Review on manufacture of aeroengine wide chord hollow fan blade
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摘要:
详细介绍了国外航空发动机风扇叶片结构及成形技术的发展与现状，从结构设计、成形工艺以及力学性能领域分析了国内钛合金宽弦空心风扇叶片研究现状。基于宽弦空心风扇叶片服役过程中现存问题，结合扩散焊接/常规塑性/超塑性成形技术，探讨了叶片空腔结构设计、成形工艺优化以及扩散焊结构力学性能三大领域的关键技术研究发展方向。结果表明：空腔结构的设计应基于结构轻量化、成形可行性及力学性能最优三大目标展开研究；成形工艺的优化着重开展多工序多目标耦合优化、数值计算精度提高、材料冷热复合加工过程形性演变精确预测与控制等方面的研究；扩散焊结构力学性能的提高应当从复杂载荷条件下焊缝裂纹扩展以及疲劳性能演变等方面展开研究。
Abstract:The development and present situation of aeroengine fan blade structure, forming technology abroad were introduced in details. The research status of titanium alloy wide chord hollow fan blade in China was analyzed from the aspects of structure design, forming process and mechanical properties. Based on the existing problems in the service process of wide-chord hollow fan blades, combining with the diffusion welding/conventional plastic/superplastic forming technology, the development direction of key technologies in the three fields of blade cavity structure design, forming process optimization and mechanical properties of multilayer diffusion welding structure were discussed. The cavity structure design should be based on three objectives: lightweight structure, feasibility of forming and optimal mechanical properties; The optimization of forming process focuses on the coupling optimization of multi-process and multi-objective, the improvement of numerical calculation accuracy, and the precise prediction and control of material shape evolution during cold and hot composite machining; The improvement of mechanical properties of diffusion welded structures should be studied from the aspects of bonding joint crack propagation and fatigue behavior evolution under complex load conditions.
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图 3 钛合金宽弦空心风扇叶片发展过程示意图
Figure 3. Schematic diagram of development process of titanium alloy wide-chord hollow fan blade
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[1] 陈懋章,刘宝杰. 大涵道比涡扇发动机风扇/压气机气动设计技术分析[J]. 航空学报,2008,29(3): 513-526. doi: 10.3321/j.issn:1000-6893.2008.03.001CHEN Maozhang,LIU Baojie. Fan/compressor aero design technology for high bypass ratio turbofan[J]. Acta Aeronautica et Astronautica Sinica,2008,29(3): 513-526. (in Chinese) doi: 10.3321/j.issn:1000-6893.2008.03.001 [2] 李志强, 杜发荣, 张力. 大涵道比涡扇发动机的宽弦空心风扇叶片技术研究[C]//大型飞机关键技术高层论坛暨中国航空学会学术年会论文集. 广州 深圳: 中国航空学会, 2007: 1320-1332. [3] 李迪,陈云永,廖连芳. 空心风扇叶片高循环疲劳试验设计与验证[J]. 航空动力学报,2017,32(6): 1359-1365. doi: 10.13224/j.cnki.jasp.2017.06.011LI Di,CHEN Yunyong,LIAO Lianfang. Experimental design and verification of hollow fan blade high cycle fatigue[J]. Journal of Aerospace Power,2017,32(6): 1359-1365. (in Chinese) doi: 10.13224/j.cnki.jasp.2017.06.011 [4] 吴心晨. 