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2017 Vol. 60, No. 10
Published: 2017-05-15
FEATURE
FORUM
NEW VIEWPOINT
RESEARCH
C0NTENTS
COVER STORY
C0NTENTS
6
C0NTENTS
2017 Vol. 60 (10): 6-10 [
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FEATURE
16
Aircraft Structures Technology Based on Power Beam Additive Manufacturing
WANG Xiangming, CUI Can, SU Yadong, WU Bin
DOI: 10.16080/j.issn1671-833x.2017.10.016
The development direction of modern aircraft structures technology are lightweight, high efficiency, long
life, multi-function, low cost, and rapid response manufacturing. Limited by traditional manufacturing technology, some innovative
structures couldn’t be made out. The additive manufacturing, using laser and electron power beam, offers an opportunity
for the engineering application of innovative structures. Based on additive manufacturing technology and in the view of
the requirements of modern aircraft structure, we developed large-scale integration, multiple gradients, and functional structure
integration, created innovative structures, made a research of the design and evaluation, and presented engineering verification
mode based on the technical maturity.
2017 Vol. 60 (10): 16-21 [
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466
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COVER STORY
26
Combination of Topology Optimization and Additive Manufacturing: an Integration Method of Structural Design and Manufacturing
LIU Shutian, LI Quhao, CHEN Wenjiong, ZHANG Yongcun
DOI: 10.16080/j.issn1671-833x.2017.10.026
Additive manufacturing (AM), acclaimed as the most representative manufacturing technology in the “third
industrial revolution”, is a manufacturing process where material is added through deposition or melting in a layer-by-layer
fashion. This special manufacturing process makes the fabrication of the structures with complex shapes and geometrical
features possible. AM has been the subject of several studies, the breakthrough in manufacturing is yet to be followed by a
breakthrough in designing process. Topology optimization (TO) is a powerful free-form design tool that couples finite element
analysis with mathematical programming to systematically design for engineering problems. It does not require a preestablished
design and is capable of giving some new, sometime unanticipated, design ideas to designers. In this paper, we
seek to leverage the full potential of this burgeoning manufacturing technology by reviewing the new design algorithms
based on topology optimization.
2017 Vol. 60 (10): 26-31 [
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855
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FORUM
34
Study on 3D Printing Process and Performance of Resin Matrix Composite Lightweight Structure
TIAN Xiaoyong, HOU Zhanghao, ZHANG Junkang, LI Dichen
DOI: 10.16080/j.issn1671-833x.2017.10.034
Resin matrix composite lightweight structure has the advantages of low density and high performance,
for use in lightweight applications such as aerospace, high-speed trains, ships and others. However, the disadvantages of
conventional forming processes, such as complex process, long process period and high cost, have limited the wide applications
of resin matrix composite lightweight structure. 3D printing is a new forming process of parts, and it is possible
to realize integrated manufacturing of high performance composite lightweight structure. This paper reviews the research
status of resin matrix composite lightweight structure 3D printing, and meanwhile presents a new integrated manufacturing
process of high performance resin matrix composite lightweight structure based on continuous fiber reinforced thermoplastic
composites 3D printing.
2017 Vol. 60 (10): 34-39 [
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385
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Additive Manufacturing of Ceramic Components and Its Potential Application in Aerospace Field
WU Jiamin1,2, CHEN Jingyan1,2, CHEN Annan1,2, CHENG Lijin1,2, XIAO Huan1,2, LIU Rongzhen1,2,SHI Yusheng1, LI Chenhui1, ZHU Xiaogang3, WANG Lianfeng3
DOI: 10.16080/j.issn1671-833x.2017.10.040
Ceramic components are expected to be widely used in aerospace field due to their excellent properties,
including high strength, low density, high-temperature capability and corrosion resistance, etc. However, some defects
existing in traditional manufacturing methods for preparing ceramic components, such as long preparation period, high
cost, the dependence on molds and difficulty in manufacturing complex structures, have greatly limited the application of
ceramic components in aerospace field. Additive manufacturing (AM) technology, which is based on the forming principle
of “discrete-accumulation”, is capable of direct fabricating components from three-dimensional data. Compared with the
traditional manufacturing method, AM technology has the advantages of high design freedom, short product development
cycle, low manufacturing cost and so on, which are in favor of quick preparation of complex structural ceramic components
without molds. This review systematically introduces the research status and limitations of the commonly used AM methods,
such as three-dimensional printing (3DP), selective laser sintering (SLS), selective laser melting (SLM), fused deposition
modeling (FDM), laminated objected manufacturing (LOM) and stereo lithography apparatus (SLA), for fabricating
ceramic components on the basis of a brief description of their forming principle and characteristics. Finally, the potential
application of AM technology for fabricating ceramic components in aerospace field is analyzed and forecasted.
