Return to search

Návrh klikového hřídele leteckého motoru / Crankshaft Design of Aircraft Engine

The main aim of this thesis is to design the cranckshaft for aircraft diesel engine with ordered basic parameters. The engine is flat with four-cylinder and opposed pistons. The thesis is focused on balancing of centrifugal and reciprocating forces and their moments, conceptual design of crankshaft and its stress calculation. The thesis is describing calculation of torsional vibrations as well.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229370
Date January 2010
CreatorsLuka, Jan
ContributorsPíštěk, Václav, Novotný, Pavel
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

Page generated in 0.2829 seconds