玻璃纤维增强铝锂合金层板单峰过载疲劳寿命性能对比研究

doi:10.7527/S1000-6893.2015.0219

Abstract

Abstract:

In order to study on fatigue life performance of the Al-Li alloy and fiber metal laminates (2/1 laminates and 3/2 laminates of glass fiber reinforced Al-Li alloy) under different loading modes, these materials are subjected to fatigue life test. Each type of the materials is applied to cyclic stress, which has different cycle characteristics (constant amplitude with the stress ratio 0.06, unimodal tensile overload and unimodal compressive overload). Nine kinds of test data on stress life are obtained and P-S-N curve of each material is fitted using the principle of sample polymerization. In addition, the differences of the S-N curve with the same material in different loading modes and different materials in the same loading mode are compared with each other. The results show that all of the three kinds of materials show the effect of overload retardation under tensile overload, Al-Li alloy material exhibits accelerated destruction effect and laminate materials exhibit a delayed effect under compressive overload. The pros and cons of fatigue performance between different structural laminates have a relationship with remote stress.

Key words: fiber metal laminates, fatigue life, fatigue test, cyclic stress, overloads

CLC Number:

V257

MENG Weiying, XIE Liyang, LIU Jianzhong, BAI Xin, TONG Anshi. Contrast study on fatigue life performance of glass fiber reinforced Al-Li alloy laminates under unimodal overload[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1536-1543.

References

[1] 吴学仁, 郭亚军. 纤维金属层板疲劳寿命预测的研究进展[J]. 力学进展, 1999, 29(3):304-316. WU X R, GUO Y J. Development of methodology for predicting fatigue life of fiber reinforced metal laminates[J]. Advances in Mechanics, 1999, 29(3):304-316(in Chinese).
[2] HOMAN J J. Fatigue initiation in fiber metal laminates[J]. International Journal of Fatigue, 2006, 28(4):366-374.
[3] CHANG P Y, YEH P C, YANG J M. Fatigue crack initiation in hybrid boron/glass/aluminum fiber metal laminates[J]. Materials Science and Engineering:A, 2008, 496(1-2):273-280.
[4] FRIZZELL R M, MCCARTHY C T, MCCARTHY M A. An experimental investigation into the progression of damage in pin-loaded fiber metal lamintes[J]. Composites Part B:Engineering, 2008, 39(6):907-925.
[5] GUMMINK J W, VLOT A, DE VRIES T J, et al. GLARE technology development 1997-2000[J]. Applied Composite Materials, 2002, 9(4):201-219.
[6] VERMEEREN C A J R, BEUMLER T, DE KANTER J L C G, et al. GLARE design aspects and philosophies[J]. Applied Composite Materials, 2003, 10(4-5):257-276.
[7] SINKE J. Development of fiber metal laminates:Concurrent multi-scale modeling and testing[J]. Material Science, 2006, 41(20):6777-6788.
[8] MARISSEN R. Fatigue crack growth in ARALL:A hybrid aluminium-aramid composite material crack growth mechanisms and quantitative predictions of the crack growth rates[D]. Delft:Delft University of Technology, 1988:12-13.
[9] HYOUNGSEOCK S. Damage tolerance and durability of GLARE laminates[D]. Los Angeles, CA:University of California Los Angeles, 2008:11-13.
[10] YEH P C. Static and dynamic behavior of high modulus hybrid boron/glass/aluminum fiber metal laminates[D]. Los Angeles, CA:University of California Los Angeles, 2011:28-37.
[11] WU G C. Mechanical behavior damage tolerance and durability of fiber metal laminates for aircraft structures[D]. Los Angeles, CA:University of California Los Angeles, 2005:17-19.
[12] 郭亚军. 纤维金属层板的疲劳损伤与寿命预测[D]. 北京:北京航空材料研究院, 1997:10-12. GUO Y J. Fatigue damage and life prediction of fiber reinforced metal laminates[D]. Beijing:Beijing Institute of Aeronautical Materials, 1997:10-12(in Chinese).
[13] 郭亚军, 吴学仁. 纤维金属层板疲劳裂纹扩展速率与寿命预测的唯象模型[J]. 航空学报, 1998, 19(3):275-282. GUO Y J, WU X R. Phenomenological model for predicting fatigue crack growth in fiber reinforced metal laminates[J]. Acta Aeronautica et Astronautica Sinica, 1998, 19(3):275-282(in Chinese).
[14] 陈琪, 关志东, 黎增山. GLARE层板性能研究进展[J]. 科技导报, 2013, 31(7):50-56. CHEN Q, GUAN Z D, LI Z S. Review of GLARE technology[J]. Technology Review, 2013, 31(7):50-56(in Chinese).
[15] ALDERLIESTEN R C, HOMAN J J. Fatigue and damage tolerance issues of GLARE in aircraft structures[J]. International Journal of Fatigue, 2006, 28(10):1116-1123.
[16] SHIM D J, ALDERLIESTEN R C, SPEARING S M, et al. Fatigue crack growth prediction in GLARE hybrid laminates[J]. Composites Science and Technology, 2003, 63(12):1759-1767.
[17] WU G C, YANG J M. The mechanical behavior of GLARE laminates for aircraft structures[J]. Failure in Structural Materials, 2005(1):72-79.
[18] 中国航空工业总公司. 金属材料轴向加载疲劳试验方法:HB5287-1996[S]. 北京:中国航空工业总公司, 1996:1-8. Aviation Industry Corporation of China. Test method for axial loading fatigue of metallic materials:HB5287-1996[S]. Beijing:Aviation Industry Corporation of China, 1996:1-8(in Chinese).
[19] 谢里阳, 刘建中. 样本信息聚集原理与P-S-N曲线拟合方法[J]. 机械工程学报, 2013, 49(15):96-104. XIE L Y, LIU J Z. Principle of sample polymerization and method of P-S-N curve fitting[J]. Journal of Mechanical Engineering, 2013, 49(15):96-104(in Chinese).
[20] 何玉定, 杨大丰. 过载对60Si₂Mn钢弯曲疲劳性能的影响[J]. 湘潭大学自然科学学报, 1997, 19(3):96-100. HE Y D, YANG D F. Effect of overload on bend fatigue property of 60Si₂Mn steel[J]. Natural Science Journal of Xiangtan University, 1997, 19(3):96-100(in Chinese).
[21] KIEBOOM O. Fatigue crack initiation and early crack growth in GLARE at different temperatures[D]. Delft:Delft University of Technology, 2000:15-18.
[22] 李绍渊. 纤维金属层压板的应力集中与疲劳裂纹扩展研究[D]. 南京:南京航空航天大学, 2011:43-47. LI S Y. Stress concentrations and fatigue crack growth in fiber metal laminate[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2011:43-47(in Chinese).
[23] VOGELESANGL B, SCHIJVE J, FREDELL R. Fiber metal laminates:Damage tolerant aerospace materials[M]//DEMAID A, DE WIT J H W. Case Studies in Manufacturing with Advanced Materials. Amsterdam:Elsevier, 1995:253-271.

