly mounted on centre drawer hinge bracket (1), and centre drawer hinge component includes centre drawer hinge (6), during rounding state, scroll spring (3) is compressive state, it is characterised in that ancillary equipment is solar wing sleeve and solar wing Boxboard;
Wherein, centre drawer hinge bracket component includes centre drawer hinge bracket (1), cheese head screw (12), axle (9), flat key (11) and scroll spring (3);Its In, the other end of centre drawer hinge bracket (1) is fixedly mounted on solar wing sleeve, and cheese head screw (12) is arranged on centre drawer hinge bracket (1), and circle The axis of head screw (12) and the axis perpendicular of axle (9);Flat key (11) is fixedly mounted on axle (9);
Centre drawer hinge component also includes flat head screw (13), square nut (14), splined nut (15) and locking bearing pin (7), wherein, it is female One end of hinge (6) is installed with locking bearing pin (7), and the other end is provided with flat head screw (13);Splined nut (15), square spiral shell Female (14) are located at the both ends of flat head screw (13) respectively, and splined nut (15) is towards centre drawer hinge (6);
Connecting separator includes locking swing rod, locating cone, torsion spring, torsion spring rotating shaft (24), shop bolt and connection detachable base (8);Wherein, connect detachable base (8) be arranged on solar wing boxboard on, and provided with locking bearing pin positioning hole and stop pin spindle guide to Groove;Locking swing rod locating slot is additionally provided with connection detachable base (8);Locking swing rod locating slot is located at the side of stop pin axle guide groove Face, and it is perpendicular with stop pin axle guide groove;Torsion spring rotating shaft is fixedly mounted on connection detachable base (8);Locking swing rod is located at In stop pin axle guide groove, one end is socketed in torsion spring rotating shaft, other end installation shop bolt;Lock swing rod locating slot by it is upper from Lower width gradual change, its bottom are keyed end;Shop bolt is in locking swing rod locating slot;One end is fixed on torsion spring rotating shaft (24) on, the other end is fixed on locking swing rod;
During rounding state, the outer end of flat key (11) is connected with centre drawer hinge (6);
During deployed condition, the flat head screw (13) in centre drawer hinge component is coaxial with the cheese head screw (12) in centre drawer hinge bracket component and connects Touch;
During connection status, the locking bearing pin (7) in centre drawer hinge component is locked in connection by the locking swing rod connected in separator In locking bearing pin positioning hole on detachable base (8);
During released state, the shop bolt on locking swing rod is positioned at the keyed end for locking swing rod locating slot;Centre drawer hinge group Part separates with being connected separator.
2. the expansion hinge of quick connection separation as claimed in claim 1, it is characterised in that the upper surface of scroll spring (3) Viscous damper is provided with, shell and the centre drawer hinge bracket (1) of viscous damper are fixedly mounted.
3. the expansion hinge of quick connection separation as claimed in claim 1, it is characterised in that the square nut (14) and tack Gap be present between (13) in screw.
4. the expansion hinge of quick connection separation as claimed in claim 1, it is characterised in that connection detachable base and centre drawer hinge The end face being in contact is provided with locating cone, and centre drawer hinge correspondence position is provided with taper hole.
5. the expansion hinge of quick connection separation as claimed in claim 1, it is characterised in that the lower surface for locking swing rod is provided with Boss.
CN201510757175.1A 2015-11-09 2015-11-09 A kind of expansion hinge of quick connection separation Active CN105387064B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510757175.1A CN105387064B (en) 2015-11-09 2015-11-09 A kind of expansion hinge of quick connection separation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510757175.1A CN105387064B (en) 2015-11-09 2015-11-09 A kind of expansion hinge of quick connection separation

Publications (2)

Publication Number Publication Date
CN105387064A CN105387064A (en) 2016-03-09
CN105387064B true CN105387064B (en) 2017-12-08

Family

ID=55419687

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510757175.1A Active CN105387064B (en) 2015-11-09 2015-11-09 A kind of expansion hinge of quick connection separation

Country Status (1)

