JP3004078B2 - Space structure attachment / detachment device - Google Patents
Space structure attachment / detachment deviceInfo
- Publication number
- JP3004078B2 JP3004078B2 JP3120233A JP12023391A JP3004078B2 JP 3004078 B2 JP3004078 B2 JP 3004078B2 JP 3120233 A JP3120233 A JP 3120233A JP 12023391 A JP12023391 A JP 12023391A JP 3004078 B2 JP3004078 B2 JP 3004078B2
- Authority
- JP
- Japan
- Prior art keywords
- latch member
- mounting side
- locking
- mounting
- latch
- 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 - Lifetime
Links
Landscapes
- Aerials With Secondary Devices (AREA)
Description
【0001】[0001]
【産業上の利用分野】この発明は、例えば宇宙空間に構
築される組立型アンテナの分割鏡面等の構造体同士を着
脱自在結合するのに用いられる宇宙用構造体の着脱装置
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a space structure attaching / detaching apparatus used for detachably connecting structures such as a split mirror surface of an assembled antenna constructed in space.
【0002】[0002]
【従来の技術】最近、宇宙開発の分野においては、宇宙
ステーション等の大型の宇宙航行体の開発が進められて
いる。ところで、このような宇宙航行体に搭載されるア
ンテナとしては、予め地上で分割して制作して、分割状
態のままで、宇宙空間に輸送し、宇宙空間において作業
用マニピュレータを用いて組立設置する組立型が輸送等
の点から有利とされている。このような組立型アンテナ
としては、例えば略中央に中央鏡面を設け、この中央鏡
面の周囲に複数分割した分割鏡面が取付けて組立てられ
て鏡面を形成する分割方式のものが考えられている。2. Description of the Related Art Recently, in the field of space development, the development of large space vehicles such as space stations has been promoted. By the way, as an antenna mounted on such a spacecraft, it is divided in advance on the ground, produced, transported to space in the divided state, and assembled and installed in space using a working manipulator. The assembly type is advantageous in terms of transportation and the like. As such an assembling antenna, for example, a split type antenna in which a central mirror surface is provided substantially at the center and a plurality of divided mirror surfaces are attached around the central mirror surface and assembled to form a mirror surface has been considered.
【0003】しかし、このような組立型アンテナにあっ
ては、単に組立可能に分割すれば良いものでなく、宇宙
環境という極限環境で、しかも遠隔的に作業用マニピュ
レータを操作して組立作業を行わなければならないこと
により、その組立及び分解作業が非常に面倒であるとい
う問題を有していた。そこで、宇宙開発において重要と
される小形・軽量化を満足し得るような簡単な構成で、
しかも、容易に所望の精度を有した組立を実現するため
の着脱装置の開発が要請されている。なお、係る事情
は、組立型アンテナに限るものでなく、宇宙ステーショ
ンに構築される各種の組立型の宇宙用構造体においても
同様のものである。[0003] However, such an assembling type antenna is not simply divided so as to be assemblable, and the assembling work is performed by operating the working manipulator remotely in an extreme environment such as a space environment. Due to the necessity, the assembling and disassembling operations are very troublesome. Therefore, with a simple configuration that can satisfy the small size and weight reduction important in space development,
Moreover, there is a demand for the development of a detachable device for easily assembling with desired accuracy. In addition, such a situation is not limited to the assembly type antenna, but also applies to various assembly type space structures constructed in the space station.
【0004】[0004]
【発明が解決しようとする課題】以上述べたように、宇
宙開発の分野にあっては、宇宙空間に構築される組立型
構造体を容易にして、高精度な結合及び分離を実現する
ための宇宙用構造体の着脱装置の開発が強く要請されて
る。As described above, in the field of space exploration, an assembling type structure constructed in outer space is facilitated to realize high-precision coupling and separation. There is a strong demand for the development of a detachable device for space structures.
【0005】この発明は上記の事情に鑑みてなされたも
ので、簡易な構成で、且つ、容易にして、高精度な結合
及び分離を実現し得るようにした宇宙用構造体の着脱装
置を提供することを目的とする。SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and provides a space structure attaching / detaching apparatus having a simple structure and capable of realizing high-precision coupling and separation. The purpose is to do.
