JPH04212986A - Movable holding device - Google Patents

Movable holding device

Info

Publication number
JPH04212986A
JPH04212986A JP2400866A JP40086690A JPH04212986A JP H04212986 A JPH04212986 A JP H04212986A JP 2400866 A JP2400866 A JP 2400866A JP 40086690 A JP40086690 A JP 40086690A JP H04212986 A JPH04212986 A JP H04212986A
Authority
JP
Japan
Prior art keywords
holding device
movable holding
electromagnets
flight simulator
magnetic poles
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.)
Withdrawn
Application number
JP2400866A
Other languages
Japanese (ja)
Inventor
Koji Tamada
玉田 康二
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2400866A priority Critical patent/JPH04212986A/en
Publication of JPH04212986A publication Critical patent/JPH04212986A/en
Withdrawn legal-status Critical Current

Links

Abstract

PURPOSE:To cause a subject to be turned up and down over a wider angle range than usual and also rotate the subject in its horizontal direction. CONSTITUTION:A plurality of permanent magnets 13 are arranged in the pattern of a check on the outer periphery of the bottom portion 13 of a spherical subject to be held (e.g. a flight simulator 11) in such a manner that different magnetic poles are arranged alternately. Also a plurality of electromagnets (14 and 15) are arranged in a check pattern beneath the permanent magnet in such a manner that different magnetic poles are arranged alternately on the inner periphery of a hemisphere having a recessed upper portion. The direction and strength of magnetic forces of the electromagnets are controlled.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は、例えばフライトシミュ
レータなどに適用される可動形保持装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a movable holding device applied to, for example, a flight simulator.

【0002】0002

【従来の技術】図3は従来のフライトシミュレータにお
いて使用されている可動形保持装置の構造説明図である
。図において、本可動形保持装置はフライトシミュレー
タ1を複数の油圧シリンダ2を介して取付台3上に保持
するようになっており、油圧シリンダ2を伸縮させるこ
とによりフライトシミュレータ1の俯仰を行うようにな
っている。
2. Description of the Related Art FIG. 3 is a structural diagram of a movable holding device used in a conventional flight simulator. In the figure, this movable holding device holds the flight simulator 1 on a mounting base 3 via a plurality of hydraulic cylinders 2, and by expanding and contracting the hydraulic cylinders 2, the flight simulator 1 is raised and lowered. It has become.

【0003】0003

【発明が解決しようとする課題】上記のような従来の可
動形保持装置において、本装着により保持されるフライ
トシミュレータ1の俯仰角度は油圧シリンダ2が伸縮す
る長さで制限されるため、フライトシミュレータ1を広
範囲な角度にわたって俯仰させることが困難である。ま
た、油圧シリンダ2の構造上フライトシミュレータ1を
水平方向に旋回させることはできない。
[Problems to be Solved by the Invention] In the conventional movable holding device as described above, the elevation angle of the flight simulator 1 held by the actual installation is limited by the length of the extension and contraction of the hydraulic cylinder 2. 1 is difficult to raise and lower over a wide range of angles. Further, due to the structure of the hydraulic cylinder 2, the flight simulator 1 cannot be rotated horizontally.

【0004】0004

【課題を解決するための手段】本発明に係る可動形保持
装置は上記課題の解決を目的にしており、球面をなす被
保持体の底部外周に碁盤目状に配設され互いに異なる磁
極が交互に並ぶ複数の永久磁石と、該永久磁石の下方に
上部が凹の半球内周に碁盤目状に配設され互いに異なる
磁極が交互に並ぶ複数の電磁石と、該電磁石の磁力の向
きおよび強度を制御する手段とを備えた構成を特徴とし
ている。
[Means for Solving the Problems] A movable holding device according to the present invention aims to solve the above problems, and is arranged in a checkerboard pattern around the bottom outer periphery of a spherical held object, and different magnetic poles are alternately arranged. A plurality of permanent magnets lined up in a row, a plurality of electromagnets arranged in a checkerboard pattern on the inner periphery of a hemisphere with a concave upper part below the permanent magnets, and with mutually different magnetic poles arranged alternately; The invention is characterized by a configuration including means for controlling.

