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Letecký motor / Aircraft engine

This thesis is focused to design piston rods for aircraft petrol six-cylinder engine with 102 kW output power and project their form. Other part deals with analysis of balancing of arranging and fort control one of piston rod.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229648
Date January 2011
CreatorsKalugin, Ivan
ContributorsRamík, 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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