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2021 Vol. 64, No. 23/24
Published: 2021-12-15

FEATURE
FORUM
RESEARCH
C0NTENTS
COVER STORY
APPROACHING SCIENCE
 
1 COVER
2021 Vol. 64 (23/24): 1-1 [Abstract] ( 107 ) HTMLNew PDF (2163 KB)  ( 85 )
       C0NTENTS
6 CONTENTS
2021 Vol. 64 (23/24): 6-10 [Abstract] ( 96 ) HTMLNew PDF (1000 KB)  ( 60 )
       FEATURE
14 Application of Hot Isostatic Pressing Technology in Tungsten Alloy
CAI Gaocan, FU Jubo, ZHANG Dongxing, HU Biao, XIN Yanxi
DOI: 10.16080/j.issn1671-833x.2021.23/24.014
Tungsten alloy has been widely used in aerospace, military and electronic fields due to its good comprehensive performance. The improvement of comprehensive performance of tungsten alloy will also promote the development of these fields, and the hot isostatic pressing technology plays a key role in improving the performance of tungsten alloy. This paper introduces the application of hot isostatic pressing technology in the field of tungsten alloy, such as strengthening tungsten alloy by hot isostatic pressing, diffusion bonding of tungsten alloy by hot isostatic pressing and numerical simulation of hot isostatic pressing for tungsten alloy. Some problems and development trend of hot isostatic pressing technology in tungsten alloy field are also pointed out.
2021 Vol. 64 (23/24): 14-20 [Abstract] ( 155 ) HTMLNew PDF (6699 KB)  ( 369 )
       COVER STORY
22 Review on Mechanical Behavior of AFP Manufactured Thermoset Composites
XU Qiang
DOI: 10.16080/j.issn1671-833x.2021.23/24.022
The automated fiber placement (AFP) technology is gaining importance in advanced manufacturing of low-cost and high-performance composites. In order to improve the layup quality based on the compression response and tackiness of prepregs, this paper reviews recent development on the deformation and bonding mechanisms of uncured prepregs over a wide range of processing conditions as well as the AFP process induced defects and effects on mechanical behavior of composites at home and abroad. The research efforts in the future are probably going to focus on the development and related scientific problems of the mechanical behavior of AFP-related composites.
2021 Vol. 64 (23/24): 22-31 [Abstract] ( 197 ) HTMLNew PDF (44357 KB)  ( 136 )
       FORUM
34 Weld Defect Identification and Testing of Aircraft Truss Based on Improved Convolutional Neural Network
LIU Xia, JIN Zhongqing
DOI: 10.16080/j.issn1671-833x.2021.23/24.034
The welding quality of aircraft truss is an important guarantee of its working strength, so the effective detection and identification of truss weld defects is the focus of current aviation manufacturing industry. Aiming at the problems of complex calculation and low recognition accuracy existing in traditional target recognition methods, in order to detect the internal defects of weld quickly and effectively, a weld defect recognition method based on improved convolutional neural network (CNN) is proposed. Firstly, the threshold value of weld image is divided to make the feature information easier to extract. Then, an improved adaptive pooling method is designed, and a new model structure of weld image defect recognition is proposed, and the corresponding model parameters and calculation method are formulated. Finally, the recognition model is used to train and test the weld image. The results show that the network model can effectively realize the recognition and classification of weld defects, and the average correct recognition rate is 98.25%, which shows that the proposed method has the advantages of fast recognition speed, high accuracy and good robustness, and provides theoretical reference for the process of weld defect recognition.
2021 Vol. 64 (23/24): 34-38 [Abstract] ( 129 ) HTMLNew PDF (4670 KB)  ( 333 )
39 Current Status and Prospect of Defect Detection of Aircraft Skin
LIU Fang,XIA Guisuo,WEN Zhihui,LI Zhe,XU Qilin
DOI: 10.16080/j.issn1671-833x.2021.23/24.039
In the process of aircraft assembly, uneven gaps and steps will be formed at the seams of the aircraft skin. In addition, dents, cracks, corrosion and other defects will be produced in the skin during the service process. Due to these defects, the strength of the skin will be weakened and the carrying capacity will be reduced, which will eventually affect the aerodynamic performance of aircraft and endanger flight safety. The detection of aircraft skin defects accounted for a large proportion in aircraft maintenance, consequently it is crucial for aircraft safety. This paper introduced seven common defects of aircraft skin, and analyzed the causes, locations and hazards of these defects. On the basis of the location of these defects, the defects were divided into three categories, and the development status of various kinds of detection technology of skin defects was systematically described. The status quo of aircraft skin detection technology was summarized, and the development prospect of skin defect detection was prospected.
