Material Engineering and Mechanical Manufacturing

Force sensor for axial force and shear force of bolts in joints

  • WANG Houbing ,
  • WEI Jingchao ,
  • CHENG Li'nan ,
  • LI Xinxiang ,
  • ZHAO Rong
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  • Aeronautics Science Technology Key Laboratory of Full Scale Aircraft Structure Static and Fatigue, Aircraft Strength Research Institute of China, Xi'an 710065, China

Received date: 2020-06-24

  Revised date: 2020-08-18

  Online published: 2020-09-04

Supported by

Civil Aircraft Scientific Research Project (MJ-2015-F-038)

Abstract

Based on a brief survey of the measurement methods for the axial force of bolts in joints and the shear force of bolts in composite multi-bolt joints, a force sensor for simultaneously measuring both the axial force and shear force of bolts in joints is presented to overcome the shortcoming of the existing test methods that only one of the forces could be measured at a time. Two test setups for the axial force and the shear force are designed for the force sensor, and two experiments conducted for the two forces. The linearity and repeatability of the load-strain curves from the test results of the force sensor are experimentally investigated. The test outcomes show that the presented force sensor satisfies the technical requirements for measuring the axial force and shear force of bolts in engineering, further verifying the suitability of the proposed force sensor. The installation angle of the force sensor has no effect on the measurement results of the axial force and shear force. The bolt tightening torques are found to significantly influence the measurement results, whereas the effects weaken slowly when the external load increases.

Cite this article

WANG Houbing , WEI Jingchao , CHENG Li'nan , LI Xinxiang , ZHAO Rong . Force sensor for axial force and shear force of bolts in joints[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021 , 42(3) : 424459 -424459 . DOI: 10.7527/S1000-6893.2020.24459

