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JPH0281799A - Holding and stabilizing device - Google Patents

Holding and stabilizing device

Info

Publication number
JPH0281799A
JPH0281799A JP23153188A JP23153188A JPH0281799A JP H0281799 A JPH0281799 A JP H0281799A JP 23153188 A JP23153188 A JP 23153188A JP 23153188 A JP23153188 A JP 23153188A JP H0281799 A JPH0281799 A JP H0281799A
Authority
JP
Japan
Prior art keywords
work
shaft
holding
skirt
stabilizing device
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.)
Pending
Application number
JP23153188A
Other languages
Japanese (ja)
Inventor
Yasushi Mori
康 森
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 JP23153188A priority Critical patent/JPH0281799A/en
Publication of JPH0281799A publication Critical patent/JPH0281799A/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は1例えば月面等の低重力空間において月面基
地設置等大質量物を取り扱う際における作業機の姿勢の
保持1作業環境の安定化に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] This invention relates to 1) maintaining the posture of a working machine when handling large objects such as setting up a lunar base in a low-gravity space such as the lunar surface; 1) stabilizing the working environment; It is about transformation.

〔従来の技術〕[Conventional technology]

近年、スペースシャトル、アリアンロケット等のロケッ
トの打ち上げ機の能力向上に伴い、宇宙基地1月面基地
の建設気運が益々増大している。このなかで1月面基地
の建設構想も各国で盛んに研究が行われている。
In recent years, as the capabilities of rocket launchers such as the Space Shuttle and Ariane rocket have improved, momentum for constructing a January space base has been increasing. In this context, the concept of constructing a base on the January surface is being actively researched in various countries.

従来の宇宙における人類の活動は、無人探査機や有人探
査機による観測、サンプル採取、観測機器の設置等の作
業が行)れている。
Traditional human activities in space include observation using unmanned and manned spacecraft, sample collection, and installation of observation equipment.

このような作業において使用されている機器の一例とし
て第7図に示すようなサンプル採取用のマニピユレータ
がある。第7図のマニピュレータは、駆動装置(lI&
cよって、腕(9)を伸ばし、エンドエフェクタ(81
Kよって探査機構体円囲へ土壌のサンプルを採取してく
るといった作業を行う。
An example of equipment used in such work is a sample collection manipulator as shown in FIG. The manipulator shown in FIG.
c Therefore, extend the arm (9) and press the end effector (81).
K therefore performs work such as collecting soil samples from around the exploration mechanism.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

従来性われている宇宙空間における作業では、サンプル
採取、観測器の設置といった小質量物を取シ扱う作業し
か存在せず作業によりて発生する内力が1作業装置や探
査機に対する外乱となることは無かりた。しかし、現在
検討がすすんでいる月面基地の建設等に含まれる作業は
1作業対象物が大質量で1作業環境が低重力環境なため
1作業によって発生する内力が作業装置や探査機に対し
て充分に大きな外乱となるという課題がめる。
In conventional work in space, there is only work that involves handling small-mass objects such as collecting samples and installing observation instruments, and the internal force generated by the work does not cause disturbance to work equipment or probes. It wasn't there. However, in the work involved in the construction of a lunar base, which is currently under consideration, one work object has a large mass and the work environment is a low gravity environment, so the internal force generated by the work is applied to the work equipment and the spacecraft. This poses the problem of creating a sufficiently large disturbance.

この発明は、かかる課題を解決する友めになされたもの
で、低重力下の作業装置や探査機に対して、大質量の作
業対象物を扱う時に充分な姿勢の保持1作業環境の安定
を持たせることが可能で1部品点数が少なく9組立調整
が比較的容易で、かつ作業装置や探査機が移動を行う必
要が生じた場合、即座に拘束を解いて移動を可能とする
という従来に無い特徴を備えた保持安定化装@Lを得る
ことを目的とするものである。
This invention was made to solve these problems, and it is necessary to maintain a sufficient posture and stabilize the working environment when handling large-mass workpieces for working equipment and probes under low gravity. It is possible to hold the robot, has a small number of parts, and is relatively easy to assemble and adjust, and when it becomes necessary to move the work equipment or probe, it can be immediately released from the restraints and moved. The purpose of this is to obtain a holding and stabilizing device @L that has features that do not exist.

