Prediction on milling distortion for aero-multi-frame parts
被引:49
作者:
Guo, H.
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Changzhou Inst Technol, Changzhou 213002, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Guo, H.
[1
,2
]
Zuo, D. W.
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Zuo, D. W.
[1
]
Wu, H. B.
论文数: 0引用数: 0
h-index: 0
机构:
Digital Mfg Technol Lab Jiangsu Prov, Huaian 223001, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Wu, H. B.
[3
]
Xu, F.
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Xu, F.
[1
]
Tong, G. Q.
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h-index: 0
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
Tong, G. Q.
[1
]
机构:
[1] Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
[2] Changzhou Inst Technol, Changzhou 213002, Peoples R China
[3] Digital Mfg Technol Lab Jiangsu Prov, Huaian 223001, Peoples R China
来源:
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING
|
2009年
/
499卷
/
1-2期
关键词:
Milling distortion;
Monolithic component;
Multi-frame;
Finite element method;
WORKPIECE;
ERROR;
D O I:
10.1016/j.msea.2007.11.137
中图分类号:
TB3 [工程材料学];
学科分类号:
0805 ;
080502 ;
摘要:
Because the multi-frame component of an airplane has thin walls of variable wall thickness, and a high fitting accuracy is required, the prediction of its milling distortion is extremely important. In this study, the finite element model of the milling distortion analysis is established firstly for the multi-frame components, and the prediction analysis of the milling distortion under different milling conditions is carried out, by means of three-dimensional finite element simulation technology. Comparing the simulation results and the measurement ones of the milling distortion, the proposed model is modified and prediction method is proved to be effective. Software system is developed specially for the prediction of the milling distortion for aero-monolithic multi-frame components. By using of the software, a platform structure with 192 frames is analyzed and its milling distortion is predicted successfully. (C) 2008 Elsevier B.V. All rights reserved