宽弦空心风扇叶片超塑成形/扩散连接工艺研究[D]. 南京: 南京航空航天大学, 2015.WU Xinchen. Research on superplastic forming and diffusion bonding technology of hollow wide-chord fan blade[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese) [5] 刘志强,李从富,贾林,等. 钛合金空心风扇叶片模拟鸟撞研究[J]. 航空科学技术,2022,33(9): 7-15. doi: 10.19452/j.issn1007-5453.2022.09.002LIU Zhiqiang,LI Congfu,JIA Lin,et al. Research on simulant bird strike of Titanium alloy hollow fan blade[J]. Aeronautical Science and Technology,2022,33(9): 7-15. (in Chinese) doi: 10.19452/j.issn1007-5453.2022.09.002 [6] 康永强,陈勇. 铺层复合材料风扇叶片榫头层间应力分析[J]. 航空动力学报,2020,35(2): 388-396. doi: 10.13224/j.cnki.jasp.2020.02.018KANG Yongqiang,CHEN Yong. Inter-laminar stress analysis of laminated composite fan blade dovetail[J]. Journal of Aerospace Power,2020,35(2): 388-396. (in Chinese) doi: 10.13224/j.cnki.jasp.2020.02.018 [7] 刘洋,王亮,郭军. 铝包边对复合材料风扇叶片抗鸟撞能力的影响[J]. 兵工学报,2018,39(增刊1): 114-120.LIU Yang,WANG Liang,GUO Jun. Infuence of aluminum package edge on bird-stike resistance of composite fan blades of an engine[J]. Acta Armamentarii,2018,39(Suppl.1): 114-120. (in Chinese) [8] 谭志刚,赵兴东,唐军,等. TiB2/7050铝基复合材料风扇叶片锻件的研制[J]. 热加工工艺,2018,47(11): 114-116, 119.TAN Zhigang,ZHAO Xingdong,TANG Jun,et al. Development of TiB2/7050 aluminium matrix composite fan blade forgings[J]. Hot Working Technology,2018,47(11): 114-116, 119. (in Chinese) [9] 肖贾光毅,陈勇,欧阳华,等. 复合材料风扇叶片-机匣碰摩振动的数值模拟[J]. 航空动力学报,2019,34(5): 997-1009.XIAO Jiaguangyi,CHEN Yong,OUYANG Hua,et al. Numerical investigation of composite fan blade vibration characteristics due to blade-casing rub[J]. Journal of Aerospace Power,2019,34(5): 997-1009. (in Chinese) [10] 刘世锋,宋玺,薛彤,等. 钛合金及钛基复合材料在航空航天的应用和发展[J]. 航空材料学报,2020,40(3): 77-94. doi: 10.11868/j.issn.1005-5053.2020.000061LIU Shifeng,SONG Xi,XUE Tong,et al. Application and development of titanium alloy and titanium matrix composites in aerospace field[J]. Journal of Aeronautical Materials,2020,40(3): 77-94. (in Chinese) doi: 10.11868/j.issn.1005-5053.2020.000061 [11] 李毅,赵永庆,曾卫东. 航空钛合金的应用及发展趋势[J]. 材料导报,2020,34(增刊1): 280-282.LI Yi,ZHAO Yongqing,ZENG Weidong. Application and development of aerial titanium alloys[J]. Materials Reports,2020,34(Suppl.1): 280-282. (in Chinese) [12] 刘强,赵龙,黄峰. 商用大涵道比发动机复合材料风扇叶片应用现状与展望[J]. 航空制造技术,2014,57(15): 58-62. doi: 10.16080/j.issn1671-833x.2014.15.006LIU Qiang,ZHAO Long,HUANG Feng. Present conditions and development of composite fan blades of high bypass ratio commercial jet engines[J]. Aeronautical Manufacturing Technology,2014,57(15): 58-62. (in Chinese) doi: 10.16080/j.issn1671-833x.2014.15.006 [13] 朱启晨,陈勇,肖贾光毅. 复合材料风扇叶片铺层设计方法研究[J]. 航空发动机,2018,44(3): 49-54.ZHU Qichen,CHEN Yong,XIAO Jiaguangyi. Study on laminate design method of composite fan blade[J]. Aeroengine,2018,44(3): 49-54. (in Chinese) [14] 康永强,陈勇. 