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2008 Vol. 51, No. 10
Published: 2008-05-15
FEATURE
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
FEATURE
26
To Implement Project for Improving Efficiency of Thousands of NC Machine Tools, To Advance Productivity of Military Industry Enteprises
DOI: 10.16080/j.issn1671-833x.2008.10.019
2008 Vol. 51 (10): 26-29 [
Abstract
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69
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(1659 KB) (
160
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COVER STORY
32
Application of Composite Forming Technique in Military Freighter A400M
DOI: 10.16080/j.issn1671-833x.2008.10.005
2008 Vol. 51 (10): 32-35 [
Abstract
] (
80
)
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(2126 KB) (
460
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FORUM
40
Manufacturing Technology and Special Equipment for Advanced Composites
DOI: 10.16080/j.issn1671-833x.2008.10.006
2008 Vol. 51 (10): 40-45 [
Abstract
] (
68
)
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(2106 KB) (
489
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46
Composite Application and Manufacturing Technology for Modern Large Aircraft
DOI: 10.16080/j.issn1671-833x.2008.10.007
2008 Vol. 51 (10): 46-48 [
Abstract
] (
74
)
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(1592 KB) (
142
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49
Research Progress of Numerical Simulation Technology for Composite Forming for Large Aircraft
DOI: 10.16080/j.issn1671-833x.2008.10.008
2008 Vol. 51 (10): 49-51 [
Abstract
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77
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(1394 KB) (
115
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52
Equiping Aviation Industry With Advanced Technology and Facilities
DOI: 10.16080/j.issn1671-833x.2008.10.021
2008 Vol. 51 (10): 52-53 [
Abstract
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85
)
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(1335 KB) (
44
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54
Current Status and Development Trend of Epoxy Resin Carbon Fiber Reinforced Composites Forming Process
DOI: 10.16080/j.issn1671-833x.2008.10.009
2008 Vol. 51 (10): 54-57 [
Abstract
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81
)
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(1759 KB) (
420
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NEW VIEWPOINT
62
Research and Realization of Data Transmission Technology Among Aviation Enterprises in Different Areas
DOI: 10.16080/j.issn1671-833x.2008.10.010
2008 Vol. 51 (10): 62-65 [
Abstract
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68
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(1611 KB) (
87
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66
Key Technology for Building Core Ability Platform of Military Product Research
DOI: 10.16080/j.issn1671-833x.2008.10.022
2008 Vol. 51 (10): 66-70 [
Abstract
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73
)
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(2013 KB) (
52
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RESEARCH
72
Preparation and Forming Character s of Ni-Cu-Sn Alloy Powder for Laser Cladding Forming
DOI: 10.16080/j.issn1671-833x.2008.10.003
The Ni-Cu-Sn alloy powder suitable for laser cladding forming is developed. By experiments, the microstructure features and the cause of faults in microstructure of laser cladding formed part are analyzed, and the methods of preventing from faults are proposed.
2008 Vol. 51 (10): 72-74 [
Abstract
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65
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(320 KB) (
88
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75
Application of Manufacturing Execution System Suited to BPR in Aeronautical Enterprise
DOI: 10.16080/j.issn1671-833x.2008.10.011
Taking the composite material workshop of a large~scale aeronautical manufacturing enterprise as an example, the information~driven principle of business process and application mechanism and method of manufacturing execution system suited to BPR are expounded. The system is based on the workflow
management model and object~oriented software development technology is used.
2008 Vol. 51 (10): 75-78 [
Abstract
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74
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(349 KB) (
90
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RESEARCH
79
Fuzzy Analysis of Thermal Comfort Temperature in Manned Spacecraft Cabin
DOI: 10.16080/j.issn1671-833x.2008.10.012
A fuzzy analysis method is presented to determine thermal comfort temperature in manned spacecraft cabin. On the base of analyzing the influence of astronaut activity level, relative humidity and set temperature on thermal comfort, the set temperature of air-condition system is determined by use of fuzzy theory, and the polling list of temperature is given. The results can direct the astronauts to set the control temperature of air-condition system according to practical condition, and provide theoretical basis for the automatic control design of air~condition system with variable set temperature.
2008 Vol. 51 (10): 79-81,86 [
Abstract
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73
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(229 KB) (
68
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82
Precision Nanopositioner Stage
DOI: 10.16080/j.issn1671-833x.2008.10.004
nanopositioner stage is built with finite element method. The displacement, stress distribution, natural frequencies and vibration modes of flexible hinge effected by some main factors are analyzed. The influences of main structure parameters on static and dynamic characteristics of the nanopositioner stage are investigated by comprehensively using orthogonal test design. The regression equations of the performances, structure sizes of nanopositioner stage are obtained by using stepwise regression analysis on numerical results, and a prototype is manufactured for verification.
2008 Vol. 51 (10): 82-86 [
Abstract
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78
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(334 KB) (
127
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87
Parametric Sensitivity Analysis of Fatigue Life of Compressor Disk
DOI: 10.16080/j.issn1671-833x.2008.10.014
Low cycle multi-axial fatigue failure is a main fail form of aeroengine compressor disks. Failure of compressor disk often causes serious consequence. The sensitivities of fatigue life to relative parameters are analyzed by means of difference method and the sensitivity of relative parameters is determined
and expressed by parametric sensitivity curves.
2008 Vol. 51 (10): 87-89,95 [
Abstract
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67
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(194 KB) (
72
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RESEARCH
90
Research on Lean and Informatization Transformation for Aircraft Manufacturing Enterprise
DOI: 10.16080/j.issn1671-833x.2008.10.015
Transformation is concerned with the environment of production, information and humanity. With researching of improving these three aspects, a lean modular production system is put forward. It combines lean production, advanced digital technologies and production practices perfectly. And the production system model and its informatization and lean tranformation process are expatiated.
2008 Vol. 51 (10): 90-95 [
Abstract
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70
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(341 KB) (
100
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