ES2098689T3 - Estructura de posicionamiento y de estabilizacion de un objeto en un punto dado en el interior de una localizacion tridimensional. - Google Patents

Estructura de posicionamiento y de estabilizacion de un objeto en un punto dado en el interior de una localizacion tridimensional.

Info

Publication number
ES2098689T3
ES2098689T3 ES93400551T ES93400551T ES2098689T3 ES 2098689 T3 ES2098689 T3 ES 2098689T3 ES 93400551 T ES93400551 T ES 93400551T ES 93400551 T ES93400551 T ES 93400551T ES 2098689 T3 ES2098689 T3 ES 2098689T3
Authority
ES
Spain
Prior art keywords
positioning
given point
point inside
dimensional location
stabilization structure
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
ES93400551T
Other languages
English (en)
Inventor
Jean-Claude Bousquet
Bernard Maupetit
Michel Auroux
Gerard Goninet
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2098689T3 publication Critical patent/ES2098689T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G7/00Simulating cosmonautic conditions, e.g. for conditioning crews
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00Testing or checking of ammunition

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Details Of Measuring And Other Instruments (AREA)
  • Aerials With Secondary Devices (AREA)
  • Manipulator (AREA)
  • Electron Beam Exposure (AREA)

Abstract

LA INVENCION SE REFIERE A UN ESTRUCTURA DE POSICIONAMIENTO DE UN OBJETO EN UNA REFERENCIA TRIDIMENSIONAL. EL OBJETIVO DE LA INVENCION ES REALIZAR UNA ESTRUCTURA QUE PERMITA ORIENTAR UN OBJETO EN EL ESPACIO SIN DESPLAZAR SU CENTRO DE GRAVEDAD. ESTE OBJETIVO SE ALCANZA MEDIANTE UNA ESTRUCTURA QUE COMPRENDE UN SOPORTE (5) AL MENOS CINCO ESLINGAS (7, 9, 11 , 13, 27) DESTINADAS A SUSPENDE EL OBJETO (33) DE DICHO SOPORTE (5) Y MEDIOS DE AJUSTE (33) DE LA LONGITUD DE CADA ESLINGA. ESTA ESTRUCTURA PERMITE MAS EN PARTICULAR POSICIONAR UN ARTEFACTO TACTICO EN EL INTERIOR DE UNA CAMARA ANECOICA.
ES93400551T 1992-03-06 1993-03-03 Estructura de posicionamiento y de estabilizacion de un objeto en un punto dado en el interior de una localizacion tridimensional. Expired - Lifetime ES2098689T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9202724A FR2688294B1 (fr) 1992-03-06 1992-03-06 Structure de positionnement et de stabilisation d'un objet en un point donne a l'interieur d'un repere tridimensionnel.

Publications (1)

Publication Number Publication Date
ES2098689T3 true ES2098689T3 (es) 1997-05-01

Family

ID=9427446

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93400551T Expired - Lifetime ES2098689T3 (es) 1992-03-06 1993-03-03 Estructura de posicionamiento y de estabilizacion de un objeto en un punto dado en el interior de una localizacion tridimensional.

Country Status (5)

Country Link
US (1) US5370349A (es)
EP (1) EP0559560B1 (es)
DE (1) DE69307168T2 (es)
ES (1) ES2098689T3 (es)
FR (1) FR2688294B1 (es)