复合材料风扇叶片榫头铺层设计及加工制造[J]. 合成纤维,2020,49(1): 44-51. doi: 10.16090/j.cnki.hcxw.2020.01.011KANG Yongqiang,CHEN Yong. Laminate design of composite fan blade dovetail[J]. Synthetic Fiber in China,2020,49(1): 44-51. (in Chinese) doi: 10.16090/j.cnki.hcxw.2020.01.011 [15] 孙煜,刘强,黄峰,等. 复合材料风扇叶片钛合金加强边胶接技术研究[J]. 复合材料科学与工程,2021(3): 78-81, 98. doi: 10.19936/j.cnki.2096-8000.20210328.012SUN Yu,LIU Qiang,HUANG Feng,et al. Study on bonding technology of titanium alloy trim/composite fan blade[J]. Composites Science and Engineering,2021(3): 78-81, 98. (in Chinese) doi: 10.19936/j.cnki.2096-8000.20210328.012 [16] 韦鑫,荆云娟,杨明杰,等. 航空发动机风扇叶片预制体研发现状及趋势[J]. 棉纺织技术,2020,48(8): 81-84.WEI Xin,JING Yunjuan,YANG Mingjie,et al. Development status and trend of aeroengine fan blade preform[J]. Cotton Textile Technology,2020,48(8): 81-84. (in Chinese) [17] 佚名. 罗罗将在发动机中用碳纤维和陶瓷基复合材料[J]. 玻璃钢/复合材料,2014(4): 98.Anonymous. Rolls-Royce will use carbon fiber and ceramic matrix composites in engines[J]. Fiber Reinforced Plastics/Composites,2014(4): 98. (in Chinese) [18] 杨洋. 英国罗罗公司首款碳钛合金风扇叶片开始飞行测试[M]//中国有色金属工业协会专家委员会组织. 中国钛业. 北京: 冶金工业出版社, 2014. [19] 石. 纳米复合材料的新用途[J]. 航空维修与工程,2008(1): 55. doi: 10.19302/j.cnki.1672-0989.2008.01.020SHI. New uses of nano-composite materials[J]. Aviation Maintenance and Engineering,2008(1): 55. (in Chinese) doi: 10.19302/j.cnki.1672-0989.2008.01.020 [20] 丁建国,胡骏,蔡显新. 某复合掠形风扇设计与内外函数值模拟研究[J]. 航空动力学报,2009,24(3): 626-633. doi: 10.13224/j.cnki.jasp.2009.03.015DING Jianguo,HU Jun,CAI Xianxin. Design and core and bypass numerical simulation of acompound swept fan[J]. Journal of Aerospace Power,2009,24(3): 626-633. (in Chinese) doi: 10.13224/j.cnki.jasp.2009.03.015 [21] 吴心晨,陈明和,谢兰生,等. 复杂外形航空发动机TC4钛合金宽弦空心风扇叶片弯扭成形[J]. 航空学报,2015,36(6): 2055-2063.WU Xinchen,CHEN Minghe,XIE Lansheng,et al. Twist-bend forming of aeroengine titanium TC4 wide-chord hollow fan blade with complex geometries[J]. Acta Aeronautica et Astronautica Sinica,2015,36(6): 2055-2063. (in Chinese) [22] 陈矛章. 风扇/压气机技术发展和对今后工作的建议[J]. 航空动力学报,2002,17(1): 1-15.CHEN Maozhang. Development of fan/compressor techniques and suggestions on further researches[J]. Journal of Aerospace Power,2002,17(1): 1-15. (in Chinese) [23] 马子于,苏震宇,魏然. 复合材料风扇叶片的发展与思考[J]. 科技与创新,2020(13): 34-37.MA Ziyu,SU Zhenyu,WEI Ran. Development and thinking of composite fan blades[J]. Science and Technology & Innovation,2020(13): 34-37. (in Chinese) [24] 侯冠群. 宽弦空心风扇叶片制造工艺的发展[J]. 航空制造工程,1994(5): 6-8.HOU Guanqun. Development of manufacturing technology of wide chord hollow fan blades[J]. Aviation Maintenance and Engineering,1994(5): 6-8. (in Chinese) [25] 梁春华,杨锐. 航空发动机宽弦空心风扇叶片的发展及应用[J]. 