CN110261152B - 一种叠加调整式多通道舵机加载系统 - Google Patents
一种叠加调整式多通道舵机加载系统 Download PDFInfo
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- CN110261152B CN110261152B CN201910525205.4A CN201910525205A CN110261152B CN 110261152 B CN110261152 B CN 110261152B CN 201910525205 A CN201910525205 A CN 201910525205A CN 110261152 B CN110261152 B CN 110261152B
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- 238000009434 installation Methods 0.000 claims abstract description 6
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- 229910000831 Steel Inorganic materials 0.000 claims description 29
- 239000010959 steel Substances 0.000 claims description 29
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- 238000000034 method Methods 0.000 abstract description 7
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- 238000004088 simulation Methods 0.000 abstract description 3
- 230000008878 coupling Effects 0.000 description 10
- 238000010168 coupling process Methods 0.000 description 10
- 238000005859 coupling reaction Methods 0.000 description 10
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M99/00—Subject matter not provided for in other groups of this subclass
- G01M99/005—Testing of complete machines, e.g. washing-machines or mobile phones
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CN110617956A (zh) * | 2019-10-21 | 2019-12-27 | 山西汾西重工有限责任公司 | 机械式延时开关用恒力弹簧的盘缠老化执行机构 |
CN112362372A (zh) * | 2020-11-24 | 2021-02-12 | 中国航天空气动力技术研究院 | 一种大功率直线舵机加载装置 |
CN114018726B (zh) * | 2021-10-22 | 2023-11-21 | 中国空空导弹研究院 | 一种刚度可调的琴簧式扭矩加载装置 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10257789A (ja) * | 1997-03-14 | 1998-09-25 | Mitsubishi Heavy Ind Ltd | モータ制御装置 |
CN101614623A (zh) * | 2009-07-20 | 2009-12-30 | 北京理工大学 | 一种测试舵机的正反拖动式电液比例加载装置 |
CN203858778U (zh) * | 2014-04-28 | 2014-10-01 | 北京精密机电控制设备研究所 | 一种基于电动加载的舵机负载模拟装置 |
CN205066985U (zh) * | 2015-10-19 | 2016-03-02 | 中国航天空气动力技术研究院 | 舵机加载装置 |
CN105632276A (zh) * | 2016-02-26 | 2016-06-01 | 南京航空航天大学 | 一种不产生多余力矩的舵机负载模拟器 |
CN108168812A (zh) * | 2017-12-12 | 2018-06-15 | 北京自动化控制设备研究所 | 一种舵机舱振动加载组合装置 |
CN109264024A (zh) * | 2018-10-24 | 2019-01-25 | 杨晓伟 | 飞行器舵机动态性能综合测试平台 |
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2019
- 2019-06-18 CN CN201910525205.4A patent/CN110261152B/zh active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10257789A (ja) * | 1997-03-14 | 1998-09-25 | Mitsubishi Heavy Ind Ltd | モータ制御装置 |
CN101614623A (zh) * | 2009-07-20 | 2009-12-30 | 北京理工大学 | 一种测试舵机的正反拖动式电液比例加载装置 |
CN203858778U (zh) * | 2014-04-28 | 2014-10-01 | 北京精密机电控制设备研究所 | 一种基于电动加载的舵机负载模拟装置 |
CN205066985U (zh) * | 2015-10-19 | 2016-03-02 | 中国航天空气动力技术研究院 | 舵机加载装置 |
CN105632276A (zh) * | 2016-02-26 | 2016-06-01 | 南京航空航天大学 | 一种不产生多余力矩的舵机负载模拟器 |
CN108168812A (zh) * | 2017-12-12 | 2018-06-15 | 北京自动化控制设备研究所 | 一种舵机舱振动加载组合装置 |
CN109264024A (zh) * | 2018-10-24 | 2019-01-25 | 杨晓伟 | 飞行器舵机动态性能综合测试平台 |
Non-Patent Citations (1)
Title |
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导弹舵机动态加载技术;汪首坤等;《北京理工大学学报》;20070331;第27卷(第3期);第247-250页 * |
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Inventor after: Chen Guangjun Inventor after: Lv Yanzhao Inventor after: Wang Jingdong Inventor after: Zhao Xuesong Inventor after: Han Ke Inventor after: Wu Shangyang Inventor after: Song Dan Inventor after: Zhao Changchun Inventor after: Zhu Xiaohong Inventor after: Xie Beimin Inventor before: Wang Jingdong Inventor before: Lv Yanzhao Inventor before: Chen Guangjun Inventor before: Zhao Xuesong Inventor before: Han Ke Inventor before: Wu Shangyang Inventor before: Song Dan Inventor before: Zhao Changchun Inventor before: Zhu Xiaohong Inventor before: Xie Beimin |
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