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2010 Vol. 53, No. 1
Published: 2010-01-01
FEATURE
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
 
       COVER STORY
26 Reforge the Spirit of AVIC Through Reform and Innovation#br#
DOI: 10.16080/j.issn1671-833x.2010.01.020
2010 Vol. 53 (1): 26-31 [Abstract] ( 63 ) HTMLNew PDF (3008 KB)  ( 303 )
       FEATURE
34 Development of Nano-Composite Coating With Brush Electronplating
DOI: 10.16080/j.issn1671-833x.2010.01.016
2010 Vol. 53 (1): 34-39 [Abstract] ( 55 ) HTMLNew PDF (2223 KB)  ( 352 )
       FORUM
44 Mechanical Property Requirements of Composites Systems for Wing Structures
DOI: 10.16080/j.issn1671-833x.2010.01.008
2010 Vol. 53 (1): 44-48 [Abstract] ( 85 ) HTMLNew PDF (2050 KB)  ( 416 )
49 Technical Basis for Large Aircraft Structures of Composites
DOI: 10.16080/j.issn1671-833x.2010.01.009
2010 Vol. 53 (1): 49-52 [Abstract] ( 79 ) HTMLNew PDF (1979 KB)  ( 457 )
53 Automated Tape-Laying Technology and Large Aircraft Composites Structure
DOI: 10.16080/j.issn1671-833x.2010.01.010
2010 Vol. 53 (1): 53-55 [Abstract] ( 56 ) HTMLNew PDF (2105 KB)  ( 269 )
56 Research and Application Progress of Key Technologies for Advanced Carbon/Carbon Aircraft Braking Composites
DOI: 10.16080/j.issn1671-833x.2010.01.001
2010 Vol. 53 (1): 56-58 [Abstract] ( 55 ) HTMLNew PDF (1952 KB)  ( 497 )
       NEW VIEWPOINT
70 Analysis of Advanced Complex Product Development
DOI: 10.16080/j.issn1671-833x.2010.01.026
2010 Vol. 53 (1): 70-73 [Abstract] ( 69 ) HTMLNew PDF (1987 KB)  ( 317 )
       RESEARCH
74 Manufacturing Process and Improvement of Silicon Coating on Niobium-Based Alloy
DOI: 10.16080/j.issn1671-833x.2010.01.002
Nb and Nb-based alloys are important high temperature structural materials because of their high melting point, corrosion resistance, and high temperature strength. However, poor high temperature oxidation resistance restricts their application. The present status of research on high temperature oxidation resistant silicon coatings of Nb-based alloys is reviewed in this paper, and the mechanism of silicide coatings manufacture and their corresponding high temperature oxidation resistance properties are expatiated. Existing problems are analyzed and possible solutions are suggested.
2010 Vol. 53 (1): 74-77 [Abstract] ( 53 ) HTMLNew PDF (496 KB)  ( 566 )
78 Performance Analysis of TA12 Titanium Alloy by Modifi ed Weld Joint Electron Beam Welding Method
DOI: 10.16080/j.issn1671-833x.2010.01.011
The vacuum electron beam welding method is used for TA12, and the surface of the sample shows well. Through optical microscopy, tensile and fatigue experiments, and other methods, the microstructure and mechanical properties of the joints are studied. The results show that the TA12 alloy joint with good performance can be obtained by electron beam welding, which meets the requirements of a welded structural component, and the microstructure is mainly martensite phase.
2010 Vol. 53 (1): 78-80 [Abstract] ( 56 ) HTMLNew PDF (756 KB)  ( 148 )
81 Effect of Ball-End Milling Structural Parameters on Surface Integrity for Titanium Alloy Milling
DOI: 10.16080/j.issn1671-833x.2010.01.003
Aiming at milling TC17 titanium alloy materials with carbide ball-end mill, effects of different ball-end cutter structural parameters on surface roughness, surface morphology, residual stress and micro-organizations are studied. The results show that when the rake γ 0=8°, fl ank α 0 =12° and helix angle β=35°, the best surface integrity for test pieces can be obtained. The surface roughness is about 0.40μm, the residual compressive stress in x direction is 324MPa, the residual compressive stress in y direction is 218MPa. And surface integrity doesn’t obriously change.
2010 Vol. 53 (1): 81-84 [Abstract] ( 70 ) HTMLNew PDF (1167 KB)  ( 263 )
85 Development and Application of High Strength Titanium Alloy BT22 in Aviation Industry
DOI: 10.16080/j.issn1671-833x.2010.01.012
BT22 is adapted for manufacture of large forgings as its highest strength after heat treatment in the high strength titanium alloys, which is widely used in aviation industry. The statement of heat treatment, mechanical properties and applications of BT22 are analyzed in this paper.
2010 Vol. 53 (1): 85-86/90 [Abstract] ( 48 ) HTMLNew PDF (454 KB)  ( 285 )
91 Hydro Forming Technology of Complex Profi le Cover Sheet of Aeroengine
DOI: 10.16080/j.issn1671-833x.2010.01.014
The key problems in forming are researched by the CAE for sheet forming and experiments. The results of the experiments are accordant with CAE very well. Finally the acceptable part is formed by hydro forming.
2010 Vol. 53 (1): 91-94/99 [Abstract] ( 58 ) HTMLNew PDF (1600 KB)  ( 266 )
95 Vibration Trouble Analysis and Solution of Turbine Jet Engine
DOI: 10.16080/j.issn1671-833x.2010.01.015
Aiming at the vibration trouble of turbine jet engine, based on vibration principle, the causes of vibration trouble are analyzed in detail. The measures for excluding vibration and prevent lons measures are presented. The basic method for checking and excluding vibration of engine is introduced, which are important to prevent vibration of engine.
2010 Vol. 53 (1): 95-99 [Abstract] ( 65 ) HTMLNew PDF (961 KB)  ( 405 )
97 Properties of Friction Stir Welding Joint by Ultrasonic Shot Peening
DOI: 10.16080/j.issn1671-833x.2010.01.013
The processing of hardening effectiveness by ultrasonic shot peening is used to deal with base metals of 7075 - T651 aluminum alloy and joint of friction stir welding, and is then compared with its original condition in fatigue comparative test. The result of the test of fatigue property shows that ultrasonic shot peening is available for improving the fatigue property of base metals of 7075 - T651 aluminum alloy and specimen of friction stir welding joint.
2010 Vol. 53 (1): 97-90 [Abstract] ( 55 ) HTMLNew PDF (774 KB)  ( 330 )
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