| 整体式挠性接头刚度测量系统设计 |
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| 引用本文： | 万德安,刘攀,孙东继.整体式挠性接头刚度测量系统设计[J].航空计测技术,2006,26(3):15-16,72. |
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| 作者姓名： | 万德安 刘攀 孙东继 |
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| 作者单位： | 同济大学现代制造技术研究所,上海200092 |
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| 摘 要： | 动力协调陀螺仪中的整体式挠性接头存在加工精度难以保证和刚度测量困难等技术难点.而挠性接头的性能好坏又将直接影响到航空航天设备的性能,因此提高挠性接头的高精度检测十分重要.本文介绍了所研制开发的一套高精度整体式挠性接头测试装置.
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| 关 键 词： | 挠性接头 刚度测量 高精度 虚拟仪器 |
| 文章编号： | 1002-6061（2006）03-0015-02 |
| 收稿时间： | 2005-12-06 |
| 修稿时间： | 2005-12-062006-04-02 |
Design of Testing System of Unitary Flexible Hinge Stiffness |
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| WAN De-an,LIU pan,SUN Dong-ji.Design of Testing System of Unitary Flexible Hinge Stiffness[J].Aviation Metrology & Measurement Technology,2006,26(3):15-16,72. |
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| Authors: | WAN De-an LIU pan SUN Dong-ji |
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| Institution: | Institute of Advanced Manufacturing Technology, Tongji University, Shanghai 200092, China |
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| Abstract: | The unitary flexible hinge stiffness exists some technical problems in the manufacture and measurement of the stiffness. Because the performance of flexible hinge directly influences the performance of spaceflight, it is urgent and important to improve the measurement equipment. The automatic testing apparatus of flexible hinge has been developed. |
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| Keywords: | flexible hinge rigidity measurement high precision virtual instrument |
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