Automated design of aircraft fuselage stiffeners using multiobjective evolutionary optimisation

被引：28

作者：

Sarangkum, Ruangrit ^{[1
]}

Wansasueb, Kittinan ^{[1
]}

Panagant, Natee ^{[1
]}

Pholdee, Nantiwat ^{[1
]}

Bureerat, Sujin ^{[1
]}

Yildiz, Ali R. ^{[2
]}

Sait, Sadiq M. ^{[3
]}

机构：

[1] Khon Kaen Univ, Fac Engn, Sustainable Infrastruct Res & Dev Ctr, Dept Mech Engn, Khon Kaen 40002, Thailand

[2] Bursa Uludag Univ, Dept Automot Engn, TR-16059 Bursa, Turkey

[3] King Fahd Univ Petr & Minerals, Dept Comp Engn, Dhahran 31261, Saudi Arabia

来源：

INTERNATIONAL JOURNAL OF VEHICLE DESIGN | 2019年 / 80卷 / 2-4期

关键词：

aircraft fuselage; multiobjective optimisation; rings and stringers; fuselage stiffeners; meta-heuristics; evolutionary algorithms; structural optimisation; constrained optimisation; aerodynamic; finite element analysis; TOPOLOGY OPTIMIZATION; DIFFERENTIAL EVOLUTION; CONCEPTUAL DESIGN; ALGORITHMS; PERFORMANCE;

D O I：

10.1504/IJVD.2019.109864

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

This paper proposes an optimisation process for the design of aircraft fuselage stiffeners using evolutionary optimisation. A new design problem is developed to find a layout for fuselage stiffeners (rings and stringers) such that the structural mass, compliance, and the first-mode natural frequency can be optimised, subject to structural constraints. The stiffeners are modelled as beam elements. Three multiobjective meta-heuristics are employed to solve the problem, and a comparative study of the results of these optimisers is carried out. It is found that the proposed layout synthesis problem for aircraft fuselage stiffeners leads to a set of efficient structural solutions, which can be used at the decision-making stage. It is an automated design strategy with high potential for further investigation.

引用

页码：162 / 175

页数：14

共 50 条

[1] Implementation of value-driven optimisation for the design of aircraft fuselage panels
Castagne, Sylvie
Curran, Richard
Collopy, Paul
[J]. INTERNATIONAL JOURNAL OF PRODUCTION ECONOMICS, 2009, 117 (02) : 381 - 388
[2] Multiobjective evolutionary optimisation for adaptive product family design
Li, L.
Huang, G. Q.
[J]. INTERNATIONAL JOURNAL OF COMPUTER INTEGRATED MANUFACTURING, 2009, 22 (04) : 299 - 314
[3] Automated multiobjective optimisation in axial compressor blade design
Voss, Christian
Aulich, Marcel
Kaplan, Burak
Nicke, Eberhard
[J]. Proceedings of the ASME Turbo Expo 2006, Vol 6, Pts A and B, 2006, : 1289 - 1297
[4] Efficient optimisation of large aircraft fuselage structures
Vankan, W. J.
Maas, R.
Grihon, S.
[J]. AERONAUTICAL JOURNAL, 2014, 118 (1199): : 31 - 52
[5] Multiobjective optimisation of fuzzy controllers using evolutionary algorithms
Klaassen, KP
Litz, L
[J]. UKACC INTERNATIONAL CONFERENCE ON CONTROL '98, VOLS I&II, 1998, : 1581 - 1586
[6] AUTOMATED EQUIPMENT CONFIGURATION IN MANEUVERABLE AIRCRAFT FUSELAGE
PASHCHENKO, OB
[J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1990, (04): : 111 - 113
[7] Management of evolutionary MAS for multiobjective optimisation
Dobrowolski, G
Kisiel-Dorohinicki, M
[J]. IUTAM SYMPOSIUM ON EVOLUTIONARY METHODS IN MECHANICS, 2004, 117 : 81 - 90
[8] The use of topology optimisation in the conceptual design of next generation lattice composite aircraft fuselage structures
Niemann, S.
Kolesnikov, B.
Lohse-Busch, H.
Huehne, C.
Querin, O. M.
Toropov, V. V.
Liu, D.
[J]. AERONAUTICAL JOURNAL, 2013, 117 (1197): : 1139 - 1154
[9] Design of a System for Aircraft Fuselage Inspection
Fernandez, Rui Filipe
Keller, Kevin
Robins, Jeffrey
[J]. 2016 IEEE SYSTEMS AND INFORMATION ENGINEERING DESIGN SYMPOSIUM (SIEDS), 2016, : 283 - 288
[10] Design and Analysis of Grid Stiffened Fuselage Panel with Curved Stiffeners
Hemanth, Bharath
Babu, N. C. Mahendra
Shivakumar, H. G.
Srikari, S.
[J]. ADVANCES IN MECHANICAL DESIGN, MATERIALS AND MANUFACTURE, 2018, 1943

← 1 2 3 4 5 →