【0006】[0006]
【課題を解決するための手段】この発明は構造体同士を
略逆三角形状の頂点の三点で結合してなる宇宙用構造体
の着脱装置において、前記構造体の取付側及び被取付側
のいずれか一方の結合部に互いに逆方向に突出されて設
けられるもので、前記略逆三角形状の同一直線上の二頂
点を構成する一対の回動軸部材と、前記構造体の取付側
及び被取付側のいずれか一方の結合部に前記一対の回動
軸部材と同一面内の他の頂点に結合方向に延出されて該
結合部方向と略平行の軸回りに回転自在に設けられるも
ので、先端部に係止溝が設けられ、基端部に操作部が設
けられたラッチ部材と、前記構造体の取付側及び被取付
側のいずれか他方の結合部に設けられて前記回動軸部材
が着脱自在に装着され、該回動軸部材を前記結合方向に
対して略直交する軸回りに回動自在に支持する一対の軸
支部材と、前記構造体の取付側及び被取付側のいずれか
他方の結合部に設けられて前記ラッチ部材が着脱自在に
装着されるもので、装着された該ラッチ部材の前記係止
溝に対向して出入り自在に設けられる係止部材を有した
保持手段と、この保持手段の係止部材を前記ラッチ部材
の係止溝を係止する方向に移動付勢する付勢手段と、前
記ラッチ部材を前記保持部材より離脱した状態で回転を
規制して前記保持手段への装着を許容し、その装着状態
で前記ラッチ部材の回転操作を許容して前記係止部材を
前記付勢手段に抗して移動付勢して該ラッチ部材の離脱
を許容する規制手段とを備えて構成したものである。SUMMARY OF THE INVENTION The present invention relates to a space structure attaching / detaching apparatus in which structures are connected to each other at three points of generally inverted triangular vertices. One of the coupling portions is provided so as to protrude in a direction opposite to each other, and a pair of rotating shaft members forming two vertexes on the same straight line of the substantially inverted triangle shape, a mounting side of the structure and a cover. At one of the connecting portions on the mounting side, extending at the other vertex in the same plane as the pair of rotating shaft members in the connecting direction and rotatably provided around an axis substantially parallel to the connecting portion direction. A latch member provided with a locking groove at a distal end portion and an operating portion at a base end portion, and a latch member provided at one of the other connecting portions on the mounting side and the mounting side of the structure, and A shaft member is detachably mounted, and the rotating shaft member is substantially orthogonal to the coupling direction. A pair of pivotal members rotatably supported around, and a latch member provided at one of the coupling portions on the mounting side and the mounting side of the structure to which the latch member is detachably mounted. Holding means having a locking member provided so as to be able to come and go in opposition to the locking groove of the latch member, and a locking member of the holding means in a direction for locking the locking groove of the latch member. A biasing means for moving and biasing, the rotation of the latch member is restricted in a state where the latch member is detached from the holding member to allow the latch member to be mounted on the holding means, and the rotation operation of the latch member is permitted in the mounted state. A regulating means for moving and urging the locking member against the urging means to allow the latch member to be released;
【0007】[0007]
【作用】上記構成によれば、取付側及び被取付側構造体
は、その一方のラッチ部材の操作部がマニピュレータに
把持されて一方が結合位置に移送されて、回動軸部材が
軸支部材に装着され、その後、取付側及び被取付側の一
方の構造体が回動軸部材を中心として回動されてラッチ
部材が保持手段に装着される。この結合の際、ラッチ部
材は、規制手段に回転が規制されており、その係止溝が
保持手段の係止部材に係止されて相互間が結合され、こ
の結合状態で規制手段が切換えられて回転規制が解除さ
れる。そして、この結合状態において、ラッチ部材は、
その操作部を介して回転操作されると、その係止溝が係
止されていた保持手段の係止部材を付勢手段の付勢力に
抗して押圧することにより、その係止が解除され、その
後、結合動作と略逆に反転して保持手段から離脱され、
ここで、回動軸部材が軸支部材から離脱されて分離され
る。According to the above construction, the operating part of one of the latch members is gripped by the manipulator and the other is transferred to the coupling position, and the rotating shaft member is connected to the pivot supporting member. After that, one of the structures on the mounting side and the mounting side is rotated about the rotation shaft member, and the latch member is mounted on the holding means. At the time of this connection, the rotation of the latch member is restricted by the restricting means, the locking groove of which is locked by the locking member of the holding means, and the latch members are connected to each other. In this connected state, the restricting means is switched. The rotation restriction is released. Then, in this coupled state, the latch member
When rotated via the operating portion, the locking is released by pressing the locking member of the holding means, whose locking groove has been locked, against the urging force of the urging means. , After which, the connection operation is reversed and detached from the holding means,
Here, the rotating shaft member is separated from the shaft supporting member.
