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Design of Wing and Landing gear for TST 14 MC Glider
Štěpánek, Jan ; Šošovička, Róbert (referee) ; Juračka, Jaroslav (advisor)
Modification of TST-14 MC glider, calculation of flight envelope, distribution of lift on the wing, calculation of loading cases of the wing, strength check of choosen construction nodes, design of the landing gear retraction mechanism, setting up loading of landing gear according to ULKM, strength check of landing gear
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Proposal of electro-hydraulic system of main landing gear actuatuon for small training aeroplane
Skřivánek, Jan ; Bencalík, Karol (referee) ; Třetina, Karel (advisor)
This thesis studies the design of an electro-hydraulic landing gear and brakes control system of a trainer aeroplane. In the first part there is a basic draft of the landing gear kinematics and its loads during gear retraction, flight and landing. Braking conditions are also analysed. The thesis then focuses on the design of hydraulic circuits and their control. Simulations for studying the dynamic characteristics of the braking proportional valve and the course of plane braking were created in Simulink. There is also a brief section about reliability of the proposed system.
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Hi-wing aircraft landing gear design
Skutil, Marek ; Vaněk, František (referee) ; Jebáček, Ivo (advisor)
This diploma thesis deals with the design of the main retractable landing gear for a small high-wing aircraft. In the thesis there is made a kinematic solution of the main landing gear retraction, it’s conceptual and structural design and also selection of relevant components. Then there are performed landing gear load calculations according to the relevant regulation as well as representation of the main landing gear leg loads based on the strength analysis created in the Autodesk Inventor program. One part of the thesis is also 3D model of the main landing gear assembly.
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Hi-wing aircraft landing gear design
Skutil, Marek ; Vaněk, František (referee) ; Jebáček, Ivo (advisor)
This diploma thesis deals with the design of the main retractable landing gear for a small high-wing aircraft. In the thesis there is made a kinematic solution of the main landing gear retraction, it’s conceptual and structural design and also selection of relevant components. Then there are performed landing gear load calculations according to the relevant regulation as well as representation of the main landing gear leg loads based on the strength analysis created in the Autodesk Inventor program. One part of the thesis is also 3D model of the main landing gear assembly.
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Proposal of electro-hydraulic system of main landing gear actuatuon for small training aeroplane
Skřivánek, Jan ; Bencalík, Karol (referee) ; Třetina, Karel (advisor)
This thesis studies the design of an electro-hydraulic landing gear and brakes control system of a trainer aeroplane. In the first part there is a basic draft of the landing gear kinematics and its loads during gear retraction, flight and landing. Braking conditions are also analysed. The thesis then focuses on the design of hydraulic circuits and their control. Simulations for studying the dynamic characteristics of the braking proportional valve and the course of plane braking were created in Simulink. There is also a brief section about reliability of the proposed system.
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Design of Wing and Landing gear for TST 14 MC Glider
Štěpánek, Jan ; Šošovička, Róbert (referee) ; Juračka, Jaroslav (advisor)
Modification of TST-14 MC glider, calculation of flight envelope, distribution of lift on the wing, calculation of loading cases of the wing, strength check of choosen construction nodes, design of the landing gear retraction mechanism, setting up loading of landing gear according to ULKM, strength check of landing gear
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