航空发动机,1999,25(2): 54-58.LIANG Chunhua,YANG Rui. Development and application of wide chord hollow fan blades for aero-engine[J]. Aeroengine,1999,25(2): 54-58. (in Chinese) [26] 王乐安. 国外航空发动机风扇叶片及其成形技术[J]. 航空科学技术,1995,6(1): 31-33.WANG Lean. Foreign aero-engine fan blades and their forming technology[J]. Aeronautical Science and Technology,1995,6(1): 31-33. (in Chinese) [27] JOSEPH A. Method of fabricating hollow gas turbine blades: US3623204[P]. 1971. [28] MICHAEL P, PETRIE J A. Method of making an aerofoil-shaped blade for a fluid flow machine: US3566493[P]. 1971-03-02. [29] BICHON M, DOUGUET C J P, LORIEUX A G H, et al. Process for manufacturing a hollow blade for a turbo-machine: US5636440[P]. 1997-06-10. [30] HAMILTON C H. Method for making metallic structures from two or more selectively bonded sheets: GB1495655A[P]. 1977-12-21. [31] COLLOT A C F, SOHIER B P C, VARELA D. Method for fabricating a hollow blade for a turbomachine: EP0500458A1[P]. 1992-08-26. [32] 李琳,薛铮. 等强度三维空心叶片的内部拓扑结构[J]. 航空动力学报,2012,27(10): 2329-2335.LI Lin,XUE Zheng. Internal structure of three-dimensional hollow blade with equal strength[J]. Journal of Aerospace Power,2012,27(10): 2329-2335. (in Chinese) [33] 阎军,张晨光,霍思旭,等. 宽弦风扇叶片空腔结构多目标轻量化设计[J]. 航空科学技术,2021,32(4): 60-64.YAN Jun,ZHANG Chenguang,HUO Sixu,et al. Multi-objective lightweight design of the cavity structure of wide-chord fan blades[J]. Aeronautical Science & Technology,2021,32(4): 60-64. (in Chinese) [34] 严林鑫. 航空发动机宽弦风扇叶片结构优化设计研究[D]. 泉州: 华侨大学, 2020.YAN Linxin. Research on structural optimization design of aero-engine wide-chord fan blade[D]. Quanzhou: Huaqiao University, 2020. (in Chinese) [35] 吴惠松,黄致建,郝艳华,等. 桁架式空心风扇叶片结构参数化设计平台开发[J]. 机械设计与制造,2013(10): 66-68,72. doi: 10.3969/j.issn.1001-3997.2013.10.022WU Huisong,HUANG Zhijian,HAO Yanhua,et al. The parametric design platform development for hollow fan blade of girder internal structure[J]. Machinery Design and Manufacture,2013(10): 66-68,72. (in Chinese) doi: 10.3969/j.issn.1001-3997.2013.10.022 [36] 于洋,张力,战鹏,等. 宽弦空心风扇转子叶片叶身结构设计参数分析[J]. 航空发动机,2010,36(1): 24-26. doi: 10.3969/j.issn.1672-3147.2010.01.006YU Yang,ZHANG Li,ZHAN Peng,et al. Analysis of design parameters of wide chord hollow fan blade structure[J]. Aeroengine,2010,36(1): 24-26. (in Chinese) doi: 10.3969/j.issn.1672-3147.2010.01.006 [37] 杨剑秋,王延荣. 基于正交试验设计的空心叶片结构优化设计[J]. 航空动力学报,2011,26(2): 376-384.YANG Jianqiu,WANG Yanrong. Structural optimization of hollow fan blade based on orthogonal experimental design[J]. Journal of Aerospace Power,2011,26(2): 376-384. (in Chinese) [38] 刚铁. 宽弦空心风扇叶片结构设计及强度分析研究[D]. 南京: 南京航空航天大学, 2005.GANG Tie. Research on structural design and stress analysis of hollow fan blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2005. (in Chinese) [39] 侯冠群,尚波生. 