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2010 Vol. 53, No. 8
Published: 2010-04-15
FEATURE
FIGURE
FORUM
RESEARCH
COVER STORY
FEATURE
26
Can Joint Technology and Aero Die Forging Hydraulic Press
DOI: 10.16080/j.issn1671-833x.2010.08.013
通过预应力钢丝缠绕技术，以坎合连接的方式将其组合为一个整体，从而替代整体铸锻结构。这种技术思路的产生，充分体现了“以小搏大”的特点，是具有创新性的重型液压机设计方法。
2010 Vol. 53 (8): 26-28 [
Abstract
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71
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COVER STORY
32
ication Progress and Development Tendency of Superplastic Forming/Diffusion Bonding Technology
DOI: 10.16080/j.issn1671-833x.2010.08.012
2010 Vol. 53 (8): 32-35 [
Abstract
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74
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943
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FORUM
38
Curing Behaviors of Ceramic Suspension in Stereolithography and Its Engineering Applications
2010 Vol. 53 (8): 38-42 [
Abstract
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74
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501
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43
Direct Rapid Manufacturing Technology for Metal Parts and Its Development Trends
DOI: 10.16080/j.issn1671-833x.2010.08.004
2010 Vol. 53 (8): 43-46 [
Abstract
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82
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575
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47
Progress on Laser Rapid Manufacturing of High Performance Metallic Components
DOI: 10.16080/j.issn1671-833x.2010.08.002
2010 Vol. 53 (8): 47-50 [
Abstract
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64
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51
Application of Rapid Prototyping in Aviation Industry
DOI: 10.16080/j.issn1671-833x.2010.08.011
2010 Vol. 53 (8): 51-54 [
Abstract
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55
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548
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55
Laser Forming Repair of Titanium Alloy Parts
DOI: 10.16080/j.issn1671-833x.2010.08.010
2010 Vol. 53 (8): 55-58 [
Abstract
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79
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316
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COVER STORY
60
Enterprise Wasting and Informatization Strategy in Aircraft Development
DOI: 10.16080/j.issn1671-833x.2010.08.023
2010 Vol. 53 (8): 60-62 [
Abstract
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58
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134
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RESEARCH
66
Research on the Cost Decision System of Integrated Product Development
DOI: 10.16080/j.issn1671-833x.2010.08.025
The cost information characteristics of product life cycle in integrated product development(IPD) circumstance is analyzed,and the cost information construction model in IPD is established.Based on this mode,cost decision model in IPD is constructed to provide support for product design.
2010 Vol. 53 (8): 66-68/75 [
Abstract
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50
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69
Design Improvement and Manufacturing Technology of Landing Gear for One Type of Aircraft
The new technology and processes are introduced in detail, which are adopted in the landing gear design improvement for one type of aircraft. The testing and advance flight validation after improvement shows that all functional performances are qualified and can meet the application requirements of the retrofit aircraft.
2010 Vol. 53 (8): 69-71 [
Abstract
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43
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71
Distribution of Aero-Engine Turbine Blades Life Based on Few Data
DOI: 10.16080/j.issn1671-833x.2010.08.008
By analyzing HPT-1 blades field failure data, 3D mathematical model is built considering the factors affect blade life, such as failure mode and maintenance condition. HPT-1 blades life distribution histogram is obtained by dimensional reduction. The error is assumed between the histogram and the Weibull distribution curve assumed with least square method, which provides an available method for field data management and a proof for HPT-1 maintenance arrangement of aviation enterprise. It is of importance for reducing downtime, and improving operation efficiency for aviation enterprise.
2010 Vol. 53 (8): 71-78/81 [
Abstract
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59
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72
Evaluation for Supplier Selection Based on Multilevel Grey Evaluation Method
DOI: 10.16080/j.issn1671-833x.2010.08.024
The selection of supplier is an important factor for enterprise development. From the perspective of the supplier development of enterprises, the supplier evaluation index consists of the system development of operating capacity, the will to cooperate and the corporate image is built. According to the gray of information for evaluation,a supplier evaluation of a multilevel gray evaluation method is presented, and an example for this method is given, an easy and simple method to select supplier for enterprise is supplied.
2010 Vol. 53 (8): 72-75 [
Abstract
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58
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79
Key Technology and Realization on Three-Dimensional Modeling of Virtual Equipment Training
DOI: 10.16080/j.issn1671-833x.2010.08.017
It is a indispensable means of virtual equipment training in knowing equipment and actually training.In this paper,a technology method applying creator to three-dimensional modeling of virtual equipment is introduced.Three key technologies about instance,LOD and billboard used in the modeling are discussed.The contradiction between accuracy and data quantity in three-dimensional modeling of virtual equipment is solved by these methods in actual application.
2010 Vol. 53 (8): 79-81 [
Abstract
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70
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82
Shape Optimization of Morphing Wing Based on the Bi-Level Optimization Strategy
DOI: 10.16080/j.issn1671-833x.2010.08.014
According to the requirements of the multi-mission missile morphing wing shape optimization design, the infl uence of morphing wing on the gross weight and fl ight permance of missile is studied.Given the initial scheme, a hybrid optimization method coupling genetic algorithm and pattern search is chosen to complete the optimization task. The results show that the gross weight and fuel consumption decrease by 5.46% and 15.25% separately.
2010 Vol. 53 (8): 82-85 [
Abstract
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51
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86
Design of Location Fixture for Concentricity of Launcher Suspension Hole
DOI: 10.16080/j.issn1671-833x.2010.08.007
The concentricity of suspension hole is one of the key dimension for launcher,which affects the suspending accuracy,and this result in the tolerance is being made necessarily tight.According to the machining process,a fi xture which is comprised of the fl atted location pin,the location key and the base plate is presented.The fixture eliminates the six freedoms when work is located.The process calculation of the jig is also carried out.Accuracy is ensured by machining suitable location features,and the clamp can be operated quickly but with safety.The qualified concentricity of suspension hole is processed to meet the demand of mass patch production.
2010 Vol. 53 (8): 86-88 [
Abstract
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64
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89
Evaluation Model of Aircraft Battle Damage Repair Capability Based on SPA
DOI: 10.16080/j.issn1671-833x.2010.08.006
The factors that effect on aircraft battle damage repair capability are analyzed, and an index system is built for repair capability evaluation. The evaluation model of aircraft battle damage repair capability based on identical discrepancy contrary(IDC) of set pair analysis(SPA) is established. At last,the practical calculation shows the evaluation model is feasible and effective.
2010 Vol. 53 (8): 89-92/96 [
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57
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93
Tool Life Prediction Model Based on BP Neural Network
DOI: 10.16080/j.issn1671-833x.2010.08.019
The dominant factors affecting tool life are analyzed. According to the nonlinear relationship between factors and tool life, the tool life prediction model based on BP neural network is built up and the computing and demonstration are carried out by using this model. The results show that the model prediction value is very closed to the expected value of tool life, so the model is proved to be reliable and effective.
2010 Vol. 53 (8): 93-96 [
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61
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Notices
·
'Aeronautical Manufacturing technology ' is included in EI database
·
China Science Citation Database (CSCD)
·
Chinese S&T Journal Citation Reports (CJCR)
·
World Journal Clout Index (WJCI) Report of Scientific and Technological Periodicals
·
Supported in China Science and Technology Journal Excellence Action Plan
·
Aeronautical Manufacturing Technology ranked No. 3 in Chinese S&T Journal Citation Reports (CJCR)
·
High Quality Sci-tech Journal Classification Catalogue in Aerospace Field （2023）
·
A Guide to the Core Journals of China (hosted by Peking University Library)
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