Detail publikace

Aircraft engine crankshaft optimisation

VOPAŘIL, J. DRÁPAL, L. NOVOTNÝ, P.

Anglický název

Aircraft engine crankshaft optimisation

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

This article presents part of the crankshaft development of a two-stroke compression-ignition engine with contra-running pistons where, for invariably specified diameters and pin lengths, the optimal crankshaft shape is searched for. The process of creating several options which are then subjected to critical evaluation followed by the selection mechanism for the final best possible design is described. As the final step of the design process the resulting crankshaft shape is examined by calculation of fatigue life.

Klíčová slova anglicky

Crankshaft, topological optimisation, fatigue life.

Vydáno

2014-12-12

Nakladatel

ČVUT v Praze MECCA

Místo

Praha

ISSN

1214-0821

Ročník

XII

Číslo

1

Strany od–do

1–6

Počet stran

6

BIBTEX


@article{BUT112215,
  author="Jan {Vopařil} and Lubomír {Drápal} and Pavel {Novotný}",
  title="Aircraft engine crankshaft optimisation",
  journal="MECCA - Journal of Middle European Costruction and Design of Cars",
  year="2014",
  volume="XII",
  number="1",
  pages="1--6",
  issn="1214-0821"
}