个人概况：
姓 名：费成巍 博士，青年研究员，博导
职 位：青年研究员
单 位👳🏽♂️：杏鑫平台
地 址：中国上海杨浦区邯郸路220号 杏鑫平台 光华楼东主楼2517室
电 话：021-65643180
Email：https://scholar.google.com.hk/citations?hl=zh-CN&user=emHi_gsAAAAJ（Google Scholar）
https://orcid.org/0000-0001-5333-1055 (ORCID)
研究方向：
教育部博士生学术新人奖🔮🍒，2012。
学术及社会兼职🦸🏼♀️：
International Journal of Fatigue, 2022, 154:106558.
[11] Han L, Shi HQ, Tao M, Fei CW*, et al. Service damage mechanism and interface cracking behavior of Ni-based superalloy turbine blades with aluminized coating [J]. International Journal of Fatigue, 2021, 153:106500.
[12] Lu C, Fei CW*, Feng YW, et al. Probabilistic analyses of structural dynamic response with modified Kriging-based moving extremum framework[J]. Engineering Failure Analysis. 2021, 125:105398. (ESI高被引，热点文章)
[13] Han L, Wang YB, Zhang Y, Lu C, Fei CW*, et al. Competitive cracking behavior and microscopic mechanism of Ni-based superalloy blade respecting accelerated CCF failure [J]. International Journal of Fatigue, 2021, 150:106306. (ESI高被引)
[14] Han L, Chen C, Guo TY, Lu C, Fei CW*, et al. Probability-based service safety life prediction approach of raw and treated turbine blades regarding combined cycle fatigue[J]. Aerospace Science and Technology, 2021, 110: 106513. (ESI高被引)
[15] Fei CW, Liu HT, Li SL, Li H, An LQ, Lu C*. Dynamic parametric modeling-based model updating strategy of aeroengine casings [J]. Chinese Journal of Aeronautics, 2021, 34 (12)：145-157 (ESI高被引)
[16] Fei CW*, Li H, Liu HT, Lu C, et al. Enhanced network learning model with intelligent operator for the motion reliability evaluation of flexible mechanism[J]. Aerospace Science and Technology, 2020, 107: 106342.
[17] Fei CW, Liu HT, Zhu ZZ, An LQ, Li SL, Lu C*. Whole-process design and experimental validation of landing gear lower drag stay with global/local linked driven optimization strategy [J]. Chinese Journal of Aeronautics, 2020, 2021, 34(2):318-328. (ESI高被引)
[18] Lu C, Feng YW, Fei CW*, Bu SQ. Improved decomposed-coordinated Kriging modeling strategy for dynamic probabilistic analysis of multi-component structures [J]. IEEE Transactions on Reliability. 2020, 69(2): 440-457.(ESI高被引)
[19] Lu C, Fei CW*, Li H, Liu HT, An LQ. Moving extremum surrogate modeling strategy for dynamic reliability estimation of turbine blisk with multi-physics fields [J]. Aerospace Science and Technology. 2020, 106: 106112.
[20] Fei CW, Li H, Liu HT, Lu C*, Keshtegar B*. Multilevel nested reliability-based design optimization with hybrid intelligent regression for operating assembly relationship [J]. Aerospace Science and Technology, 2020, 103: 105906. (ESI高被引)
[21] Lu C, Feng YW, Fei CW*, Bu SQ. Improved decomposed-coordinated Kriging modeling strategy for dynamic probabilistic analysis of multi-component structures [J]. IEEE Transactions on Reliability. 2020, 69(2): 440-457. (ESI高被引)
[22] Fei CW*, Lu C, Liem R.P. Decomposed-coordinated surrogate modelling strategy for compound function approximation and a turbine blisk reliability evaluation [J]. Aerospace Science and Technology, 2019, 95🐉：105466.
[23] Song LK, Bai GC, Fei CW*, Tang WZ. Multi-failure probabilistic design for turbine bladed disks using neural network regression with distributed collaborative strategy [J], Aerospace Science and Technology, 2019, 92: 464-477.
