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2010 Vol. 53, No. 23
Published: 2010-12-01
FEATURE
FIGURE
NEW VIEWPOINT
RESEARCH
COVER STORY
 
       FEATURE
26 Finish Machining of Joints Between Aircraft Major Parts
DOI: 10.16080/j.issn1671-833x.2010.23.001
2010 Vol. 53 (23): 26-29 [Abstract] ( 51 ) HTMLNew PDF (1378 KB)  ( 323 )
       COVER STORY
32 Digital Assembly Technology System of Aircraft
DOI: 10.16080/j.issn1671-833x.2010.23.002
2010 Vol. 53 (23): 32-37 [Abstract] ( 51 ) HTMLNew PDF (2453 KB)  ( 861 )
       NEW VIEWPOINT
38 Development, Equipment Research and Application of Electromagnetic Riveting
DOI: 10.16080/j.issn1671-833x.2010.23.003
2010 Vol. 53 (23): 38-41 [Abstract] ( 52 ) HTMLNew PDF (1283 KB)  ( 487 )
       RESEARCH
46 Digital Measurement System for Aircraft Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.004
The characteristics and advantages of digital measurement system for aircraft assembly is expounded. The functions and effects of digital measurement equipment in common use for aircraft assembly is introduced. The framework of digital measurement software environment is discussed in details. Station arrangement planning and simulation, automatic searching and tracking algorithm of measurement points, measurement error compensation methods for aircraft assembly and quality analysis method of aircraft part assembly are researched.
2010 Vol. 53 (23): 46-48/59 [Abstract] ( 53 ) HTMLNew PDF (1202 KB)  ( 453 )
49 Measurement Planning Technology Based on Uncertainty for Flexible Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.005
Digital measurement technology has now become one of the key technologies of aircraft fl exible assembly. Uncertainty caused by digital measurement is one of the hotspot. Based on the next-generation geometrical product specifi cation, the overall technical framework of the measurement system is constructed,which covers uncertainty assessment, scheme planning and integration of measuring and data-processing. Some key technologies in the field are discussed.
2010 Vol. 53 (23): 49-51/55 [Abstract] ( 56 ) HTMLNew PDF (1346 KB)  ( 428 )
52 Application of Digital Measurement System in Major Part Butt
DOI: 10.16080/j.issn1671-833x.2010.23.006

The function and the composition of the measurement system are analyzed. Aiming at one major-part butt item, the aided assembly process, the measurement data treatment and the measurement environmental layout are expatiated. Through the study, our technical base is expanded for the engineering application of the digital measurement technology in the aircraft assembly. 
2010 Vol. 53 (23): 52-55 [Abstract] ( 58 ) HTMLNew PDF (1282 KB)  ( 252 )
56 Research on Key Technology of MBD-Based Aviation First Article Inspection
DOI: 10.16080/j.issn1671-833x.2010.23.007
The MBD-based aviation first article inspection method is put forward, in order to achieve three-dimensional digital inspection. Based on the analysis of MBD technical application system, the aviation first article inspection standard is studied, key technologies of first article inspection in the MBD environment are pointed out, the difficulties and key points in the informatization and digitization of fi rst article inspection process are investigated, technique supports and guides for the implementation of MBD-based aviation fi rst article inspection system are provided.
2010 Vol. 53 (23): 56-59 [Abstract] ( 52 ) HTMLNew PDF (1486 KB)  ( 379 )
60 Normal Measurement and Adjustment for Skin Drilling
DOI: 10.16080/j.issn1671-833x.2010.23.008
A method of the normal adjustment for skin drilling is presented. The theory and application of the normal measurement and adjustment are discussed, and an example with some questions is described.
2010 Vol. 53 (23): 60-62/66 [Abstract] ( 43 ) HTMLNew PDF (1546 KB)  ( 246 )
63 Application of Digital Measurement and Air-Cushion Technology in Aircraft Major Part Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.009
Function,characteristic,system composition of digital measurement and air-cushion technology are introduced. Application in aircraft assembly both at home and abroad is also presented.
