JP2507351Y2 - Holding and releasing device - Google Patents

Holding and releasing device

Info

Publication number
JP2507351Y2
JP2507351Y2 JP1990056928U JP5692890U JP2507351Y2 JP 2507351 Y2 JP2507351 Y2 JP 2507351Y2 JP 1990056928 U JP1990056928 U JP 1990056928U JP 5692890 U JP5692890 U JP 5692890U JP 2507351 Y2 JP2507351 Y2 JP 2507351Y2
Authority
JP
Japan
Prior art keywords
holder
bracket
hook
solar cell
opening
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
Application number
JP1990056928U
Other languages
Japanese (ja)
Other versions
JPH0416100U (en
Inventor
昭夫 辻畑
雅行 冨田
学 蒲ケ原
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP1990056928U priority Critical patent/JP2507351Y2/en
Publication of JPH0416100U publication Critical patent/JPH0416100U/ja
Application granted granted Critical
Publication of JP2507351Y2 publication Critical patent/JP2507351Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【考案の詳細な説明】 〔産業上の利用分野〕 この考案は,人工衛星に搭載される展開型太陽電池パ
ドルを,収納状態で衛星本体に固定し,軌道上にて固定
状態を解除する為の保持解放装置に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] This invention is for fixing the deployable solar cell paddle mounted on an artificial satellite to the satellite body in the stored state and releasing the fixed state in orbit. The present invention relates to a holding / releasing device.

〔従来の技術〕 第5図(a),(b),第6図および第7図(a)
(b)は従来の保持解放装置の例を示すものでは(1)
は人工衛星本体,(2)は太陽電池パドル,(3)はブ
ラケツト,(4)は前記ブラケツト(3)を前記人工衛
星本体(1)に固定するボルト,(5)は前記ブラケツ
ト(3)の中を摺動するスライド・シヤフト,(6)は
前記スライド・シヤフト(5)に組込まれたコイルバ
ネ,(7)はクランプロツド,(8)はブロツク,
(9)は前記クランプロツド(7)と前記ブロツク
(8)に固定された板バネ,(11)はフツク,(12)は
前記ブラケツト(3)に固定されたピン,(13)前記ピ
ン(12)に組込まれたスペーサ,(14)はナツト,(1
5)は前記フツク(11)に組込まれたボルト,(16)は
前記ボルト(15)に明けられた穴を通るワイヤ,(17)
はナツト,(18)は前記太陽電池パドル(2)の端部に
組込まれたブツシユ,(19)はワイヤ切断機構(詳細は
省く)である。
[Prior Art] Figs. 5 (a), 5 (b), 6 and 7 (a)
(B) shows an example of a conventional holding and releasing device (1)
Is a satellite body, (2) is a solar array paddle, (3) is a bracket, (4) is a bolt for fixing the bracket (3) to the satellite body (1), and (5) is the bracket (3). A slide shaft that slides in the inside, (6) a coil spring incorporated in the slide shaft (5), (7) a clamp rod, (8) a block,
(9) is a leaf spring fixed to the clamp rod (7) and the block (8), (11) is a hook, (12) is a pin fixed to the bracket (3), (13) is the pin (12 ), Spacer (14) is nut, (1
5) is a bolt incorporated in the hook (11), (16) is a wire passing through a hole formed in the bolt (15), (17)
Is a nut, (18) is a bush installed at the end of the solar cell paddle (2), and (19) is a wire cutting mechanism (details are omitted).

従来の保持解放装置は上記のように構成され,収納状
態の太陽電池パドル(2)を板バネ(9)によりブツシ
ユ(18)を介してブラケツト(3)上に押え込み,この
時クランプロツド(7)をスライドシヤフト(5)に設
けた穴hの中にはめ込み且つ,ワイヤ(16)を矢印Aの
方向に引張ることにより,ピン(12)回りに回転可能な
フツク(11)を介してスライドシヤフト(5)を矢印B
の方向に押し込むことによりクランプロツド(7)を固
定して太陽電池パドル(2)を人工衛星本体(1)に固
定する。
The conventional holding / releasing device is configured as described above, and the solar cell paddle (2) in the housed state is pressed by the leaf spring (9) onto the bracket (3) via the bush (18), and at this time, the clamp rod (7). By inserting the wire (16) into the hole h provided in the slide shaft (5) and pulling the wire (16) in the direction of the arrow A, the slide shaft (11) is rotatable around the pin (12). 5) Arrow B
The clamp rod (7) is fixed by pushing in the direction of to fix the solar cell paddle (2) to the artificial satellite body (1).