1)5唖の 〔課題を解決#;写苫芋七手段〕 この発明に係る保持安定化装置は、液体を噴霧するノズ
ルと、ヒータを内蔵したシャフトと、前記ノズルが取シ
付いて、前記シャフトの回りを駆動装置により設定した
向きに回転可能なスカートとにより構成するものでおる
1) 5 [Solving the Problem #; 7 Means for Sharing] The holding and stabilizing device according to the present invention includes a nozzle for spraying a liquid, a shaft having a built-in heater, and a shaft to which the nozzle is attached. It consists of a skirt that can be rotated around the shaft in a set direction by a drive device.

〔作 用〕[For production]

この発明における保持安定化装置は、設置時において1
作業機等の脚部先端で、ヒータが内蔵されているシャフ
ト部が月面等の作業環境に接地され、前記シャフトの回
9t−駆動装置によって回転自在に動くスカートにより
シャフトと作業環境との接地箇所への直接の太陽照射を
さえぎシ、シャフト部の宇宙空間への放射冷却によりシ
ャフト部を低温化させ、その後、前記スカートに複数設
置されたノズルより、シャフト部の低温箇所で凍結する
液体を噴霧することにより1作業機等の前記シャフト部
と月面等の作業環境との拘束が行え、また、前記スカー
トを反転させ前記シャフト部に太陽照射が行われるよう
にしたり、前記シャフト部に内蔵されているヒータに通
電することにより、低温箇所の凍結を解凍して拘束が解
除できるというものである。
The holding and stabilizing device in this invention has 1
At the tip of the leg of a working machine, a shaft with a built-in heater is grounded in a working environment such as the moon surface, and a skirt that is rotatably moved by a drive device connects the shaft to the working environment. The shaft part is cooled by radiation cooling into outer space by blocking direct sunlight irradiation to the part, and then the liquid that freezes at the low temperature part of the shaft part is cooled by multiple nozzles installed on the skirt. By spraying, it is possible to restrain the shaft part of a working machine, etc., from the work environment such as the moon surface, and also to invert the skirt so that the shaft part is irradiated with sunlight, or to make the shaft part built in the shaft part By energizing the heater, the freeze in the low-temperature area can be thawed and the restraint can be released.

〔実施例〕〔Example〕

第1図は、この発明における保持安定化装置を組み込ん
だ月面作業機の一実施例を示す図でおる。第1図におい
て・、α2Fi3本の指から構成され地面を掘ったり、
物を保持することが可能なエンドエフェクタ、α3は前
記エンドエフェクタαのと第1のアーム(lSy−つな
ぎ。
FIG. 1 is a diagram showing an embodiment of a lunar surface work machine incorporating a holding and stabilizing device according to the present invention. In Figure 1, α2Fi is composed of three fingers and digs the ground,
The end effector α3 capable of holding an object is connected to the first arm (lSy-connector) of the end effector α.

エンドエフェクタaX5″Ik:第1図紙面垂直方向の
回転軸に関して回転させることが可能な駆動装置、 (
141は前記第1のアームfIs中に同軸に組み込まれ
て前記エンドエフェクタa’a@前記第1のアームUS
の軸まわシに回転させることが可能な駆動装置、α61
は前記第1のアーム+isと第2のアームtty+’6
つなぎ、前記第1のアーム+isより先端の部分(駆動
装置α4も含む)を第1図紙面垂直方向の回転軸に関し
て回転させることが可能な駆動装置、 Qlは前記第2
のアーム顛とペース@をつなぎ、前記第2のアーム(1
ツより先端の部分を第1図紙面垂直方向の回転軸に関し
て回転させることが可能な駆動装置、α9は前記ペース
(至)と作業機本体c!3’t−つなぎ、前記ペース■
よシ先端のアーム全体をWI1図紙面面内で作業機本体
@に垂直な回転軸に関して回転させることが可能な駆動
装置、@ハ前記作業機本体□□□に取υ付き作業機の移
動、姿勢変更に用いられるスラスタ、C2υは作業機の
進行方向や、エンドエフェクタの状態をモニタするのに
用いられる視覚装置、@は本作業機の制御や動力供給を
行うユニットが収納された制御/動力源装置、@、@は
前記各部より構成される月面作業機を、低重力場の環境
において1例えば月面等の作業環境に対して容易に同定
し、また移動の必要が生じ友時に簡単にその拘束を解除
することが可能な保持安定化装置でるる。
End effector aX5''Ik: A drive device that can rotate about a rotation axis perpendicular to the paper surface of Figure 1, (
141 is coaxially incorporated into the first arm fIs and the end effector a'a@the first arm US
A drive device that can rotate around the shaft of α61
are the first arm +is and the second arm tty+'6
a drive device capable of rotating a portion at the tip of the first arm +is (including the drive device α4) about a rotation axis perpendicular to the paper surface of the first drawing; Ql is the second arm;
Connect the arm length and pace @, and connect the second arm (1
α9 is a drive device capable of rotating the tip portion of the tip about the rotation axis in the direction perpendicular to the plane of the first drawing. 3't-connection, the above pace ■
A drive device capable of rotating the entire arm at the tip of the horizontal axis about a rotation axis perpendicular to the work machine body within the WI1 drawing plane; The thruster used to change the attitude, C2υ is a visual device used to monitor the direction of movement of the work machine and the state of the end effector, @ is the control/power unit that houses the unit that controls and supplies power to this work machine. The source device, @, @ is used to easily identify the lunar surface working machine consisting of the above-mentioned parts in a working environment such as the lunar surface in a low gravity field environment, and also to easily identify it when moving is necessary. There is a holding and stabilizing device that can release the restraint.