2021 Vol. 64 (23/24): 39-50 [Abstract] ( 131 ) HTMLNew PDF (3526 KB)  ( 1243 )
51 Research on Straightness Detection System for Shaft Parts
XU Hongtu,ZHANG Qi,LUO Wei,TIAN Tiantai,LI Wenhao,WANG Jucun
DOI: 10.16080/j.issn1671-833x.2021.23/24.051
By analyzing the advantages and disadvantages of the existing straightness detection methods of shaft parts, a new non-contact straightness measurement method is proposed. In this method, several laser displacement sensors are used to discretize the points on several generatrix of shaft parts. The center coordinate of each section is calculated based on the least square method, and the actual axis of the parts is fitted to judge the straightness error of the parts. Based on the above method, a straightness detection system was designed and developed. Through measurement accuracy research and error analysis, the measurement accuracy of the system was within 0.1mm/m. The experimental results show that the system has the advantages of wide application range, high measurement accuracy, fast measurement speed and high repeat accuracy.
2021 Vol. 64 (23/24): 51-56 [Abstract] ( 111 ) HTMLNew PDF (4492 KB)  ( 224 )
57 Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light
WANG Dezhong, HUANG Xiang, LI Shuanggao, LI Gen
DOI: 10.16080/j.issn1671-833x.2021.23/24.057
As for rivet flatness measuring, the measurement methods using traditional gage measurement or non-contact point cloud scanning have disadvantages such as large limitations, long preparation periods and difficult data processing. In response to the above problems, this paper proposes a method for measuring the flatness of rivets based on binocular multi-line structured light. Firstly, binocular matching and reconstruction are performed on the structured light image collected by the binocular system, and the measured coordinate system is extracted and fitted. Next, discrete point screening proportional coefficient is introduced to optimize the fitting accuracy of local skin plane and then the discrete point screening scale factor is introduced to further optimize the fitting accuracy of the local skin plane, and finally it is substituted into the rivet flatness measurement model to perform calculations to obtain results. Compared with the traditional contact measurement and point cloud scanning, this method saves a lot of time for point cloud data processing and improves the measurement efficiency, and can complete the detection task of narrow cavity such as the aircraft inlet by mechanical arm equipped with a small measurement terminal, which reduces limitations. The experimental results show that this method is applicable to both concave and convex features of the rivet head, and the maximum measurement error of rivet flatness is less than 0.03mm, which meets the requirements of visual measurement of rivet flatness
2021 Vol. 64 (23/24): 57-65 [Abstract] ( 122 ) HTMLNew PDF (7876 KB)  ( 153 )
       APPROACHING SCIENCE
66 Committed to Plastic Processing Precision Forming to Promote Aerospace Complex Component Manufacturing Technology
2021 Vol. 64 (23/24): 66-67 [Abstract] ( 127 ) HTMLNew PDF (606 KB)  ( 51 )
       RESEARCH
68 Research on Design and Processing Characteristics of Disc Cutter in Ultrasonic Vibration Cutting Nomex Honeycomb Composites
SHANG Wenjun, FENG Pingfa, ZHA Huiting, XU Jie, YAN Jianhui, LIU Shijie, FENG Feng
DOI: 10.16080/j.issn1671-833x.2021.23/24.068
The influence of the outside diameter, wedge angle and thickness of disc cutter on the mode and resonant frequency of ultrasonic machining system was studied by finite element simulation technology. The Nomex honeycomb composites experimental platform was built. A comparative experiment between conventional machining and ultrasonic assisted machining was carried out. Taking cutting force and surface quality as evaluation indexes, the improvement effect of ultrasonic vibration on Nomex honeycomb composites under different processing parameters was analyzed. The research results show that the resonant frequency of the system decreases with the increase of disc cutter diameter, increases with the increase of thickness, and decreases with the increase of wedge angle. The influence of the cutter diameter and thickness is more remarkable. The system frequency can be designed by adjusting the outside diameter and thickness of the tool. The size of wedge angle affect the sharpness and intensity of tools, the proper wedge angle should be choosed. The average cutting force in ultrasonic machining is 34.9% and 50.5% lower than that in conventional machining in cutting width direction and feed direction, respectively. The machined surface of composites in ultrasonic assisted machining is smoother, with fewer and shorter burrs.
