20.500.12556/DKUM-84296 Zasnova in izdelava aktivnega aerodinamičnega spojlerja diplomsko delo Design and production of the active aerodynamic spoiler V diplomski nalogi je opisana zasnova in izdelava aktivnega aerodinamičnega krila, v okviru česar so bili najprej raziskani in opisani osnovni fizikalni principi, ki so bili v nadaljevanju dokazani s simulacijo poteka zračnega pretoka skozi izdelan osnovni sklop krila in nosilca, ki sta bila v nadaljevanju ustrezno nadgrajena. Po izbiri ustreznih aktuatorjev za premik posameznih v nadaljevanju izdelanih komponent krila je sledil proces konstruiranja s pomočjo programskega paketa Solidworks, v okviru česar je bil najprej dovršen glavni nosilec krila, ki mu je sledila še nadgradnja osnovnega krila in izdelava ostalih potrebnih komponent. Vse zasnovane komponente so bile po dovršitvi 3D natisnjene. V naslednji fazi je sledila izbira vseh potrebnih elektrotehničnih komponent za omogočitev delovanja sistema nato pa je sledil zapis programov za krmiljenje sistema. V zadnjem delu je opisana sestava vseh izdelanih in naknadno izbranih komponent, predelava prtljažnih vrat in sestava krmilja. The diploma thesis describes the design and production of an active aerodynamic wing, in which the basic physical principles were first investigated and described, which were later proven by simulating the course of the air flow through the 3D constructed basic assembly of the wing and the wing carrier, which were further appropriately upgraded. After the selection of the appropriate actuators for the movement of the individual components of the wing, which were subsequently manufactured, the design process followed with the help of the Solidworks software package, in the framework of which the main wing support was first completed, followed by the upgrade of the basic wing and the manufacture of the other necessary components. All designed components were 3D printed after completion. In the next phase all of the necessary electrotechnical components to enable the system to function were selected, followed by the writing of the programs for controlling the system. In the last stage, the composition of all manufactured and subsequently selected components and the upgrading of the tailgate are described. Thesis is completed with the description of the control circuit build. aerodinamika konstruiranje 3D tiskanje programiranje sestava aerodynamics 3D modelling 3D printing programming assembling true true false [K. M. Reisman] Slovenski jezik Angleški jezik Diplomsko delo/naloga 2023-05-17 19:56:48 2023-10-05 13:40:21 2024-02-24 03:08:18 0000-00-00 00:00:00 2023 0 Maribor 0 Maribor 1 spletni vir (1 datoteka PDF (XIV, 74.)) 0000-00-00 NiDoloceno NiDoloceno NiDoloceno 0000-00-00 0000-00-00 0000-00-00 681.513.3:629.3.025.3(043.2) 186554115 VS_Reisman_Kristjan_Mihael_2023.pdf VS_Reisman_Kristjan_Mihael_2023.pdf 1 8DD0BA86CAB738482EC635F487C26E45 d4444e8a3b37669242f12c402587ca34c3932f2427efe2fe4bf9932935e186cc 03eb6bf1-4697-11ee-93d5-00155d000105 https://dk.um.si/Dokument.php?lang=slv&id=170792 Fakulteta za strojništvo 0 0 0