材料工程与机械制造

用于质量特性参数测量的新型气浮扭摆台

  • 王秋晓 ,
  • 孔波 ,
  • 汪飞 ,
  • 姜怀芳
展开
  • 1. 重庆大学 机械传动国家重点实验室, 重庆 400030;
    2. 重庆大学 机械工程学院, 重庆 400030;
    3. 华中科技大学 数字制造装备与技术国家重点实验室, 武汉 430074
王秋晓 男,博士,副教授,硕士生导师。主要研究方向:机械电子。Tel:023-65429037 E-mail:wqxiao1963@163.com

收稿日期: 2013-05-29

  修回日期: 2013-08-22

  网络出版日期: 2013-08-28

基金资助

国家自然科学基金(51175529)

New Kind of Gas Bearing Torsion Pendulum Used for Mass Property Parameters Measurement

  • WANG Qiuxiao ,
  • KONG Bo ,
  • WANG Fei ,
  • JIANG Huaifang
Expand
  • 1. The State Key Laboratory of Mechanical Transmission, Chongqing University, Chongqing 400030, China;
    2. College of Mechanical Engineering, Chongqing University, Chongqing 400030, China;
    3. State Key Laboratory of Digital Manufacturing Equipment & Technology, Huazhong University of Science and Technology, Wuhan 430074, China

Received date: 2013-05-29

  Revised date: 2013-08-22

  Online published: 2013-08-28

Supported by

National Natural Science Foundation of China (51175529)

摘要

常规扭摆台采用滚动轴承和扭杆振动结构,纵向尺寸大、测量精度低、抗倾覆力矩小,不能满足质量特性参数综合试验台的要求,必须对其进行结构的分析和优化。本文提出交叉弹簧板结构替换扭杆,减少了扭摆台纵向尺寸,分析和实验表明该结构具有和扭杆相同的振动效果。将滚动轴承替换为气浮轴承,提高了抗倾覆力矩,测量精度最高达0.1%;采用有限元法对柱坐标系下修正的雷诺方程进行仿真计算,研究气浮轴承结构参数对承载能力和抗倾覆力矩的影响规律,确定了给定轴承外径下的最优几何参数。实验表明,改进的试验台提高了测量精度和振动稳定性,对卫星等飞行体质量特性参数的测量有重要的意义。

本文引用格式

王秋晓 , 孔波 , 汪飞 , 姜怀芳 . 用于质量特性参数测量的新型气浮扭摆台[J]. 航空学报, 2014 , 35(3) : 885 -893 . DOI: 10.7527/S1000-6893.2013.0371

Abstract

The conventional torsion pendulum adopts a rolling bearing and torsion bar vibrating structure. It suffers from excessive length in the vertical direction, low measurement accuracy, poor load capacity, and poor anti-overturning moment, and it cannot meet the requirements of a comprehensive test platform for mass property parameters. The cross-shaped spring block structure is proposed to replace the torsion bar structure, and the size of the torsion pendulum is reduced in the vertical direction. Analysis and experiment prove that the new structure has the same effect as the torsion bar. As the rolling bearing is replaced by the gas bearings, the anti-overturning moment of the torsion pendulum is improved and measurement accuracy reaches up to 0.1%. The finite element method is adopted to simulate the re-corrected Reynolds equation under a cylindrical coordinate system,and then the influence of basic gas bearings structural parameters on load capacity and anti-overturning moment is studied. Finally, the optimized geometrical parameters of a given outer radius bearing are determined. Experimental results demonstrate that the improved test-bed improves the measurement accuracy and vibration stability. It is significant for mass property parameters measurement of spacecraft, such as satellites.

参考文献

[1] Wang Q X, Wang Y. A new measurement method for mass property parameters[J]. Journal of Chongqing University, 2011, 34(12): 23-28. (in Chinese) 王秋晓, 王迎. 飞行器质量特性参数测量[J]. 重庆大学学报, 2011, 34(12): 23-28.

