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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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The conception of tail unit arrangement on aircraft
Podhorský, Matěj ; Pejchar, Jan (referee) ; Píštěk, Antonín (advisor)
This bachelor thesis provides a basic overview of empennage layout designs. It contains a theoretical introduction explaining terms necessary to understand the empennage problematics. In the main part, the most frequent empennage layout designs are described, each one with a brief description of construction, its benefits and drawbacks and airplanes with such empennage layout design.
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Tail units design of VUT 100 aircraft made out composite
Berka, Martin ; Cejpek, Jakub (referee) ; Mališ, Michal (advisor)
This Master´s thesis describes the design of composite horizontal tail of VUT 100 aircraft. Load calculation and selection of the critical load cases is performed. Internal structure of stabilizer and right elevator is designed. Construction materials are chosen and the structure of the composite materials is proposed. FEM models of stabilizer and the right elevator are created in MSC Patran system and consequently the strength test of the models for the selected load cases is executed using MSC Nastran software and COMPOST.
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Tail units design of VUT 100 aircraft made out composite
Berka, Martin ; Cejpek, Jakub (referee) ; Mališ, Michal (advisor)
This Master´s thesis describes the design of composite horizontal tail of VUT 100 aircraft. Load calculation and selection of the critical load cases is performed. Internal structure of stabilizer and right elevator is designed. Construction materials are chosen and the structure of the composite materials is proposed. FEM models of stabilizer and the right elevator are created in MSC Patran system and consequently the strength test of the models for the selected load cases is executed using MSC Nastran software and COMPOST.
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|
|
The conception of tail unit arrangement on aircraft
Podhorský, Matěj ; Pejchar, Jan (referee) ; Píštěk, Antonín (advisor)
This bachelor thesis provides a basic overview of empennage layout designs. It contains a theoretical introduction explaining terms necessary to understand the empennage problematics. In the main part, the most frequent empennage layout designs are described, each one with a brief description of construction, its benefits and drawbacks and airplanes with such empennage layout design.
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|
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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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