Contrast study on fatigue life performance of glass fiber reinforced Al-Li alloy laminates under unimodal overload

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	LYU Shuaishuai, YANG Yu, WANG Binwen, YIN Chenfei. A crack identification method of aircraft structure based on improved FaceNet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525463-525463.
[2]	GUO Qiong, LIU Wei, PEI Lianjie, GUO Junhao. Static and fatigue test technology for full-scale composite fuselage barrels [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525816-525816.
[3]	YANG Yu, WANG Binwen, QI Xiaofeng. Acoustic emission monitoring technology for fatigue test of full-scale civil aircraft structure [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527044-527044.
[4]	WANG Yupeng, TIAN Wenpeng, SONG Pengfei, XIA Feng, FENG Jianmin. Research and verification of comprehensive acceleration technology for civil aircraft full-scale fatigue test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 224919-224919.
[5]	XU Luopeng, HU Shi, LIU Qingsong, WANG Qingyuan. High-frequency fatigue infrared heat dissipation of new Al-Li alloy AA2198 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 224482-224482.
[6]	LI Yuhai, WANG Chengbo, CHEN Liang, DONG Hongda, GUAN Yu, DI Hongliang, GU Yuxuan. Overview on development of advanced fighter life design and extension technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525791-525791.
[7]	QI Xiaofeng, YANG Yu, KANG Weiping, WANG Qian. Fatigue damage monitoring of lug joints with random load spectrum based on acoustic emission [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524518-524518.
[8]	SUN Xiasheng, SU Shaopu, SUN Hanbin, DONG Dengke. Current status and prospect of overseas research on aeronautical fatigue [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524791-524791.
[9]	MA Zhanqi, SUN Xiuwen, WANG Lingqi. Temperature design and control of rotor drag-hinge self-lubrication bush fatigue test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524217-524217.
[10]	YANG Zhengwei, ZHAO Zhibin, LI Yin, SONG Yuanjia, KOU Guangjie, LI Lei, CHENG Pengfei. Infrared radiation characteristics of CFRP laminate surface under compressive fatigue load [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524239-524239.
[11]	ZHANG Fuze. Principle and method of calculating real corrosion tolerance value of aircraft struture [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524457-524457.
[12]	ZHANG Junrui, ZHENG Xitao, YUAN Lin, ZHONG Guiyong, LI Guochen. Fatigue life prediction method for hybrid multi-bolted joints based on damage weight [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524306-524306.
[13]	WANG Lianqing, HU Ya'nan, CHE Zhigang, WU Shengchuan. Fatigue performance of laser shock processed fusion welded 7075 Al alloy [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524320-524320.
[14]	LIU Binchao, BAO Rui, SUI Fucheng. A mean-stress model including material cyclic constitutive in uniaxial fatigue [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 224735-224735.
[15]	TAN Xiaoming, ZHANG Danfeng, ZHAN Guipan, WANG De. Damage mechanism of shot peened ultra-high strength steel under combined action of marine environment and fatigue load [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(8): 223631-223631.