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2010 Vol. 53, No. 5
Published: 2010-03-01
FEATURE
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
FORUM
0
The Latest Movement and Development Trend of Laser Shock Processing
DOI: 10.16080/j.issn1671-833x.2010.05.016
2010 Vol. 53 (5): 0-42 [
Abstract
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106
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(1329 KB) (
564
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FEATURE
26
Spindle Unit of NC Machine Tool in Aviation Manufacturing and Its Development Trend
DOI: 10.16080/j.issn1671-833x.2010.05.018
2010 Vol. 53 (5): 26-29 [
Abstract
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104
)
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(1423 KB) (
561
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COVER STORY
32
Independent Innovation for High-Level Machine Tool
DOI: 10.16080/j.issn1671-833x.2010.05.022
2010 Vol. 53 (5): 32-35 [
Abstract
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89
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(1849 KB) (
405
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FORUM
43
Development of Electrical Discharge Forming Technology
DOI: 10.16080/j.issn1671-833x.2010.05.003
2010 Vol. 53 (5): 43-46 [
Abstract
] (
95
)
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(1558 KB) (
1021
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47
Current Status and Prospect of Electrochemical Machining Technology
DOI: 10.16080/j.issn1671-833x.2010.05.002
2010 Vol. 53 (5): 47-50 [
Abstract
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119
)
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(1445 KB) (
961
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51
Research Situation of Laser Cladding Technology in Aviation Manufacturing
DOI: 10.16080/j.issn1671-833x.2010.05.010
2010 Vol. 53 (5): 51-54 [
Abstract
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117
)
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(1640 KB) (
586
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NEW VIEWPOINT
66
Development and Prospect of High-Efficiency Grinding Technology and Equipment
DOI: 10.16080/j.issn1671-833x.2010.05.001
2010 Vol. 53 (5): 66-70 [
Abstract
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137
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(1501 KB) (
553
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RESEARCH
72
Analysis and Modeling of Plunge Milling Force on PH13-8Mo#br#
DOI: 10.16080/j.issn1671-833x.2010.05.007
Plunge milling can reduce the radial cutting force, the deformation of the workpiece, the machine tool power consumption, and cut diffi cult-to-cut materials with great effi ciency. The application of plunge milling is more and more widely. In view of the characteristic of machinability of precipitation hardening stainless steel PH13-8Mo,an experiment platform for cutting force testing is established, and the experiment is designed by the orthogonal methods. The plunge milling force model of PH13-8Mo is built by multiple linear regression on the basis of experiment data. The changing law of cutting force is studied. The research supplies important reference to the research on the plunge milling of precipitation hardening stainless steel.
2010 Vol. 53 (5): 72-74/80 [
Abstract
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90
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(1395 KB) (
257
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75
Machining of Typical Deep Hole or Cavity for Aircraft Landing Gear
DOI: 10.16080/j.issn1671-833x.2010.05.014
The machining of the typical deep hole or cavity of landing gear is concluded and summarized with practical cases, which is the important reference for enhancing the surface quality and machining effi ciency.
2010 Vol. 53 (5): 75-76/80 [
Abstract
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108
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(1293 KB) (
269
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77
Design Method of Mechanical Part Fitting Based on Evidential Reasoning
DOI: 10.16080/j.issn1671-833x.2010.05.008
In the design of mechanical part fitting, the factors that infl uence the selection of fi tting can be called evidences. After the introduction of evidences classifi cation and effect, a method of mechanical part fitting based on evidential reasoning is proposed. The vector quantization of main evidences combines the use of fuzzy expression and exact computation. Then, with other evidences, the result can be fi gured out. Examples show that this method can be applied to general mechanical part fitting design.
2010 Vol. 53 (5): 77-80 [
Abstract
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97
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(1573 KB) (
153
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81
Parametric Design of Typical Aircraft Part Joggle
DOI: 10.1608/j.issn1671-833x.2010.05.017
2010 Vol. 53 (5): 81-83/86 [
Abstract
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121
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(1517 KB) (
155
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84
Research of Development and Application of Polishing Test for Blisk Blade
DOI: 10.16080/j.issn1671-833x.2010.05.013
The Polishing test for blisk blade by automatically grinding machine is introduced. According to the test data,the characteristic of this machining method is analyzed and some methods are adopted in the process of grinding. It provides some reference experience for the application of the machining method.
2010 Vol. 53 (5): 84-86 [
Abstract
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103
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(1232 KB) (
327
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87
Digital Design of Protection Circuit of Aircraft Generator Control Unit#br#
DOI: 10.16080/j.issn1671-833x.2010.05.012
According to the fact that components in traditional controllers are very sensitive to environment, a digital aircraft generator control unit(GCU) is designed and implemented with a digital signal processor(DSP)based on the principle of analog voltage regulation and digital control and protection.And the key design points are introduced. Experimental results show more reliability and more stability in fault treatment of the digital controllers comparing with the traditional ones.
2010 Vol. 53 (5): 87-90 [
Abstract
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96
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(1383 KB) (
259
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91
FEM Simulation and Experiment on Spinning Process of Titanium Alloy Wheel Rim
DOI: 10.16080/j.issn1671-833x.2010.05.011
The spinning process of wheel rim is simulated by the FEM software of ANSYS/LS-DYNA, and the experimental research is conducted on hot-spinning flange of TC4 titanium alloy, based on which the proper hot spinning scheme of wheel rim of titanium alloy is determined.
2010 Vol. 53 (5): 91-95 [
Abstract
] (
94
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(2017 KB) (
289
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