2010 Vol. 53 (23): 63-66 [Abstract] ( 39 ) HTMLNew PDF (1448 KB)  ( 575 )
67 Deformation Analysis and Application of Automatic Riveting for Wing Panel
DOI: 10.16080/j.issn1671-833x.2010.23.010
Over the last years, automatic riveting systems are widely used in the aircraft assembly of the foreign aerospace industries. Chinese aerospace companies have purchased automatic riveting equipment, but there are several problems need to be solved, such as the parameter optimization and controlling of the small variation in the process of automatic riveting. Based on the process flow of the automatic riveting, the analysismethods of stress and strain in rivet and sheet metals are summarized respectively. Key problems for interference-fitriveting of composite material are also represented.
2010 Vol. 53 (23): 67-72 [Abstract] ( 52 ) HTMLNew PDF (1578 KB)  ( 512 )
73 Digital and Flexible Assembly and Intelligent Drilling System of Panel
DOI: 10.16080/j.issn1671-833x.2010.23.011
Aircraft panel is applied widely.A set of fl exible locater and intelligent drilling jig are adopted to meet distinct dimensions, distinct curvature of skin panel. This method economizes jig number, reduces produce prepare period over 50%, and raises enterprise answer ability quickly for new product.
2010 Vol. 53 (23): 73-75/78 [Abstract] ( 47 ) HTMLNew PDF (1269 KB)  ( 543 )
76 Joining Technology of Interference Blind Fastener System for Composites Structure
DOI: 10.16080/j.issn1671-833x.2010.23.012
The structure and installation sequence of the interference blind fastener system, and the analysis of joint property are discussed. The structural fatigue life and pin load distribution are improved, and the lifetime of overall structures are progressed by using the interference blind fastener system.
2010 Vol. 53 (23): 76-78 [Abstract] ( 43 ) HTMLNew PDF (1239 KB)  ( 236 )
79 Manufacturing Technology of British System Light-Weight Titanium Alloy Bolt
DOI: 10.16080/j.issn1671-833x.2010.23.013
The features of light-weight bolt are introduced,and key manufacturing technology is depicted ,especially the whole profile grinding for workpiece,shortened runout thread forming, aluminum corrosion inhibiting coatings,etc. Light-weight bolt is realized manufacturing in China.
2010 Vol. 53 (23): 79-81 [Abstract] ( 40 ) HTMLNew PDF (1371 KB)  ( 428 )
82 Domestic Manufacturing of British System Light-Weight Titanium Alloy Bolt
DOI: 10.16080/j.issn1671-833x.2010.23.014
The structure features of light-weight Ti-alloy bolt is introduced, and the manufacturing process and the technical diffi culties are discussed in details. Detailed qualifi cation tests are carried out .
2010 Vol. 53 (23): 82-84 [Abstract] ( 60 ) HTMLNew PDF (1241 KB)  ( 231 )
85 Application of Automation Studio Software in Helicopter Rotor Folding System
DOI: 10.16080/j.issn1671-833x.2010.23.022
The character and function about Automation Studio software are introduced, the simulation system about rotor blade folding system is built by using above software based on the analysis of folding system of a helicopter (including hydraulic and electrical complex system). The work principle and running situation of this system are visually and dynamically presented, and the demand for actual work is satisfi ed, the availability tool for failure analysis and technology training are offered.
2010 Vol. 53 (23): 85-88/92 [Abstract] ( 55 ) HTMLNew PDF (1712 KB)  ( 248 )
89 Research and Application of Digital Virtual Manufacturing Technology
DOI: 10.16080/j.issn1671-833x.2010.23.015
Along with the computer software and hardware technology development, the digitization application is more and more extensive, its fi eld involving medical, military, manufacturing industries. the concept of digital virtual manufacturing technology and the domestic and foreign development present situation are discussed, the purpose and significance of this technology are analyzed, and the digital virtual manufacturing technology in our company's research and application is introduced.
2010 Vol. 53 (23): 89-92 [Abstract] ( 35 ) HTMLNew PDF (1089 KB)  ( 287 )
93 Integrated Control Technology of Automatic Butt for Aircraft Major Part
DOI: 10.16080/j.issn1671-833x.2010.23.024
Integrated control technology is the pivotal technology for aircraft major parts butt. The Integrated control method includes digital measuring technology, synchronic movement control technology, data management technology for assembly information and the movement simulation technology. these methodologies are focused on. One aircraft wing butt system which is recently designed is introduced, and this system’s confi guration, main function, the process sequence are illustrated.
