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2009 Vol. 52, No. 6
Published: 2009-03-15

 
26 Advanced Forging Manufacturing Technology and Its Application in Aviation Industry
2009 Vol. 52 (6): 26-29 [Abstract] ( 58 ) HTMLNew PDF (986 KB)  ( 306 )
32 Machining Deformation of Aircraft Structure and Its Control
2009 Vol. 52 (6): 32-35 [Abstract] ( 61 ) HTMLNew PDF (2238 KB)  ( 471 )
41 Development and Prospection of PCBN Cutting Tool in The 21st Century#br#
2009 Vol. 52 (6): 41-44 [Abstract] ( 68 ) HTMLNew PDF (1811 KB)  ( 197 )
45 New Structure and High Efficiency Dual-cut Gear Hob
2009 Vol. 52 (6): 45-47 [Abstract] ( 54 ) HTMLNew PDF (1098 KB)  ( 148 )
48 Latest Development of PCBN Cutting Tool in Hard Cutting Process
2009 Vol. 52 (6): 48-51 [Abstract] ( 60 ) HTMLNew PDF (1403 KB)  ( 291 )
52 Discussion of Future Cutting Tool Development Based on Machining Challenge
2009 Vol. 52 (6): 52-54 [Abstract] ( 58 ) HTMLNew PDF (876 KB)  ( 119 )
55 New Type High-Efficiency Drilling Head for Machining Aluminum Alloy
2009 Vol. 52 (6): 55-57 [Abstract] ( 62 ) HTMLNew PDF (1277 KB)  ( 131 )
58 Development and Application of Hole Helical Milling Technology in Aviation Manufacturing Assembly Industry
2009 Vol. 52 (6): 58-60 [Abstract] ( 55 ) HTMLNew PDF (561 KB)  ( 301 )
66 Current Status and Development of Ultra High Pressure Waterjet Cutting Machine
2009 Vol. 52 (6): 66-68 [Abstract] ( 64 ) HTMLNew PDF (1150 KB)  ( 319 )
69 Application of Remanufacturing Engineering on a Military Aeroengine
2009 Vol. 52 (6): 69-71 [Abstract] ( 80 ) HTMLNew PDF (344 KB)  ( 399 )
74 Framework of Intelligent Design System for Knowledge—Based Investment Casting Die of Aeroengine Turbo Blade

In order to solve the problems in the turbo blade investment casting die design process,such as long design time,lower utilization of expert experience and lower level of intelligence,the knowledge engineering is introduced in the turbo blade investment casting die design,and an intelligent knowledge—based investment casting die design system is developed and the key technologies of the system are researched.The practical application results indicate that this system can reuse the expert experience efficiently and improve the efficiency and quality of die design.

2009 Vol. 52 (6): 74-77,84 [Abstract] ( 72 ) HTMLNew PDF (888 KB)  ( 214 )
80 Effect of Adhesive on Interlaminar Stress of Composite Stiffened Structure
The effect of adhesive on inter-laminar stress of composite stiffened structures is investigated.A 3-D finite element model is established for interlaminar stress of composite stiffened structures by dealing near interface composite witlI laminar and out of near interface composite with homogeneous orthotrothie
material.
2009 Vol. 52 (6): 80-84 [Abstract] ( 70 ) HTMLNew PDF (502 KB)  ( 255 )
85 Research on Aeroengine Lubricant System Fault Diagnosis Based on Wavelet Neural Network

Fault detection and diagnosis methods for non—linear system based on wavelet neural networks are researched.Wavelet analysis and feed-forward neural networks are fused,and the algorithm is inferred.Method of wavelet neural networks is used in fault diagnosis for the lubricant system of the oA!roen-sine.Results of simulation and tests show that this method,which is good to fault diagnosis for non-linear systems,does better in convergence speed,and is not sensitive to the inputs of the network.

2009 Vol. 52 (6): 85-89 [Abstract] ( 62 ) HTMLNew PDF (301 KB)  ( 310 )
90 Properties Research of Solid Film Lubricant for Preventing Titanium Alloy From Fretting Wear

The properties of solid film hbri·cant including resistance of wear,high temperature,temperature alternating and oil are researched and compared with the friction wear properties of silver coating.Experiments indicate that the graphite solid film lubricant has less wear value and lower friction CO.efficient,has good properties of resistance of wear,high temperature,temperature alternating and oil,and has loss weight properties.Therefore,the lubricant possess-es excellent lubricating and reducing friction properties.

2009 Vol. 52 (6): 90-92 [Abstract] ( 70 ) HTMLNew PDF (214 KB)  ( 187 )
93 Near—Isothermal Forging of GH4169 AHoy

The near—isothermal forging exo periment of GH4169 alloy is carried out.The results show that the microstructure and tensile properties have hish sensitization to the temperature pattern.but low sensitization to the deformation and strain rate,which is benefit to the near—isothermal forming of GH4169 alloy.

2009 Vol. 52 (6): 93-95 [Abstract] ( 57 ) HTMLNew PDF (305 KB)  ( 232 )
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