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FR2714180B1 (fr) * 1993-12-22 1996-03-08 Aerospatiale Attache de câble à rotule, notamment pour le positionnement d'un objet en chambre anéchoïque.
FR2810734B1 (fr) * 2000-06-21 2002-10-04 Aerospatiale Matra Missiles Dispositif de support d'un engin volant a moteur dans une soufflerie
IL164229A (en) * 2004-09-22 2010-05-17 Rafael Advanced Defense Sys Vibration damping pylon
CN102050230B (zh) * 2010-11-10 2013-06-19 湖北航天技术研究院总体设计所 一种平衡重力的级间分离试验装置及试验方法
CN102175391B (zh) * 2010-12-15 2012-08-29 河北汉光重工有限责任公司 红外制导导弹导引头重心位置的测量装置及其测量方法
CN102935901B (zh) * 2012-10-22 2015-12-30 浙江工业大学 二维主动跟随减重吊挂装置
CN102935900B (zh) * 2012-10-22 2015-12-30 浙江工业大学 恒张力减重吊挂装置
CN103085992B (zh) * 2012-11-23 2015-11-25 北京理工大学 空间微重力模拟实验系统
CN103010493B (zh) * 2012-12-06 2015-04-29 上海裕达实业公司 一种悬挂式重力补偿的太阳翼地面三维展开试验装置
CN103407589B (zh) * 2013-07-25 2016-01-13 北京空间飞行器总体设计部 一种二维展开太阳翼重力卸载装置
CN103482089B (zh) * 2013-10-09 2015-04-08 北京航空航天大学 一种无约束悬挂式主动重力补偿系统
CN103600856A (zh) * 2013-11-26 2014-02-26 北京卫星环境工程研究所 航天器垂直被动式分离试验设备
CN104743145B (zh) * 2013-12-31 2017-02-15 中国科学院沈阳自动化研究所 一种1/6g低重力平衡吊挂装置的控制系统
CN103925854B (zh) * 2014-04-03 2015-12-02 北京星航机电装备有限公司 一种基于三维坐标转换原理的导弹水平测量方法
CN104118580B (zh) * 2014-07-14 2016-10-19 上海宇航系统工程研究所 一种低重力模拟装置及方法
CN104385302B (zh) * 2014-10-15 2016-01-20 天津航天机电设备研究所 一种用于模拟多刚体机械臂运动的空间微低重力补偿方法
CN104406764B (zh) * 2014-10-29 2018-09-04 中国航空工业集团公司哈尔滨空气动力研究所 基于空间平行四边形原理的低速风洞张线振荡机构
CN104483089B (zh) * 2014-12-11 2017-03-15 中国航天空气动力技术研究院 全自由飞子母弹抛撒分离试验系统
CN104390529B (zh) * 2014-12-12 2016-03-02 中国航天空气动力技术研究院 半自由飞子母弹抛撒分离风洞试验系统
CN105836158A (zh) * 2016-04-21 2016-08-10 北京理工大学 一种地面展开柔性太阳翼重力卸载装置
CN105905320B (zh) * 2016-06-13 2017-11-10 北京航空航天大学 一种具有偏航随动的主动重力补偿系统
CN106323583B (zh) * 2016-08-31 2018-08-21 武汉一冶钢结构有限责任公司 一种风洞拐角组对方法
CN108725851A (zh) * 2018-05-21 2018-11-02 哈尔滨工业大学 一种四索并联式重力补偿机构及控制方法

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US2135394A (en) * 1934-09-05 1938-11-01 Rheinmetall Borsig Ag Power plant suspension means
US2953969A (en) * 1957-07-25 1960-09-27 Allen P Pepple Demonstration mirror and suspending and tilting system therefor
DE1070403B (es) * 1957-08-15 1959-12-03
US2869901A (en) * 1957-08-15 1959-01-20 Avro Aircraft Ltd Ball and socket coupling having air bearing means
US3032308A (en) * 1957-12-23 1962-05-01 Dansk Rontgen Teknik As Arrangement in suspending in cords or similar flexible carrying means, an x-ray tube or the like
US3160060A (en) * 1961-12-21 1964-12-08 Lockheed Aircraft Corp Missile transporting and launching system
US3421363A (en) * 1965-07-01 1969-01-14 Nasa Harness for vertically supporting slender bodies for vibration testing
US3516628A (en) * 1967-04-21 1970-06-23 Menasco Mfg Co Suspension system
US3469814A (en) * 1968-02-15 1969-09-30 Sheldon & Co E H Mirror suspension
US3731898A (en) * 1971-07-27 1973-05-08 Pneumo Dynamics Corp Missile suspension system
US4115845A (en) * 1977-03-31 1978-09-19 Kapcoa Corp. Automatic locking and support device for high mast lighting structure
US4135688A (en) * 1977-05-26 1979-01-23 Westinghouse Electric Corp. Anti-tilting resilient support system for aimed airborne pod-enclosed sensor instruments
GB1538035A (en) * 1977-06-21 1979-01-10 Bulychev G Device suspending an aircraft model in a wind tunnel
US4198022A (en) * 1978-03-10 1980-04-15 Johns-Manville Corporation Power cable guide for high-mast luminaire raising and lowering system
JPS60174924A (ja) * 1984-02-21 1985-09-09 Toshiba Corp 被試験体支持装置
US4604938A (en) * 1984-08-02 1986-08-12 The United States Of America As Represented By The Secretary Of The Navy Arresting and recovery system for test missiles

Also Published As

Publication number Publication date
FR2688294B1 (fr) 1994-05-27
EP0559560B1 (fr) 1997-01-08
EP0559560A1 (fr) 1993-09-08
FR2688294A1 (fr) 1993-09-10
US5370349A (en) 1994-12-06
DE69307168T2 (de) 1997-06-26
DE69307168D1 (de) 1997-02-20

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