Assembly Technology of Structure Stability Control for High Precision Gyroscope

doi:10.3901/JME.2018.09.145

Abstract

Abstract: As an important inertial instrument widely used in aeronautic, astronautic and navigation, high precision gyroscope has supreme requirements for the assembly process. The components structure stability is the key problem for the high precision gyroscope manufacturing process. The assembly stress is the main factor affecting the structure stability. Therefor the assembly stress control technology become one of the most interesting research directions for the high precision gyroscope. An errors model is established for the gyroscope based on its structure character and the errors sources. The relationship between the structure stability of components and the precision of the gyroscope is also analysed. Threaded fastening and adhesive bonding technologies for the gyroscope are studied, and one method of an assembly stress control for gyroscope is brought forward.

Key words: adhesive bonding technology, assembly stress, gyroscope, preload of threaded fastening

CLC Number:

YAO Zhuxian, HU Jianzhong, ZHANG Zhijing. Assembly Technology of Structure Stability Control for High Precision Gyroscope[J]. Journal of Mechanical Engineering, 2018, 54(9): 145-152.

References

[1] 于洋. 典型精密结构体制造特性对其力学性能的影响研究[D]. 北京:北京理工大学, 2015. YU Yang. The study of effect of manufacturing characteristics on the stress of typical precise structures[D]. Beijing:Beijing Institute of Technology, 2015.
[2] 韩飞. 陀螺仪装配工艺设计[J]. 现代制造工程, 2008(12):126-128. HAN Fei. Assembly process design of gyroscope[J]. Modern Manufacturing Engineering, 2008(12):126-128.
[3] MCCUNE R W, MURPHY A, PRICE M, et al. The influence of friction stir welding process idealization on residual stress and distortion predictions for future airframe assembly simulations[J]. Journal of Manufacturing Science and Engineering, 2012, 134(3):031011-1-9.
[4] 王晶. 飞机液压管道初始装配应力仿真[J]. 航空计算技术, 2012, 42(6):54-57. WANG Jin. Simulation of initial assembly stress for aircraft hydraulic pipeline[J]. Aeronautical Computing Technique, 2012, 42(6):54-57.
[5] 阖耀保. 电液伺服阀阀套组件装配应力有限元分析[J]. 液压气动与密封, 2010, 30(12):28-32. YIN Yaobao. Analysis of the assembly stress of sleeve of electro-hydraulic servovalve based on FEM[J]. Hydraulics Pneumatics & Seals, 2010, 30(12):28-32.
[6] KATNAM K B, DHÔTE J X, YOUNG T M. Experimental analysis of the bondline stress concentrations to characterize the influence of adhesive ductility on the composite single lap joint strength[J]. The Journal of Adhesion, 2013, 89(6):486-506.
[7] 刘昌发,黄明辉,孙振起. 胶层尺寸对铝锂合金单搭接胶接接头剪切强度的影响[J]. 机械工程材料, 2012, 36(3):85-88. LIU Changfa, HUANG Minghui, SUN Zhenqi. Effect of adhesive layer size on shear strength of Al-Li alloy single-lap adhesive joint[J]. Materials for Mechanical Engineering, 2012, 36(3):85-88.
[8] 杜正兴,高宗战,岳珠峰. 胶瘤对单搭接胶接接头应力分布影响的数值分析[J]. 机械强度, 2008, 30(5):839-843. DU Zhengxing, GAO Zongzhan, YUE Zhufeng. Simulation of the effect of spew on stresses in adhesively -bonded single lap joints[J]. Journal of Mechanical Strength, 2008, 30(5):839-843.
[9] 兰凤崇. 铝镁合金单搭接胶接接头应力分布及强度预测[J]. 吉林大学学报, 2015, 45(3):725-732. LAN Fengchong. Stress distribution and strength prediction of aluminum-magnesium alloy adhesivebonded single-lap joints[J]. Journal of Jilin University, 2015, 45(3):725-732.
[10] 陆元九. 惯性器件[M]. 北京:中国宇航出版社, 1990. LU Yuanjiu. Inertia device[M]. Beijing:China Astronautic Publishing House, 1990.
[11] BICKFORD J H. Introduction to the design and behavior of bolted joints:non-gasketed joints[M]. 4th ed. London:Taylor & Francis Group, 2008.
[12] CLEMENT B, BAZERGUI A. A study of the preload relationship in bolting technology:Experimental design and analysis[C]//Prepared for Bolting Technology Council, New York, October, 1989.
[13] CHAPMAN I, SHARMA S. Choosing the optimum fastening system for the assembly of threaded fasteners[J]. Assembly, 2002, 5:1.