【0005】[0005]

【作用】即ち、本発明に係る可動形保持装置においては
、球面をなす被保持体の底部外周に複数の永久磁石が互
いに異なる磁極が交互に並ぶように碁盤目状に配設され
るとともにこの永久磁石の下方に複数の電磁石が上部が
凹の半球内周に互いに異なる磁極が交互に並ぶように碁
盤目状に配設されこの電磁石の磁力の向きおよび強度が
制御されるようになっており、電磁石の磁力の向きおよ
び強度を適宜制御することにより電磁石の磁力と永久磁
石の磁力とによるリニアモーターと同様の作用により被
保持体を浮上させながら俯仰、旋回させる。
[Operation] That is, in the movable holding device according to the present invention, a plurality of permanent magnets are arranged in a checkerboard pattern on the outer periphery of the bottom of the spherical held body so that different magnetic poles are arranged alternately. Below the permanent magnet, a plurality of electromagnets are arranged in a grid pattern on the inner periphery of a hemisphere with a concave top so that different magnetic poles are arranged alternately, and the direction and strength of the magnetic force of these electromagnets is controlled. By appropriately controlling the direction and strength of the magnetic force of the electromagnet, the held object is elevated, elevated, and rotated while being levitated by an action similar to that of a linear motor due to the magnetic force of the electromagnet and the magnetic force of the permanent magnet.

【0006】[0006]

【実施例】図1および図2は本発明の一実施例に係る可
動形保持装置の構造説明図である。図において、本実施
例に係る可動形保持装置は戦闘機訓練用のフライトシミ
ュレータにおいて使用されており、図に示すようにフラ
イトシミュレータ11を磁力により鉄心15上に浮上さ
せて支持するようになっている。即ち、フライトシミュ
レータ11の底部12は球形ドーム状になっており、こ
の底部12の外周に永久磁石13が碁盤目状に取り付け
られ、この永久磁石13のS極、N極が縦横交互に並ぶ
ように配列されている。また、鉄心15は半円球の籠形
をしており、この内側に巻線14が取り付けられ、巻線
14、鉄心15、巻線14に電流を供給する電線17、
電流を制御する制御装置18などにより電磁石を構成し
ている。この電磁石もそのS極、N極が縦横交互に並ぶ
ように、碁盤目状に配列されている。鉄心15は取付台
16により床上に固定されている。電磁石から発生する
磁力の発生方向および強度は制御装置18により巻線1
4に流す電流を制御することにより変化させることがで
き、フライトシミュレータ11をこの電磁石上に載置し
て浮上させながら俯仰、旋回させるようになっている。
DESCRIPTION OF THE PREFERRED EMBODIMENTS FIGS. 1 and 2 are structural diagrams of a movable holding device according to an embodiment of the present invention. In the figure, the movable holding device according to the present embodiment is used in a flight simulator for fighter jet training, and as shown in the figure, the flight simulator 11 is suspended and supported on an iron core 15 by magnetic force. There is. That is, the bottom part 12 of the flight simulator 11 has a spherical dome shape, and permanent magnets 13 are attached to the outer periphery of the bottom part 12 in a grid pattern, so that the S and N poles of the permanent magnets 13 are arranged alternately vertically and horizontally. are arranged in Further, the iron core 15 has a cage shape of a semicircular sphere, and the winding 14 is attached to the inside thereof, and the winding 14, the iron core 15, the electric wire 17 that supplies current to the winding 14,
An electromagnet is constituted by a control device 18 that controls current. These electromagnets are also arranged in a checkerboard pattern so that their S and N poles are alternately arranged vertically and horizontally. The iron core 15 is fixed on the floor by a mounting base 16. The direction and strength of the magnetic force generated from the electromagnet are controlled by the control device 18 in the winding 1.
The flight simulator 11 can be changed by controlling the current flowing through the electromagnet 4, and the flight simulator 11 is placed on this electromagnet and is raised, raised, and turned while being levitated.

