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2011 Vol. 54, No. 10
Published: 2011-05-15
FEATURE
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
 
       FEATURE
26 Research on the CNC Polishing Process and Process Equipment Technology of Blisk
DOI: 10.16080/j.issn1671-833x.2011.10.001
2011 Vol. 54 (10): 26-29 [Abstract] ( 110 ) HTMLNew PDF (1291 KB)  ( 785 )
       
32 Research Development and Application of Multi - Point Forming Technology
DOI: 10.16080/j.issn1671-833x.2011.10.002
2011 Vol. 54 (10): 32-34 [Abstract] ( 153 ) HTMLNew PDF (1974 KB)  ( 375 )
       FORUM
40 Application of DYNAFORM in Stamp-Forming Process
DOI: 10.16080/j.issn1671-833x.2011.10.004
2011 Vol. 54 (10): 40-44 [Abstract] ( 93 ) HTMLNew PDF (2531 KB)  ( 348 )
52 Delcam Toolmaker for 3D Mould Design
DOI: 10.16080/j.issn1671-833x.2011.10.007
2011 Vol. 54 (10): 52-54 [Abstract] ( 103 ) HTMLNew PDF (1047 KB)  ( 206 )
       NEW VIEWPOINT
56 Research on Flexible Multi-Point Supporting Technology for Aircraft Components
DOI: 10.16080/j.issn1671-833x.2011.10.025
2011 Vol. 54 (10): 56-59 [Abstract] ( 100 ) HTMLNew PDF (1305 KB)  ( 247 )
       RESEARCH
64 Practice of Software Development Process With Agile Method
DOI: 10.16080/j.issn1671-833x.2011.10.016

In order to improve the effi ciency of the software development team within aeronautical manufacturing enterprises which has strict secrecy systems, agile methods and classic software develop process in a concrete project is adopted. After three years’ practice, some experiences about how to improve our software process in a bottom-up way is obtained and a software develop process model for this kind of enterprises is found.
2011 Vol. 54 (10): 64-67 [Abstract] ( 99 ) HTMLNew PDF (1072 KB)  ( 445 )
68 Application of ANSYS Structure Optimization Technology in Mechanical Design
DOI: 10.16080/j.issn1671-833x.2011.10.021
ANSYS optimization design model is introduced, and the concrete design steps for mechanical structure optimization are given out. Basic thought and key steps is introduced to realize structure optimization design on ANSYS with the instance, which proves the feasibility of ANSYS optimized analysis function to realize the structure optimization analysis. So that the new method is provided to the optimized analysis for the other complicated structures. New methods and thinking are provided for designer engaged in this aspect.
2011 Vol. 54 (10): 68-71/85 [Abstract] ( 84 ) HTMLNew PDF (1005 KB)  ( 609 )
72 Design of Optical Projecting System and Image Processing System
DOI: 10.16080/j.issn1671-833x.2011.10.023
An optical projecting system design for our high-precision and fully automatic tool presetter is introduced. High effective step motors enables all measuring axes to be accurately positioned. With the aid of the Easy-WebSet measuring software, the cutting edge will automatically be identifi ed and checked with micron accuracy by means of the CCD image processing system.
2011 Vol. 54 (10): 72-74 [Abstract] ( 77 ) HTMLNew PDF (1349 KB)  ( 135 )
78 Design and Realization of Hydraulic Rotational Flight Simulator’s Control System Based on xPC Realtime Control
DOI: 10.16080/j.issn1671-833x.2011.10.026
The internal popular RT control systems were compacted , principle of xPC rapid prototype were presented. Control system model of hydraulic rotational fl ight simulator was constructed ,and with this, RT control system of one hydraulic rotational fl ight simulator was actualized.
2011 Vol. 54 (10): 78-80/88 [Abstract] ( 100 ) HTMLNew PDF (1810 KB)  ( 113 )
81 Key Technology in Modeling of Blade Surface Based on Data Point of Contour Measurement
DOI: 10.16080/j.issn1671-833x.2011.10.008
Thin-walled blades are widely used in aviation and aerospace industry, the measurement and modeling are the key process of reverse manufacturing. According to geometric features of blade, contour measurement method is used to measure blade surface. The key technology of modeling process is studied. The works on measurement and modeling of blade surface are carried out, including the method of the probe radius compensation, eliminating of bad points, creating the leading and trailing edge by single-arc method, creating the section curves of the suction side and the pressure side by NURBS curve method , jointing section curves of suction(pressure) side and the leading(trailing) edge, and creating of the equidistant curves. Finally, a solid model is generated through a measurement example, and the quality and precision of blade surface are excellent. This method is proved simple and easy to apply.
2011 Vol. 54 (10): 81-85 [Abstract] ( 101 ) HTMLNew PDF (2070 KB)  ( 198 )
86 Simulation of Proportional Flow Control Valve Based on AMESim
DOI: 10.16080/j.issn1671-833x.2011.10.008
A simulation model for the study of a proportional fl ow control valve based on AMESim is established. It simulates the real conditions of application. Some parameters are optimized so as to improve the design of the valve.
2011 Vol. 54 (10): 86-88 [Abstract] ( 83 ) HTMLNew PDF (1167 KB)  ( 559 )
89 Confi guration-Based Quality Management of Single Military Aircraft
DOI: 10.16080/j.issn1671-833x.2011.10.027
The life cycle quality data management model for single military aircraft is proposed for demand characteristics of the single military aircraft refined management. This model aims to describe the unique product object structural characteristics by the methods of configuration management, and also through the detailed classification of the configuration baseline management to achieve the tiered management of quality objective. Quality characteristics will be the class attribute to follow configuration items/ configuration components to collect quality data information from configuration project establishment to delivery and application, and through the confi guration life cycle management to achiev
2011 Vol. 54 (10): 89-93 [Abstract] ( 96 ) HTMLNew PDF (1741 KB)  ( 269 )
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