EN
A Study on Topology Optimization of Landing Gear Parts
Öz
In the aviation industry, one of the most complex industries in the world, the importance of low-weight design of aircraft is increasing day by day. While the requirements and related regulations regarding the efficient use of energy and minimizing environmental impacts are increasingly included in the legal framework, the importance of designing aircraft with low weight and therefore advantageous in terms of fuel consumption in the aviation sector, where competition is quite intense, is also increasing rapidly day by day. As a result of this situation, structural and parametric optimization, especially topology optimization studies, for the design of aircraft components with low weight, emerge as an indispensable element of design processes in the aviation industry. In this study, a Torque link and Trunnion landing gear parts were used. Firstly, the topology optimization study is performed as one conditional with separated two load cases. Afterward, the multi-conditional topology optimization is done with the aforementioned load cases. A weighted compliance parameter is generated to use in multi-conditional optimizations as a constraint or objective. While generating weighted compliance value, proportional weighted compliance (PWC) method is compared to the equal-effect weighted compliance (EEWC) method. With the EEWC method, on the torque link parts, 43% volume fraction is achieved and 34% volume fraction is obtained with the PWC method. Similar study has been done once again with landing gear Trunnion part and there were seen that the PWC method is a more effective approach in multi-conditional topology optimizations.
Anahtar Kelimeler
Kaynakça
- [1] N. Kaya and S. Yudar, “Hava taşıt kanallarında topoloji ve boyut optimizasyonu ile ağırlık azaltımı,” in Tusaş genç mühendisler semineri, Ankara, 2019.
- [2] Raicevic et al 2023. Fatigue life prediction of topologically optimized torque link adjusted for additive manufacturing. International Journal of Fatigue; volume 176, 107907.
- [3] G. L. Srinivas and A. Javed 2020. Topology optimization of rigid-links for industrial manipulator considering dynamic loading conditions. Mechanism and Machine Theory; 153: 1-16.
- [4] https://www.tennesseeaircraft.net/2012/11/10/1964-182-sid-survey-part-2/ (Accessed: 05.08.2024)
- [5] https://www.azom.com/article.aspx?ArticleID=9365 (Accessed: 01.08.2024)
- [6] https://www.safran-group.com/products-services/boeing-fa-18-nose-landing-gear (Accessed: 05.08.2024)
- [7] Infante et al 2017. Failure analysis of a nose landing gear fork. Engineering Failure Analysis; 82: 554-565.
- [8] Freitas et al 2019. Failure analysis of the nose landing gear axle of an aircraft. Engineering Failure Analysis; 101: 113-120.
Ayrıntılar
Birincil Dil
İngilizce
Konular
Matematikte Optimizasyon, Sayısal Analiz, Sonlu Elemanlar Analizi
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
27 Haziran 2025
Gönderilme Tarihi
26 Ağustos 2024
Kabul Tarihi
4 Aralık 2024
Yayımlandığı Sayı
Yıl 2025 Cilt: 21 Sayı: 2
APA
Piçak, S. C., Yahşi, M., & Gültekin, E. (2025). A Study on Topology Optimization of Landing Gear Parts. Celal Bayar University Journal of Science, 21(2), 35-46. https://doi.org/10.18466/cbayarfbe.1539030
AMA
1.Piçak SC, Yahşi M, Gültekin E. A Study on Topology Optimization of Landing Gear Parts. Celal Bayar University Journal of Science. 2025;21(2):35-46. doi:10.18466/cbayarfbe.1539030
Chicago
Piçak, Sait Cumhur, Mehmet Yahşi, ve Erol Gültekin. 2025. “A Study on Topology Optimization of Landing Gear Parts”. Celal Bayar University Journal of Science 21 (2): 35-46. https://doi.org/10.18466/cbayarfbe.1539030.
EndNote
Piçak SC, Yahşi M, Gültekin E (01 Haziran 2025) A Study on Topology Optimization of Landing Gear Parts. Celal Bayar University Journal of Science 21 2 35–46.
IEEE
[1]S. C. Piçak, M. Yahşi, ve E. Gültekin, “A Study on Topology Optimization of Landing Gear Parts”, Celal Bayar University Journal of Science, c. 21, sy 2, ss. 35–46, Haz. 2025, doi: 10.18466/cbayarfbe.1539030.
ISNAD
Piçak, Sait Cumhur - Yahşi, Mehmet - Gültekin, Erol. “A Study on Topology Optimization of Landing Gear Parts”. Celal Bayar University Journal of Science 21/2 (01 Haziran 2025): 35-46. https://doi.org/10.18466/cbayarfbe.1539030.
JAMA
1.Piçak SC, Yahşi M, Gültekin E. A Study on Topology Optimization of Landing Gear Parts. Celal Bayar University Journal of Science. 2025;21:35–46.
MLA
Piçak, Sait Cumhur, vd. “A Study on Topology Optimization of Landing Gear Parts”. Celal Bayar University Journal of Science, c. 21, sy 2, Haziran 2025, ss. 35-46, doi:10.18466/cbayarfbe.1539030.
Vancouver
1.Sait Cumhur Piçak, Mehmet Yahşi, Erol Gültekin. A Study on Topology Optimization of Landing Gear Parts. Celal Bayar University Journal of Science. 01 Haziran 2025;21(2):35-46. doi:10.18466/cbayarfbe.1539030
Cited By
STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS
Mühendislik Bilimleri ve Tasarım Dergisi
https://doi.org/10.21923/jesd.1828769