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Ballistic rescue system installation into a light sports aircraft
Gebrlín, Jakub ; Sklenář, Jiří (oponent) ; Horák, Marek (vedoucí práce)
The aim of this diploma thesis is to design the installation of a parachute system in a small sport aircraft. The individual steps of the thesis are chronologically classify in the order in which they were approached. The introductory part of the thesis describes the main parameters of the parachute rescue system and the aircraft which the rescue system is designed for. Next, the German LTF-UL regulation and related regulations are discussed in detail, from which all calculation procedures are subsequently derived. In the second part, the thesis deals with the calculation of the dynamic force load of the aircraft structure and the adjustment of individual parts of the structure. At the end of the work, a method of testing is proposed.
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Design of a landing gear of an airplane competition kit
Gebrlín, Jakub ; Katrňák, Tomáš (oponent) ; Bartoněk, Jaroslav (vedoucí práce)
The purpose of this bachelor thesis is to design a landing gear for a competition model of aircraft. The introductory part of this work is focused mainly on study about landing gears and their comparison in terms of advantages and disadvantages for the new competition model both in terms of arrangement and in terms of sliding or fixed chassis. In the second, the practical part the work is focused on computation of load, the strength calculation and the design of chassis.
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Ballistic rescue system installation into a light sports aircraft
Gebrlín, Jakub ; Sklenář, Jiří (oponent) ; Horák, Marek (vedoucí práce)
The aim of this diploma thesis is to design the installation of a parachute system in a small sport aircraft. The individual steps of the thesis are chronologically classify in the order in which they were approached. The introductory part of the thesis describes the main parameters of the parachute rescue system and the aircraft which the rescue system is designed for. Next, the German LTF-UL regulation and related regulations are discussed in detail, from which all calculation procedures are subsequently derived. In the second part, the thesis deals with the calculation of the dynamic force load of the aircraft structure and the adjustment of individual parts of the structure. At the end of the work, a method of testing is proposed.
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Design of a landing gear of an airplane competition kit
Gebrlín, Jakub ; Katrňák, Tomáš (oponent) ; Bartoněk, Jaroslav (vedoucí práce)
The purpose of this bachelor thesis is to design a landing gear for a competition model of aircraft. The introductory part of this work is focused mainly on study about landing gears and their comparison in terms of advantages and disadvantages for the new competition model both in terms of arrangement and in terms of sliding or fixed chassis. In the second, the practical part the work is focused on computation of load, the strength calculation and the design of chassis.
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