2017 Vol. 60 (10): 40-49 [
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501
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Research Progress of Multi-Scale Multi-Physics Modeling for Selective Melting Process
YAN Wentao, QIAN Ya, LIN Feng
DOI: 10.16080/j.issn1671-833x.2017.10.050
Selective melting is a powder bed based metal additive manufacturing processes, and capable of manufac-turing components with complex shapes and manipulating the material micro-structures and properties locally and globally. Computational modeling of the manufacturing processes provides valuable instructions to advance the technologies. This paper introduces the research progress in this regard. Firstly, the principle and characteristics of laser/electron beam selec-tive melting are introduced. The state-of-the-art of numerical modeling of the manufacturing processes is summarized. The multi-scale multi-physics models for electron beam selective melting will be presented in detail, which consist of (1) a mi-cro-scale electron-material interaction model; (2) meso-scale models of powder particles from being spread to being heated, melted and solidified; (3) a macro-scale model of part fabrication process.
2017 Vol. 60 (10): 50-58 [
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467
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Study on the Influence of Polymer Additive Manufacturing Technology on Development of Aviation Manufacturing Industry of China
CHEN Bosheng, LAI Duan, YANG Ge, CHEN Li
DOI: 10.16080/j.issn1671-833x.2017.10.059
Only 2 cases that the aircraft parts made by metal additive manufacturing have been authenticated by profes-sional authority worldwide. On the contrary, additive manufacturing parts made by polymer additive manufacturing have been used about 20 years long formally by Boeing Airplane, the cumulative total of more than 100000 units. Deeply integrating the additive manufacturing technology and aviation industry, making overall planning and do the top-level design well, attaching equal importance to both polymer and metal additive manufacturing technology to make aircraft parts directly, these are the key point to promote healthy and sustainable development of additive manufacturing industry .
2017 Vol. 60 (10): 59-63 [
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373
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NEW VIEWPOINT
64
An Adaptive Control Method of Floating Fixture for NC Machining of Complex Structural Parts
WANG Binli, LI Yingguang, HAO Xiaozhong, LIU Changqing
DOI: 10.16080/j.issn1671-833x.2017.10.064
In order to reduce the deformation of complex structural parts caused by NC machining, and to meet the requirement of adaptive adjustment of fixtures, an adaptive control method is proposed based on the machining principle of floating fixture. The floating fixture units communicate with each other by CAN (Controller Area Network) bus. Part condi-tion monitoring method based on multiple sensors is developed, machine tool condition is monitored based on OPC tech-nology, the floating fixtures and CNC machine tool interact based on PLC. The floating clamping adaptive control system is developed. The adaptive control system for floating fixtures has been verified in the aviation manufacturing enterprise during the machining of aircraft structural parts, the control system can realize the adaptive adjustment of floating clamping and meet the industrial application requirement.
2017 Vol. 60 (10): 64-69 [
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241
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RESEARCH
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Research on Detection of Skin Seam Based on 3D Laser Scanning
YAN Cheng1, HUANG Xiang1, LI Shuanggao1, LI Dong2
DOI: 10.16080/j.issn1671-833x.2017.10.070
Concerning the difficulties such as large errors and low efficiency in traditional detection method of the skin seam and the defects based on 2D laser scanning, a method of the skin seam based on 3D laser scanning is proposed and corresponding software is developed. Methods and steps of de-noising, critical points recognition and extraction for the skin seam testing based on 3D point cloud are proposed. Based on the influence of gap and flush on the aerodynamic shape, the actual geometry structures are analyzed. Compared with theoretical structures, the mathematical model of gap and flush is established. The calculate accuracy is verified through experiments of simulation work piece. Field experiments show that the detection method is feasible and compared with two-dimensional laser detection, the accuracy and repeatability are better. The gap measurement accuracy reaches 0.04mm as well as the flush measurement accuracy reaches 0.02mm, which meet the needs of the skin seam detection and provid the numerical basis for the analysis of the influence of gap and flush on the assembly quality.
2017 Vol. 60 (10): 70-74 [
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309
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75
Study on the Process of PECM Blade Surface
HUANG Mingtao, ZHANG Mingqi, CHENG Xiaoyuan, FU Junying, LI Hongying, ZHANG Zhijin
DOI: 10.16080/j.issn1671-833x.2017.10.075
Blades can be shaped by precise electrochemical machining with short production cycle and low production
costs. A series of experiments using this machining method is performed on GH4169G alloy blades. The results indicated
that the characteristics of flow field between electrode and cathode are significantly improved. Electrode passivation
is reduced and high surface machining quality is obtained. The optimum parameters are voltage of 15V, electrode vibrating
frequency of 25Hz, opening angle of 150°-195°, pulse frequency of 3000Hz. Blades produced with profile tolerance of
-0.012 - +0.013mm and roughness of Ra 0.51μm meet the machining requirements.
2017 Vol. 60 (10): 75-78 [
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283
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79
Microstructure and Mechanical Properties of Welded Joint of TC17 Titanium Alloy
JIN Junlong, WAN Xiaohui, GUO Delun
DOI: 10.16080/j.issn1671-833x.2017.10.079
TC17 titanium alloy sheet is welded with tungsten inert gas arc welding (TIG) and electron beam welding
(EBW), and tensile tests are carried out. Based on tensile test result and fracture morphology, relationship between mechanical
properties with microstructure of welded joint is analyzed. The research results show, when TC17 alloy is heated
by TIG arc, grains in the weld bead and heat affected zone (HAZ) are badly coarsening. The heat affected zone of EBW is
relatively narrow, and there is no coarse grain zone. Tensile strength of two welding methods are both strong as the base
metal and the relative elongation is deceased, mainly because of the microstructure change of the heat affected zone and the
weld. Compared with EBW, the micro structure of TIG joint is more coarse.