【0008】[0008]
【実施例】以下、この発明の実施例について、図面を参
照して詳細に説明する。Embodiments of the present invention will be described below in detail with reference to the drawings.
【0009】図1はこの発明の一実施例に係る宇宙用構
造体の着脱装置を示すもので、取付側構造体10と被取
付側構造体11は略逆三角形状の頂点に対応する三点で
相互結合される。FIG. 1 shows a space structure attaching / detaching apparatus according to an embodiment of the present invention. A mounting-side structure 10 and a mounting-side structure 11 have three points corresponding to substantially inverted triangular vertices. Are interconnected.
【0010】すなわち、取付側構造体10には、その係
合部に略逆三角形状の同一直線上の二頂点に位置決め用
の一対の回動軸部材12a,12bが互いに逆方向に突
出されて設けられ、この一対の回動軸部材12a,12
bと同一面内の他の頂点にはラッチ部材13が結合方向
(矢印A.B方向)に突出させて配設される。ラッチ部
材13は図2に示すように、先端部に係止溝13aが設
けられ、その基端部にはマニピュレータ操作部13bが
設けられる。このラッチ部材13は、その中間部が軸受
部材14を介して結合方向と略平行な軸回りに回動自在
に支持される。そして、ラッチ部材13は、その軸受1
4とマニピュレータ保持部13bとの間にばね部材15
が一定の方向に所定のトルクを付与するように係着さ
れ、軸方向の移動が規制されている。That is, a pair of rotating shaft members 12a and 12b for positioning are projected from opposite sides of the mounting-side structure 10 at two apexes of a substantially inverted triangular shape on the same straight line. The pair of rotating shaft members 12a, 12
At the other apex in the same plane as b, a latch member 13 is disposed so as to protrude in the coupling direction (the direction of arrows AB). As shown in FIG. 2, the latch member 13 is provided with a locking groove 13a at a distal end and a manipulator operating portion 13b at a proximal end thereof. The latch member 13 has a middle portion supported by a bearing member 14 so as to be rotatable about an axis substantially parallel to the coupling direction. Then, the latch member 13 is mounted on the bearing 1.
4 and the spring member 15 between the manipulator holding portion 13b.
Are attached so as to apply a predetermined torque in a certain direction, and the movement in the axial direction is restricted.
【0011】また、ラッチ部材13にはロックピン13
cが設けられる。このロックピン13cは、例えば軸受
部材14に図3に示すように矢印A,B方向(結合方向
と略平行な方向)に移動自在に設けられたロックレバー
16のロック部16aに選択的に係止されてラッチ部材
13の回転を規制する。ロックレバー16は一端にばね
部材17が係着され、他端には押圧部16bが設けられ
ており、この押圧部16bがばね部材17の付勢力に抗
して押圧されると、ロック部16aがロックピン13c
から離脱されてラッチ部材13の回転操作を許容する。The latch member 13 has a lock pin 13
c is provided. The lock pin 13c is selectively engaged with, for example, a lock portion 16a of a lock lever 16 provided on the bearing member 14 so as to be movable in the directions of arrows A and B (a direction substantially parallel to the coupling direction) as shown in FIG. It is stopped to restrict the rotation of the latch member 13. The lock lever 16 has a spring member 17 at one end and a pressing portion 16b provided at the other end. When the pressing portion 16b is pressed against the urging force of the spring member 17, the locking portion 16a Is the lock pin 13c
To allow the latch member 13 to rotate.
