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2010 Vol. 53, No. 19
Published: 2010-10-01
FEATURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
 
       FEATURE
26 Aerodynamic Configuration Design of Future Large Aircra
DOI: 10.16080/j.issn1671-833x.2010.19.006
2010 Vol. 53 (19): 26-29 [Abstract] ( 54 ) HTMLNew PDF (1174 KB)  ( 781 )
       COVER STORY
32 Automated Fastening of Aircraft Cagro Door Structures With a Standard Articulating Robot System
DOI: 10.16080/j.issn1671-833x.2010.19.016
2010 Vol. 53 (19): 32-35 [Abstract] ( 52 ) HTMLNew PDF (1800 KB)  ( 539 )
       FORUM
38 NC Machining Characteristics of Aviation Parts
DOI: 10.16080/j.issn1671-833x.2010.19.010
2010 Vol. 53 (19): 38-41 [Abstract] ( 53 ) HTMLNew PDF (1388 KB)  ( 330 )
42 Key Technology and Application Prospect of Turning/Milling Machining#br#
DOI: 10.16080/j.issn1671-833x.2010.19.001
2010 Vol. 53 (19): 42-45 [Abstract] ( 47 ) HTMLNew PDF (814 KB)  ( 735 )
46 Development of NC Machining Technology for Large Titanium Blade
DOI: 10.16080/j.issn1671-833x.2010.19.017
2010 Vol. 53 (19): 46-49 [Abstract] ( 59 ) HTMLNew PDF (1273 KB)  ( 339 )
50 Investigating on Optimization Techniques of NC Machining Process Based on Typical Characteristic of Aeronautical Components
DOI: 10.16080/j.issn1671-833x.2010.19.007
2010 Vol. 53 (19): 50-54 [Abstract] ( 72 ) HTMLNew PDF (1091 KB)  ( 351 )
56 SINUMERIK 840D sl Qualified for Various Application Requirement
DOI: 10.16080/j.issn1671-833x.2010.19.018
2010 Vol. 53 (19): 56-58 [Abstract] ( 57 ) HTMLNew PDF (1261 KB)  ( 149 )
       NEW VIEWPOINT
78 evelopment of Airship Technology
DOI: 10.16080/j.issn1671-833x.2010.19.008
2010 Vol. 53 (19): 78-81 [Abstract] ( 61 ) HTMLNew PDF (878 KB)  ( 973 )
       RESEARCH
82 Comparative Study of Friction and Wear Behavior of Carbon/Carbon Composites and Copper Alloy for Bearing#br#
DOI: 10.16080/j.issn1671-833x.2010.19.002

Friction tester(UMT-200)and surface topograply (Talysurf CCI 2000) were used to characterize the friction and wear behavior of carbon/carbon composites, copper alloy and copper alloy with MoS 2 coating. In the result, under the same condition, the friction coeffi cient of copper alloy is approximately 0.65, the friction coefficient of copper alloy with MoS 2 coating lies between 0.25 and 0.3, moreover its liner wear rate is merely one third to that of copper alloy. However because of the destroy of MoS 2 coating during the casting experimental stage, its friction coeffi cient increased to around 0.35. The friction coefficient of carbon/carbon composites always kept at 0.12~0.13, and its liner wear rate is just one sixth as much as that of copper alloy. The wear-resistance and self-lubrication properties of carbon/carbon composites were performed well.
2010 Vol. 53 (19): 82-83/86 [Abstract] ( 58 ) HTMLNew PDF (772 KB)  ( 249 )
84 MMS: The Latest Green Skin Machining System
DOI: 10.16080/j.issn1671-833x.2010.19.003
Mirror milling system(MMS) is the latest skin machining system developed by DUFIEUX company, also it’s the latest green machining technology which can replace the hand dressing and the chemical milling. This paper introduces the working principle and the application status of the MMS, compared with the traditional skin machining system, MMS is an advanced, environment protected and promotional system.
2010 Vol. 53 (19): 84-86 [Abstract] ( 89 ) HTMLNew PDF (824 KB)  ( 358 )
87 Method of Part Process Assignment Planning and Its Evaluation
DOI: 10.16080/j.issn1671-833x.2010.19.005
Aiming for solving part process assignment planning, a method named process assignment planning based on shop capability is proposed and the method of process assignment route is researched. In this method, shop capability model is built by the capability of machine tools and process unit and manufacturing shop is selected by shop capability and status and the route is formed. On the basis, multi-candidate routes are evaluated by multi-fuzzy comprehensive appraisement to select optimal process assignment route. Finally, the method is verified by an example.
2010 Vol. 53 (19): 87-91 [Abstract] ( 42 ) HTMLNew PDF (971 KB)  ( 201 )
92 Application of Laser Tracker in Assembly Jig Manufacturing for Aircraft
DOI: 10.16080/j.issn1671-833x.2010.19.014
The hardware components, measurement principles and performance parameters of the laser tracker (LTD500) are expounded. Then the laser tracker for aircraft jig installation and measurement steps are introduced in detail and advantages and measurement error of installing jig by using laser tracker are analyzed.
2010 Vol. 53 (19): 92-94/97 [Abstract] ( 62 ) HTMLNew PDF (744 KB)  ( 510 )
95 Capability Study of Aviation Sub-Contracting Manufacture Based on SPM
DOI: 10.16080/j.issn1671-833x.2010.19.020
With the request of manufacture capability in aviation sub-contracting manufacture (ASCM) to the aviation enterprises, the evaluation factors of ASCM Capability are analysed, the ASCM capability model and three-dimensional mult-levels capability structure are established based on Supplier Performance Measurement(SPM),and the capability evaluation method is given for aviation enterprises to evaluate their capability. This capability evaluation model and method can be introduced to aviation enterprises to analyse the ASCM capability state and point out the developing directions.
2010 Vol. 53 (19): 95-97 [Abstract] ( 51 ) HTMLNew PDF (666 KB)  ( 199 )
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