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National Repository of Grey Literature 3 records found  Search took 0.00 seconds. 
Modification of JA-400 aircraft landing gear
 Rakušan, Miroslav ; Vaněk, František (referee) ; Jebáček, Ivo (advisor)
The master‘s thesis is focused to design and to calculation of tailwheel-type landing gear for ultralight aircraft JA-400 according to rules UL 2 part I. – ULL and LTF UL. In the first part is search about aiplanes with three types of landing gear. Then there is rule comparison, with result what rule will the calculation meet. Then the concept and design of landing gear is proved. In the end the improve of lift option is mentioned.
Detailed record
Overview tail gear design solutions and their application in practice
 Zlámal, Zbyněk ; Dubnický, Lukáš (referee) ; Šplíchal, Miroslav (advisor)
This thesis deals with the characteristics of aircraft spur landing gears. Together with their geometrical arrangement, the elements of stability around individual axes during movement along the runway are discussed. For the destabilising elements acting on the aircraft, the causes of their occurrence and the factors by which they are influenced are analysed. The same analysis was performed on the elements which, on the other hand, promote stability. This is followed by an analysis of the evolution of the spur landing gear from the beginning of aviation to the present. It is also pointed out that experimental designs of landing gears were designed to increase the stability of the landing gear. Finally, the gained knowledge is applied to the landing gear of the selected aircraft with subsequent evaluation and suggesti-on of modifications that would positively affect its stability.
Detailed record
Modification of JA-400 aircraft landing gear
 Rakušan, Miroslav ; Vaněk, František (referee) ; Jebáček, Ivo (advisor)
The master‘s thesis is focused to design and to calculation of tailwheel-type landing gear for ultralight aircraft JA-400 according to rules UL 2 part I. – ULL and LTF UL. In the first part is search about aiplanes with three types of landing gear. Then there is rule comparison, with result what rule will the calculation meet. Then the concept and design of landing gear is proved. In the end the improve of lift option is mentioned.
Detailed record

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