Product detail

Crankshaft of Aircraft Two-cylinder Engine

DRÁPAL, L. NOVOTNÝ, P. PÍŠTĚK, V.

English title

Crankshaft of Aircraft Two-cylinder Engine

Type

Functioning sample

Language

en

Original abstract

This crankshaft is designed for a supercharged two-stroke compression-ignition opposed-piston aircraft engine. Crankshaft construction, therefore, largely reflects the requirements of high stiffness and low weight simultaneously. Semi-finished crankshaft is smith forging of material 32CrMo4. The final design is whole machined and there is used chemical-heat treatment of the exposed areas.

Keywords in English

crankshaft, two-cylinder engine, aircraft engine

Create date

2011-12-12

Location

Laboratoře C3 Ústavu automobilního a dopravního zařízení Fakulty strojního inženýrství Vysokého učení technického v Brně – Technická 2896/2, 616 69 Brno

BIBTEX


@misc{BUT75621,
  author="Lubomír {Drápal} and Pavel {Novotný} and Václav {Píštěk}",
  title="Crankshaft of Aircraft Two-cylinder Engine",
  year="2011",
  url="http://www.iae.fme.vutbr.cz/cs/system/files/2011_FV_Drapal_--_Klikovy_hridel_letadlovy.pdf",
  note="Functioning sample"
}