宽弦风扇叶片技术的发展[J]. 国际航空,2002(12): 45-47.HOU Guanqun,SHANG Bosheng. Development of wide chord fan blade technology[J]. International aviation,2002(12): 45-47. (in Chinese) [40] 陈明和,吴心晨,谢兰生,等. 复杂结构的钛合金宽弦空心风扇叶片的双层制造工艺及其毛坯优化设计[J]. 稀有金属材料与工程,2019,48(6): 1717-1724.CHEN Minghe,WU Xinchen,XIE Lansheng,et al. Two-layer process and optimal blank design for hollow titanium wide-chord fan blades with complex geometries[J]. Rare Metal Materials and Engineering,2019,48(6): 1717-1724. (in Chinese) [41] 吴心晨,陈明和,谢兰生,等. TC4钛合金空心风扇叶片面板成形缺陷的蠕变修复[J]. 稀有金属材料与工程,2016,45(11): 2942-2947.WU Xinchen,CHEN Minghe,XIE Lansheng,et al. Creep repair of skin defects for the titanium TC4 wide-chord hollow fan blade[J]. Rare Metal Materials and Engineering,2016,45(11): 2942-2947. (in Chinese) [42] WANG Ning,CHEN Minghe,XIE Lansheng. Hot flow behavior characterization for predicting the titanium alloy TC4 hollow blade surface Sinkage defects in the SPF/DB process[J]. International Journal of Material Forming,2019,12(5): 827-844. doi: 10.1007/s12289-018-1454-z [43] 王荣华. 翼类钛合金零件超塑成形/扩散连接关键工艺研究[D]. 南京: 南京航空航天大学, 2009.WANG Ronghua. Research on the superplastic forming and diffusion bonding technology for aerofoil part of titanium alloy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009. (in Chinese) [44] ZHAO Bing,LI Zhiqiang,HOU Hongliang,et al. Three dimensional FEM simulation of titanium hollow blade forming process[J]. Rare Metal Materials and Engineering,2010,39(6): 963-968. doi: 10.1016/S1875-5372(10)60106-3 [45] 门向南. TC4三层板结构超塑成形/扩散焊接工艺研究[D]. 南京: 南京航空航天大学, 2010.MEN Xiangnan. Research on superplastic forming and diffusion bonding for three-sheet structure of TC4 titanium alloy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010. (in Chinese) [46] 高庆峰. 宽弦空心风扇叶片超塑成形的数值仿真研究[D]. 南京: 南京航空航天大学, 2008.GAO Qingfeng. Research and application of numerical simulation of superplastic forming hollow fan blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008. (in Chinese) [47] 徐伟. 某航空发动机叶片超塑成形/扩散连接工艺参数优化[D]. 沈阳: 沈阳航空航天大学, 2012.XU Wei. Some earoengine leaf SPF/DB parameters optimization[D]. Shenyang: Shenyang Aerospace University, 2012. (in Chinese) [48] 江志伟,赵正彩,傅玉灿,等. 钛合金宽弦空心风扇叶片进排气边加工变形预测[J]. 航空制造技术,2017,60(19): 86-91.JIANG Zhiwei,ZHAO Zhengcai,FU Yucan,et al. Machining deformation prediction of titanium alloy wide chord hollow fan blade[J]. Aeronautical Manufacturing Technology,2017,60(19): 86-91. (in Chinese) [49] 徐九华, 赵正彩, 傅玉灿, 等. 钛合金宽弦空心风扇叶片数控切削加工关键技术[J]. 南京航空航天大学学报, 2014, 46(5): 659-666.XU Jiuhua, ZHAO Zhengcai, FU Yucan, et al. Key technologies of NC machining of titanium wide chord hollow fan blade[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2014, 46(5): 659-666. (in Chinese) [50] 佚名. 