[1]	ZHANG Yongmeng, GUO Kechen, SUN Jiangkun, YU Sheng, XIAO Dingbang, WU Xuezhong. Research on Damping Error Tuning and Compensating Technology of Whole Angle Mode Hemispherical Resonator Gyroscope [J]. Journal of Mechanical Engineering, 2022, 58(16): 145-152.
[2]	XI Xiang, XIAO Dingbang, LI Wei, LU Kun, SHI Yan, YUAN Chao, WU Xuezhong. Analysis of Assembly Errors and Design of Precise Micro-regulator for Micro-hemispherical Resonator Gyroscope (mHRG) [J]. Journal of Mechanical Engineering, 2020, 56(13): 77-83.
[3]	JIANG Shaona, CHEN Xiaoyang, GU Jiaming, ZHANG Tao. Analysis of Friction Moment of Gyroscope Frame Bearing [J]. Journal of Mechanical Engineering, 2016, 52(7): 60-68.
[4]	Zhu Jun,Liu Huijun,Li Xiangjun,Wang Dong. The Multi-Sensor Information Fusion Research of Self-Balancing Two-Wheeled Electric Vehicle Based on EKF [J]. Journal of Electrical Engineering, 2016, 11(6): 25-32.
[5]	ZHAO Xijing;WANG Lixin;HE Zhikun;YANG Jian. Modeling of Temperature Drift Based on Improved Fuzzy Inference for Fiber Optic Gyroscope [J]. , 2014, 50(6): 15-21.
[6]	MA Li;OUYANG Hangkong;XIE Wei;HE Zhengfeng;RONG Weibin;SUN Lining. Slope-contact-type Cavity Adjustment Method and Experiment Study for Ring Laser Gyroscope [J]. , 2014, 50(1): 10-17.
[7]	FAN Jixiang;ZHOU Di. Nonlinear Attitude Control of Spacecraft Based on Scissor Pairs of Control Moment Gyroscope [J]. , 2010, 46(8): 154-159.
[8]	DONG Guimei;LIN Yuchi;FENG Li;QI Yongyue;LI Guiyong. Adaptive Intelligent Lowering System of Gyroscope [J]. , 2010, 46(6): 77-82.
[9]	ZHENG Shiqiang;FANG Jiancheng;HAN Bangcheng. Compensation Control Method and Experimental Study of Magnetic Bearing to Improve Dynamic Response Ability of Double Gimbal Magnetically Suspended Control Moment Gyroscope [J]. , 2010, 46(20): 22-28.
[10]	WEI Tong;FANG Jiancheng;LIU Zhurong. Moving-gimbal Effects Compensation of Double Gimbal Magnetically Suspended Control Moment Gyroscope Based on Compound Control [J]. , 2010, 46(2): 159-165.
[11]	SHI Qin;DING Rongzheng;SU Yan;QIU Anping. Device-level Vacuum Packaging of Silicon Microgyroscopes [J]. , 2009, 45(2): 243-246.
[12]	JIANG Tao;WANG Anlin;LIU Guangjun;ZHANG Ying;JIAO Jiwei. STATISTICAL ANALYSIS ON OUTPUT CAPACITANCE OF TUNING FORK VIBRATORY MICROMACHINED GYROSCOPE [J]. , 2007, 43(8): 114-118.
[13]	LIU Guangjun;WANG Anlin;JIANG Tao;JIAO Jiwei;ZHANG Zhengfu. SELF-ORGANIZING OPTIMIZATION METHOD OF STRUCTURAL SHAPE OF MICROMACHINED GYROSCOPE [J]. , 2007, 43(7): 99-104.
[14]	WEI Tong;FANG Jiancheng. ADAPTIVE CONTROL BASED ON VARIANT OPERATING-POINT LINEARIZATION IN MAGNETIC BEARINGS OF MSCMG [J]. , 2007, 43(6): 110-115.
[15]	LIU Guangjun;WANG Anlin;JIANG Tao;JIAO Jiwei;ZHANG Zhengfu. DETECTION CAPACITANCE ANALYSIS METHOD FOR TUNING FORK VIBRATORY MICROMAC-HINED GYROSCOPE BASED ON SUBSTRUCTURE MODEL [J]. , 2006, 42(9): 97-102.