Thematische Bibliographien / Letadlový motor

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  1. Dissertationen

Auswahl der wissenschaftlichen Literatur zum Thema „Letadlový motor“

Autor: Grafiati
Veröffentlicht am 28. Juni 2021
Zuletzt aktualisiert am 3. Februar 2022

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Dissertationen zum Thema "Letadlový motor"

1

Kučera, Ondřej. „Čtyřválcový řadový zážehový letecký motor“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-444959.

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The thesis deals with the structural design of a steel connecting rod for the aircraft engine Walter Mikron III, which is currently still manufactured and developed by company PARMA-TECHNIK, s.r.o. The proposed connecting rod would replace the current duralumin connecting rod. The work also contains a strength analysis of the designed component, in which it was aimed to verify the stress on the connecting rod, based on which the fatigue safety factor was performed. This is crucial for dynamically stressed parts of internal combustion engines. Furthermore, was investigated the effect of the change of the connecting rod on the torsional vibration of the crank mechanism. For this purpose, was built a discrete torsion model. The output of the whole work is the drawing documentation of the new connecting rod, meeting the requirements for application in an aircraft engine.
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2

Donutil, Jan. „Zážehový pětiválcový hvězdicový letecký motor“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2019. http://www.nusl.cz/ntk/nusl-399287.

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This thesis deals with configuration of radial five-cylinder engine with attention to crank mechanism. Covered topics are motion of crank mechanism with articulated connecting rod, force analysis and balancing of inertial forces. The second part discusses FEM analysis and calculation of safety factor of selected component.
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3

Poledno, Martin. „Návrh letadlové energetické jednotky“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2010. http://www.nusl.cz/ntk/nusl-229010.

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This diploma thesis deals with basic design and calculation of an aircraft power unit (APU). For desired shaft power the thermal cycle is calculated. Basic dimensions of compressor, turbine and exhaust system are calculated as well as thermodynamic parameters of air and hot gases along the motor. Corresponding compressor map, turbine map and characteristics of the exhaust system are designed. Based on these characteristics, an effective shaft power is being calculated in various off-design conditions. Dependency of the shaft power vs. altitude is also presented. All the calculations are made in MATLAB. Finally, simplified motor cross-section is created.
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4

Valuch, Tomáš. „Okamžitá diagnostika stavu letadlových proudových motorů“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2016. http://www.nusl.cz/ntk/nusl-254322.

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In this diploma thesis is elaborated design of diagnostic system for small jet engines. The aim is to describe the types of possible failures of jet engines, to determine important parameters characterizing the immediate state of engine and define methods for measurement of selected parameters. The first part is devoted to a description of selected types of small turbojet engines, followed by a summary of the most widely used diagnostic methods for assessing the health condition of the engine during operation. The next chapter contains calculation of the engine thermal cycle with characteristics of construction components. Then there is analysis of small jet engine failures with a description of their causes and possibilities of identification by diagnostic system. Thesis continues with a description of measurement methods and selection of the required sensors. Next chapter is focused on the proposed diagnostic system for condition monitoring of the engine. The last part is devoted to an excursion in laboratory for jet engine testing at the Technical University in Košice.
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5

Korytář, Jan. „Aspekty ovlivňující trendy v technologii provozu letadlové techniky civilního letectví“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-443765.

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The aim of the work is a general description of the effects on air traffic and aircraft. The first part of the work is devoted to a brief description of the development of individual technical parameters and performance of aircraft from the 1920s to the present with an assessment of the effects. The second part of the work is about the influence of current requirements and the third part is a general view of the future development of construction and technology for more economical and environmentally friendly air transport
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6

Veselý, Jan. „Motorové oleje v letectví“. Master's thesis, Česká zemědělská univerzita v Praze, 2016. http://www.nusl.cz/ntk/nusl-257783.

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The aim of this thesis was to handle the problems of the literary tribodiagnostic, aviation oils using in piston engines and to provide analysis from taking oil samples from monitoring engines during working, evaluate it and recommend corection in maintanence service of these engines on based results typify as graphs. In chapter Analysis of the present state, there is described principle of working oil system in aviation engines including attributes of motor oils and demand requirements. The last part in this chapter is devoted to tribodiagnistic. In chapter Objective and methodology of thesis, there are described the machine on which the measurement was carried out and the methodology of individual tribodiagnostic analysis and sampling. Chapter Results contains the graphs based on the measured values including partial conclusion of the measurement and discussion.
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7

Formánek, Michael. „Regulátoru napětí palubní sítě letadel s motory WALTER M337“. Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2020. http://www.nusl.cz/ntk/nusl-413185.

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The work deals with the issue of the current solution of on-board network regulation in aircraft using Walter-made Czech engines, especially Walter M137 and M337. The work deals with the style of the currently used solution for operating the generator and the possibilities of its replacement using modern technologies. The design and production of the newly designed device follows. An essential part of the work is also the identification of the system of the original solution and the associated design of a new controller. The work compares the original and proposed solution in several defined points. The following text also includes the certification page of the proposal, financial evaluation and recommendations for further direction.
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8

Koštial, Rostislav. „Návrh zástavby vodíkové tlakové nádrže na křídlo letounu VUT 001 Marabu“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2010. http://www.nusl.cz/ntk/nusl-229318.

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The content of this Master thesis to design installation of hydrogen pressure tanks for airplane VUT RAY 051. Survey was conducted of the available fuel cell on the market. Position of the tank was chosen over the wing using components for mounting a jet engine TJ100 M for aircraft VUT 001 MARABU. For fuel tanks were designed fairings. Further was calculated mass and centre of gravity analysis of aircraft, basic flight performance of aircraft and the drag variation in the location of the tanks above the wing. Further the strain and strength of hinges was calculated.
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9

Bencalík, Karol. „Návrh úprav letounu VUT 001 MARABU s pohonem vodíkovými palivovými články a bateriemi“. Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2009. http://www.nusl.cz/ntk/nusl-374587.

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The main topic of this thesis is a design of VUT 001 airplane fuel transformation by means of fuel cells and storage batteries. A list of components available on the market was drawn up, their building in the airplane and the engineering design for mounting the electric motor into the structure. The thesis also includes the mass and centering analysis of flight performance and stability control.
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