【0012】一方、被取付側構造体11には、その結合
部に一対の軸支部材18a,18bが取付側構造体10
の回動軸部材12a,12bに対応して設けられる。こ
の軸支部材18a,18bは逆三角角形状の直線上の二
頂点を形成するもので(図4参照)、略V字状の案内部
19a,19bがそれぞれ設けられる。そして、被取付
側構造体11の結合部には軸支部材18a,18bと同
一面上の頂点を形成する保持部材20がラッチ部材13
に対応して設けられる。保持部材20は図5に示すよう
に、嵌合孔20aがラッチ部材13に対応して設けら
れ、この嵌合孔20aには係止部21が結合方向と略直
交する方向(即ち、ラッチ部材13の挿入方向と略直交
する方向)に出入り自在に設けられる。係止部21はば
ね部材22の一端が係着されており、このばね部材22
の付勢力が付与されて嵌合孔20a内に突出されてい
る。なお、回動軸部材12a,12bは、例えば金属や
複合材料等でチューブ構造に形成されて、周囲部に潤滑
処理が施される。On the other hand, a pair of support members 18a and 18b are provided at the joint of the structure 11 to be mounted on the mounting side.
Are provided corresponding to the rotating shaft members 12a and 12b. The shaft support members 18a and 18b form two vertices on a straight line having an inverted triangular shape (see FIG. 4), and are provided with substantially V-shaped guide portions 19a and 19b, respectively. A holding member 20 that forms a vertex on the same plane as the shaft supporting members 18a and 18b is provided at a joint portion of the attached-side structure 11 with the latch member 13.
Is provided in correspondence with. As shown in FIG. 5, the holding member 20 is provided with a fitting hole 20a corresponding to the latch member 13, and a locking portion 21 is provided in the fitting hole 20a in a direction substantially perpendicular to the coupling direction (that is, the latch member 13). 13 (in a direction substantially perpendicular to the insertion direction). One end of a spring member 22 is engaged with the locking portion 21.
And is projected into the fitting hole 20a. The rotating shaft members 12a and 12b are formed in a tube structure using, for example, a metal, a composite material, or the like, and a peripheral portion is subjected to a lubrication process.
【0013】上記構成において、取付側構造体10を被
取付側構造体11に結合させる場合は、先ず図示しない
作業用マニピュレータを操作して、そのマニピュレータ
操作部13bを保持して取付側構造体10を移送させ、
その回動軸部材12a,12bを被取付側構造体11の
軸支部材18a,18bに装着する。ここで、取付側構
造体10は被取付側構造体11に対して仮位置決めされ
る。そして、取付側構造体10が作業用マニピュレータ
(図示せず)を介して回動付勢され、そのラッチ部材1
3が被取付側構造体11の保持部材20の嵌合孔20a
に挿入される。この際、ラッチ部材13は、そのロック
ピン13cがロックレバー16のロック部16aに係止
されて、その回転が規制されており、その係止溝13a
に保持部材20の係止部21が係止され、ここに、取付
側構造体10が被取付側構造体11に固定位置決めされ
る。In the above configuration, when the mounting-side structure 10 is to be connected to the mounting-side structure 11, first, a work manipulator (not shown) is operated to hold the manipulator operation portion 13b and to hold the mounting-side structure 10 Is transported,
The rotating shaft members 12a and 12b are mounted on the shaft supporting members 18a and 18b of the mounting-side structure 11. Here, the mounting-side structure 10 is provisionally positioned with respect to the mounting-side structure 11. Then, the mounting-side structure 10 is rotationally urged via a working manipulator (not shown), and the latch member 1
3 is a fitting hole 20a of the holding member 20 of the attached structure 11
Is inserted into. At this time, the lock pin 13c of the latch member 13 is locked by the lock portion 16a of the lock lever 16, and its rotation is restricted.