[2] Xu J, Yang Q J, Bao G, et al. Research on lateral disturbance force of the 5-DoF air-bearing spacecraft simulator [J]. Journal of Astronautics, 2009, 30(5): 1823-1828. (in Chinese) 许剑, 杨庆俊, 包钢, 等. 五自由度气浮台平动时侧向干扰力问题的研究[J]. 宇航学报, 2009, 30(5): 1823-1828.

[3] Zhang X L, Tang S, Wang J, et al. Research on measuring technology of moment of inertia for objects with complex shape [J]. Aerospace Manufacturing Technology, 2011(1): 17-20.(in Chinese) 张晓琳, 唐松, 王军, 等. 复杂形状物体转动惯量测量技术研究[J]. 航天制造技术, 2011(1): 17-20.

[4] Zou Y, Xia Y. A universal measurement method for apparatus moment of inertia in hardware-in-the-loop simulation[J]. Aerospace Control, 2008, 26(5): 74-76.(in Chinese) 邹莹, 夏阳. 一种通用的设备转动惯量测量方法[J]. 航天控制, 2008, 26(5): 74-76.

[5] Kastait J P, Lin W, Lin W J. Design and development of orifice-type aerostatic thrust bearing[J]. SIMTech Technical Reports, 2005, 6(1): 7-12.

[6] Hou W. A measuring method on moment of inertia of large-scale ammunition[J]. Journal of China Ordnance Society, 2005, 1(1): 41-45.

[7] Boynton R, Wiener K. A new high accuracy instrument for measuring moment of inertia and center of gravity[C]//47th Annual Conference of SAWE, 1988.

[8] Mohamed E, Eleshaky. CFD investigation of pressure depressions in aerostatic circular thrust bearings[J]. Tribology International, 2009, 42(7): 1108-1117.

[9] Long W. Study on loading characteristics of orifice compenstated aerostatic thrust bearing[D]. Harbin: School of Mechatronics Engineering, Harbin Institute of Technology, 2010.(in Chinese) 龙威. 平面空气静压轴承承载特性研究[D]. 哈尔滨:哈尔滨工业大学机电工程学院, 2010.

[10] Du J J, Zhang G Q, Liu D. Influences of pressure-equalizing groove on the load capacity of externally pressurized gas journal bearings[J]. Journal of Mechanical Engineering, 2012, 48(15): 107-112.(in Chinese) 杜建军, 张国庆, 刘暾. 均压槽与静压气体轴颈轴承承载特性的关系研究[J]. 机械工程学报, 2012, 48 (15): 107-112.

[11] Guo L B, Wang Z W, Bao G, et al. Finite element analysis of the pressure distribution of externally pressurized spherical gas bearings with inherent compensation[J]. Tribology, 2004, 24(6): 531-535.(in Chinese) 郭良斌, 王祖温, 包钢, 等. 新型环面节流静压气体球轴承压力分布的有限元计算 [J]. 摩擦学学报, 2004, 24(6): 531-535.

[12] Liu D, Liu Y H, Chen S J. Externally pressurized gas lubrication[M]. Harbin: Harbin Institute of Technology Press, 1990: 122-153. (in Chinese) 刘暾, 刘育华, 陈世杰. 静压气体润滑[M]. 哈尔滨:哈尔滨工业大学出版社, 1990:122-153.

[13] Charki A, Diop K, Champmartin S, et al. Numerical simulation and experimental study of thrust air bearings with multiple orifices[J]. International Journal of Mechanical Sciences, 2013, 72: 1-11.

[14] Li Y T, Han D. A simplified calculation method on the performance analysis of aerostatic thrust bearing with multiple pocketed orifice-type restrictors[J]. Tribology International, 2012, 56: 66-67.

[15] Guo L B. Design of configuration parameters of externally pressurized circular[J]. Journal of Wuhan University of Science and Technoloy, 2012, 35(1): 62-64. (in Chinese) 郭良斌. 基于静特性分析的环面节流静压圆盘[J].武汉科技大学学报, 2012, 35(1): 62-64.

文章导航

/