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2009 Vol. 52, No. 19
Published: 2009-10-01

 
26 Welding Technology of Aircraft Manufacturing
DOI: 10.16080/j.issn1671-833x.2009.19.010
2009 Vol. 52 (19): 26-29 [Abstract] ( 106 ) HTMLNew PDF (589 KB)  ( 327 )
32 Review of Intelligent Aeroengine
DOI: 10.16080/j.issn1671-833x.2009.19.009
2009 Vol. 52 (19): 32-37 [Abstract] ( 92 ) HTMLNew PDF (1328 KB)  ( 408 )
42 High-Performance NC Machining of Ti-Alloy Aircraft Structure Part
DOI: 10.16080/j.issn1671-833x.2009.19.015
2009 Vol. 52 (19): 42-45 [Abstract] ( 95 ) HTMLNew PDF (860 KB)  ( 217 )
46 Application of Parallel Link Machine Tool in Aircraft Structure Part Machining
DOI: 10.16080/j.issn1671-833x.2009.19.014
2009 Vol. 52 (19): 46-48 [Abstract] ( 78 ) HTMLNew PDF (613 KB)  ( 144 )
49 New Generation of High-Speed Grinding Technology for Aeroengine Rotor Tip
DOI: 10.16080/j.issn1671-833x.2009.19.013
2009 Vol. 52 (19): 49-51 [Abstract] ( 105 ) HTMLNew PDF (560 KB)  ( 107 )
52 Application of NC High-Speed Machining in Aviation Product Manufacturing#br# DOI:10.16080/j.issn1671-833x.2009.19.012
DOI: 10.16080/j.issn1671-833x.2009.19.012
2009 Vol. 52 (19): 52-55 [Abstract] ( 92 ) HTMLNew PDF (677 KB)  ( 159 )
60 Review of Ceramic Core for Superalloy Hollow Blade
DOI: 10.16080/j.issn1671-833x.2009.19.011
2009 Vol. 52 (19): 60-64 [Abstract] ( 98 ) HTMLNew PDF (608 KB)  ( 508 )
66 Influence of Heat Treatment on Tensile Properties of Friction Stir Welded 6061-T6 Joint
DOI: 10.16080/j.issn1671-833x.2009.19.001
2009 Vol. 52 (19): 66-68 [Abstract] ( 88 ) HTMLNew PDF (845 KB)  ( 156 )
69 Friction Stir Welding Joint Corrosion of 2024 Aluminum Alloy Under Different Conditions
DOI: 10.16080/j.issn1671-833x.2009.19.005
2009 Vol. 52 (19): 69-71 [Abstract] ( 79 ) HTMLNew PDF (965 KB)  ( 122 )
72 Meshing Method of Fiber Placement Track for S-Shaped Inlet
DOI: 10.16080/j.issn1671-833x.2009.19.019

The meshing method is applied to the placement track planning of S-shaped inlet model. Namely, CAD software model of inlet is meshed by using UG meshing generator and the meshing data is created. Based on these data, the topology relation between meshing element and nodes is set up. The normal vector of placement track and track points are calculated in each meshing element. The simulation test shows that this method has some performances such as high speed program performing, the smooth curve of placement track, no mutation of track and so on. So this method has certain application value in engineering. It is put forward to develop a meshing tool for the track generation by using the secondary development function of UG.

2009 Vol. 52 (19): 72-78 [Abstract] ( 90 ) HTMLNew PDF (1774 KB)  ( 245 )
79 Research of Dynamic Alliance Structure Model and Operating Mode Based#br# on Small and Medium Enterprise
DOI: 0.16080/j.issn1671-833x.2009.19.027
Based on the study of establishment process, form and structure layer of the dynamic allinace, a general structure model of the small and medium enterprise
dynamic alliance based on the net mode is proposed. And the organization layer, function, operating mode are studied.
2009 Vol. 52 (19): 79-84 [Abstract] ( 56 ) HTMLNew PDF (965 KB)  ( 142 )
85 A New Copper Alloy Defect Ingot and Preventive Measure
DOI: 10.16080/j.issn1671-833x.2009.19.004
The causes and the factors affecting the formation of the structure fl aw in copper alloy are disscussed through analyzing the characteristic, solidification
process of alloy. The countermeasures for preventing the fl aw are put forward.
2009 Vol. 52 (19): 85-86 [Abstract] ( 85 ) HTMLNew PDF (758 KB)  ( 269 )
87 Generation and Control of Residual Stress for Thin-Wall Part Turning
DOI: 10.16080/j.issn1671-833x.2009.19.003
Residual stresses are generated in the machined layer for thin-wall parts cutting. The residual stresses impacts the working performance and fatigue strength of parts. The reasons of residual stress generation in the thin-wall parts cutting process are expounded. Affecting factors of residual stresses are also analyzed. At the same time, the domestic test methods of residual stress that  are commonly using at present are summarized. Finally, several feasible methods are resented to control and regulate residual stresses in thin-wall parts cutting.
2009 Vol. 52 (19): 87-90,95 [Abstract] ( 93 ) HTMLNew PDF (865 KB)  ( 222 )
91 Analysis on Springback of Big Diameter Thin-Wall Tube Bending Forming
DOI: 10.16080/j.issn1671-833x.2009.19.006

Based on plastic mechanics total strain theory, big diameter thin-walled tube bending forming is researched by assuming that only axial stress and strain in every fiber layer exist during tube bending process. The strain calculation equations of tube bending process are created by assuming the function of neutral layer offset angle and cuneiform angle with the angle coordinate. Then the stresses are gained by the relation of strain and stress, and the contact pressure and friction between die and tube are obtained through the integrating of stress on section and the force equilibrium in differential element. Outside force is calculated through the integrating of inner force on boundary. At last the coefficient of the function of neutral layer offset and cuneiform angle in bending segment are calculated through the force equilibrium equation and energy equilibrium equation. Thereby the springback angle is calculated and the infl uence law some process parameters to springback is analyzed.

2009 Vol. 52 (19): 91-95 [Abstract] ( 71 ) HTMLNew PDF (1397 KB)  ( 177 )
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