2017 Vol. 60 (10): 79-81 [
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295
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Surface Residual Stress of Gamma Titanium Aluminide in Milling Process
XU Weifeng, YAN Ran, LIU Weiwei
DOI: 10.16080/j.issn1671-833x.2017.10.082
In order to explore the influence law of milling parameters on residual stress induced in the process of milling
ideal high-temperature structural material of gamma-TiAl alloy, the extreme difference analysis method is used based
on orthogonal experiment data processing. The relationships between different levels of process factors and residual stress
are established, as well as the thermal-mechanical mechanisms are analyzed. At the same time, a sensitivity mathematical
model of machining factors to residual stress is obtained, which determines the parameters optimization range to get larger
residual compressive stress. Research shows that during the range of experimental parameters, the residual stresses along
the direction of stepper and feed are all compressive caused by cold plasticity deformation mainly. With regard to cutting
parameter sensitivity analysis, it has been found that the residual stress is most sensitive to the milling speed, as one of design
variables, while nearly the same degree to feed per tooth, cutting depth and cutting width, which provides a theoretical
basis to control surface residual stress in the milling process of titanium aluminium alloy.
2017 Vol. 60 (10): 82-85 [
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322
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86
Study on Tensile Property and Microstructure of Laser Cladding Repaired of 15-5PH Stainless Steel
LIU Haitao1, SI Chaoyang1, HUO Dengping1, ZHANG Qingrong1,YANG Donghui2
DOI: 10.16080/j.issn1671-833x.2017.10.086
The affect of cladding reparation rate(25%, 50%, 75% and 100%) on mechanical property of 15-5PH
precipitation hardening stainless steel is studied. Cladding repairing samples are also used for testing fractograph, metallographic
structure, internal flaws and microstructure hardness. The results show that the tensile strength under different cladding
reparation rate is higher than the matrix; however its ductility decreases with the increase of cladding reparation rate.
Among all the studied samples, the tensile strength and mechanical property reach the peak under 25% cladding reparation
rate sample. The metallographic structures of cladding reparation area, heat-affected zone and undamaged matrix is compact.
Among them, the structure of heat-affected zone shows apparent direction, with refined grains and flawless interface
and surface. The microstructure hardness rises from cladding reparation to matrix, with peak value in heat-affected zone.
The adhesive force of cladding area is weaker than that of inner matrix. The results show that fractograph of samples all
resemble V shape.
2017 Vol. 60 (10): 86-90 [
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295
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Friction Stir Welding Techniques for Lap Structure of Aluminium Alloy
WANG Guoqing1, ZHAO Yanhua2, DU Yanfeng2, YU Haijing2, ZHANG Lina2
DOI: 10.16080/j.issn1671-833x.2017.10.091
An introduction of working principle and features is given regarding to friction stir welded aluminium lap
joints. By the analysis of present research, development and application statuses in China and abroad, the trend is pointed
out that friction stir welding is a promising method in joining lap structure and its constant development emphasis has been
expected.
2017 Vol. 60 (10): 91-98 [
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Finite Element Simulation of 34CrNiMo6 Steel After Dual Shot Peening
DOI: 10.16080/j.issn1671-833x.2017.10.099
To study the effect of dual peening, the periodic 3D finite element model of 34CrNiMo6 shot peening with
a number of random projectiles is established using finite element analysis software ABAQUS. At first, the proposed periodic
model is verified by experiment. Then the strengthening effect of shot peening and the influence of Almen intensity on
residual stress field are analyzed with the proposed periodic model. The results show that the residual stress on surface layer
of 34CrNiMo6 caused by dual shot peening is larger than that caused by single shot peening, and the residual stress distribution
on surface is more uniform, but the depth of maximum residual stress is the same. Dual shot peening can attain less
surface roughness.
2017 Vol. 60 (10): 99-103 [
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Equipment Scheduling of Aircraft Assembly System Based on Extended Petri Net
CHAI Meng, YAN Jinfeng
DOI: 10.16080/j.issn1671-833x.2017.10.104
Aiming at the complexity of the facilities scheduling in the aircraft assembly process, a new method to
build equipment scheduling model based on extended Petri net is proposed. The definition process and modeling methods
of this model are discussed by considering the characteristics of aircraft assembly process. The model is based on the objectoriented
Petri net to express the aircraft assembly process, which is related to the auxiliary equipment by timed Petri net,
and it is optimized by the hybrid algorithm with the time and equipment utilization. The fuselage assembly process of a certain
airliner is taken as an example to build the model and dispatch, and the experimental results show that the method has
great guiding significance to the actual assembly equipment scheduling.
2017 Vol. 60 (10): 104-108 [
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