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Replica Design of L-40 "Meta Sokol " Airctaft - fuselage
Růžička, Miroslav ; Pešák, Miroslav (referee) ; Píštěk, Antonín (advisor)
This diploma thesis deals with the design of all-metal construction of fuselage of the replica L-40 Meta Sokol aircraft on the basis of CS-VLA regulation. As far as the aircraft is concerned, the thesis establishes the load of tail surfaces, landing gear and engine bed. Futhermore, it designs the construction of fuselage, tail landing gear, including the system of its retraction, wing-fuselage connection, engine bed and the primary design of cockpit. In the end, the thesis focuses on the fuselage production technology.
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Replica design of Aircraft "Meta Sokol" - Basic dimensions - technology
Lipková, Alica ; Šošovička, Róbert (referee) ; Píštěk, Antonín (advisor)
The object of the diploma thesis is a preparation of fundamentals for realization for replica of the aircraft L-40 „Meta Sokol“ matching the requirements of Certification Specification for Very Light Aeroplanes (CS-VLA). The preamble of the work deals with the changes made on the original aircraft necessary to satisfy the criterias of the above-mentioned specification. One of the main contents of the first part of the thesis is the definition of replica’s basic dimensions and preparation of aerostatic fundamentals, including longitudinal stability control. As next a suitable engine is chosen and calculation of corresponding performances is made. A detailed weight analysis and a determination of centre of gravity position (c.g. position), important for solving the stability of an airplane, is also presented. Finally, a brief description of the manufacturing process of individual components and also factors influencing the technology are discussed.
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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 single seat aiirplane by the UL - 2 regulation
Kövér, Ondřej ; Schoř, Pavel (referee) ; Píštěk, Antonín (advisor)
Bachelor´s thesis solves conceptual design of oneseater aircraft by the UL-2 regulations, that is up to 300 kilograms of take-off weight. In the first part of the thesis, there is survey of similar aircrafts and summary of their important characteristics. In further section are possible conceptions and the best choice of them outlined. Afterwards are characteristics of carrier surfaces, load calculation and flight envelope mentioned. The last part deals with calculation and design of engine mounting.
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The conception of wing arrangement on aircraft
Líška, Lukáš ; Janhuba, Luboš (referee) ; Píštěk, Antonín (advisor)
The subject of this bachelor thesis is the vertical alignment of wing at civil and military aircraft as well as the influence of this choice on aerodynamic, flight and operational characteristics. The aim is to show differences between technical, structural and operational requirements on each type of aircraft and the resulting options for wing placement. The summary of this paper are the advantages and disadvantages of low, mid and high wing airplanes following some examples from daily life.
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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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Aircraft design regulations
Seďa, Ondřej ; Pešák, Miroslav (referee) ; Píštěk, Antonín (advisor)
Baccalaureate work includes set of regulatins needs for aircraft construction. Out of printed are caregory qualification and using after european regulations CS, american regulations FAR and regulations for ultra-light aeroplanes. Mentioned are also regulations for operation and pilots training.
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