第4図、第5図、第6図は、この発明における保持安定
化装置の一実施例を示す図である。
FIG. 4, FIG. 5, and FIG. 6 are diagrams showing an embodiment of the holding and stabilizing device according to the present invention.

第4図、第5図、第6図の(1)は作業機等の脚部の先
端について月面等の作業環境と接地を行うシャフト、+
21は前記シャフト(1)に取り付き、接地時のシャフ
トの安定t−はかるサボ−)、(31は前記シャフト(
1)に対して、駆動装[(41i介して1回転自在に取
り付けられ太陽照射をさえぎるように設定を行うスカー
ト。
(1) in Figures 4, 5, and 6 is a shaft that connects the tip of the leg of a working machine to the working environment such as the lunar surface; +
21 is attached to the shaft (1), and 31 is attached to the shaft (1) to stabilize the shaft when it touches the ground.
1), the driving device [(41i) is attached to the skirt so that it can rotate freely once and is set to block sunlight.

(5)は前記シャフト(1)に内蔵されシャフト(1)
金めたためることが可能なヒータ、 (61,(7)は
前記スカート(3)に取υ付き液体全噴霧するノズル、
@は以上の各構成品を包み外界の熱環境から保持安定装
置e断熱するインシエレーション、@は前記ノズル+6
1. (7+に液体を供給する補給管である。
(5) is built in the shaft (1) and the shaft (1)
A heater that can be filled with gold, (61, (7) is a nozzle attached to the skirt (3) and sprays all of the liquid,
@ is an insulation that wraps each of the above components and insulates them from the external thermal environment, @ is the nozzle + 6
1. (This is a supply pipe that supplies liquid to 7+.

次に動作について説明する。Next, the operation will be explained.

このような第1図に示す月面作業機が1月面基地建設等
の作業を実施する場合に想定される作業としては、建設
予定地の地ならし。
When the lunar surface work machine shown in Figure 1 carries out work such as the construction of a base on the January surface, the expected work is leveling the ground at the planned construction site.

建設資材の運搬、建設資材の組み立て等1重量物を扱り
たり、大出力を要求される作業が考えられる。その−例
として、第2図に地ならし作業、第3図KIA投資材の
運搬の模様を示す。
Possible tasks include transporting construction materials, assembling construction materials, and other tasks that involve handling heavy objects or requiring large outputs. As examples, Figure 2 shows the ground leveling work, and Figure 3 shows the transportation of KIA investment materials.

第2図、第3図にも示すように1月面作業機が地ならし
、資材の運搬等の大出力な作用カバ、を要求される作業
を実施する場合、必ず作業対象物からの反カイ、口を受
ける。宇宙機器は打ち上げ時の重量制限から極力軽量化
されて製造が行われているので、自重は同様の地上機器
に比べて非常に軽いと考えて良く、シかも、低重力場に
おいて作業を行うので自重は増々軽くなり1作業実施時
の反力によって月面作業機自体の横滑り、横転等が生じ
る可能性がある。
As shown in Figures 2 and 3, when a surface work machine performs work that requires a high-output cover such as grading the ground or transporting materials, it is sure to receive anti-chip from the work object. Receive your mouth. Space equipment is manufactured to be as light as possible due to weight restrictions at the time of launch, so it can be considered that its own weight is much lighter than similar ground equipment. As its own weight becomes lighter and lighter, there is a possibility that the lunar surface work machine itself may skid or roll over due to the reaction force when performing one task.

