CN108860665A - 一种阻尼可控的对接机构传动缓冲系统 - Google Patents
一种阻尼可控的对接机构传动缓冲系统 Download PDFInfo
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- 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
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109573112A (zh) * | 2018-12-10 | 2019-04-05 | 上海航天控制技术研究所 | 一种航天器对接机构主动对接控制方法 |
CN109572846A (zh) * | 2019-01-15 | 2019-04-05 | 北京史河科技有限公司 | 一种连接装置及具有该连接装置的机器设备 |
CN113277127A (zh) * | 2021-06-15 | 2021-08-20 | 北京邮电大学 | 一种基于陀螺结构的空间软对接装置 |
CN113893128A (zh) * | 2021-09-23 | 2022-01-07 | 北京邮电大学 | 一种用于上肢可穿戴式康复机械臂的双模驱动关节 |
Citations (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4809936A (en) * | 1987-10-08 | 1989-03-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Space module assembly apparatus with docking alignment flexibility and restraint |
US4858857A (en) * | 1988-12-30 | 1989-08-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Docking mechanism for spacecraft |
JPH115600A (ja) * | 1997-06-17 | 1999-01-12 | Nissan Motor Co Ltd | ブースタロケットの結合装置 |
US6354540B1 (en) * | 1998-09-29 | 2002-03-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Androgynous, reconfigurable closed loop feedback controlled low impact docking system with load sensing electromagnetic capture ring |
CN101323377A (zh) * | 2008-08-06 | 2008-12-17 | 哈尔滨工业大学 | 三臂型非合作目标对接机构 |
US7543779B1 (en) * | 2007-01-19 | 2009-06-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low-impact mating system |
CN104335697B (zh) * | 2006-08-30 | 2011-03-30 | 上海宇航系统工程研究所 | 空间对接机构缓冲试验台 |
US8056864B2 (en) * | 2004-03-18 | 2011-11-15 | Michigan Aerospace Corporation | Docking system |
CN102294690A (zh) * | 2011-05-12 | 2011-12-28 | 哈尔滨工业大学 | 面向空间大型机械臂和交会对接的大容差对接捕获装置 |
CN102923318A (zh) * | 2012-11-26 | 2013-02-13 | 上海宇航系统工程研究所 | 异体同构、刚度阻尼闭环反馈控制的弱撞击式对接系统 |
CN103303499A (zh) * | 2013-06-26 | 2013-09-18 | 哈尔滨工业大学 | 一种空间非合作目标卫星的对接捕获装置 |
CN106507773B (zh) * | 2012-06-18 | 2014-10-22 | 上海新跃仪表厂 | 航天产品对接机构控制驱动装置 |
CN104335699B (zh) * | 2007-11-16 | 2015-04-29 | 上海宇航系统工程研究所 | 飞行器对接机构旋转式双向缓冲装置 |
CN104913018A (zh) * | 2015-05-11 | 2015-09-16 | 上海宇航系统工程研究所 | 一种具有缓冲耗能功能的驱动装置 |
CN105021379A (zh) * | 2014-04-28 | 2015-11-04 | 上海航天设备制造总厂 | 一种可控阻尼器测试装置 |
US20150314893A1 (en) * | 2014-05-02 | 2015-11-05 | Macdonald Dettwiler & Associates Inc. | Spacecraft capture mechanism |
CA2910438A1 (en) * | 2014-10-24 | 2016-04-24 | Thales | Manipulation of a satellite in space |
CN105711859A (zh) * | 2016-01-25 | 2016-06-29 | 上海宇航系统工程研究所 | 异体同构、缓冲阻尼半主动控制对接系统及方法 |
CN105836164A (zh) * | 2016-04-27 | 2016-08-10 | 北京空间飞行器总体设计部 | 一种航天器级间适配结构 |
CN106143952A (zh) * | 2016-07-05 | 2016-11-23 | 中国空间技术研究院 | 一种用于卫星对接的缓冲消旋阻尼装置 |
CN106240849A (zh) * | 2016-07-22 | 2016-12-21 | 上海宇航系统工程研究所 | 航天器对接系统及方法 |
RU2624959C1 (ru) * | 2016-04-28 | 2017-07-11 | Акционерное общество "Научно-производственное объединение им. С.А.Лавочкина" | Адаптер для попутного выведения полезных нагрузок |
US20170259946A1 (en) * | 2017-05-30 | 2017-09-14 | Wayne Neville White, JR. | Interplanetary spacecraft |
CN107975546A (zh) * | 2017-12-08 | 2018-05-01 | 阿尔特汽车技术股份有限公司 | 电磁式牙嵌离合器结构 |
CN108507543A (zh) * | 2017-09-07 | 2018-09-07 | 哈尔滨工业大学 | 航天器对接捕获过程的位姿测量装置及柔顺控制方法 |
-
2018
- 2018-09-11 CN CN201811057025.XA patent/CN108860665B/zh active Active
Patent Citations (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4809936A (en) * | 1987-10-08 | 1989-03-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Space module assembly apparatus with docking alignment flexibility and restraint |