矢印Aの方向に張力がかけられたワイヤ(16)は人工
衛星本体(1)上を引き廻して,ワイヤ切断機構(19)
にて固定される。前記状態にて打ち上げ後,軌道上でワ
イヤ切断機構(19)を作動させてワイヤ(16)の張力を
解放するとフツク(11)は矢印Cの方向へ回転し同時に
スライドシヤフト(5)が矢印Dの方向に滑べる。する
とクランプロツド(7)はスライドシヤフト(5)の凹
部hより自由となり板バネ(9)の力により矢印Eの方
向に巻上げられることにより太陽電池パドル(2)の固
定が解放され,展開可能な状態となる。
The wire (16), which is tensioned in the direction of arrow A, is drawn around the artificial satellite body (1) to form the wire cutting mechanism (19).
Fixed in. When the wire cutting mechanism (19) is operated on the track to release the tension of the wire (16) after launching in the above state, the hook (11) rotates in the direction of arrow C and at the same time the slide shaft (5) moves in the direction of arrow D. You can slide in the direction of. Then, the clamp rod (7) becomes free from the recess h of the slide shaft (5) and is wound up in the direction of the arrow E by the force of the leaf spring (9) to release the fixing of the solar cell paddle (2) and the deployable state. Becomes

〔考案が解決しようとする課題〕[Problems to be solved by the device]

上記のような従来の保持解放装置では,スライドシヤ
フト(5)がブラケツト(3)の中をスライドするため
高真空,熱膨張あるいは熱収縮を考慮してシヤフト
(5)とブラケツト(3)がかみ合わないよう材料を選
定しなければならずかつ,スライドシヤフト(5)のス
ライド部表面の仕上にも多大の注意を払つて製作しなけ
れば打ち上げ後の太陽電池パドルの解放が出来なくなる
可能性が出てくるという課題があつた。
In the conventional holding and releasing device as described above, since the slide shaft (5) slides in the bracket (3), the shaft (5) and the bracket (3) are engaged with each other in consideration of high vacuum, thermal expansion or thermal contraction. The material must be selected so that it will not be released, and the solar paddle after launch may not be released unless the slide surface of the slide shaft (5) is manufactured with great care. There was a problem of coming.

この考案はかかる課題を解決する為になされたもので
太陽電池パドルの保持解放の方法を従来のスライド方式
から回転方式に変更することにより打ち上げ後太陽電池
パドルの解放において従来より数段の成功率(信頼性)
を向上させることを目的とする。もちろん従来の利点で
ある太陽電池パドルを保持状態とする時に作業製が良
く,しかもワイヤ張力の測定が行い易く,また打ち上げ
時の振動によりワイヤが振れて太陽電池パドルに接触す
ることを防止出来ることをも損なわないようにしてあ
る。
This invention was made in order to solve such a problem.By changing the method of holding and releasing the solar cell paddle from the conventional slide method to the rotation method, the success rate of the solar cell paddle after launch is several stages higher than before. (reliability)
The purpose is to improve. Of course, the workability is good when the solar cell paddle is held, which is the conventional advantage, and the wire tension can be easily measured, and it is possible to prevent the wire from swinging and coming into contact with the solar cell paddle due to vibration at launch. I try not to spoil it.

〔課題を解決するための手段〕[Means for solving the problem]

この考案に係る保持解放装置は,従来の構成をほとん
ど変えないで,太陽電池パドルを保持するためのブラケ
ツトに組み込まれているスライドシヤフトを,スライド
方式から回転方式にした。
In the holding / releasing device according to the present invention, the slide shaft incorporated in the bracket for holding the solar cell paddle is changed from the slide type to the rotary type without changing the conventional configuration.

〔作用〕[Action]

この考案においては,太陽電池パドルの収納解放の方
法を回転方式にしたため,従来より太陽電池パドルの収
納解放が容易に出来かつ,そのための部品の製作も容易
に出来るものである。
In this invention, since the method of storing and releasing the solar cell paddles is the rotation method, the solar cell paddles can be stored and released more easily than before, and the components therefor can be easily manufactured.

