[1]申世军,倪勇军,齐海雁,等.2219铝锂合金网格壁板增量成形有限元仿真[J].塑性工程学报,2014,21(2):71-75.
Shen S J,Ni Y J,Qi H Y,et al. Finite element simulation of incremental forming for 2219 aluminium integrally stiffened panel[J].Journal of Plasticity Engineering,2014,21(2):71-75.
[2]李卫东,万敏,阎昱.整体壁板压弯成形中性层及回弹解析[J].塑性工程学报,2014,21(5):156-161.
Li W D,Wan M,Yan Y.Neutral layer and springback analysis in press bend forming of aircraft integral panels[J].Journal of Plasticity Engineering,2014,21(5):156-161.
[3]Yan Y,Wan M,Wang H.FEM equivalent model for press bend forming of aircraft integral panel[J].Transactions of Nonferrous Metals Society of China,2009,19:414-421.
[4]赖松柏,于登云,陈同祥.整体壁板结构弯曲成形分析的等效塑性模型[J].宇航学报,2012,33(6):809-815.
Lai S B,Yu D Y,Chen T X.Plastic equivalent model for integrally stiffened panel in bending forming[J].Journal of Astronautics,2012,33(6):809-815.
[5]Yan Y,Wang H B,Wan M.Prediction of stiffener buckling in press bend forming of integral panels [J].Transactions of Nonferrous Metals Society of China, 2011,21(11):2459-2465.
[6]Yan Y,Wang H B,Wan M.Prediction of fracture in press bend forming of aluminum alloy highstiffener integral panels [J].Computational Materials Science,2011,50(7):2232-2244.
[7]张敏,田锡天,李波.整体壁板压弯成形的形状控制[J].航空学报,2020,41(7):66-77.
Zhang M,Tian X T,Li B.Shape control for press bend forming of integral panels[J].Acta Aeronautica et Astronautica Sinica, 2020,41(7):66-77.
[8]王忠堂,吴凯琦,张宏亮,等.AZ31镁合金网格式壁板级进压弯成形试验研究[J].热加工工艺,2023,52(3):88-91.
Wang Z T,Wu K Q,Zhang H L,et al.Experrimental study on progressive compression bending of AZ31 magnesium alloy grid panel[J].Hot Working Technology,2023,52(3):88-91.
[9]刘相柱,陈沛,刘晓,等.航天器X型整体壁板加工变形控制技术研究[J].机械科学与技术,2023,42(2):223-230.
Liu X Z,Chen P,Liu X,et al.Study on deformation control technology of Xshape integral panel for spacecraft[J].Mechanical Science and Technology for Aerospace Engineering,2023,42(2):223-230.
[10]乐晨,曹昱,杨帆,等.基于Abaqus的等边三角形网格加筋壳建模分析方法及试验验证研究[J].导弹与航天运载技术,2019(2):12-16.
Le C,Cao Y,Yang F,et al.The analysis method and experimental verification of isogrid stiffened shell based on Abaqus[J].Missiles and Space Vehicles,2019(2):12-16.
[11]Muoz C Leon, Kohlgrüber D, Langrand B.Analysis of fuselage skin reinforcements with beam element models in flexible aircraft panels for ditching simulations[J].IOP Conference Series:Materials Science and Engineering,2021,1024(1):012054.
[12]Boitsov V B,Gavva M L,Endogur I A, et al.Stressstrain state and buckling problems of structurallyanisotropic aircraft panels made of composite materials in view of production technology[J].Russian Aeronautics,2018,61(4):524-532.
[13]章润喆,马云龙,刘丹阳,等. 2195铝锂合金力学性能和组织与冷热变形过程的相关性[J].稀有金属, 2021,45(2):129-136.
Zhang R Z,Ma Y L,Liu D Y,et al. Dependence of mechanical properties and microstructures of 2195 AlLi alloy on cold and hot deformation process[J]. Chinese Journal of Rare Metals, 2021,45(2):129-136.
[14]马雪菲,王赫男,鄂顺,等. 化学转化处理时间对2198铝锂合金硝酸铈转化膜耐蚀性的影响[J]. 稀有金属, 2023,47(11):1477-1485.
Ma X F,Wang H N,E S,et al. Corrosion resistance of Ce(NO3)3 conversion film on 2198 AlLi alloy with different chemical conversion time[J]. Chinese Journal of Rare Metals,2023,47(11):1477-1485.
[15]王文波,闫亮明,胡强,等. 冷却预处理对7055铝合金板材组织与晶间腐蚀性能的影响[J].稀有金属, 2024,48(10):1378-1387.
Wang W B,Yan L M,Hu Q,et al.Microstructures and intergranular corrosion properties of 7055 alloy plate with cooling pretreatment[J]. Chinese Journal of Rare Metals, 2024,48(10):1378-1387.
[16]甘国强,李萍,薛克敏. 汽车件高强铝合金板件热冲压工艺研究进展[J]. 稀有金属, 2024,48(4):564-574.
Gan G Q,Li P,Xue K M. Research progress on hot stamping process of high strength aluminum alloy plates for automotive parts[J]. Chinese Journal of Rare Metals, 2024,48(4):564-574.
[17]张景新,郭沛欣,白杰.先进铝锂合金机身壁板结构承载能力研究[J].航空科学技术,2013(3):23-26.
Zhang J X,Guo P X,Bai J.Strength evaluation of advanced aluminumlithium fuselage panels[J].Aeronautical Science & Technology,2013(3):23-26.
|