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Návrh úpravy letadla WT10 Advantic s pevným podvozkem dle předpisu CS-23 / Modification of the WT10 aircraft for the fixed landing gear according to the CS-23 requirements

In this thesis, we deal with the design of a shock absorber variant for the type of main landing gear design of the aircraft WT10 Advantic. Then we focus on the design of the selected variant of the main landing gear. Next, we follow regulation CS-23 demands to calculate the load cases for the selected main lending gear. Then we design shock absorber based on the load during landing. We compile the equation of motion of the aircraft, which describes motion of the aircraft during landing, then we compute the equation. Finally, we focus on a stress analysis of the main landing gear and the shock absorber.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:318135
Date January 2017
CreatorsKubiena, Jaromír
ContributorsJuračka, Jaroslav, Vaněk, František
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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