制造院自主研制的钛合金宽弦空心风扇叶片在CJ-1000AX首台整机上完成装配[J]. 航空精密制造技术,2018,54(1): 63.Anonymous. Titanium alloy wide chord hollow fan blade independently developed by the manufacturing institute was assembled on the first CJ-1000AX machine[J]. Aerospace Precision Manufacturing Technology,2018,54(1): 63. (in Chinese) [51] 蒋少松. TC4钛合金超塑成形精度控制[D]. 哈尔滨: 哈尔滨工业大学, 2009.JIANG Shaosong. Accuracy control of superplastic forming for TC4 titanium alloy[D]. Harbin: Harbin Institute of Technology, 2009. (in Chinese) [52] 林立. 复杂薄壁叶片加工误差分析与研究[D]. 北京: 北京交通大学, 2011.LIN Li. Analysis and research on error of manufacturing complex thin-walled blade surface[D]. Beijing: Beijing Jiaotong University, 2011. (in Chinese) [53] 郝炜,蔺小军,单晨伟,等. 薄壁叶片前后缘加工误差补偿技术研究[J]. 机械科学与技术,2011,30(9): 1446-1450. doi: 10.13433/j.cnki.1003-8728.2011.09.019HAO Wei,LIN Xiaojun,SHAN Chenwei,et al. Research on the machining error compensation for the leading and trailing edges of thin-walled blades[J]. Mechanical Science and Technology for Aerospace Engineering,2011,30(9): 1446-1450. (in Chinese) doi: 10.13433/j.cnki.1003-8728.2011.09.019 [54] 乔虎,邓瑞祥,伍娅,等. MTS1600-500六轴数控砂带磨床构建及磨削仿真验证[J]. 机床与液压,2021,49(24): 153-158.QIAO Hu,DENG Ruixiang,WU Ya,et al. Construction and grinding simulation verification of MTS1600-500 Si x axis CNC belt grinder[J]. Machine Tool & Hydraulics,2021,49(24): 153-158. (in Chinese) [55] 平波. 钛合金圆弧榫齿高效精密加工技术研究[D]. 南京: 南京航空航天大学, 2015.PING Bo. Research on high efficiency and precision machining of titanium circular-arc rabbet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese) [56] 张宏之,梁巧云,陈盛天,等. 航发钛合金风扇叶片自适应砂带磨削实验研究[J]. 金刚石与磨料磨具工程,2018,38(5): 67-72.ZHANG Hongzhi,LIANG Qiaoyun,CHEN Shengtian,et al. Research on adaptive belt grinding aeroengine titanium alloy fan blades[J]. Diamond & Abrasives Engineering,2018,38(5): 67-72. (in Chinese) [57] 刘树生. 航空钛合金叶片数控砂带磨削关键技术[J]. 航空制造技术,2011,54(4): 34-38. doi: 10.3969/j.issn.1671-833X.2011.04.003LIU Shusheng. Key technology of NC abrasive belt grinding for titanium blade[J]. Aeronautical Manufacturing Technology,2011,54(4): 34-38. (in Chinese) doi: 10.3969/j.issn.1671-833X.2011.04.003 [58] 吴为,张凯锋,龚泰宾. TB2钛合金扩散焊接头强度的影响因素[J]. 宇航材料工艺,2002,32(2): 55-59. doi: 10.3969/j.issn.1007-2330.2002.02.014WU Wei,ZHANG Kaifeng,GONG Taibin. Influencing factors of strength of diffusion bonding TB2 alloy joint[J]. Aerospace Materials and Technology,2002,32(2): 55-59. (in Chinese) doi: 10.3969/j.issn.1007-2330.2002.02.014 [59] 程耀永,马文利,郭万林. TC4合金TLP扩散焊的组织与性能[J]. 