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2009 Vol. 52, No. 1
Published: 2009-01-01
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
COVER STORY
28
Key Manufacturing Technologies of Large Aircraft Development in China
DOI: 10.16080/j.issn1671-833x.2009.01.009
2009 Vol. 52 (1): 28-31 [
Abstract
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79
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(1372 KB) (
662
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FIGURE
34
Current and Development Status of Sheet Metal Equipment and Technology in Chinese Aviation Industry
DOI: 10.16080/j.issn1671-833x.2009.01.010
2009 Vol. 52 (1): 34-39 [
Abstract
] (
85
)
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(1774 KB) (
436
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FORUM
44
NC Machining Equipment and Advanced Machining Technology for Large Aircraft Component
DOI: 10.16080/j.issn1671-833x.2009.01.012
2009 Vol. 52 (1): 44-47 [
Abstract
] (
92
)
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(998 KB) (
975
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48
Discussion on Effeciency Problems of NC Equipment Application
DOI: 10.16080/j.issn1671-833x.2009.01.024
2009 Vol. 52 (1): 48-50 [
Abstract
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81
)
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(1019 KB) (
247
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51
Digital Manufacturing Assists the Development of Aviation Industry
DOI: 10.16080/j.issn1671-833x.2009.01.013
2009 Vol. 52 (1): 51-53 [
Abstract
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80
)
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(931 KB) (
355
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54
Application of Siemens' SINUMERIK 840D in Five-Axis Machining
DOI: 10.16080/j.issn1671-833x.2009.01.014
2009 Vol. 52 (1): 54-56 [
Abstract
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89
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(1581 KB) (
203
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NEW VIEWPOINT
70
Research and Application of Virtual Assembly Technology
DOI: 10.16080/j.issn1671-833x.2009.01.016
2009 Vol. 52 (1): 70-73 [
Abstract
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86
)
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(1290 KB) (
425
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74
Nanometer Radar Absorption Composite and Its Application on Stealth Aircraft
DOI: 10.16080/j.issn1671-833x.2009.01.017
2009 Vol. 52 (1): 74-75 [
Abstract
] (
79
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(876 KB) (
697
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RESEARCH
78
Experimental Investigation of Combined Ultrasonic and Electrochemical Micro-machining of Cemented Carbide
DOI: 10.16080/j.issn1671-833x.2009.01.001
The combined ultrasonic and electrochemical micro-machining technology has many excellences in machining productivity, precision, environmental safety, and also has technical predominance and development potential in aspects of machining micro-structures of cemented carbide. In this paper, the machining mechanism and test device of combined ultrasonic and electrochemical micro-machining is expatiated. Many comparative machining tests of cemented carbide are carried out. The influence of machining parameters such as voltage, feeding force and electrolyte on machining result is analyzed. By optimizing the machining parameters and machining conditions, the micro-machining accuracy of cemented carbide microstructures is increased.
2009 Vol. 52 (1): 78-82 [
Abstract
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73
)
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(4145 KB) (
373
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83
Rapid Process Planning Technology Based on 3D-PLM for Aircraft Manufacturing Enterprise
DOI: 10.16080/j.issn1671-833x.2009.01.018
In order to effectively solve the problem of rapid process planning in aircraft manufacturing enterprise, the approach to rapid process planning based on 3D-PLM is put forward. The process design and management as well as the application state of CAPP technology application in aircraft manufacturing enterprise are analyzed. The process characteristics and needs of rapid process planning based on 3D-PLM in aircraft manufacuring enterprise are described in detail. Technological architecture of rapid process planning based on 3D-PLM is presented.
2009 Vol. 52 (1): 83-87/92 [
Abstract
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96
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(4039 KB) (
355
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88
Agile Manufacturing-Oriented Dynamic Process Planning
DOI: 10.16080/j.issn1671-833x.2009.01.019
Enterprises based on the agile manufacturing mode must rapidly respond the requirements of their customers. A general process planning model based on manufacturing features of parts is proposed. Furthermore, a system is implemented to minimize the whole process time of product by using genetic algorithm and according to the real-time resources status of the shop floor and to realize dynamic process planning of product to meet the requirement of modern flexible manufacturing.
2009 Vol. 52 (1): 88-92 [
Abstract
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74
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(1888 KB) (
216
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93
Manufacture Process and Quality Control of Composites Cover Panel of Wing Fuel Tank
DOI: 10.16080/j.issn1671-833x.2009.01.020
One-step co-curing process of manufacturing the composites cover panel with stiffeners for wing fuel tank by applying open expansive silicon rubber die is presented. In view of more serious defects existing in the parts of initial manufacturing stage, including warp, stiffeners size out-of-tolerance, delamination and dense voids, the corresponding design modification, process improvements and quality control measures, are introduced. Perfect parts are obtained eventually, and the function check and flight tests with these parts are passed.
2009 Vol. 52 (1): 93-95 [
Abstract
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74
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(578 KB) (
238
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