折叠翼展开机构测试装置设计与试验验证

中国机械工程 ›› 2015, Vol. 26 ›› Issue (14): 1857-1861.

折叠翼展开机构测试装置设计与试验验证

胡明1;章斌1;陈文华1;田芳菲1;张;虹2;周小红2

1.浙江理工大学机电产品可靠性技术研究浙江省重点实验室,杭州,310018
2.北京机电工程研究所,北京,100074

出版日期:2015-07-25 发布日期:2015-08-05
基金资助:
国家自然科学基金资助项目(51375458);浙江省自然科学基金资助项目(LZ12E05004);高等学校博士学科点基金优先发展项目(20123318130001)

Test Device Design and Experimental Verification of Deployable Mechanism of Folding-wing

Hu Ming1;Zhang Bin1;Chen Wenhua1;Tian Fangfei1;Zhang Hong2;Zhou Xiaohong2

1.Zhejiang Province's Key Laboratory of Reliability Technology for Mechanical and Electrical Products,Zhejiang Sci-Tech University,Hangzhou,310018
2.Beijing Research Institute of Mechanical & Electrical Engineering.Beijing,100074

Online:2015-07-25 Published:2015-08-05
Supported by:
National Natural Science Foundation of China（No. 51375458）;Zhejiang Provincial Natural Science Foundation of China（No. LZ12E05004）

摘要/Abstract

摘要：

基于折叠翼展开机构的工作原理和功能需求，确定了折叠翼展开机构性能参数测试方法，完成了其测试装置的设计及原理样机研制。应用所研制的折叠翼展开机构测试装置进行折叠翼展开性能试验，获得其各项性能指标，并通过不同转矩下折叠翼展开机构测试装置试验，分析其性能参数变化规律。结果表明：弹翼能迅速展开到位，锁紧销与过位挡块能实现翼面准确定位、可靠锁定，且展开过程中各部件之间相互无干涉，满足设计要求。

关键词: 折叠翼, 展开机构, 测试装置, 试验验证

Abstract:

Based on working principles and functional requirements of folding-wing deployable mechanism,the performance parameter measurement method of a folding-wing deployable mechanism was determined,the test device design and development of principle prototype was completed.Using the developed test device of the deployable mechanism of folding-wing,spread experiments were carried out and the various performance indicators were obtained.According to multiple spreading experiments in different torques,performance parameters the regulations were researched.The group test data show that the folding-wing can unfurl to the appointed place quickly,can be located accurately and locked reliably,and there is no interference between each part during the deployment process.

Key words: folding-wing;deployable mechanism;test device;experimental , verification

胡明, 章斌, 陈文华, 田芳菲, 张, 虹, 周小红. 折叠翼展开机构测试装置设计与试验验证[J]. 中国机械工程, 2015, 26(14): 1857-1861.

Hu Ming, Zhang Bin, Chen Wenhua, Tian Fangfei, Zhang Hong, Zhou Xiaohong. Test Device Design and Experimental Verification of Deployable Mechanism of Folding-wing[J]. China Mechanical Engineering, 2015, 26(14): 1857-1861.

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