ATE252017T1 - Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen - Google Patents

Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen

Info

Publication number
ATE252017T1
ATE252017T1 AT99500146T AT99500146T ATE252017T1 AT E252017 T1 ATE252017 T1 AT E252017T1 AT 99500146 T AT99500146 T AT 99500146T AT 99500146 T AT99500146 T AT 99500146T AT E252017 T1 ATE252017 T1 AT E252017T1
Authority
AT
Austria
Prior art keywords
coupled
structures
components
damping properties
stiffness
Prior art date
Application number
AT99500146T
Other languages
English (en)
Inventor
Doncel Miguel Lancho
Revuelta Enrique Cabrera
Castan Fernando Cespedosa
Original Assignee
Const Aeronauticas Sa
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 Const Aeronauticas Sa filed Critical Const Aeronauticas Sa
Application granted granted Critical
Publication of ATE252017T1 publication Critical patent/ATE252017T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F3/00—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/50—Bridged by diverse connector
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/59—Manually releaseable latch type
    • Y10T403/591—Manually releaseable latch type having operating mechanism
    • Y10T403/593—Remotely actuated
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/21—Elements
    • Y10T74/2121—Flywheel, motion smoothing-type
    • Y10T74/2132—Structural detail, e.g., fiber, held by magnet, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Road Paving Structures (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Body Structure For Vehicles (AREA)
  • Bridges Or Land Bridges (AREA)
AT99500146T 1998-11-18 1999-08-17 Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen ATE252017T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009802421A ES2166234B1 (es) 1998-11-18 1998-11-18 Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.

Publications (1)

Publication Number Publication Date
ATE252017T1 true ATE252017T1 (de) 2003-11-15

Family

ID=8305834

Family Applications (1)

Application Number Title Priority Date Filing Date
AT99500146T ATE252017T1 (de) 1998-11-18 1999-08-17 Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen

Country Status (10)

Country Link
US (1) US6305871B1 (de)
EP (1) EP1002717B1 (de)
JP (1) JP2000154667A (de)
CN (1) CN1107615C (de)
AT (1) ATE252017T1 (de)
CA (1) CA2287066A1 (de)
DE (1) DE69912070T2 (de)
ES (1) ES2166234B1 (de)
RU (1) RU2237601C2 (de)
UA (1) UA61950C2 (de)

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GB2372976B (en) * 2000-09-18 2004-07-07 Saab Ericsson Space Ab An Adaptor for a Spacecraft
SE0003315L (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
ES2307813T3 (es) * 2002-12-04 2008-12-01 Eads Casa Espacio, S.L. Dispositivo atenuador.
US7222823B2 (en) * 2004-07-06 2007-05-29 Ata Engineering, Inc. Payload adapter
US20060145016A1 (en) * 2004-12-30 2006-07-06 The Boeing Company Mating of spacecraft components using shape memory materials
US7748663B1 (en) * 2005-05-24 2010-07-06 Lockheed Martin Corporation Launch vehicle stage integration device
US7905453B2 (en) * 2006-12-21 2011-03-15 Intelsat Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary
US7866607B2 (en) * 2006-12-21 2011-01-11 Intelsat Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite
EP2989345B1 (de) 2013-04-24 2019-04-10 Marquette University Aktuator mit variabler steifigkeit und grossem steifheitsbereich
CN105339640B (zh) 2013-07-02 2018-07-17 Mra系统有限责任公司 发动机和带状夹具
CN104058103A (zh) * 2014-06-27 2014-09-24 北京空间飞行器总体设计部 一种用于航天器柔性充气展开结构的刚柔连接结构
CN106864775A (zh) * 2015-12-11 2017-06-20 天津航天瑞莱科技有限公司 一种航天器有效载荷减冲击装置
CN109476023B (zh) 2016-04-14 2020-04-14 马凯特大学 可变刚度串联式弹性致动器
CN108638593A (zh) * 2018-03-09 2018-10-12 北京宇航系统工程研究所 一种蜂窝阻尼颗粒冲击减缓装置
CN109693810B (zh) * 2018-12-29 2022-04-26 西北工业大学 一种用于空间碎片清理的纳星结构
CN109823576B (zh) * 2019-02-20 2020-11-24 上海卫星工程研究所 用于行星着陆器的承载连接结构
CN111619831B (zh) * 2020-04-29 2021-11-16 航天东方红卫星有限公司 一种连杆式星箭分离机构
CN112249364A (zh) * 2020-10-28 2021-01-22 哈尔滨工业大学 小卫星的结构系统、小卫星及组装小卫星的方法
CN113152708A (zh) * 2021-02-10 2021-07-23 国机集团科学技术研究院有限公司 以水平抗震为主的振震双控控制策略
CN113415440B (zh) * 2021-07-20 2022-06-17 哈尔滨工业大学 一种快速展开支撑装置
CN115853962B (zh) * 2022-11-25 2025-07-11 上海卫星工程研究所 被动式航天器太阳翼挠性振动抑制装置及航天器
CN117246530B (zh) * 2023-10-12 2026-04-17 航天科工火箭技术有限公司 一种卫星及火箭
CN122040788A (zh) * 2025-02-20 2026-05-15 中国科学院微小卫星创新研究院 一种具环形减振器的航天飞行器