材料工程,1999,27(12): 31-34. doi: 10.3969/j.issn.1001-4381.1999.12.010CHENG Yaoyong,MA Wenli,GUO Wanlin. The microstructure and properties of TLP diffusion bonding joints of TC4 alloys[J]. Journal of Materials Engineering,1999,27(12): 31-34. (in Chinese) doi: 10.3969/j.issn.1001-4381.1999.12.010 [60] 熊进辉, 高福洋, 陈斌, 等. TC4钛合金真空扩散焊工艺研究[C]//中国有色金属工业协会钛锆铪分会2014年会论文集. 辽宁 大连: 中国有色金属工业协会, 2014: 213-219. [61] LI Hong,ZHANG Chao,LIU Hongbin,et al. Bonding interface characteristic and shear strength of diffusion bonded Ti-17 titanium alloy[J]. Transactions of Nonferrous Metals Society of China,2015,25(1): 80-87. doi: 10.1016/S1003-6326(15)63581-6 [62] 贾旭,胡绪腾,朱自佳,等. FOD缺口型损伤对TC4疲劳极限强度的影响[J]. 航空动力学报,2018,33(7): 1584-1594.JIA Xu,HU Xuteng,ZHU Zijia,et al. Effect of FOD notch-type damage on fatigue limit strength of TC4[J]. Journal of Aerospace Power,2018,33(7): 1584-1594. (in Chinese) [63] 周克印,徐来,林兆荣,等. TC4 钛板扩散连接后的疲劳断裂特性[J]. 机械强度,1998,20(2): 112-115.ZHOU Keyin,XU Lai,LIN Zhaorong,et al. Fatigue and fracture characteristics of titanium alloy boards bonded by diffusion[J]. Journal of Mechanical Strength,1998,20(2): 112-115. (in Chinese) [64] 谢佩玉. TC4扩散焊接头疲劳性能研究[D]. 南京: 南京航空航天大学, 2016.XIE Peiyu. Research on fatigue properties of TC4 diffusion bonding joints[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016. (in Chinese) [65] 刘小刚,谢佩玉,郭海丁,等. TC4钛合金扩散焊接头的力学性能[J]. 航空动力学报,2017,32(6): 1342-1348.LIU Xiaogang,XIE Peiyu,GUO Haiding,et al. Mechanical properties of TC4 titanium alloy diffusion bonded joints[J]. Journal of Aerospace Power,2017,32(6): 1342-1348. (in Chinese) [66] 刘小刚,朱笑林. 钛合金扩散焊接头复合型疲劳裂纹扩展[J]. 航空动力学报,2019,34(11): 2395-2402. doi: 10.13224/j.cnki.jasp.2019.11.011LIU Xiaogang,ZHU Xiaolin. Mixed-mode fatigue crack propagation of titanium alloy diffusion bonded joints[J]. Journal of Aerospace Power,2019,34(11): 2395-2402. (in Chinese) doi: 10.13224/j.cnki.jasp.2019.11.011 [67] 招文龙,刘小刚,谢佩玉,等. TC4钛合金扩散焊接头剪切疲劳性能研究[J]. 航空发动机,2020,46(3): 99-102. doi: 10.13477/j.cnki.aeroengine.2020.03.018ZHAO Wenlong,LIU Xiaogang,XIE Peiyu,et al. Study on shear fatigue performance of TC4 titanium alloy diffusion bonded joints[J]. Aeroengine,2020,46(3): 99-102. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2020.03.018 [68] 赵萍,何清华,杨治国. 航空发动机叶片疲劳断裂研究领域与方法概述[J]. 航空发动机,2009,35(3): 58-61,4.ZHAO Ping,HE Qinghua,YANG Zhiguo. Summarize of investigation and method for blade fatigue fracture of aeroengine[J]. Aeroengine,2009,35(3): 58-61,4. (in Chinese) [69] 关玉璞,陈伟,高德平. 航空发动机叶片外物损伤研究现状[J]. 航空学报,2007,28(4): 851-857.GUAN Yupu,CHEN Wei,GAO Deping. Present status of investigation of foreign object damage to blade in aeroengine[J]. Acta Aeronautica et Astronautica Sinica,2007,28(4): 851-857. (in Chinese) [70] 李百洋. SPF/DB宽弦空心叶片单元件弯曲疲劳性能研究[D]. 南京: 南京航空航天大学, 2018.LI Baiyang. Research on bending fatigue behaviors of SPF/DB wide-chord hollow blade specimen[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2018. (in Chinese) [71] 黄家经. 