Detail publikace

THE CFRP SAILPLANE WING SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT

MALIŠ, M. URÍK, T.

Originální název

THE CFRP SAILPLANE WING SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The application of filament placement technology on sailplane wing is discussed in the paper. Two structure designs, based on high speed CNC milling foam core mandrels, are compared. Performed finite element and real experiments shows that used low cost foam mandrel has some limitations when it is used in wing structure. On the other side automation of sailplane wing manufacturing can offer reasonable benefits.

Klíčová slova

wing, filament winding, sailplane

Autoři

MALIŠ, M.; URÍK, T.

Rok RIV

2012

Vydáno

23. 9. 2012

ISBN

978-0-9565333-1-9

Kniha

28TH CONGRESS OF THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES

Edice

ICAS 2012 PROCEEDINGS

Číslo edice

1

Strany od

1

Strany do

7

Strany počet

7

BibTex

@inproceedings{BUT95582,
  author="Michal {Mališ} and Tomáš {Urík}",
  title="THE CFRP SAILPLANE WING SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT",
  booktitle="28TH CONGRESS OF THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES",
  year="2012",
  series="ICAS 2012 PROCEEDINGS",
  number="1",
  pages="1--7",
  isbn="978-0-9565333-1-9"
}