[24] Tian J, Ai YT, Fei CW*, Zhang FL. Dynamic modeling and simulation of inter-shaft bearings with localized defects excited by time-varying displacement [J]. Journal of Vibration and Control, 2019, 25(8): 1436-1446.
[25] Song LK, Bai GC, Fei CW*, Wen J. Probabilistic LCF life assessment of turbine discs using DC-based wavelet neural network regression [J]. International Journal of Fatigue 2019, 119: 204-219.
[26] Lu C, Feng YW, Rhea. P Liem, Fei CW*. Improved kriging with extremum response surface method for structural dynamic reliability and sensitivity analyses [J]. Aerospace Science and Technology, 2018, 76:164-175.
学术专著：
Ø 费成巍、路成、闫成、李坚。基于先进代理模型的航空结构可靠性设计理论方法[M]. 科学出版社，2023🙁；
Ø 费成巍🚢，艾延廷♿，田晶. 基于信息融合的航空发动机整机振动故障诊断技术 [M]. 科学出版社, 2020；
Ø 费成巍，复杂机械动态装配可靠性设计理论与方法研究[D],博士学位论文，2014. 航空宇航科学与技术学科全国优秀博士学位论文。
出版教材：
《航空航天结构智能可靠性设计》💇🏼，工信部十四五规划教材🥏，2024👨🏻，排名👵🏼👩🦱：第1；
申请专利：
u 一种组合式XX结构, ZL 2016 2 0617689.7, 实用新型, 2016.
u 一种可调节末级压降的XX结构👩🏽⚖️，ZL 202010409025.2, 发明专利，2020.
u 涡轮机械XXX概率优化设计方法，发明专利, 2020.
u 复杂工程结构系统逼近分析的XXX方法，发明专利, 2020.
u 工程结构可靠性设计的XXX方法，发明专利, 2020.
u 复杂机械动态装配关系XXX设计方法，发明专利, 2020.
u 飞机XXX的联合驱动全过程优化技术，发明专利, 2020.
u 一种基于XXX模型的复杂工程系统可靠性设计方法🍐，发明专利.
u Last-Stage Pressure Drop-Adjustable Multistage Brush Seal Structure⏳，美国发明专利, 2020.
u 一种XXX参数识别的综合方法, 发明专利. 2021.
u 一种基于矢量XXX可靠性设计方法，发明专利. 2021；
u 一种基于矢量混合代理模型的XXXX可靠性设计方法🤣。发明专利, 2021
u Complex Structure reliability design method based on hybrid vector surrogate model, 南非发明专利，2021⭕️💂♂️。
u 一种涡轮叶盘低周疲劳寿命预测方法及系统👩🔬，2022.
软件著作权：
u 低频振荡信号模态识别软件V1.0，2021SR0678115, 2021.
u 航空发动机结构疲劳寿命预测可靠度灵敏度分析软件(Aero-Life)🧘，2021SR1879601🏋🏿♀️，2021.
u 基于有向支持向量机的结构可靠性分析软件V1.0，2023SR0311543，2023
招生/招聘
欢迎有志于从事航空航天事业👩🏫、且具有航空发动机、飞行器设计、机械工程🚼、力学🧛🏻、大数据、人工智能等相关学科背景的优秀学生和学者加入本课题组🤚🏼，包括
Ø 本校本科生开展大学生科创项目研究🌝；
Ø 保送或报考硕士研究生和博士研究生🧑🏿⚖️🏋🏼♀️；
Ø 优秀博士进站从事博士后研究⛹️♂️👩✈️，将提供具有竞争力的薪金和津贴📘；
Ø 长期招聘教授🧍♂️、青年研究员🙎、青年副研究员等职位🍿，详见杏鑫主页招聘信息：/rczpxx/list.htm；
以上优异者可推荐至香港😀⚽️、新加坡等海外顶尖学府进行联合培养或交流。有意者请联系：cwfei@fudan.edu.cn。