〔実施例〕〔Example〕

第1図(a)(b)はこの考案の一実施例を示す図
で,第1図(a)は太陽電池パドルの収納状態を示す平
面図,第1図(b)は展開(解放)状態を示す平面図,
第2図は太陽電池パドルの収納状態を示す正面図,第3
図はこの考案の全体を示す正面図,第4図はこの考案の
保持解放装置を用いて太陽電池パドルを人工衛星本体に
取付けた状態図である。
1 (a) and 1 (b) are views showing an embodiment of the present invention, FIG. 1 (a) is a plan view showing a stored state of a solar cell paddle, and FIG. 1 (b) is a developed (released) state. A plan view showing the state,
FIG. 2 is a front view showing the storage state of the solar cell paddle, and FIG.
FIG. 4 is a front view showing the whole of the present invention, and FIG. 4 is a state view in which a solar cell paddle is attached to an artificial satellite body using the holding and releasing device of the present invention.

図において(1)〜(4),(7)〜(9),(11)
〜(19)は上記従来装置と同じであるが,異なるところ
は,フツク(11),ピン(12),スペーサ(13),ナツ
ト(14),(17),ボルト(15)およびワイヤ(16)を
第1図(a)及び第2図に示すように収納状態の太陽電
池パドル(2)の外側に配置するとともにへの字形状の
フツク(11)で,太陽電池パドル(2)の下にボルト
(4)によつて固定された箱形で1方向側だけオープン
となつているブラケツト(3)に従来使用していたスラ
イド式のスライドシヤフト(5)のかわりに役目を果た
す回転式のホルダー(10)を押し込む方式とすることに
よりクランプロツド(7)を固定するようにしたところ
にある。尚,このホルダー(10)には一端をブラケツト
(3)に固定したスプリング(20)が組み込まれてお
り,前記ホルダー(10)をフツク(11)側へ回転させよ
うとする力が働らくようにしてある。又,ホルダー(1
0)自身もピン(21)によりブラケツト(3)に組み込
まれている。
In the figure, (1) to (4), (7) to (9), (11)
~ (19) is the same as the above conventional device, except that the hook (11), the pin (12), the spacer (13), the nut (14), (17), the bolt (15) and the wire (16). ) Is placed on the outside of the solar array paddle (2) in the housed state as shown in FIGS. 1 (a) and 2 and a hook-shaped hook (11) is provided under the solar array paddle (2). A rotary type that serves as a substitute for the slide type slide shaft (5) that is conventionally used for the bracket (3) that is box-shaped and is open only on one side by bolts (4). The clamp rod (7) is fixed by pushing the holder (10). A spring (20) having one end fixed to the bracket (3) is incorporated in the holder (10) so that the force for rotating the holder (10) to the hook (11) side is exerted. I am doing it. Also, the holder (1
0) itself is also incorporated in the bracket (3) by the pin (21).

次にこの考案の動作を説明すぜ。 Next, I will explain the operation of this device.

まず収納状態の太陽電池パドル(2)を板バネ(9)
によりブツシユ(18)を介してブラケツト(3)上に押
え込み,この時クランプロツド(7)をホルダ(10)に
設けた凹部hの中にはめ込み且つ,ワイヤ(16)を矢印
Aの方向に引張ることにより,ピン(12)回りに回転可
能なフツク(11)を介してホルダー(10)を矢印Bの方
向に押し付けることにより太陽電池パドル(2)を人工
衛星本体(1)に固定する。前記ホルダー(10)には,
一端をブラケツト(3)に固定したスプリング(20)が
組み込まれており,前記ホルダー(10)をフツク(11)
側へ常に回転させようとする力が働らくようにしてあ
る。またホルダー(10)自身もピン(21)によりブラケ
ツト(3)に組み込まれている。
First, install the solar cell paddle (2) in the stored state into the leaf spring (9).
By pushing it onto the bracket (3) through the bush (18), at this time, the clamp rod (7) is fitted into the recess h provided in the holder (10), and the wire (16) is pulled in the direction of arrow A. Thus, the solar cell paddle (2) is fixed to the artificial satellite body (1) by pressing the holder (10) in the direction of arrow B through the hook (11) rotatable around the pin (12). In the holder (10),
A spring (20) with one end fixed to the bracket (3) is incorporated, and the holder (10) is hooked (11).
The force that always tries to rotate to the side works. The holder (10) itself is also incorporated in the bracket (3) by the pin (21).