The locking portion 21 of the holding member 20 is locked to the mounting structure 10, where the mounting-side structure 10 is fixedly positioned on the mounting-side structure 11.
【0014】また、上記のように結合された取付側構造
体10を被取付側構造体11から離脱させる場合は、先
ず、ラッチ部材13のマニピュレータ操作部13bを回
転させる。この際、ラッチ部材13は、その回転を規制
するロックレバー16の押圧部16bが被取付側構造体
11に当接してばね部材17の付勢力に抗して押圧さ
れ、そのロックピン13cがロック部16aから離脱さ
れて回転可能となっており、回転操作に連動して回転さ
れる。すると、ラッチ部材13は保持部材20の係止部
21をばね部材22の付勢力に抗して押圧して、その係
止溝13aから保持部材20の係止部21が離脱され、
保持部材20の嵌合孔20aから引抜き可能となり、以
後上述した結合動作と略逆の手順で分離される。When the mounting-side structure 10 coupled as described above is detached from the mounting-side structure 11, first, the manipulator operating portion 13b of the latch member 13 is rotated. At this time, the latch member 13 is pressed against the urging force of the spring member 17 by the pressing portion 16b of the lock lever 16 that regulates the rotation of the latch member 13 coming into contact with the attached-side structure 11, and the lock pin 13c is locked. It is detachable from the part 16a and is rotatable, and is rotated in conjunction with the rotation operation. Then, the latch member 13 presses the locking portion 21 of the holding member 20 against the urging force of the spring member 22, and the locking portion 21 of the holding member 20 is released from the locking groove 13a.
The holding member 20 can be pulled out from the fitting hole 20a, and is separated in a procedure substantially opposite to the above-described connecting operation.
【0015】このように、上記組立型アンテナの着脱装
置は取付側構造体10に一対の回動軸部材12a,12
bとマニピュレータ操作部13bを有したラッチ部材1
3を略逆三角形状に配設し、被取付側構造体11に一対
の軸支部材18a,18bと保持部材20を同様に略逆
三角形状に配設し、ラッチ部材13のマニピュレータ操
作部13bを保持して回動軸部材12a,12bを軸支
部材18a,18bに装着して回動させ、そのラッチ部
材13を保持部材20に装着して該保持部材20にラッ
チさせて結合を実現し、マニピュレータ操作部13bを
操作してラッチ部材13を回動式に保持部材20による
ラッチを解除させて分離を行うように構成した。これに
よれば、作業用マニピュレータでラッチ部材13のマニ
ピュレータ操作部13bを保持した状態で、結合及び分
離動作が実現されることにより、可及的に簡便な取扱い
操作が実現されることより、特に宇宙空間における各種
組立式構造物の高精度な組立に好適される。As described above, the mounting and dismounting device for the assembling type antenna includes the pair of rotating shaft members 12a and 12
member 1 having a b and a manipulator operating portion 13b
3 is disposed in a substantially inverted triangular shape, and a pair of shaft support members 18a and 18b and a holding member 20 are similarly disposed in a substantially inverted triangular shape on the mounting-side structure 11, and the manipulator operating portion 13b Is held, the rotating shaft members 12a, 12b are mounted on the shaft supporting members 18a, 18b and rotated, and the latch member 13 is mounted on the holding member 20 and latched by the holding member 20 to realize coupling. By operating the manipulator operating portion 13b, the latch member 13 is rotatably released from the latch by the holding member 20 to perform separation. According to this, in a state where the manipulator operating portion 13b of the latch member 13 is held by the work manipulator, the coupling and separating operations are realized, so that the handling operation as simple as possible is realized. It is suitable for high-precision assembly of various assembly-type structures in outer space.
