Gelişen teknolojiyle birlikte insansız hava araçları sivil ve askeri alanlarda çeşitli görevlerde yaygın şekilde kullanılmaya başlanmıştır. Özellikle afet yönetimi ve acil durumlarda, hayati öneme sahip ekipmanların hızlı ve güvenilir bir şekilde ulaştırılması çok önemlidir. Bu çalışma, acil durum ve afet yönetimi için optimize edilmiş bir gripper mekanizmalı hexacopter yapısındaki hava aracının tasarımı ve bu tasarımın statik analizine odaklanmaktadır. Hexacopter yapısındaki hava aracının tasarımında karbon fiber malzeme ve eklemeli imalat yöntemleri kullanılarak hem dayanıklı hem de maliyet etkin bir çözüm sunulmuştur. İnsansız hava aracına monte edilen gripper mekanizması ise, ilk yardım ekipmanları gibi yüklerin taşınması için tasarlanmış ve optimize edilmiştir. Bu makale, söz konusu tasarımın teorik temellerini, tasarım süreçlerini ve sonlu elemanlar metodu kullanılarak yapılan statik analizi ele almaktadır.
With the developing technology, unmanned aerial vehicles have been widely used in various missions in civil and military fields. Especially in disaster management and emergency situations, it is very important to deliver vital equipment quickly and reliably. This study focuses on the design and static analysis of a hexacopter shaped aerial vehicle with a gripper mechanism optimized for emergency and disaster management. In the design of the hexacopter shaped aerial vehicle, carbon fiber material and additive manufacturing methods are used to provide a durable and cost-effective solution. The gripper mechanism mounted on the unmanned aerial vehicle is designed and optimized for carrying loads such as first aid equipment. This article discusses the theoretical basis of the design, design processes and static analysis using the finite element method.
| Primary Language | Turkish |
|---|---|
| Subjects | Automation Engineering |
| Journal Section | Research Article |
| Authors | |
| Submission Date | February 14, 2025 |
| Acceptance Date | August 7, 2025 |
| Early Pub Date | December 11, 2025 |
| Publication Date | December 19, 2025 |
| Published in Issue | Year 2025 Volume: 30 Issue: 3 |
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