矢印Aの方向に張力がかけられたワイヤ(16)は人工
衛星本体(1)上を引き廻して,ワイヤ切断機構(19)
にて固定される。前記状態にて打ち上げ後,軌道上でワ
イヤ切断機構(19)を作動させてワイヤ(16)の張力を
解放するとフツク(11)は矢印Cの方向へ回転し同時に
フツク(11)によりブラケツト(3)内に押し込まれて
いたホルダー(10)が解放状態となりホルダー(10)に
組み込まれたスプリング(20)によつてホルダー(10)
がフツク(11)側すなわち矢印D方向へブラケツト
(3)の底面にホルダー(10)が当たるまで回転する。
The wire (16), which is tensioned in the direction of arrow A, is drawn around the artificial satellite body (1) to form the wire cutting mechanism (19).
Fixed in. After launching in the above state, when the wire cutting mechanism (19) is operated on the orbit to release the tension of the wire (16), the hook (11) rotates in the direction of the arrow C and at the same time, the hook (11) causes the bracket (3) to move. The holder (10) pushed into the holder (10) is released, and the spring (20) built into the holder (10) allows the holder (10) to be released.
Rotates in the direction of the hook (11), that is, in the direction of arrow D until the holder (10) contacts the bottom surface of the bracket (3).

すると,クランプロツド(7)はホルダー(10)の凹
部hより自由となり板バネ(9)の力によぬ矢印Eの方
向に巻き上げられることにより,太陽電池パドル(2)
の固定が解放され,展開可能な状態となる。
Then, the clamp rod (7) becomes free from the recess h of the holder (10) and is wound up in the direction of arrow E without the force of the leaf spring (9), so that the solar cell paddle (2)
The fixation of is released, and it becomes a deployable state.

〔考案の効果〕[Effect of device]

この考案は以上説明した通り従来の基本的構成を変え
ることなくフツクおよびワイヤを収納状態の太陽電池パ
ドルの外側に配置しかつフツクで回転しようとするホル
ダーを押さえ込む方式とすることにより,太陽電池パド
ルを保持状態とする時に作業性が良いのはもちろんのこ
としかもワイヤの張力測定が容易で,また打ち上げ時の
振動によりケーブルが振れて太陽電池パドルに接触する
ことを防止出来,打ち上げ後太陽電池パドルを解放する
時,従来のスライドシヤフトをスライドさせる方式から
ホルダーを回転させる方式にしたことにより太陽電池パ
ドルを解放させる成功率(信頼性)が向上出来る効果が
ある。
As described above, the present invention has a structure in which the hook and wire are arranged outside the solar cell paddle in the stored state without changing the conventional basic structure, and the holder that is to be rotated by the hook is pressed down to make the solar cell paddle. The workability is not only good when it is held, but also the tension of the wire can be easily measured, and it is possible to prevent the cable from swaying and coming into contact with the solar array paddle due to the vibration during launch. When releasing the solar cell, the success rate (reliability) of releasing the solar cell paddle can be improved by changing the method of rotating the holder from the conventional method of sliding the slide shaft.

【図面の簡単な説明】[Brief description of drawings]

第1図(a)(b)はこの考案の一実施例を示す平面
図,第2図はその正面図,第3図は同じくこの考案の一
実施例を示す全体の正面図,第4図はこの考案の一実施
例の人工衛星本体への取付状態を示す図,第5図(a)
(b)は各々従来の保持解放装置正面図および平面図,
第6図は従来の保持解放装置の全体図,第7図(a)
(b)は各々従来の保持解放装置の保持状態,解放状態
を示す概念図である。 図において(1)は人工衛星本体,(2)は太陽電池パ
ドル,(3)はブラケツト,(4)はボルト,(5)は
スライドシヤフト,(6)はコイルバネ,(7)はクラ
ンプロツド,(8)はブロツク,(9)は板バネ,(1
0)はホルダー,(11)はフツク,(12)はピン,(1
3)はスペーサ,(14)はナツト,(15)はボルト,(1
6)はワイヤ,(17)はナツト,(18)はブツシユ,(1
9)はワイヤ切断機構,(20)はスプリング,(21)は
ピンである。 なお,図中同一符号は同一または相当部分を示す。
1 (a) and 1 (b) are plan views showing an embodiment of the present invention, FIG. 2 is a front view thereof, and FIG. 3 is an overall front view showing an embodiment of the present invention, FIG. Fig. 5 (a) is a diagram showing a state of attachment to the artificial satellite body of one embodiment of the present invention.
(B) is a front view and a plan view of a conventional holding and releasing device,
FIG. 6 is an overall view of a conventional holding and releasing device, FIG. 7 (a)
(B) is a conceptual diagram which shows the holding | maintenance state and the releasing state of the conventional holding | maintenance releasing device, respectively. In the figure, (1) is a satellite body, (2) is a solar array paddle, (3) is a bracket, (4) is a bolt, (5) is a slide shaft, (6) is a coil spring, (7) is a clamp rod, ( 8) is a block, (9) is a leaf spring, (1
(0) is a holder, (11) is a hook, (12) is a pin, (1
3) is a spacer, (14) is a nut, (15) is a bolt, (1
6) is a wire, (17) is a nut, (18) is a bush, (1)
9) is a wire cutting mechanism, (20) is a spring, and (21) is a pin. The same reference numerals in the drawings indicate the same or corresponding parts.