【0007】このように、本装置はフライトシミュレー
タ11の半球状の底部12の外周に永久磁石13をその
S極、N極が交互に並ぶように配列するとともに、籠状
の鉄心15の内側に巻線14を取り付けて電流を巻線1
4に供給することにより磁力を発生させる電磁石のS極
、N極が交互に並ぶように配列しており、巻線14に電
流を供給することにより鉄心15に発生する磁力を制御
装置18により電流をコントロールして適宜制御するこ
とにより、電磁石の磁力と永久磁石13の磁力とによる
リニアモーターと同様の作用によりフライトシミュレー
タ11を浮上させながら俯仰、旋回させることができる
ので、従来のフライトシミュレータに比べて実際の戦闘
機に近い動作を模擬することができ、特に従来のフライ
トシミュレータでは困難であった空間識の認識の訓練も
可能になる。
In this way, this device arranges the permanent magnets 13 around the outer periphery of the hemispherical bottom 12 of the flight simulator 11 so that their S and N poles are arranged alternately, and also arranges the permanent magnets 13 inside the cage-shaped iron core 15. Attach winding 14 and transfer current to winding 1
The magnetic force generated in the iron core 15 by supplying current to the winding 14 is converted into a current by the control device 18. By appropriately controlling the magnetic force of the electromagnet and the magnetic force of the permanent magnet 13, the flight simulator 11 can be raised, raised, and turned while being levitated by the action similar to that of a linear motor due to the magnetic force of the electromagnets and the magnetic force of the permanent magnet 13. It is possible to simulate the movements of an actual fighter jet, and in particular, it is possible to train spatial awareness, which is difficult with conventional flight simulators.

【0008】なお、永久磁石13をフライトシミュレー
タ11の外周全体に取り付ければ、フライトシミュレー
タ11を360度にわたって俯仰、旋回させることがで
きる。また、本装置はフライトシミュレータの他にレジ
ャー用ジェットコースタのシミュレータや宇宙遊泳シミ
ュレータなどの駆動装置としても適用が可能である。
[0008] If the permanent magnet 13 is attached to the entire outer circumference of the flight simulator 11, the flight simulator 11 can be raised, raised, and rotated over 360 degrees. In addition to flight simulators, this device can also be used as a driving device for leisure roller coaster simulators, spacewalk simulators, and the like.

【0009】[0009]

【発明の効果】本発明に係る可動形保持装置は前記の通
り構成されており、リニアモーターと同様の作用により
被保持体を浮上させながら俯仰、旋回させるので、被浮
上体を従来よりも広範囲な角度に俯仰させるとともに水
平方向にも旋回させることができる。
[Effects of the Invention] The movable holding device according to the present invention is constructed as described above, and because it levitates the object to be held by the same action as a linear motor, it can be lifted up, down, and rotated, so that the object to be held can be moved over a wider range than before. It can be tilted up and down at different angles and also rotated horizontally.

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

【図1】図1は本発明の一実施例に係る可動形保持装置
の断面図である。
FIG. 1 is a sectional view of a movable holding device according to an embodiment of the present invention.

【図2】図2(a)はその要部正面図、同図(b)は要
部断面図である。
FIG. 2(a) is a front view of the main part thereof, and FIG. 2(b) is a sectional view of the main part.

【図3】図3は従来の可動形保持装置の斜視図である。FIG. 3 is a perspective view of a conventional movable holding device.