【0016】なお、上記実施例では、回動軸部材12
a,12b及びラッチ部材13を取付側構造体10に設
け、軸支部材18a,18b及び保持部材20を被取付
側構造体11に設けて構成したが、これに限ることな
く、逆に回動軸部材12a,12b及びラッチ部材13
を被取付側構造体11に設け、軸支部材18a,18b
及び保持部材20を取付側構造体10に設けて構成する
ことも可能である。よって、この発明は上記実施例に限
ることなく、その他、この発明の要旨を逸脱しない範囲
で種々の変形を実施し得ることは勿論のことである。In the above embodiment, the rotating shaft member 12
a, 12b and the latch member 13 are provided on the mounting-side structure 10, and the shaft support members 18a, 18b and the holding member 20 are provided on the mounting-side structure 11. However, the present invention is not limited to this. Shaft members 12a, 12b and latch member 13
Are provided on the mounting-side structure 11, and the support members 18a, 18b
It is also possible to provide the holding member 20 in the mounting-side structure 10. Therefore, it is needless to say that the present invention is not limited to the above-described embodiment, and that various modifications can be made without departing from the scope of the present invention.
【0017】[0017]
【発明の効果】以上詳述したように、この発明によれ
ば、簡易な構成で、且つ、容易にして、高精度な結合及
び分離を実現し得るようにした宇宙用構造体の着脱装置
を提供することができる。As described above in detail, according to the present invention, there is provided a space structure attaching / detaching apparatus capable of realizing high-precision coupling and separation with a simple structure and easily. Can be provided.
【図1】この発明の一実施例に係る宇宙用構造体の着脱
装置を示した図。FIG. 1 is a view showing a space structure attaching / detaching device according to an embodiment of the present invention.
【図2】図1のラッチ部材を取出して示した図。FIG. 2 is a view showing a latch member of FIG. 1 taken out;
【図3】図2のラッチ部材の要部を取出して示した図。FIG. 3 is a diagram showing a main part of the latch member of FIG.
【図4】図1の被取付側構造体の結合部を示した図。FIG. 4 is a view showing a coupling portion of the mounting-side structure shown in FIG. 1;
【図5】図1の保持部材を取り出して示した図。FIG. 5 is a view showing the holding member of FIG. 1 taken out.
10…取付側構造体、11…被取付側構造体、12a,
12b…回動軸部材、13…ラッチ部材、13a…係止
溝、13b…マニピュレータ操作部、13c…ロックピ
ン、14…軸受部材、15,17,22…ばね部材、1
6…ロックレバー、16a…ロック部、16b…押圧
部、18a,18b…軸支部材、19a,19b…案内
部、20…保持部材、20a…嵌合孔、21…係止部。10: mounting side structure, 11: mounting side structure, 12a,
12b: rotating shaft member, 13: latch member, 13a: locking groove, 13b: manipulator operating portion, 13c: lock pin, 14: bearing member, 15, 17, 22: spring member, 1
6 Lock lever, 16a Lock part, 16b Press part, 18a, 18b Support member, 19a, 19b Guide part, 20 Holding member, 20a Fitting hole, 21 Lock part.
Claims (1)
で結合してなる宇宙用構造体の着脱装置において、前記
構造体の取付側及び被取付側のいずれか一方の結合部に
互いに逆方向に突出されて設けられるもので、前記略逆
三角形状の同一直線上の二頂点を構成する一対の回動軸
部材と、前記構造体の取付側及び被取付側のいずれか一
方の結合部に前記一対の回動軸部材と同一面内の他の頂
点に結合方向に延出されて該結合部方向と略平行の軸回
りに回転自在に設けられるもので、先端部に係止溝が設
けられ、基端部に操作部が設けられたラッチ部材と、前
記構造体の取付側及び被取付側のいずれか他方の結合部
に設けられて前記回動軸部材が着脱自在に装着され、該
回動軸部材を前記結合方向に対して略直交する軸回りに
回動自在に支持する一対の軸支部材と、前記構造体の取
付側及び被取付側のいずれか他方の結合部に設けられて
前記ラッチ部材が着脱自在に装着されるもので、装着さ
れた該ラッチ部材の前記係止溝に対向して出入り自在に
設けられる係止部材を有した保持手段と、この保持手段
の係止部材を前記ラッチ部材の係止溝を係止する方向に
移動付勢する付勢手段と、前記ラッチ部材を前記保持部
材より離脱した状態で回転を規制して前記保持手段への
装着を許容し、その装着状態で前記ラッチ部材の回転操
作を許容して前記係止部材を前記付勢手段に抗して移動
付勢して該ラッチ部材の離脱を許容する規制手段とを具
備したことを特徴とする宇宙用構造体の着脱装置。1. A space structure attaching / detaching device in which structures are connected to each other at three points of a substantially inverted triangular vertex, wherein one of the connecting portions on the mounting side and the mounting side of the structure is attached to the connecting portion. A pair of rotating shaft members that are provided so as to protrude in opposite directions to each other and form two apexes on the same straight line of the substantially inverted triangle, and one of the mounting side and the mounting side of the structure body The connecting portion extends at the other vertex in the same plane as the pair of rotating shaft members in the connecting direction and is rotatably