───────────────────────────────────────────────────── フロントページの続き (72)考案者 蒲ケ原 学 神奈川県鎌倉市上町屋730番地 三菱電 機エンジニアリング株式会社鎌倉事業所 内 (56)参考文献 実開 平2−141599(JP,U) ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Creator Kamagahara Manabu 730 Kamimachiya, Kamakura City, Kanagawa Mitsubishi Electric Engineering Co., Ltd., Kamakura Plant (56) References: Mitsuihei 2-141599

Claims (1)

(57)【実用新案登録請求の範囲】(57) [Scope of utility model registration request] 【請求項1】人工衛星に搭載される展開型太陽電池パド
ル用の保持解放装置において、人工衛星本体の前記太陽
電池パドル保持位置に固定された、開口部を有するブラ
ケットと、前記ブラケットの開口部に組込まれ、かつピ
ンにより回転支持された凹部を有するホルダーと、上記
ホルダーの凹部に出入り自由なクランプロッドと、前記
クランプロッドと収納状態の前記太陽電池パドルの最外
パネルの周縁部に設けられたブロックとで両端が固定さ
れ自由状態にて円弧を描くように成形された2枚の板バ
ネと、前記太陽電池パドル包絡域の外側にて前記ブラケ
ットに固定され、ピンにより回転支持されたへの字形の
フックと、前記フックに固定され、張力が与えられるこ
とにより、前記フックを回動させて上記フックを上記ホ
ルダーに当接させるとともに、前記フックの回動に伴な
い、前記クランプロッドが前記ホルダーの凹部と上記ブ
ラケットの開口部内壁との間に保持されるように前記ホ
ルダーを回動させるためのワイヤと、前記ブラケットに
設けられ、前記ホルダーの凹部が前記ブラケットの開口
部の開口方向に向くように前記ワイヤとフックによるホ
ルダーの回動方向に対し、反対方向の回動力を前記ホル
ダーに常時作用させるためのスプリングと、前記ワイヤ
の切断機構とを具備したことを特徴とする保持解放装
置。
1. A holding / releasing device for a deployment type solar cell paddle mounted on an artificial satellite, the bracket having an opening fixed to the solar cell paddle holding position of the artificial satellite body, and the opening of the bracket. A holder having a concave portion that is incorporated into and is rotatably supported by a pin, a clamp rod that can freely move in and out of the concave portion of the holder, and the clamp rod and the peripheral edge portion of the outermost panel of the solar cell paddle that is in a housed state. 2 leaf springs, which are fixed at both ends with a block and are shaped to draw an arc in a free state, and fixed to the bracket outside the solar cell paddle envelope area and rotatably supported by pins. It is fixed to the hook and the tension is applied to the hook so that the hook is rotated to bring the hook into contact with the holder. A wire for rotating the holder so that the clamp rod is held between the recess of the holder and the inner wall of the opening of the bracket as the hook rotates is provided on the bracket. A spring for constantly applying a turning force to the holder in a direction opposite to the rotation direction of the holder by the wire and the hook so that the recess of the holder faces the opening direction of the bracket opening; A holding / releasing device comprising a wire cutting mechanism.
JP1990056928U 1990-05-30 1990-05-30 Holding and releasing device Expired - Lifetime JP2507351Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1990056928U JP2507351Y2 (en) 1990-05-30 1990-05-30 Holding and releasing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1990056928U JP2507351Y2 (en) 1990-05-30 1990-05-30 Holding and releasing device

Publications (2)

Publication Number Publication Date
JPH0416100U JPH0416100U (en) 1992-02-10
JP2507351Y2 true JP2507351Y2 (en) 1996-08-14

Family

ID=31581189

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1990056928U Expired - Lifetime JP2507351Y2 (en) 1990-05-30 1990-05-30 Holding and releasing device

Country Status (1)

Country Link
JP (1) JP2507351Y2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02141599U (en) * 1989-04-26 1990-11-28

Also Published As

Publication number Publication date
JPH0416100U (en) 1992-02-10

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