US4858857A (en) * | 1988-12-30 | 1989-08-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Docking mechanism for spacecraft |
JPH115600A (ja) * | 1997-06-17 | 1999-01-12 | Nissan Motor Co Ltd | ブースタロケットの結合装置 |
US6354540B1 (en) * | 1998-09-29 | 2002-03-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Androgynous, reconfigurable closed loop feedback controlled low impact docking system with load sensing electromagnetic capture ring |
US8056864B2 (en) * | 2004-03-18 | 2011-11-15 | Michigan Aerospace Corporation | Docking system |
CN104335697B (zh) * | 2006-08-30 | 2011-03-30 | 上海宇航系统工程研究所 | 空间对接机构缓冲试验台 |
US7543779B1 (en) * | 2007-01-19 | 2009-06-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low-impact mating system |
CN104335699B (zh) * | 2007-11-16 | 2015-04-29 | 上海宇航系统工程研究所 | 飞行器对接机构旋转式双向缓冲装置 |
CN101323377A (zh) * | 2008-08-06 | 2008-12-17 | 哈尔滨工业大学 | 三臂型非合作目标对接机构 |
CN102294690A (zh) * | 2011-05-12 | 2011-12-28 | 哈尔滨工业大学 | 面向空间大型机械臂和交会对接的大容差对接捕获装置 |
CN106507773B (zh) * | 2012-06-18 | 2014-10-22 | 上海新跃仪表厂 | 航天产品对接机构控制驱动装置 |
CN102923318A (zh) * | 2012-11-26 | 2013-02-13 | 上海宇航系统工程研究所 | 异体同构、刚度阻尼闭环反馈控制的弱撞击式对接系统 |
CN103303499A (zh) * | 2013-06-26 | 2013-09-18 | 哈尔滨工业大学 | 一种空间非合作目标卫星的对接捕获装置 |
CN105021379A (zh) * | 2014-04-28 | 2015-11-04 | 上海航天设备制造总厂 | 一种可控阻尼器测试装置 |
US20150314893A1 (en) * | 2014-05-02 | 2015-11-05 | Macdonald Dettwiler & Associates Inc. | Spacecraft capture mechanism |
CA2910438A1 (en) * | 2014-10-24 | 2016-04-24 | Thales | Manipulation of a satellite in space |
CN104913018A (zh) * | 2015-05-11 | 2015-09-16 | 上海宇航系统工程研究所 | 一种具有缓冲耗能功能的驱动装置 |
CN105711859A (zh) * | 2016-01-25 | 2016-06-29 | 上海宇航系统工程研究所 | 异体同构、缓冲阻尼半主动控制对接系统及方法 |
CN105836164A (zh) * | 2016-04-27 | 2016-08-10 | 北京空间飞行器总体设计部 | 一种航天器级间适配结构 |
RU2624959C1 (ru) * | 2016-04-28 | 2017-07-11 | Акционерное общество "Научно-производственное объединение им. С.А.Лавочкина" | Адаптер для попутного выведения полезных нагрузок |
CN106143952A (zh) * | 2016-07-05 | 2016-11-23 | 中国空间技术研究院 | 一种用于卫星对接的缓冲消旋阻尼装置 |
CN106240849A (zh) * | 2016-07-22 | 2016-12-21 | 上海宇航系统工程研究所 | 航天器对接系统及方法 |
US20170259946A1 (en) * | 2017-05-30 | 2017-09-14 | Wayne Neville White, JR. | Interplanetary spacecraft |
CN108507543A (zh) * | 2017-09-07 | 2018-09-07 | 哈尔滨工业大学 | 航天器对接捕获过程的位姿测量装置及柔顺控制方法 |
CN107975546A (zh) * | 2017-12-08 | 2018-05-01 | 阿尔特汽车技术股份有限公司 | 电磁式牙嵌离合器结构 |
Non-Patent Citations (6)
Title |
---|
张华等: "空间对接机构缓冲试验台分离性能分析", 《载人航天》 * |
张崇峰等: "飞船空间对接机构技术", 《中国科学:技术科学》 * |
沈涛等: "一种新型弱撞击对接机构运动学分析", 《航空学报》 * |
邱华勇等: "空间对接机构热真空环境对接与分离试验技术研究", 《载人航天》 * |
陈宝东等: "对接机构分系统研制", 《上海航天》 * |
高金忠等: "一种对接机构转子杯式电磁阻尼器设计研究", 《上海航天》 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109573112A (zh) * | 2018-12-10 | 2019-04-05 | 上海航天控制技术研究所 | 一种航天器对接机构主动对接控制方法 |
CN109572846A (zh) * | 2019-01-15 | 2019-04-05 | 北京史河科技有限公司 | 一种连接装置及具有该连接装置的机器设备 |
CN113277127A (zh) * | 2021-06-15 | 2021-08-20 | 北京邮电大学 | 一种基于陀螺结构的空间软对接装置 |
CN113893128A (zh) * | 2021-09-23 | 2022-01-07 | 北京邮电大学 | 一种用于上肢可穿戴式康复机械臂的双模驱动关节 |
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Inventor after: Qiu Huayong Inventor after: Zhang Chongfeng Inventor after: Yuan Huiling Inventor after: Yao Jian Inventor after: Ding Lichao Inventor after: Liu Lujiang Inventor after: Gao Jinzhong Inventor after: Liu Zhi Inventor after: Shi Junwei Inventor before: Qiu Huayong Inventor before: Zhang Chongfeng Inventor before: Yuan Huiling Inventor before: Yao Jian Inventor before: Ding Lichao Inventor before: Gao Jinzhong Inventor before: Liu Zhi Inventor before: Shi Junwei |
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