复合材料结构用高锁螺栓的动态复合加载失效特性

doi:10.3969/j.issn.1000-1093.2019.10.021

兵工学报 ›› 2019, Vol. 40 ›› Issue (10): 2142-2150.doi: 10.3969/j.issn.1000-1093.2019.10.021

复合材料结构用高锁螺栓的动态复合加载失效特性

惠旭龙，刘小川，白春玉，张宇, 舒挽，葛宇静

（中国飞机强度研究所结构冲击动力学航空科技重点实验室，陕西西安 710065）

收稿日期:2019-01-04 修回日期:2019-01-04 上线日期:2019-12-18
作者简介:惠旭龙（1989—），男，工程师，硕士。E-mail:742839400@qq.com
基金资助:
国家自然科学基金项目（11702260）

Failure Characteristics of High-lock Bolts for Composite Structures under Dynamic Combined Loading

XI Xulong, LIU Xiaochuan, BAI Chunyu, ZHANG Yu, SHU Wan, GE Yujing

（Aviation Key Laboratory of Science and Technology on Structures Impact Dynamics, Aircraft Strength Research Institute of China, Xi'an 710065, Shaanxi, China）

Received:2019-01-04 Revised:2019-01-04 Online:2019-12-18

摘要/Abstract

摘要： 为研究复合材料结构用高锁螺栓的动态复合加载失效特性，基于高速液压伺服材料实验机设计专用的实验支持装置，提出碰撞式实验加载方法。实现中国商用飞机有限责任公司紧固件工艺标准CFBL1001-6-6/CFNT1003CY6抗剪型高锁螺栓在0.01 m/s、0.10 m/s、1.00 m/s加载速度及纯拉伸、30°拉伸-剪切耦合、45°拉伸-剪切耦合、60°拉伸-剪切耦合、纯剪切状态下的失效测试，并基于实验结果拟合得到高锁螺栓的失效参数。结果表明：提出的测试方法能够有效获取高锁螺栓的动态失效参数;CFBL1001-6-6/CFNT1003CY6高锁螺栓的失效模式和失效载荷受加载方式影响较大,受加载速度影响较小;拟合获得的失效方程可较好地表征高锁螺栓的失效特性。

关键词: 高锁螺栓, 复合材料, 复合加载, 动态拉伸, 失效参数

Abstract: In order to study the failure characteristics of high-lock bolts used in composite structures under dynamic combined loading, a special experimental support device is designed based on the high velocity hydraulic servo-testing machine, and a loading method of collision type is proposed. Failure tests of CFBL1001-6-6/ CFNT1003CY6 high-lock bolts were conducted under the conditions of 0.01 m/s, 0.10 m/s and 1.00 m/s loading speeds, and pure tensile, 30° tensile-shear coupling, 45° tensile-shear coupling, 60° tensile-shear coupling and pure shear state, and the parameters of failure equation were obtained by fitting the experimental results. The experimental results show that the failure parameters of high-lock bolts under dynamic combined loading can be effectively obtained by using the proposed experimental method, and the failure mode and failure load of high-lock bolts are affected greatly by the loading mode and less at the loading speed.The experimental results are good agreement with the predicted results of failure equation, which indicates that the failure characteristics of high-lock bolts can be well represented by the failure equation. Key

Key words: high-lockbolt, composite, combinedloading, dynamictensile, failureparameter

中图分类号:

O347.3

惠旭龙，刘小川，白春玉，张宇, 舒挽，葛宇静. 复合材料结构用高锁螺栓的动态复合加载失效特性[J]. 兵工学报, 2019, 40(10): 2142-2150.

XI Xulong, LIU Xiaochuan, BAI Chunyu, ZHANG Yu, SHU Wan, GE Yujing. Failure Characteristics of High-lock Bolts for Composite Structures under Dynamic Combined Loading[J]. Acta Armamentarii, 2019, 40(10): 2142-2150.

