Strength Calculation of UAV‘s Wing Connector Tube

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https://doi.org/10.52651/sam.a.2021.2.28-31

Autor: Eva POPARDOVSKÁ, Vladimír POPARDOVSKÝ, Lukáš NOVOTNÝ

In: Science & Military

ISSN: 2453-7632

Ročník: 16

Číslo: 2

Strany: 28 - 31

Rok vydania: 2021

Vydavateľ: Akadémia ozbrojených síl generála Milana Rastislava Štefánika, Liptovský Mikuláš

Abstrakt: The use of unmanned vehicles - both civilian and military - is clearly a technological trend today. It is reasonable to assume that this trend will continue in the future. Especially in the military field, an unmanned vehicle can be considered a benefit, especially in applications where the use of "standard" equipment is difficult or impossible. This is especially true of Unmanned Aerial Vehicle (UAV). The flight itself represents a number of different types of stress affecting the design of the unmanned aircraft. Therefore, the design of such a device must be subjected in the first step to a computational strength analysis and subsequently to a real stress test. Our paper deals with the strength analysis of the most exposed structural element - the wing connector. Proper sizing of the wing connector is therefore crucial for the successful operation of the UAV.

Kľúčové slová: UAV; Wing connector; Normal bending stress; Strength calculation.

Citácia:
POPARDOVSKÁ Eva, Vladimír POPARDOVSKÝ a Lukáš NOVOTNÝ. Strength Calculation of UAV‘s Wing Connector Tube. In: Science & Military [online]. Liptovský Mikuláš: Akadémia ozbrojených síl generála Milana Rastislava Štefánika, 2021, 16 (2), s. 28-31. ISSN: 1336-8885 (print). ISSN: 2453-7632 (online). Dostupné na internete: https://doi.org/10.52651/sam.a.2021.2.28-31