2010 Vol. 53 (23): 93-96/120 [Abstract] ( 38 ) HTMLNew PDF (1574 KB)  ( 411 )
97 Digital Factory Technology of Spacecraft Final Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.016
Domestic and foreign present states of digital factory technolgy(DFT) are introduced briefl y,and the technical base DFT depends are described, also implementary points of DFT in spacecraft final assembly are analyzed. Positive signifi cances on improving batch production capacity and industrialization capacity by DFT are indicated.
2010 Vol. 53 (23): 97-100 [Abstract] ( 54 ) HTMLNew PDF (1267 KB)  ( 455 )
101 Importance of Supply Chain Control of Manufacturing Process in Digital Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.017
Aircraft assembly is a huge system of multi-department collaboration and multi-discipline integrated application, and would be influenced by various factors in quality and efficiency. The successful application of monomial technology must rely on the whole assembly process of effective supply chain control system and the environment. This environment from the design process to material distribution runs throughout the whole process of aircraft assembly, and through digital measuring coupling detection model and real object, quality closed-loop control is completed in assembly site. The environment is a multi-level efficient integration of planning, technology and logistics, affects the overall efficiency, and plays a very important role in assembly process.
2010 Vol. 53 (23): 101-103 [Abstract] ( 46 ) HTMLNew PDF (1130 KB)  ( 277 )
104 Application of Industrial Robot in Aircraft Digital Assembly
DOI: 10.16080/j.issn1671-833x.2010.23.025
Through the analysis of the industrial robot development and background, the technology importance in the aircraft assembly is shown, and its eight main application areas are expatiated separately. The key technologies of its application development are pointed out. At last, the developing direction and trend of the intelligent industrial robot are prospected in the aeronautical manufacture and assembly field.
2010 Vol. 53 (23): 104-108 [Abstract] ( 52 ) HTMLNew PDF (1575 KB)  ( 780 )
109 Design of Digital Servo Controller Based on CAN Bus
DOI: 10.16080/j.issn1671-833x.2010.23.026

A digital servo controller based on CAN bus is introduced.Three pivotal techniques of the servo, including the hardware design, the motor control arithmetic and the software design are mainly studied, the hardware design is described particularly. The results show the correctness and effectiveness of the digital servo controller.
2010 Vol. 53 (23): 109-113 [Abstract] ( 43 ) HTMLNew PDF (1577 KB)  ( 150 )
114 Application of SIMOTION in Multi-Axis Synchronization Control of Digital Butt System
DOI: 10.16080/j.issn1671-833x.2010.23.018
Aimed at the digital butt system, virtual axis method based on motion control system SIMOTION is presented to implement multi-axis synchronization control, and software interface is developed to transfer data and command reliably. Experiment results of digital butt system validate multi-axis synchronization control method proposed.
2010 Vol. 53 (23): 114-116 [Abstract] ( 41 ) HTMLNew PDF (1317 KB)  ( 265 )
117 Technical Research of NC Positioner for Major Part Butt
DOI: 10.16080/j.issn1671-833x.2010.23.019
The technology of NC positioner of aircraft digital assembly technology is researched. The working principle of NC positioner is introduced, synthetically considering the technics of manufacture,assembly,maintenance and support. The project and frame is designed, and the technical diffi culties are summarized and resolved in the process of design,manufacture and assembly.
2010 Vol. 53 (23): 117-120 [Abstract] ( 56 ) HTMLNew PDF (1548 KB)  ( 482 )
  Notices
· 'Aeronautical Manufacturing technology ' is included in EI database
· China Science Citation Database (CSCD)
· Chinese S&T Journal Citation Reports (CJCR)
· World Journal Clout Index (WJCI) Report of Scientific and Technological Periodicals
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· Aeronautical Manufacturing Technology ranked No. 3 in Chinese S&T Journal Citation Reports (CJCR)
· High Quality Sci-tech Journal Classification Catalogue in Aerospace Field （2023）
· A Guide to the Core Journals of China (hosted by Peking University Library)
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