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1)  integrative flexible joint
一体式挠性支承
1.
This dissertation, based on the eleventh 5-year explorative project 'research of precision maching techniques of flexible structural component used in satellite' (project code: 02413180901003, supported by China Aerospace Science and Technology Corporation, is a special exploration for the integrative flexible joint.
论文是在中国航天科技集团公司八院“十一五”预研项目“卫星用挠性结构件精密加工技术研究”,(编号:02413180901003)资助下,对一体式挠性支承进行的专门研究。
2)  flexure hinge
挠性支承
1.
Design for high-precision quartz vibrating-beam accelerometer flexure hinge;
高精度石英振梁加速度计挠性支承设计研究
2.
In this paper,the design of the flexure hinge positioning system having arelative wide range is studied.
对宽范围挠性支承精密调焦系统进行了设计研究,给出了挠性支承的设计计算方法及公式,设计了两级杠杆放大式挠性支承机构及相应的驱动控制部分,试验证明,所研制的系统具有180μm的运动范围,系统分辨率优于0。
3)  flexural pivot
挠性支承
1.
An important characteristic is that the fine mirror is supported by a flexural pivot ,and that a high loop bandwidth is obtained and the disturbance is greatly diminished by using coarse/fine combination multiple feed control technique.
该技术的重要特征是采用挠性支承精稳反射镜组件以及粗/精多回路复合控制技术以获得高回路带宽和对扰动的大幅度衰减。
4)  spring-loaded structure
挠性支承结构
1.
Performance of micro inertial device primarily depends on the mechanical characteristic of its spring-loaded structure.
微惯性器件的性能首先取决于其挠性支承结构的力学性能。
5)  Crab-leg flexural suspension
蟹脚型挠性支承
6)  flexible supporting device
挠性支承装置
补充资料:连续性与非连续性(见间断性与不间断性)


连续性与非连续性(见间断性与不间断性)
continuity and discontinuity

11an父ux泊g四f“山。麻以角g、.连续性与非连续性(c。nt,n琳t:nuity一)_见间断性与不间断性。and diseo红ti-
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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