provided around an axis substantially parallel to the connecting portion direction. A latch member provided with a groove and an operation portion provided at a base end portion, and the rotation shaft member provided at one of the other connecting portions on the mounting side and the mounting side of the structure so as to be detachably mounted. And the rotatable shaft member is supported so as to be rotatable around an axis substantially orthogonal to the coupling direction. A pair of shaft support members, and the latch member is provided at the other connecting portion on either the mounting side or the mounted side of the structure, and the latch member is removably mounted. Holding means having a locking member provided so as to be able to come in and out facing the stop groove, and urging means for moving and urging the locking member of the holding means in a direction for locking the locking groove of the latch member; The rotation of the latch member is restricted by detaching the latch member from the holding member to allow the latch member to be mounted on the holding means, and the latch member is allowed to rotate in the mounted state to urge the locking member. And a restricting means for allowing the latch member to be disengaged by moving and biasing against the means.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3120233A JP3004078B2 (en) | 1991-05-24 | 1991-05-24 | Space structure attachment / detachment device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3120233A JP3004078B2 (en) | 1991-05-24 | 1991-05-24 | Space structure attachment / detachment device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH04345599A JPH04345599A (en) | 1992-12-01 |
| JP3004078B2 true JP3004078B2 (en) | 2000-01-31 |
Family
ID=14781153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3120233A Expired - Lifetime JP3004078B2 (en) | 1991-05-24 | 1991-05-24 | Space structure attachment / detachment device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3004078B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6831561B2 (en) * | 2015-12-11 | 2021-02-17 | 国立研究開発法人宇宙航空研究開発機構 | Coupling device |
-
1991
- 1991-05-24 JP JP3120233A patent/JP3004078B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH04345599A (en) | 1992-12-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2536538B1 (en) | Driver accessory | |
| US4773123A (en) | Automatically extensible and retractable wheel unit for mounting on a corner of a suitcase | |
| JP2602815B2 (en) | Joint device | |
| JPS6058868B2 (en) | lever-operated wheelchair | |
| JPH0725045B2 (en) | Robot | |
| JP2004122353A (en) | Articulated arm transfer device | |
| JP3004078B2 (en) | Space structure attachment / detachment device | |
| US4570340A (en) | Tool having a multi-positional handle | |
| US5513544A (en) | Locking, retracting mechanism for crank handles | |
| KR100193305B1 (en) | Handle bar of the stroller | |
| JP2690829B2 (en) | Joint movement type robot | |
| JP3048970B2 (en) | Fixing device and workpiece transfer jig | |
| JPH042396B2 (en) | ||
| JP3027764B2 (en) | Method for attaching and detaching a heald shaft of a loom to and from a driving device and the loom | |
| JPH0253278B2 (en) | ||
| JP3155767B2 (en) | Detachable device for assembled antenna | |
| JPS5837327A (en) | Safety coupling device | |
| JP3124054B2 (en) | Detachable device for assembled antenna | |
| TW201408420A (en) | Handling device | |
| JPS6316892Y2 (en) | ||
| JP3349762B2 (en) | Assembling device for assembly type antenna reflector | |
| JPS5892019A (en) | Remote control system | |
| CN220682660U (en) | Folding frame and unmanned aerial vehicle | |
| CN223734893U (en) | Rotating member and robot device | |
| JP3865464B2 (en) | Space equipment coupling equipment |