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Hnací ústrojí šestiválcového leteckého motoru / Powertrain design of a six-cylinder aircraft engine

The purpose of this thesis is design of a six-cylinder engine arrangement with given main parameters (bore, stroke, etc.), powertrain design, possibilities of firing order, balancing inertia forces and its moments, in case of need, balancing shaft design and calculation of torsion vibrations.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:227900
Date January 2008
CreatorsDrápal, Lubomír
ContributorsNovotný, Pavel, Píštěk, Václav
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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