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Construction of ultralight aircraft control
Marek, Ondřej ; Šplíchal, Jan (referee) ; Juračka, Jaroslav (advisor)
This bachelor thesis deals with control of ultralight glider D-14. Based on the research of applied construction solutions of ultralight airplanes I designed my own solution of the specific elements and construction nodes. Also, in accordance with the UL-2 directive load of main control systems are determined. 3D model of the glider fuselage with the elements of the particular assemblies is attached.
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Motion control of an aileron
Kotrlý, Michal ; Kozubík, Michal (referee) ; Veselý, Libor (advisor)
This bachelor’s thesis aims to design, assemble and test an electromechanical model of an aileron with a dual actuator configuration that would verify used control algorithms. Mainly those that mitigate force fight between actuators and reduce mechanical stress affecting lifespan of the aileron. Algorithms are implemented in a PLC which supplies power to actuators/sensors and controls the position and movement of the aileron.
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Replica Design of L-40 "Meta Sokol " Aircraft - wing
Pluhař, Tomáš ; Jebáček, Ivo (referee) ; Píštěk, Antonín (advisor)
This diploma thesis targets in concept of wing, aileron, flap and main undercarriage of the ultralight replication of the plane L-40 called Meta Sokol. The thesis developed from cooperation with two other members of the team – Alice Lipková (aerodynamics, power) and Miroslav Růžička (fuselage, tail unit and rear gear). The first part of this diploma thesis is concerned with load and concept of structure of the wing. At first the flight envelope is specified, then charakteristics of shearing force, bending moment and torsion moment are determined spanwise. The concept and subsequent strength verification of structure of the wing is also solved. The same process is claimed to concept of the aileron and the flap. The second part of this diploma thesis is dealt with main landing gear, its support, structure, springing and the principle of retraction. The final passage is devoted to load of the undercarriage.
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Design of Aileron of Composite Materials
Dvořák, Vlastimil ; Klement, Josef (referee) ; Urík, Tomáš (advisor)
This diploma thesis called „Aileron Design of Composite Materials” deals with the technologies of production used in aricraft industries. It shows appropriate conceptions of composite structures for the airplane aileron of Aero L-159A/B as well as a proposal of an accetable structure for RTM process.
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Designe of a control system for powered sailplane SONG
Cejpek, Jakub ; Šplíchal, Jan (referee) ; Mališ, Michal (advisor)
The objective of this work is to adopt and further expand the type design of the SONG motor glider. The study will result in the basic aerodynamic calculation and the design of lateral control system including structural strength inspection of selected parts. Subsequently, the proposal will allow for further calculation to be made (of flight mechanics, wings strength or fuselage and empennage firmness) and for more specific constructional design of individual components of the glider.
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Construction parts and Elements of the of Large transport aircraft Wing structure
Malcová, Alica ; Vaněk, František (referee) ; Juračka, Jaroslav (advisor)
Wings are a complex aircraft structure and must meet various requirements, such as aerodynamic, strength and technological requirements. When designing the wings, great consideration is given to the structure and the materials used. This bachelor’s thesis focuses on the design of the wings of large transport aircraft and its execution. The individual parts of the structure are systematically arranged and explained. The work is divided into certain sections starting with the general requirements for the wing, followed by the choice of materials used, the internal structure, individual elements of the wing and structural hitch of the wing. At the end of the work, I point out the differences and similarities in the construction and materials used for the metal and composite wings. For a better understanding of the issue, the work is supplemented with pictures and a diagram. The appendix of the thesis is a presentation intended for educational purposes.
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Motion Control Of An Aileron
Kotrlý, Michal
This article covers a Bachelor’s thesis with an aim to design, assemble and test an electromechanical model of an aileron that would verify used control algorithms. Mainly those that mitigate force fight between actuators and reduce mechanical stress affecting lifespan of the aileron. Algorithms are implemented in a PLC which supplies power to actuators / sensors and controls the position and movement of the aileron.
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Motion control of an aileron
Kotrlý, Michal ; Kozubík, Michal (referee) ; Veselý, Libor (advisor)
This bachelor’s thesis aims to design, assemble and test an electromechanical model of an aileron with a dual actuator configuration that would verify used control algorithms. Mainly those that mitigate force fight between actuators and reduce mechanical stress affecting lifespan of the aileron. Algorithms are implemented in a PLC which supplies power to actuators/sensors and controls the position and movement of the aileron.
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Designe of a control system for powered sailplane SONG
Cejpek, Jakub ; Šplíchal, Jan (referee) ; Mališ, Michal (advisor)
The objective of this work is to adopt and further expand the type design of the SONG motor glider. The study will result in the basic aerodynamic calculation and the design of lateral control system including structural strength inspection of selected parts. Subsequently, the proposal will allow for further calculation to be made (of flight mechanics, wings strength or fuselage and empennage firmness) and for more specific constructional design of individual components of the glider.
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Design of Aileron of Composite Materials
Dvořák, Vlastimil ; Klement, Josef (referee) ; Urík, Tomáš (advisor)
This diploma thesis called „Aileron Design of Composite Materials” deals with the technologies of production used in aricraft industries. It shows appropriate conceptions of composite structures for the airplane aileron of Aero L-159A/B as well as a proposal of an accetable structure for RTM process.
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