Recent progress in precision measurement and assembly optimization methods of the aero-engine multistage rotor: A comprehensive review

被引:14
作者
Zhang, Maowei [1 ,2 ]
Liu, Datong [1 ,2 ]
Liu, Yongmeng [3 ,4 ]
机构
[1] Harbin Inst Technol, Sch Elect & Informat Engn, Harbin 150080, Peoples R China
[2] Harbin Inst Technol, Zhengzhou Res Inst, Zhengzhou 450000, Peoples R China
[3] Harbin Inst Technol, Ctr Ultraprecis Optoelect Instrument Engn, Harbin 150080, Peoples R China
[4] Minist Ind & Informat Technol, Harbin Inst Technol, Key Lab Ultraprecis Intelligent Instrumentat, Harbin 150080, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Precision measurement; Assembly optimization; Aero-engine; Blade sequence; Bolt tightening; JACOBIAN-TORSOR MODEL; TOLERANCE ANALYSIS; STRAIGHT-BUILD; BOLTED FLANGES; TIP CLEARANCE; PROPAGATION; COMPONENTS; UNBALANCE; PREDICTION; JOINT;
D O I
10.1016/j.measurement.2024.114990
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Due to the high standard of assembly accuracy, relying solely on the improvement of manufacturing accuracy of rotor has become difficult to meet the requirements of efficient and precise assembly on site, which is also difficult to avoid the accumulation of assembly errors. To solve this problem, the precision measurement and assembly optimization methods of the aero-engine multistage rotor have been reported in many literature. However, a comprehensive review focusing on precision measurement and assembly methods is lacking. To bridge this gap, this paper reviews the recent progress in precision measurement and assembly optimization methods of the aero-engine multistage rotor. First, the measurement and assembly optimization methods of the axial and radial geometric errors of multistage rotor are summarized, and the transmission model of geometric error, measurement datum, assembly datum, and optimization objective are analyzed. At the same time, the profile measurement methods of rotor are discussed, and three typical measurement equipment for the geometric error of multistage rotor are compared. Second, the measurement and assembly optimization methods of the unbalance error of multistage rotor are summarized, and blade sequence optimization methods of rotor are discussed. Furthermore, the vibration suppression method of aero-engine based on the control of unbalance error are summarized. Third, tightening and inspection of connecting bolts of multistage rotor are analyzed. Finally, summary is given to provide reference and theoretical guidance for precision measurement and assembly of the aero-engine multistage rotor.
引用
收藏
页数:14
相关论文
共 121 条
[41]   Research on optimizing-assembly and optimizing-adjustment technologies of aero-engine fan rotor blades [J].
Li-li, Li ;
Kun, Chen ;
Jian-min, Gao ;
Liu, Jun-kong ;
Zhi-yong, Gao ;
Hong-wei, Dai .
ADVANCED ENGINEERING INFORMATICS, 2022, 51
[42]   Measurement method of bolt hole assembly stress based on the combination of ultrasonic longitudinal and transverse waves [J].
Liu, Enxiao ;
Liu, Yongmeng ;
Chen, Yuanlin ;
Wang, Xiaoming ;
Ma, Huiping ;
Sun, Chuanzhi ;
Tan, Jiubin .
APPLIED ACOUSTICS, 2022, 189
[43]   Ultrasonic Measurement Method of Bolt Axial Stress Based on Time Difference Compensation of Coupling Layer Thickness Change [J].
Liu, Enxiao ;
Liu, Yongmeng ;
Wang, Xiaoming ;
Ma, Huiping ;
Chen, Yuanlin ;
Sun, Chuanzhi ;
Tan, Jiubin .
IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2021, 70
[44]   Design of acoustic Fresnel zone plate for contact stress measurement of aero-engine rotor mating surface [J].
Liu, Enxiao ;
Liu, Yongmeng ;
Wang, Xiaoming ;
Zhi, Junjie ;
Chen, Yuanlin ;
Sun, Chuanzhi ;
Tan, Jiubin .
JOURNAL OF SOUND AND VIBRATION, 2021, 500
[45]   Studies on dynamic characteristics of the joint in the aero-engine rotor system [J].
Liu Shuguo ;
Ma Yanhong ;
Zhang Dayi ;
Hong Jie .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2012, 29 :120-136
[46]   A Review of Tip Clearance in Propeller, Pump and Turbine [J].
Liu, Yabin ;
Tan, Lei ;
Wang, Binbin .
ENERGIES, 2018, 11 (09)
[47]   Review of modern low emissions combustion technologies for aero gas turbine engines [J].
Liu, Yize ;
Sun, Xiaoxiao ;
Sethi, Vishal ;
Nalianda, Devaiah ;
Li, Yi-Guang ;
Wang, Lu .
PROGRESS IN AEROSPACE SCIENCES, 2017, 94 :12-45
[48]   A novel cylindrical profile measurement model and errors separation method applied to stepped shafts precision model engineering [J].
Liu, Yongmeng ;
Mei, Yingjie ;
Sun, Chuanzhi ;
Li, Ruirui ;
Wang, Xiaoming ;
Wang, Hongye ;
Tan, Jiubin ;
Lu, Qing .
MEASUREMENT, 2022, 188
[49]   A coaxiality measurement model based on multi-systematic errors separation for turbine shaft [J].
Liu, Yongmeng ;
Li, Ruirui ;
Sun, Chuanzhi ;
Mei, Yingjie ;
Wang, Xiaoming ;
Tan, Jiubin ;
Wang, Hongye .
MEASUREMENT, 2021, 186
[50]   Influence of different ultrasonic transducers on the precision of fastening force measurement [J].
Liu, Yongmeng ;
Zhi, Junjie ;
Liu, Enxiao ;
Chen, Yuanlin ;
Wang, Xiaoming ;
Sun, Chuanzhi ;
Zifei, Cao ;
Ma, Huiping ;
Tan, Jiubin .
APPLIED ACOUSTICS, 2022, 185