Static Analysis of Main Body Parts Designed Using Carbon Fiber Material for Hexacopter Structure Drone

Year 2024, Volume: 14 Issue: 4, 1758 - 1781, 15.12.2024

Muhammet Aydın Metin , Kenan Şentürk

https://doi.org/10.31466/kfbd.1474166

Cited By: 1

https://izlik.org/JA35XF69GK

Abstract

Drones, which entered our lives with the development of technology, are used in many areas that make our lives easier today. It is seen the effect of drones in photography, cargo transportation, mapping, defense industry, and agricultural sectors. In order for the drones used in these areas to fulfil the desired task, the mechanical and static structure of the drone is of great importance along with the software and electronic cards used. It is possible to perform the desired task in a mechanically stable and optimized air vehicle with integrated payloads. In particular, most of the electronic equipment and payloads of the drone are integrated on the parts that make up the body. For this reason, it is inevitable to examine the effect of both equipment and payloads on whether the drone can perform the desired task or not. In this study, the static analysis of the parts made of carbon fiber material forming the construction of the body of the uniquely designed drone is carried out. These analyses were performed in terms of the total deformation, the strain, and the stress with different mesh structures such as multizone, tetrahedrons, and hex dominant method mesh were performed on the body parts. The results obtained indicated that the body parts of the uniquely designed drone presented in this study can be produced by using carbon fiber materials and they will be suitable for different missions.

Keywords

Drone body , Stability , Carbon fiber material , Static analysis , Meshes

Hexacopter Yapısındaki Drone için Karbon Fiber Malzeme Kullanılarak Tasarlanan Ana Gövde Parçalarının Statik Analizi

https://izlik.org/JA35XF69GK

Abstract

Teknolojinin gelişmesiyle birlikte hayatımıza giren drone'lar, günümüzde hayatımızı kolaylaştıran birçok alanda kullanılıyor. Fotoğrafçılık, kargo taşımacılığı, haritalama, savunma sanayi ve tarım sektörlerinde droneların etkisi görülmektedir. Bu alanlarda kullanılan drone'ların istenilen görevi yerine getirebilmesi için kullanılan yazılım ve elektronik kartlarla birlikte drone'un mekanik ve statik yapısı da büyük önem taşıyor. Mekanik olarak stabil ve optimize edilmiş bir hava aracında entegre faydalı yükler ile istenilen görevin gerçekleştirilmesi mümkündür. Özellikle drone'un elektronik ekipmanlarının ve faydalı yüklerinin büyük bir kısmı gövdeyi oluşturan parçaların üzerine entegre edilmektedir. Bu nedenle hem ekipmanların hem de faydalı yüklerin drone'un istenilen görevi yerine getirip getiremeyeceği üzerindeki etkisinin incelenmesi kaçınılmazdır. Bu çalışmada, özgün tasarımlı drone'un gövde konstrüksiyonunu oluşturan karbon fiber malzemeden yapılmış parçaların statik analizi yapılmıştır. Bu analizler toplam deformasyon, şekil değiştirme ve gerilme açısından çok bölgeli, tetrahedron ve altıgen baskın yöntem ağ yapısı gibi farklı ağ yapılarıyla gövde parçaları üzerinde gerçekleştirilmiştir. Elde edilen sonuçlar, bu çalışmada sunulan özgün tasarımlı drone'un gövde parçalarının karbon fiber malzemeler kullanılarak üretilebileceğini ve farklı görevlere uygun olacağını gösterdi.

Keywords

Drone gövdesi , Stabilite , Karbon fiber malzeme , Statik analiz , Ağ örgüsü

Ethical Statement

Makale içinde sunduğum verileri, bilgileri ve dokümanları akademik ve etik kurallar çerçevesinde elde ettiğimi, • Tüm bilgi, belge, değerlendirme ve sonuçları bilimsel etik ve ahlak kurallarına uygun olarak sunduğumu, • Bu çalışmada yararlandığım eserlerin tümüne uygun atıfta bulunarak kaynak gösterdiğimi, • Kullanılan verilerde herhangi bir değişiklik yapmadığımı, • Bu çalışmada sunduğum çalışmanın özgün olduğunu, bildirir, aksi bir durumda aleyhime doğabilecek tüm hak kayıplarını kabullendiğimi beyan ederim.

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