Proceedings of the 2024 3rd International Conference on Information Economy, Data Modelling and Cloud Computing (ICIDC 2024)

An Analytical Method for the Trade-off Between Comfort and Economy of Aircraft based on the Weight of Fuselage Structure

Authors
Lu Bai1, *, Jingze Hu1, Xiuying Wang1, Rong Cui1, Dongyue Pan1, Jian Tang1
1COMAC Beijing Aircraft Technology Research Institute, Beijing, 102211, China
*Corresponding author. Email: bailu@comac.cc
Corresponding Author
Lu Bai
Available Online 31 August 2024.
DOI
10.2991/978-94-6463-504-1_17How to use a DOI?
Keywords
comfort of aircraft; weight of fuselage; DOC; economy of aircraft
Abstract

Both comfort and economy need to be considered in aircraft design, and fuselage structural weight, as one of the key design parameters, has a significant impact on both. The aim of this study is to explore an analysis method based on fuselage structural weight to balance comfort and economy, and to provide guidance for optimising aircraft design. Through literature study and methodological research, this paper proposes a systematic analysis framework covering the definition of comfort indicators, analysis of economy-related indicators, and analysis of the overall trade-off of indicators. Finally, by analysing the impact of different comfort indicators on weight, and thus on aircraft economy, the trade-offs between comfort and economy indicators are discussed, and a methodology for trade-offs in the design of future aircraft indicators is proposed.

Copyright
© 2024 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Download article (PDF)

Volume Title
Proceedings of the 2024 3rd International Conference on Information Economy, Data Modelling and Cloud Computing (ICIDC 2024)
Series
Advances in Computer Science Research
Publication Date
31 August 2024
ISBN
978-94-6463-504-1
ISSN
2352-538X
DOI
10.2991/978-94-6463-504-1_17How to use a DOI?
Copyright
© 2024 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Cite this article

TY  - CONF
AU  - Lu Bai
AU  - Jingze Hu
AU  - Xiuying Wang
AU  - Rong Cui
AU  - Dongyue Pan
AU  - Jian Tang
PY  - 2024
DA  - 2024/08/31
TI  - An Analytical Method for the Trade-off Between Comfort and Economy of Aircraft based on the Weight of Fuselage Structure
BT  - Proceedings of the 2024 3rd International Conference on Information Economy, Data Modelling and Cloud Computing (ICIDC 2024)
PB  - Atlantis Press
SP  - 165
EP  - 179
SN  - 2352-538X
UR  - https://doi.org/10.2991/978-94-6463-504-1_17
DO  - 10.2991/978-94-6463-504-1_17
ID  - Bai2024
ER  -