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Proposal of electro-hydraulic control system for the nose gear of small transport aircraft
Vodička, Petr ; Janhuba, Luboš (referee) ; Třetina, Karel (advisor)
The diploma thesis is focused on design of electrohydraulic system for nose gear control on small civil airliners. First part consists of brief review of small civil airliners, nose gears and CS 23 restrictions relevant for the design. In practical part a typical small civil airliner is defined and kinematic of landing gear mechanisms is designed. Then the electrohydraulic system itself is designed and parameters of some components are suggested. The wheel steering mechanism is simulated and, in conclusion, the whole system is evaluated.
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Design of VUT200 TwinCobra landing gear
Novák, Josef ; Horák, Marek (referee) ; Katrňák, Tomáš (advisor)
The goal of following master thesis is to design variety of configuration and retraction options of VUT200 TwinCobra landing gear. For each option are a wheel base and a gauge set up by possibility of main landing gear retraction. Next, CS 23 demands and stress analysis are followed. There is a view of twin engine aircraft landing gear disclosed as well.
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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 control system for the nose gear of small transport aircraft
Vodička, Petr ; Janhuba, Luboš (referee) ; Třetina, Karel (advisor)
The diploma thesis is focused on design of electrohydraulic system for nose gear control on small civil airliners. First part consists of brief review of small civil airliners, nose gears and CS 23 restrictions relevant for the design. In practical part a typical small civil airliner is defined and kinematic of landing gear mechanisms is designed. Then the electrohydraulic system itself is designed and parameters of some components are suggested. The wheel steering mechanism is simulated and, in conclusion, the whole system is evaluated.
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Design of VUT200 TwinCobra landing gear
Novák, Josef ; Horák, Marek (referee) ; Katrňák, Tomáš (advisor)
The goal of following master thesis is to design variety of configuration and retraction options of VUT200 TwinCobra landing gear. For each option are a wheel base and a gauge set up by possibility of main landing gear retraction. Next, CS 23 demands and stress analysis are followed. There is a view of twin engine aircraft landing gear disclosed as well.
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