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Non-destructive inspection methods of aircraft selected parts
Kníř, Jakub ; Třetina, Karel (referee) ; Trefilová, Helena (advisor)
Non-destructive testing (NDT) is a broad scientific field. This bachelor thesis provides an insight into NDT’s methods. It can’t embrace the whole field in any case because it’s needed to have knowledge from variety of other scientific fields in order to understand NDT completely. This thesis outlines basic testing methods and their usage for particular components of aircrafts. The thesis also includes a list of Czech and European standards relevant to the topic.
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Aircraft Maintenance
Phung, Nhu Binh ; Třetina, Karel (referee) ; Finda, Jindřich (advisor)
This thesis is summarized knowledge the broblems and evaluation of current status in process plan in manitenance of small transport aircraft. State characteristics and applicability to non-destructive inspection methods in the maintenance of aircraft
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Aircraft Fuel Systems
Pergl, Kamil ; Bencalík, Karol (referee) ; Třetina, Karel (advisor)
Special literature related to aircraft fuel systems is usually separately divided into airframe fuel systems and engine fuel systems literature. Both systems have to work together, so airframe fuel system and engine fuel systems are joined together into one in this document. First part of this thesis describes aircraft fuel systems in general terms. There are shown primary structural parts and there are mentioned important fuel systems requirements. Also there are said some basic crew and maintenance steps. Second part of the thesis is more practical oriented. There is shown how great is the impact of the fuel on maximum takeoff weight. Also there is explained work of the real aircraft fuel system.
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Aircraft air-conditioning systems
Lednický, Ondřej ; Horák, Marek (referee) ; Třetina, Karel (advisor)
The bachelor thesis is focused on the aircraft air-conditioning systems, their functions and basic tasks needed for a safe and comfortable flight. The thesis is divided into several chapters: the first one deals with the most important factors influencing human health. Next chapter is focused on a description of the assurance of main components which are composing the aircraft air-conditioning system. Final chapter of the thesis deals with oxygen systems, which are essential for the survivor of the passengers in the case of an accident.
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Aircraft Hydraulic Systems
Puller, Tomáš ; Vaněk, František (referee) ; Třetina, Karel (advisor)
Work "Hydraulic system of aircraft" is focused on the issue of hydraulic transmission of forces to control the airplane. The first and second part summarizes the main characteristics of hydraulic systems and the basic physical properties of liquids.The third section describes various components of hydraulic systems and their characteristics. The fourth part contains a description and diagrams of different types of hydraulic circuits and the fifth part describes types of servocontrol systém of aircraft. In chapters 6 and 7 are descriptions of hydraulic systems of two Czech airplanes, L - 159 and L – 410. The next part contains statistical summary of power installations in small and medium-sized airplanes, and comparison of properties of different forms of transmission power. Finally, the evaluation of the statistical summary is carried out.
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Rocket Engine Design
Cejpek, Jakub ; Konečný,, Pavel (referee) ; Třetina, Karel (advisor)
The objective of this study is to design a solid rocket fuel engine with sufficient power to propel 500 grams to 1500 meters of altitude. Furthermore to draft a design of a rocket that will utilize this category of solid rocket fuel engine. This study will begin with a theoretical exploration of the means to formulate the correct propellant closest to the theoretical solid rocket fuel formula. This section of the exploration will exclude the construction materials, technology, and the propellant availability. After the theoretical exploration the calculations will continue, respecting the availability of construction materials, technology, and the propellant; to investigate the means to formulate the correct propellant closest to the theoretical formula. Then, according to the new propellant formulation, re-design the engine.
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