商用发动机钛合金宽弦空心风扇叶片振动特性及疲劳研究[C]//2015年第二届中国航空科学技术大会论文集. 北京: 中国航空学会, 2015: 313-316. [72] LI G Y,TAN M J,LIEW K M. Three-dimensional modeling and simulation of superplastic forming[J]. Journal of Materials Processing Technology,2004,150(1/2): 76-83. [73] CHEN Y,KIBBLE K,HALL R,et al. Numerical analysis of superplastic blow forming of Ti-6Al-4V alloys[J]. Materials & Design,2001,22(8): 679-685. [74] 李百洋,刘小刚,郭海丁. FOD对TC4合金扩散焊板材HCF性能影响[J]. 航空发动机,2018,44(5): 93-97. doi: 10.13477/j.cnki.aeroengine.2018.05.014LI Baiyang,LIU Xiaogang,GUO Haiding. Effect of foreign object damage (FOD) on the high cycle fatigue (HCF) performance of TC4 alloy diffusion bonding plate[J]. Aeroengine,2018,44(5): 93-97. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2018.05.014 [75] 丁进. 外物损伤对TC4扩散焊结构疲劳性能影响研究[D]. 南京: 南京航空航天大学, 2017.DING Jin. Research on effects of foreign object damage to TC4 diffusion bonding structure on fatigue properties[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017. (in Chinese) [76] 孙青平. 空心风扇叶片桁架式夹芯结构件疲劳特性研究[D]. 南京: 南京航空航天大学, 2014.SUN Qingping. On the fatigue behaviors of truss stiffened structure used in hollow fan blade[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014. (in Chinese) [77] Australian Transport Safety Bureau. Engine failure involving Airbus[R]. The 62th Northbourne Avenue Canberra: Australian Capital Territory, ATSB Report No: AO-2017-066, 2020. [78] ANDERSON C R, TOMEO P V. Gas turbine engine fan blade lock assembly: US9376926[P]. 2016-06-28. [79] 陈继乐. 铝合金焊接接头焊缝区力学性能理论与试验研究[D]. 辽宁 大连: 大连海事大学, 2018.CHEN Jile. Theoretical and experimental study on mechanical properties of weld zone of aluminum alloy welded joints[D]. Dalian Liaoning: Dalian Maritime University, 2018. (in Chinese) [80] 杨磊. 钛合金扩散焊接头焊缝区显微力学行为研究[D]. 南京: 南京航空航天大学, 2017.YANG Lei. Study on micromechanical behavior of weld zone of diffusion welded joint of titanium alloy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017. (in Chinese) [81] 宋凯,毛小南,辛社伟,等. 钛合金焊接接头组织性能研究进展[J]. 材料导报,2018,32(增刊2): 336-340.SONG Kai,MAO Xiaonan,XIN Shewei,et al. Research progress on microstructure and properties of titanium alloy welded joints[J]. Materials Review,2018,32(Suppl.2): 336-340. (in Chinese) [82] HUANG C A,WANG T H,LEE C H,et al. A study of the heat-affected zone (HAZ) of an Inconel 718 sheet welded with electron-beam welding (EBW)[J]. Materials Science and Engineering:A,2005,398(1/2): 275-281. [83] LEE H K,KIM K S,KIM C M. Fracture resistance of a steel weld joint under fatigue loading[J]. Engineering Fracture Mechanics,2000,66(4): 403-419. doi: 10.1016/S0013-7944(00)00017-5 -
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