Detail publikace

Aircraft engine crankshaft optimisation

VOPAŘIL, J. DRÁPAL, L. NOVOTNÝ, P.

Originální název

Aircraft engine crankshaft optimisation

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

Crankshaft, topological optimisation, fatigue life.

Autoři

VOPAŘIL, J.; DRÁPAL, L.; NOVOTNÝ, P.

Rok RIV

2014

Vydáno

12. 12. 2014

Nakladatel

ČVUT v Praze MECCA

Místo

Praha

ISSN

1214-0821

Periodikum

MECCA - Journal of Middle European Costruction and Design of Cars

Ročník

XII

Číslo

1

Stát

Česká republika

Strany od

1

Strany do

6

Strany počet

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"
}