この為1月面作業機を月面等作業環境にしっかりと固定
する事が1作業1+施するうえで、ぜひとも必要となっ
てくる。しかし1月面基地の建設等では、その作業範囲
が非常に広範囲におよぶため、移動が必要となった際に
は1作業環境に対する固定vh単に解除することも可能
でなければならない。このような要求を満たすために1
月面作業機等では第1図、第2図、第3図に示すように
1作業機の下面に月面等の作業環境を容易に固定、解除
可能なように、保持安定化felt(至)、四の具備が
必要となる。
For this reason, it is absolutely necessary to securely fix the lunar surface work equipment to the lunar surface or other working environment in order to carry out 1 work 1+. However, in the case of construction of a base on the January surface, etc., the scope of work is extremely wide, so when it becomes necessary to move, it must be possible to simply release the fixed VH for one work environment. In order to meet these requirements, 1
As shown in Figures 1, 2, and 3, in lunar surface work machines, holding and stabilizing felts are installed on the underside of each work machine so that the work environment, such as the lunar surface, can be easily fixed and released. ), four items are required.

保持安定化装置の具体的動作について説明する。The specific operation of the holding and stabilizing device will be explained.

第4図は、保持安定化装置の作業環境への接地前の概観
及び構成品の概要を示している。第5図は0作業環境へ
保持安定化装置が接地した状態を示している。前記(3
)のスカートは駆動制御装置t(図中省略)より信号を
受けて、前記(1)のシャフトの回りを回転する躯動装
(III (41によって、太陽光が照射される向きに
設置され、前記シャフト(11,サポート(2)周辺全
放射冷却により低温下する。前記スカート(3)に設置
されているノズル+61. (71よりi体二が噴霧さ
れ、前記シャツ) (1)、 サポート(2)周辺に結
露が生じる。
FIG. 4 shows an overview of the holding and stabilizing device before it is grounded in the working environment and an overview of its components. FIG. 5 shows a state in which the holding and stabilizing device is grounded to the zero working environment. Said (3
) is installed in the direction in which sunlight is irradiated by the sliding device (III (41) that rotates around the shaft of (1) in response to a signal from the drive control device t (not shown). The entire area around the shaft (11, support (2) is cooled by radiation cooling. Nozzle +61 installed on the skirt (3). 2) Condensation forms around the area.

第6図は、前記第5図の状態を継続した場合に、噴霧さ
れた液体二が、固体ホに変化し作業環境と保持安定化装
置の拘束を完了した状態を示す。
FIG. 6 shows a state in which the sprayed liquid 2 changes to solid E and the work environment and the holding and stabilizing device are completely restrained when the state shown in FIG. 5 is continued.

拘束を解除する場合には、前記駆動装&(4)を駆動制
御装置(図中省略)により逆回転させ、前記スカー) 
(31t−逆転させ、前記シャ7H1)、サポート(2
)周辺部に直接太陽光照射を当てるとともに、前記ヒー
タ(5)に通′区して加熱させることによシ、前記固体
ホを解凍し拘束の解除を行う。
To release the restraint, the drive unit & (4) is reversely rotated by a drive control device (not shown), and the scar
(31t-reverse, said shaft 7H1), support (2
) The solid body is thawed and released from restraint by directly irradiating the surrounding area with sunlight and passing through the heater (5) to heat it.

〔発明の効果〕〔Effect of the invention〕

以上のようにこの発明によれば、複雑な機構や大規模な
作業環境の整備を必要とせずに、前記の保持安定化装置
を容易に構成でき。
As described above, according to the present invention, the above-mentioned holding and stabilizing device can be easily configured without requiring a complicated mechanism or a large-scale work environment.

