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Design of Trainer Aircraft with Tandem Seats
Dycka, Jan ; Urík, Tomáš (referee) ; Juračka, Jaroslav (advisor)
The diploma thesis deals with the project of composite constuction of aeroplane VUT 001 Marabu and its FEM stress-deformation analysis. The project of pilt´s cockpit is solved in the light of basic ergonomic requirements. Mass analysis, calculation and resulting selection of conclusive events of load are parts of the work. The results are applied on FEM model of fuselage and the state of stress in individual sections of composite structure are determined by the MSC Patran/Nastran system.
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Structural design of fuselage and tail for racing model
Skála, Adam ; Hájek, Tomáš (referee) ; Pejchar, Jan (advisor)
This bachelor’s thesis surveys fuselage and empennage improvement of an already existing competition aircraft FabricK. Firstly, the introductory part explains the Air Cargo Challenge contest and describes the model. A research then presents possible empennage designs, which is followed by a brief overview of production F3B aircraft. The practical part of thesis introduces construction project of the empennage and the fuselage as well as a weight distribution analysis. Finally, the concluding part will evaluate the imporvement.
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History of Civil Aviation 1970-2000
Zubrvalčík, Jan ; Šplíchal, Miroslav (referee) ; Chlebek, Jiří (advisor)
The main aim of this bachelor‘s thesis is utilize consice summary of history of civil aviation between year 1970 to 2000 and compare their performance. This era is typical with out-set of airplanes with large capacity and new construction solutions. This thesis is focused on planes for long distance with large capacity, but also on planes for middle and short distances too. Thesis is divided by range of airplanes and special charter is about supersonic civil planes.
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Fuselage and control system design of VUT 081 Kondor
Kalný, Jan ; Šplíchal, Jan (referee) ; Mališ, Michal (advisor)
This master’s thesis deals with VUT 081 Kondor composite fuselage design and control system layout design. Load computation and selection of critical load cases are made. Principal inner surfaces of the fuselage are designed with respect to basic ergonomic requirements of the crew. Construction materials are chosen and a layup of composite materials is performed. Fuselage FEM model is made in MSC Patran/Nastran system and the structure-strength analysis is given for chosen load cases.
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Construction parts and Elements of the of Large transport aircraft Fuselage structure
Zubaľ, Filip ; Dubnický, Lukáš (referee) ; Juračka, Jaroslav (advisor)
Fuselage design is an area of aerospace engineering that combines aerodynamics with mechanical and material engineering. Many factors affect the construction and design of the fuselage. The bachelor thesis is focused on the processing and systematic ordering of individual structural units used in large transport aircraft. It points out the diversity of individual structural nodes in the design of the aircraft. The work is divided according to sections of the fuselage, where the specific design solutions for the node are then discussed. At the end of the work, I present a comparison of the two most famous competing aircraft models of Airbus and Boeing company. I pointed out the individual combinations of structural elements. Compared data are processed using tables and schematic figures. The bachelor thesis was also translated into a form of presentation intended for educational purposes.
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Fusalage and Tail of Competition Model Airplane
Kminiaková, Tatiana ; Hájek, Tomáš (referee) ; Janhuba, Luboš (advisor)
This bachelor’s thesis deals with empennage and fuselage design of new aircraft for design competition SAE Aero Design East 2020. The introduction is focused on regulations of this competiton and their subsequent analysis. The research part of the thesis takes in consideration possible configurations of the empennage and fuselage and their basic parameters. The most suitable configurations are compared and basic stability and load calculations are done. In the last part structural design is completed.
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Design of competition model fuselage
Bednář, Peter ; Löffelmann, František (referee) ; Hájek, Tomáš (advisor)
This bachelor’s thesis deals with the design of the fuselage of the competing model aircraft. The introduction describes the student team, Chicken Wings, and also explains the upcoming Air Cargo Challenge 2019. Furthermore, the search section lists the individual types of materials and carbon composite manufacturing technologies. The second part of the thesis deals with the individual phases of the aircraft design and the definition of fuselage. Moreover, the practical part of the thesis begins with a statistical overview of mass-produced models F3B and F5J categories and the subsequent design of the individual parts of the fuselage and the mass analysis of the model. The conclusion justifies the choice of individual parameters.
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History of Civil Aviation 1970-2000
Zubrvalčík, Jan ; Šplíchal, Miroslav (referee) ; Chlebek, Jiří (advisor)
The main aim of this bachelor‘s thesis is utilize consice summary of history of civil aviation between year 1970 to 2000 and compare their performance. This era is typical with out-set of airplanes with large capacity and new construction solutions. This thesis is focused on planes for long distance with large capacity, but also on planes for middle and short distances too. Thesis is divided by range of airplanes and special charter is about supersonic civil planes.
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