Selecting composite materials considering cost and environmental impact in the early phases of aircraft structure design

被引：38

作者：

Calado, Elcin Aleixo ^{[1
]}

Leite, Marco ^{[1
]}

Silva, Arlindo ^{[2
]}

机构：

[1] Univ Lisbon, Inst Super Tecn, IDMEC, Av Rovisco Pais, P-1049001 Lisbon, Portugal

[2] Singapore Univ Technol & Design, Engn Prod Dev Pillar, 8 Somapah Rd, Singapore 487372, Singapore

来源：

JOURNAL OF CLEANER PRODUCTION | 2018年 / 186卷

关键词：

Aircraft composites stacking; DMS optimization; FEA optimization; Integrated LCA/LCC; MULTIOBJECTIVE OPTIMIZATION; GENETIC ALGORITHM; FUSELAGE FRAMES; WEIGHT DESIGN; MINIMUM-COST; PART;

D O I：

10.1016/j.jclepro.2018.02.048

中图分类号：

X [环境科学、安全科学];

学科分类号：

08 ; 0830 ;

摘要：

The main aim of this study is to develop a computer-aided material selection tool that supports the designer in the selection of the most suitable carbon fiber-reinforced composite configuration (orientations, the number of plies, material type) for aircraft structures. The selection procedure is based on technical, economic and environmental performance objectives for a given design, in a multidisciplinary and multi-objective optimization scenario. Economic and environmental performance evaluation is based on an integrated Life Cycle Assessment (LCA)/Life Cycle Costing (LCC) model. Technical performance evaluation is done using Hypermesh-Optistruce (R) solver. Direct multi-search (DMS) solver is used for the optimization framework. A cargo aircraft elevator design is optimized using the proposed material selection tool. Results show that the material selection tool is a suitable guide for reducing weight during the early phases of design and promoting sustainable development in the aircraft industry. (C) 2018 Published by Elsevier Ltd.

引用

页码：113 / 122

页数：10

共 36 条

[1] Design optimization of composite laminated structures using genetic algorithms and finite element analysis
Almeida, F. S.
Awruch, A. M.
[J]. COMPOSITE STRUCTURES, 2009, 88 (03) : 443 - 454
[2] [Anonymous], 26 C ICAS 8 AIAA ATI
[3] Coello C. A. C., 1999, Knowledge and Information Systems, V1, P269
[4] DIRECT MULTISEARCH FOR MULTIOBJECTIVE OPTIMIZATION
Custodio, A. L.
Madeira, J. F. A.
Vaz, A. I. F.
Vicente, L. N.
[J]. SIAM JOURNAL ON OPTIMIZATION, 2011, 21 (03) : 1109 - 1140
[5] Materials selection for an automotive structure by integrating structural optimization with environmental impact assessment
Ermolaeva, NS
Castro, MBG
Kandachar, PV
[J]. MATERIALS & DESIGN, 2004, 25 (08) : 689 - 698
[6] Materials selection combined with optimal structural design: concept and some results
Ermolaeva, NS
Kaveline, KG
Spoormaker, JL
[J]. MATERIALS & DESIGN, 2002, 23 (05) : 459 - 470
[7] The multi-disciplinary design of a large-scale civil aircraft wing taking account of manufacturing costs
Gantois, K
Morris, AJ
[J]. STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2004, 28 (01) : 31 - 46
[8] Optimum stacking sequence design of composite materials Part II: Variable stiffness design
Ghiasi, Hossein
Fayazbakhsh, Kazem
Pasini, Damiano
Lessard, Larry
[J]. COMPOSITE STRUCTURES, 2010, 93 (01) : 1 - 13
[9] ENERGY-EFFICIENCY IMPROVEMENT POTENTIAL OF COMMERCIAL AIRCRAFT
GREENE, DL
[J]. ANNUAL REVIEW OF ENERGY AND THE ENVIRONMENT, 1992, 17 : 537 - 573
[10] Humbert S., 2012, IMPACT 2002 USER GUI

← 1 2 3 4 →