2021 Vol. 64 (23/24): 68-74 [Abstract] ( 104 ) HTMLNew PDF (9855 KB)  ( 66 )
75 Development of Medium-Voltage Long Focal Distance High-Power Electron Beam Gun
WANG Zhuang, SANG Xinghua, XU Haiying, ZUO Congjin,YANG Bo, PENG Yong
DOI: 10.16080/j.issn1671-833x.2021.23/24.075
In order to obtain a high-quality electron beam source, based on the in-depth analysis of the electron beam gun structure, the key parameters affecting the beam quality were simulated and optimized, and a set of medium-voltage long focal distance high-power electron beam gun was designed and manufactured by using the optimized parameters. On the beam source quality test platform, the maximum working distance and maximum welding depth of the developed electron beam gun were tested. The test results show that the working distance of the developed electron beam gun is 200–600mm, the maximum weld depth for welding TC4–DT titanium alloy reaches 60mm, and the weld aspect ratio can reach 10:1.
2021 Vol. 64 (23/24): 75-79 [Abstract] ( 109 ) HTMLNew PDF (8827 KB)  ( 80 )
80 Heredity and Evolution of Carbide and Oxide in Nickel-Based PM Superalloys and Their Effect on Microstructure-Properties
ZHANG Ying
DOI: 10.16080/j.issn1671-833x.2021.23/24.080
Due to its unique production process, powder metallurgy superalloy often produces defects such as inclusions, previous particle boundary (PPB) in the formed parts. In this paper, the heredity and evolution of carbide and oxide in alloy were traced back according to the manufacturing process of Ni–based powder metallurgy (PM) superalloy, and their effects on microstructure, crack growth rate and fatigue life of formed parts were analyzed. The schemes of restraining and eliminating defects were proposed.
2021 Vol. 64 (23/24): 80-86 [Abstract] ( 190 ) HTMLNew PDF (11167 KB)  ( 102 )
87 Dynamic Cold Expansion Method of Holed Structures Based on Electromagnetic Load
ZHENG Guo, CAO Zengqiang, HUANG Xinping
DOI: 10.16080/j.issn1671-833x.2021.23/24.087

A novel dynamic cold expansion method based on electromagnetic load was developed to enhance the fatigue life of open hole structures. The experiments were conducted to investigate the method, and the corresponding static cold expansion method was also investigated as comparison. The expansion resistance was evaluated. The geometric dimension varieties of holes after cold expansion were measured. Moreover, the fatigue life of specimens after both methods were assessed, and the fatigue failure and fatigue life enhancement mechanisms were discussed. The results show that dynamic cold expansion can obviously reduce expansion resistance compared with static cold expansion and generate more uniform hole diameter distribution along the hole axial direction after cold expansion. In fatigue tests, specimens worked by dynamic cold expansion method exhibited the higher fatigue life than that worked by static cold expansion method, especially under high load level. Furthermore, through fatigue fracture observed dynamic cold expansion specimen will often appear many fatigue source, general along the horizontal direction and the fatigue crack propagation, and the tradition of cold expansion specimen fatigue crack initiation in the entrance of mandrel and extend to the exit, that along the axial dynamic cold expansion method could get more even than the static methods of residual stress, therefore, the fatigue life of the open hole structure is improved.

2021 Vol. 64 (23/24): 87-93 [Abstract] ( 115 ) HTMLNew PDF (32656 KB)  ( 98 )
94 Automatic Drilling and Riveting Process Parameter Optimization Method Based on BP Neural Network and Multi-Objective Particle Swarm Optimization Algorithm
LI Chao, WANG Zhongqi, CHANG Zhengping, MA Jianzhi
DOI: 10.16080/j.issn1671-833x.2021.23/24.094
Interference connection is widely used in automatic drilling and riveting of aircraft panel. The coordinated control of the degree of uniformity of interference and panel deformation is an urgent problem to be solved. In this paper, an optimization method based on BP neural network (BPNN) is proposed. Taking the riveting force, riveting process time, riveting retention time and clamping force as variables, and taking the simulation data as samples, the prediction model of interference uniformity and wall deformation was established by using BP neural network. Multi-objective particle swarm optimization (MOPSO) algorithm was used for multi-objective optimization. The simulation and experimental results show that the optimized parameters can significantly improve the uniformity of interference and effectively reduce the deformation degree of plate.
2021 Vol. 64 (23/24): 94-102 [Abstract] ( 119 ) HTMLNew PDF (5445 KB)  ( 405 )
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