Family Cites Families (20)

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Publication number Priority date Publication date Assignee Title
US3346929A (en) * 1966-03-04 1967-10-17 James E Webb Latching mechanism
US3458217A (en) * 1966-11-25 1969-07-29 Joseph D Pride Jr Tubular coupling having low profile band segments with means for preventing relative rotation
US3505925A (en) * 1967-10-16 1970-04-14 Mc Donnell Douglas Corp Structure release system
US3529417A (en) * 1967-11-16 1970-09-22 Trw Inc Fluid pressure actuated linear force generating means
US3633456A (en) * 1969-07-03 1972-01-11 Mc Donnell Douglas Corp Power-actuated separation system
US3564564A (en) * 1969-11-21 1971-02-16 Nasa Latching mechanism
US3737117A (en) * 1971-07-06 1973-06-05 Nasa Docking structure for spacecraft
FR2516893A1 (fr) * 1981-11-26 1983-05-27 Aerospatiale Systeme permettant le maintien temporaire et la liberation de deux parties, plus particulierement dans le domaine spatial
FR2648199B1 (fr) 1989-06-09 1991-09-27 Aerospatiale Dispositif de liaison temporaire, notamment pour appendice de satellite artificiel, et procede de liberation d'une telle liaison
JP2609729B2 (ja) * 1989-11-02 1997-05-14 宇宙開発事業団 衛星とロケットおよびアポジ・キック・エンジンとの結合／分離方法
FR2664338B1 (fr) * 1990-07-04 1992-10-23 Aerospatiale Dispositif de liaison entre deux objets par plusieurs points de fixation.
US5244170A (en) * 1991-10-15 1993-09-14 General Dynamics Corporation, Space Systems Division Passive nonlinear interface strut (PNIS)
RU2066799C1 (ru) * 1992-07-02 1996-09-20 Дмитрий Юганесович Аллик Виброизолирующая опора
US5352061A (en) * 1993-01-05 1994-10-04 Honeywell Inc. Anti-rotation ring joint
RU2044661C1 (ru) * 1994-08-29 1995-09-27 Волжское муниципальное производственно-техническое предприятие "АВТОПРОМ" Пневматическая подвеска
FR2735099B1 (fr) * 1995-06-06 1997-08-29 Aerospatiale Dispositif adaptateur basculant pour l'emport de plusieurs charges utiles sur un meme lanceur.
ES2120338B1 (es) 1995-10-16 1999-05-01 Const Aeronauticas Sa Sistema de fijacion y separacion para satelites.
FR2758791B1 (fr) * 1997-01-29 1999-03-26 Centre Nat Etd Spatiales Dispositif de suspension d'une charge utile dans un lanceur spatial
US5961078A (en) * 1997-06-27 1999-10-05 Mcdonnell Douglas Corporation Passive axial vibration isolation system for a spacecraft launch vehicle
ES2131476B1 (es) 1997-09-26 2000-03-01 Const Aeronauticas Sa Sistema de fijacion y separacion de satelites.

Also Published As

Publication number Publication date
EP1002717B1 (de) 2003-10-15
ES2166234B1 (es) 2003-02-16
UA61950C2 (en) 2003-12-15
CN1253898A (zh) 2000-05-24
CA2287066A1 (en) 2000-05-18
US6305871B1 (en) 2001-10-23
DE69912070D1 (de) 2003-11-20
ES2166234A1 (es) 2002-04-01
EP1002717A3 (de) 2000-10-11
DE69912070T2 (de) 2004-08-05
RU2237601C2 (ru) 2004-10-10
CN1107615C (zh) 2003-05-07
EP1002717A2 (de) 2000-05-24
JP2000154667A (ja) 2000-06-06

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