しかも作業領域を移動する際に保持安定装置を簡単に固
定、解除できるという効果がるる。
Moreover, the holding and stabilizing device can be easily fixed and released when moving around the work area.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図、第2図、第3図は、この発明における保持安定
化fe置全全組込んだ月面作業機の一実施例を示す図で
、第1図は1月面作業機の各構成要素を説明する図で、
第2図は、その月面作業機が作業全実施している状態を
示す図、第3図は1月面作業機が建設資材等の大質量物
を取シ扱りている状態を示す図、第4図、i5図、第6
図は、この発明による保持安定化f、lilの一実施例
を示す図で、第4図は接地前状態、第5図は作業環境接
地状態を示す図で、第6図は作業拘束状態會示す図、第
7図は、従来、宇宙空間における作業において使用され
ている機器の一例を示す図である。 図においてα2はエンドエフェクタ、 Q3. α41
゜ne、α11.(19は駆動装置、cJJはスラスタ
、+29は視覚装置、(社)は制御/動力源装置、(至
)は作業機本体、Q4.(ハ)は保持安定化装置、田は
ベース、19は第1のアーム、aηは第2のアーム、(
1)はシャフト、(2)はサポート、(3)はスカート
、(4)は駆動装置、 +5)Vi上ヒータ  +61
. (7)はノズル、(8)はエンドエフェクタ、(9
)は腕、α1は駆wJ装置、αυは探査機構体である。 なお1図中同一符号は、同一または相当部分を示す。
Figures 1, 2, and 3 are diagrams showing an embodiment of the lunar surface working machine in which the holding and stabilizing FE system of the present invention is fully incorporated. A diagram explaining the components,
Figure 2 shows the state in which the lunar surface work machine is performing all the work, and Figure 3 shows the state in which the lunar surface work machine is handling large objects such as construction materials. , Figure 4, Figure i5, Figure 6
The figures show an embodiment of the holding and stabilizing f, lil according to the present invention, in which Fig. 4 shows the state before contact with the ground, Fig. 5 shows the state of contact with the work environment, and Fig. 6 shows the state of the work restraint state. The figure shown in FIG. 7 is a diagram showing an example of equipment conventionally used in work in outer space. In the figure, α2 is the end effector, Q3. α41
゜ne, α11. (19 is the drive device, cJJ is the thruster, +29 is the visual device, Co., Ltd. is the control/power source device, (to) is the work equipment body, Q4. (c) is the holding and stabilizing device, ta is the base, 19 is The first arm, aη, is the second arm, (
1) is shaft, (2) is support, (3) is skirt, (4) is drive device, +5) Vi upper heater +61
.. (7) is a nozzle, (8) is an end effector, (9
) is the arm, α1 is the driving wJ device, and αυ is the exploration mechanism. Note that the same reference numerals in Figure 1 indicate the same or corresponding parts.

Claims (1)

【特許請求の範囲】[Claims] 月面や小惑星等の低重力環境を移動しつつ所定の作業を
行う作業機の保持安定化装置において、地面と接するシ
ャフトと、前記シャフトの回りを回転するスカートと、
前記スカートに取付けられ、地面と接する上記シャフト
周辺部に液体を噴霧するノズルと、上記シャフトを加熱
するためのヒータと、作業機の地面への固定時、上記ス
カートを太陽光照射の方向に位置するように回転させる
とともに上記ノズルを作動させる手段と、作業機の固定
解除時、上記スカートを上記固定時と逆方向に回転させ
るとともに上記ヒータを駆動する手段とを具備した保持
安定化装置。
In a holding and stabilizing device for a working machine that performs a predetermined work while moving in a low gravity environment such as the moon surface or an asteroid, the device includes: a shaft in contact with the ground; a skirt that rotates around the shaft;
a nozzle that is attached to the skirt and sprays a liquid around the shaft that is in contact with the ground; a heater that heats the shaft; and a heater that positions the skirt in the direction of sunlight irradiation when the working machine is fixed to the ground. A holding and stabilizing device comprising means for rotating the nozzle and operating the nozzle so as to rotate the skirt in a direction opposite to that when the work machine is fixed and driving the heater when the working machine is unfixed.
JP23153188A 1988-09-16 1988-09-16 Holding and stabilizing device Pending JPH0281799A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23153188A JPH0281799A (en) 1988-09-16 1988-09-16 Holding and stabilizing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23153188A JPH0281799A (en) 1988-09-16 1988-09-16 Holding and stabilizing device

Publications (1)

Publication Number Publication Date
JPH0281799A true JPH0281799A (en) 1990-03-22

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP23153188A Pending JPH0281799A (en) 1988-09-16 1988-09-16 Holding and stabilizing device

Country Status (1)

Country Link
JP (1) JPH0281799A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016014320A1 (en) 2014-07-22 2016-01-28 Ethridge Edwin Microwave extraction of volatiles from planetary bodies

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016014320A1 (en) 2014-07-22 2016-01-28 Ethridge Edwin Microwave extraction of volatiles from planetary bodies
EP3172293A4 (en) * 2014-07-22 2018-07-11 Ethridge, Edwin Microwave extraction of volatiles from planetary bodies
EP3760694A1 (en) * 2014-07-22 2021-01-06 Ethridge, Edwin Microwave extraction of volatiles from planetary bodies

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