References

[1] 谢鸣九. 复合材料连接[M]. 上海:上海交通大学出版社,2011:129-137. XIE M J. Joint for composites materials[M]. Shanghai:Shanghai Jiaotong University Press, 2011:129-137(in Chinese).
[2] 中国航空研究院. 复合材料连接手册[M]. 北京:航空工业出版社,1994:1-15. Institute of Aeronautics China. Handbook of joint for composites materials[M]. Beijing:Aviation Industry Press, 1994:1-15(in Chinese).
[3] ABUSREA M R, ARAKAWA K. Improvement of an adhesive joint constructed from carbon fiber-reinforced plastic and dry carbon fiber laminates[J]. Composite Part B, 2016, 97:368-373.
[4] DAVIDSON P, WAAS A M. The effects of defects on the compressive response of thick carbon composites:An experimental and computational study[J]. Composite Structure 2017, 176:582-596.
[5] YANG C Q, WANG X L, JIAO Y J, et al. Linear strain sensing performance of continuous high strength carbon fiber reinforced polymer composites[J]. Composites Part B, 2016, 102:86-93.
[6] LIU F R, LU X H, ZHAO L B, et al. An interpretation of the load distributions in highly torqued single-lap composite bolted joints with bolt-hole clearances[J]. Composites Part B, 2018, 138:194-205.
[7] 赵丽滨,刘丰睿,黄伟,等. 复合材料螺栓连接失效分析研究进展[J]. 强度与环境,2017,44(3):1-11. ZHAO L B, LIU F R, HUANG W, et al. Advances in failure analysis methods of bolted composite joints[J]. Structure & Environment Engineering, 2017, 44(3):1-11(in Chinese).
[8] 邢堃,刘检华,唐承统,等. 一种基于垫片式力传感器的螺栓组连接预紧力测量方法[J].航空制造技术, 2015,16:90-95. XING K, LIU J H, TANG C T, et al. Bolt group preload measuring method based on gasket force sensor[J]. Aeronautical Manufacturing Technology, 2015, 16:90-95(in Chinese).
[9] 杜刚民,李东风,曹树林. 螺栓轴向应力超声测量技术[J].无损检测:试验研究,2006, 28(1):20-25. DU G M, LI D F, CAO S L. Bolt axial stress measurement by ultrasonic testing[J]. Nondestructive Testing:Test Research, 2006, 28(1):20-25(in Chinese).
[10] 魏涛,王洋,李红松,等. 基于应变的螺栓拧紧轴力测量研究[J].内燃机与动力装置, 2011,5:1-3. WEI T, WANG Y, LI H S, et al. Study on axis force of bolt tightening based on strain measurement[J]. Internal Combustion Engineer & Powerplant, 2011, 5:1-3(in Chinese).
[11] 宋恩鹏,刘文珽,谢鸣九,等. 刚度比对复合材料多钉连接钉载分配影响研究[J]. 飞机设计, 2005, 4:29-32. SONG E P, LIU W T, XIE M J, et al. Investigation of the influence of jointed member stiffness on fastener load distribution for composite multiple-bolted joint[J]. Aerocraft Design, 2005, 4:29-32(in Chinese).
[12] LAWLOR V P, MCCARTHY M A, STANLEY W F. An experimental study of bolt-hole clearance effects in double-lap multi-bolt composite joints[J]. Composite Structures, 2005,71(2):176-190.
[13] STARIKOV R, SCHÖN J. Fatigue resistance of composite joints with countersunk composite and metal fasteners[J]. International Journal of Fatigue, 2002, 24(1):39-47.
[14] ASCIONE F. A preliminary numerical and experimental investigation on the shear stress distribution on multi-row bolted FRP joints[J]. Mechanics Research Communications, 2010, 37(2):164-168.
[15] 张建宇,刘丰睿,山美娟,等. 复合材料多钉连接钉载矢量传感器[J]. 复合材料学报,2015,32(5):1420-1427. ZHANG J Y, LIU F R, SHAN M J, et al. Bolt of load vector of composite multi-bolt joints[J]. Acta Materiae Composite Sinica, 2015, 32(5):1420-1427(in Chinese).
[16] KELLY G. Load transfer in hybrid (bonded/bolted) composite single-lap joints[J]. Composite Structures, 2005, 69(1):35-43.
[17] EKH J, SCHÖN J. Load transfer in multi-row, single shear, composite-to-aluminium lap joints[J]. Composite Science and Technology, 2006, 66(7-8):875-885.
[18] STANLEY W F, MCCARTHY M A, LAWLOR V P. Measurement of load distribution in multi-bolt, composite joints, in the presence of varying clearance[J]. Journal of Plastics, Rubber and Composites, 2002,31(9):412-418.
[19] EKH J, SCHÖN J. Finite element modeling and optimization of load transfer in multi-fastener joins using structural elements[J]. Composite Structure, 2008,82:245-256.
[20] GRAY P J, MCCARTHY C T. A global bolted joint model for finite element analysis of load distributions in multi-bolt composite joints[J]. Composite part B, 2010, 41(4):317-325.
[21] 李念,任飞翔,陈普会,等. GBJM方法的改进及其在含钉群复合材料结构钉载分配和承载能力分析中的应用[J]. 复合材料学报,2015,32(1):176-181. LI N, REN F X, CHEN P H, et al. An improved GBJM method and its application in bolt load distribution and load capacity analysis of composite structures with bolt group[J]. Acta Materiae Composite Sinica, 2015,32(1):176-181(in Chinese).
[22] KIM J, YOON J C, KANG B S. Finite element analysis and modeling of structure with bolted joints[J]. Appl math Model, 2007, 31(5):895-911.
[23] ANDRIAMAMPIANINA J, ALKATAN F, STEPHAN P, et al. Determining load distribution between the different rows of fasteners of a hyrid load transfer bolted joint assembly[J]. Aerospace Science Technolgy, 2012,23:312-320.
[24] MCCARTHY C T, GRAY P J. An analytical model for the prediction of load distribution in highly torqued multi-bolt composite joints[J]. Composite Structure, 2011,93(2):287-298.
[25] LIU F R, ZHANG J Y, ZHAO L B, et al. An analytical joint stiffness model for load transfer analysis in highly torqued multi-bolt composite joints with clearances[J]. Composite Structure, 2015, 131:625-636.
[26] MCCARTHY M A, MCCARTHY C T, PADHI G S. A simple method for determining the effects of bolt-hole clearance on load distribution in single-column multi-bolt composite joints[J]. Composite Structure, 2006,73:78-87.
[28] XIANG J, ZHAO S, LI D, et al. An improved spring method for calculating the load distribution in multi-bolt composite joints[J]. Composite Part B, 2017, 117:1-8.
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