【符号の説明】[Explanation of symbols]

11  フライトシミュレータ 12  フライトシミュレータの底部 13  永久磁石 14  巻線 15  鉄心 17  電線 18  制御装置 11 Flight simulator 12 Bottom of flight simulator 13 Permanent magnet 14 Winding wire 15 Iron core 17 Electric wire 18 Control device

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】  球面をなす被保持体の底部外周に碁盤
目状に配設され互いに異なる磁極が交互に並ぶ複数の永
久磁石と、該永久磁石の下方に上部が凹の半球内周に碁
盤目状に配設され互いに異なる磁極が交互に並ぶ複数の
電磁石と、該電磁石の磁力の向きおよび強度を制御する
手段とを備えたことを特徴とする可動形保持装置。
Claim 1: A plurality of permanent magnets arranged in a grid pattern on the outer periphery of the bottom of a held body having a spherical surface and having mutually different magnetic poles arranged alternately; A movable holding device comprising a plurality of electromagnets arranged in a grid pattern and having different magnetic poles arranged alternately, and means for controlling the direction and strength of the magnetic force of the electromagnets.
JP2400866A 1990-12-07 1990-12-07 Movable holding device Withdrawn JPH04212986A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2400866A JPH04212986A (en) 1990-12-07 1990-12-07 Movable holding device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2400866A JPH04212986A (en) 1990-12-07 1990-12-07 Movable holding device

Publications (1)

Publication Number Publication Date
JPH04212986A true JPH04212986A (en) 1992-08-04

Family

ID=18510736

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2400866A Withdrawn JPH04212986A (en) 1990-12-07 1990-12-07 Movable holding device

Country Status (1)

Country Link
JP (1) JPH04212986A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2358524A (en) * 1999-10-27 2001-07-25 Moog Inc Two-axis pointing motor
KR100417950B1 (en) * 1999-12-30 2004-02-11 주식회사 케이티 Satellite motion control testing experiment
JP2006204006A (en) * 2005-01-20 2006-08-03 Sony Corp Electromagnetic actuator and electronic apparatus
KR100903435B1 (en) * 2007-10-18 2009-06-18 샬롬엔지니어링 주식회사 A train simulation apparatus
CN112513474A (en) * 2018-07-27 2021-03-16 穆格公司 Actuator
EP4012324A1 (en) * 2012-05-22 2022-06-15 Haptech, Inc. Method and apparatus for firearm recoil simulation
US11512919B2 (en) 2012-05-22 2022-11-29 Haptech, Inc. Methods and apparatuses for haptic systems

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2358524A (en) * 1999-10-27 2001-07-25 Moog Inc Two-axis pointing motor
KR100417950B1 (en) * 1999-12-30 2004-02-11 주식회사 케이티 Satellite motion control testing experiment
JP2006204006A (en) * 2005-01-20 2006-08-03 Sony Corp Electromagnetic actuator and electronic apparatus
JP4615318B2 (en) * 2005-01-20 2011-01-19 ソニー株式会社 Electromagnetic actuator and electronic equipment
KR100903435B1 (en) * 2007-10-18 2009-06-18 샬롬엔지니어링 주식회사 A train simulation apparatus
EP4012324A1 (en) * 2012-05-22 2022-06-15 Haptech, Inc. Method and apparatus for firearm recoil simulation
US11512919B2 (en) 2012-05-22 2022-11-29 Haptech, Inc. Methods and apparatuses for haptic systems
US11656053B2 (en) 2012-05-22 2023-05-23 Haptech, Inc. Method and apparatus for firearm recoil simulation
CN112513474A (en) * 2018-07-27 2021-03-16 穆格公司 Actuator
JP2022511235A (en) * 2018-07-27 2022-01-31 ムーグ べスローテン フェンノートシャップ Actuator with snubber assembly
US11506230B2 (en) 2018-07-27 2022-11-22 Moog Bv Actuator with snubber assembly
CN112513474B (en) * 2018-07-27 2023-10-17 穆格公司 Actuator with a spring

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Legal Events

Date Code Title Description
A300 Application deemed to be withdrawn because no request for examination was validly filed

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 19980312