Country Link
CN (1) CN105387064B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU220268U1 (en) * 2023-05-16 2023-09-05 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" OPENING SWIVEL

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108730325B (en) * 2018-07-02 2019-09-17 上海卫星工程研究所 A kind of low impact applied to deployable structure is from locking hinge
DE102018132674A1 (en) * 2018-12-18 2020-06-18 Endress+Hauser Conducta Gmbh+Co. Kg Wing hinge for a field device housing and field device housing with wing hinge
CN110525688B (en) * 2019-08-06 2020-09-25 北京空间飞行器总体设计部 On-orbit reconfigurable extensible satellite system
CN113002804B (en) * 2021-03-26 2022-06-24 上海埃依斯航天科技有限公司 Solar wing hinge driven by elastic force
CN113958597B (en) * 2021-10-18 2022-08-23 北京微纳星空科技有限公司 Triggering locking hinge device
CN113734472B (en) * 2021-11-05 2022-02-11 北京微焓科技有限公司 Satellite battery plate unfolding device
CN114992231B (en) * 2022-08-03 2022-10-25 银河航天(北京)网络技术有限公司 Adjustable locking mechanism and use method
CN116605421B (en) * 2023-07-20 2023-10-20 银河航天(北京)网络技术有限公司 Solar wingspan opening time sequence linkage control device and solar wingspan opening method

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19649741C2 (en) * 1996-11-30 1999-07-15 Daimler Benz Aerospace Ag Hinge for unfolding and locking a solar panel or a reflector
US6158088A (en) * 1999-04-05 2000-12-12 Lockheed Martin Corporation Deployable hinge assembly providing end of travel damping
CN103267098B (en) * 2013-05-16 2015-07-29 北京空间飞行器总体设计部 A kind of hinge of quadratic crank mechanism locking
CN204355286U (en) * 2014-10-31 2015-05-27 北京空间飞行器总体设计部 One is inserted into locking type solar wing hinge
CN204239446U (en) * 2014-11-18 2015-04-01 中国科学院沈阳自动化研究所 Outspreading sailboard of solar cell locking framework

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU220268U1 (en) * 2023-05-16 2023-09-05 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" OPENING SWIVEL

Also Published As

Publication number Publication date
CN105387064A (en) 2016-03-09

Similar Documents

Publication Publication Date Title
CN105387064B (en) A kind of expansion hinge of quick connection separation
US10384761B2 (en) Unmanned aerial vehicle arm adjustment device and unmanned aerial vehicle
US10383248B1 (en) Locking mechanism and server having the same
US8752793B2 (en) Door assembly, in particular for a helicopter, provided with an emergency release device
US8672261B2 (en) Engine mount of aircraft and aircraft
US10137996B2 (en) Positive lock latching mechanism
US20120012694A1 (en) Fail-safe aircraft engine mounting apparatus
TWI505959B (en) Energy absorbing coupler
KR102091959B1 (en) Small store suspension and release unit
US7448588B2 (en) Supporting device used for sustaining an apparatus within a portable computer
CN110001372A (en) Lockable mechanism, fast-changed support component and electric vehicle for battery pack
US20180094473A1 (en) Locking device and opening and closing mechanism having the same
CN110871910A (en) Micro-nano satellite
CN103267098A (en) Hinge for locking four-bar mechanism
CN110450973B (en) Reverse-thrust centering supporting device with adjustable length
CN216233082U (en) Satellite unfolding and locking mechanism
US9150309B2 (en) Fastening system for hanging mountable overhead containers
CN113348772B (en) Single-point unlocking two-stage linkage space unfolding mechanism
CN219790559U (en) Quick detach formula undercarriage for unmanned aerial vehicle
CN115523223B (en) Statically Determined Tape Hinge
CN218468059U (en) Hinge structure for folding solar wing
CN215043818U (en) Unfolding mechanism
CN202271870U (en) Quick-disassembly mechanism of back row seats for automobile
CN113353238B (en) UAV wing folding mechanism and UAV
EP1843077B1 (en) Support arrangement for monitors and similar equipment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant