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2009 Vol. 52, No. 22
Published: 2009-11-15

 
26 Application Analysis of Precise Vibrating Electrochemical Machining in High-Temperature Alloy Disk
DOI: 10.16080/j.issn1671-833x.2009.22.001
2009 Vol. 52 (22): 26-29 [Abstract] ( 87 ) HTMLNew PDF (549 KB)  ( 573 )
32 Summary of Manufacturing Technology of Large Composite Primary-Load-Carrying Structure
DOI: 10.16080/j.issn1671-833x.2009.22.006
2009 Vol. 52 (22): 32-35 [Abstract] ( 106 ) HTMLNew PDF (2526 KB)  ( 481 )
40 Application of Composite Technology in Modern Aircraft Structure
DOI: 10.16080/j.issn1671-833x.2009.22.010
2009 Vol. 52 (22): 40-42 [Abstract] ( 85 ) HTMLNew PDF (420 KB)  ( 623 )
43 Development of the Filament Winding/Tape Layer/Fiber Placement Machine
DOI: 10.16080/j.issn1671-833x.2009.22.009
2009 Vol. 52 (22): 43-46 [Abstract] ( 90 ) HTMLNew PDF (813 KB)  ( 447 )
47 Low-Cost Program of Advanced Composite Material Autoclave Co-Cured Technology
DOI: 10.16080/j.issn1671-833x.2009.22.008
2009 Vol. 52 (22): 47-49 [Abstract] ( 82 ) HTMLNew PDF (495 KB)  ( 155 )
50 Application and Proposal Sample of Composite Automatic Tape-Laying Technology
DOI: 10.16080/j.issn1671-833x.2009.22.007
2009 Vol. 52 (22): 50-54 [Abstract] ( 81 ) HTMLNew PDF (969 KB)  ( 451 )
62 Challenge in Structural Health Monitoring of Large Aircraft Development
DOI: 10.16080/j.issn1671-833x.2009.22.017
2009 Vol. 52 (22): 62-67 [Abstract] ( 109 ) HTMLNew PDF (655 KB)  ( 429 )
68 Research on the Properties of Thickness Aluminum Alloy for Aircraft by FSW
DOI: 10.16080/j.issn1671-833x.2009.22.016
2009 Vol. 52 (22): 68-71 [Abstract] ( 87 ) HTMLNew PDF (621 KB)  ( 176 )
72 Mechanical Property Comparison Between FSW and Rivet Joints of Aircraft Aluminum
DOI: 10.16080/j.issn1671-833x.2009.22.015
2009 Vol. 52 (22): 72-75 [Abstract] ( 108 ) HTMLNew PDF (1195 KB)  ( 196 )
78 Research on TC17 Titanium Alloy Surface Roughness and Parameters Sensitivity in High Speed Milling Process
DOI: 10.16080/j.issn1671-833x.2009.22.005

The single factor experiment was processed for the study on the effect of the cutting parameters on the TC17 titanium alloy surface roughness using the carbide tool on the condition of the high speed. The purpose is to provide the experimental references for the high speed cutting optimizing for machining of the titanium alloy blade or blisk. The sensitivity analysis for the cutting parameters show that the surface roughness is most sensitive to the feed per tooth, and less sensitive to the cutting speed and cutting depth.

2009 Vol. 52 (22): 78-82 [Abstract] ( 77 ) HTMLNew PDF (976 KB)  ( 184 )
83 Development of MoN-Based Hard Coating
DOI: 10.16080/j.issn1671-833x.2009.22.004

The MoCN, MoSiN, MoAlN, and MoWN coatings are synthesized on the substrates of stainless steel or silicon (100) with reactive magnetron sputtering method by using Mo, C, Si, Al and W composite target. The microstructure of these fi lms were analyzed by XRD XPS SEMand HRTEM, and the hardness and oxidation
resistance of these fi lms are characterized by nano-indentation and TGA. The results illustrate that the hardness and oxidation resistance of the MoN-based fi lms can be greatly enhanced through the nano-composite method and solid solution strengthening. Therefore, MoN-based hard coatings possess good comprehensive performance and would be applied widely in the aviation industry.

2009 Vol. 52 (22): 83-85,91 [Abstract] ( 75 ) HTMLNew PDF (844 KB)  ( 275 )
86 Study on Aircraft Composites Workshop Production Plan
DOI: 10.16080/j.issn1671-833x.2009.22.014

In order to achieve product plan for the composite digital production line and make it more operational, Based on the difference of material used to main process of production line, the composite production plan is departed in two stages: Partition plan and Machine plan. By analyzing project of aircraft composites workshop production plan, the methods are given to make partition plan and machine plan for composite components, and this system is taken into practices for composite workshop in digital production line. Practice shows that this type of approach can be effective during making practical production planning, and improve the  ystem’s development, maintenance, and good scalability.

2009 Vol. 52 (22): 86-91 [Abstract] ( 66 ) HTMLNew PDF (1344 KB)  ( 131 )
92 Design and Implementation of Production Process Monitoring System Based on Workflow
DOI: 10.16080/j.issn1671-833x.2009.22.023

According to the problems such as incomplete information collection, feedback delay, lowlevel share of information during production process monitoring of manufacturing industry workshop, the workflow technology is introduced into process modeling and business drive, which can realize the automatic circulation of business process, the automatic collection and feedback of the information. The convenience of terminal application is enhanced by landing touch screen with reading card, and the monitoring results are displayed by using methods such as Gantt chart and so on. The production process monitoring system is developed based on the Primeton EOS middleware platform, which is applied in practical production.

2009 Vol. 52 (22): 92-97 [Abstract] ( 70 ) HTMLNew PDF (1197 KB)  ( 137 )
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