参考文献

［1］刘风雷, 徐鑫良, 孙文东. 复合材料结构用紧固件技术［J］. 宇航总体技术, 2018, 2(4):8-12.
LIU F L, XU X L, SUN W D. Fastener technology for composite structures［J］. Aerospace Systems Engineering Technology, 2018, 2(4):8-12.(in Chinese)
［2］魏景超, 柴亚南, 刘风雷, 等. 单面螺纹抽钉干涉配合复合材料连接结构的疲劳性能研究［J］. 航空制造技术,2017(22):50-55.
WEI J C, CHAI Y N, LIU F L, et al. Effect of several influencing factors on fatigue behaviour of interference-fit bolted composite joints［J］. Aeronautical Manufacturing Technology, 2017(22):50-55. (in Chinese)
［3］谢阶栋, 陈果, 曾馨靓, 等. 高锁螺栓装配的最佳干涉量实验与仿真研究［J］. 机械强度, 2018, 40(6): 1321-1329.
XIE J D, CHEN G, ZENG X L, et al. Experiment and simulation research of the optimum interference of hi-lock assembly［J］. Journal of Mechanical Strength, 2018, 40(6): 1321-1329. (in Chinese)
［4］魏景超. 复合材料结构新型紧固件连接强度与失效机理［D］.西安:西北工业大学, 2014.
WEI J C. Strength and failure mechanisms of bolted composite joints with new fastener［D］. Xi'an:Northwestern Polytechnical University, 2014. (in Chinese)
［5］ ARCAN M, HASHIN Z, VOLOSHIN A. A method to produce uniform plane-stress states with applications to fiber-reinforced materials［J］. Experimental Mechanics, 1978, 18(4):141-146.
［6］ PREVITALI F, ANGHILERI M. Combined numerical/experimental approach for rivet strength assessment ［C］∥Proceedings of the 7th European LS-DYNA Conference. Salzburg, Austria: DYNAmore GmbH, 2009.
［7］ LANGRAND B, DELETOMBE E, MARKIEWICZ E, et al. Riveted joint modeling for numerical analysis of airframe crashworthiness［J］. Finite Elements in Analysis and Design, 2001, 38(1): 21-44.
［8］杨沛, 郭亚洲, 李玉龙. 航空铆钉的动态力学性能测试［J］．航空学报, 2014, 35(11):3012-3024.
YANG P, GUO Y Z, LI Y L. Dynamic mechanical test of aeronautic rivets ［J］. Acta Aeronautic et Astronautic Sinica, 2014, 35(11):3012-3024. (in Chinese)
［9］解江, 白春玉, 舒挽, 等. 航空铆钉动态加载失效实验［J］. 爆炸与冲击, 2017, 37(5):879-886.
XIE J, BAI C Y, SHU W, et al. Dynamic loading failure experiment of aeronautic rivet［J］. Explosion and Shock Waves, 2017, 37(5):879-886. (in Chinese)

［10］ SEBASTIAN H, SEBASTIAN S, JORG B, et al. Static and dynamic failure behaviour of bolted joints in carbon fibre composites［J］. Composites Part A: Applied Science and Manufacturing, 2013, 47:91-101.
［11］ EGAN B, MCCARTHY C T, MCCARTHY M A, et al. Static and high-rate loading of single and multi-bolt carbon-epoxy aircraft fuselage joints［J］. Composites Part A: Applied Science and Manufacturing, 2013, 53:97-108.
［12］ XAVIER J, OLIVEIRA M, MORAIS J, et al. Measurement of the shear properties of clear wood by the Arcan test［J］. Holzforschung, 2009, 63(2):217-225.
［13］ ALFONSO L, UGUEN A, BADULESCU C, et al. Determination of the 3D failure envelope of a composite based on a modified Arcan test device［J］. Composite Structures, 2015, 131:585-593.
［14］惠旭龙, 牟让科, 白春玉, 等. TC4钛合金动态力学性能及本构模型研究［J］. 振动与冲击, 2016, 35(22):161-168.
XI X L, MU R K, BAI C Y, et al. Dynamic mechanical property and constitutive model for TC4 titanium alloy［J］. Journal of Vibration and Shock, 2016, 35(22):161-168. (in Chinese)

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复合材料结构用高锁螺栓的动态复合加载失效特性

Failure Characteristics of High-lock Bolts for Composite Structures under Dynamic Combined Loading

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