Detail publikace

Aplikace 3D tkanin na kompozitní konstrukci kluzáku.

JURAČKA, J.

Český název

Aplikace 3D tkanin na kompozitní konstrukci kluzáku.

Anglický název

3D Fabric Application on Glider Structures

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

en

Originální abstrakt

A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength and shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads.

Český abstrakt

Článek informuje o aplikaci 3D tkanin na kompozitní konstrukci kluzáku.

Anglický abstrakt

A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength and shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads.

Klíčová slova česky

parabeam, paraglass, pěna, 3D, smykové zkoušky, kompozitní materiál

Klíčová slova anglicky

parabeam, paraglass, form, 3D, share test, composite material

Rok RIV

2005

Vydáno

13.03.2005

Nakladatel

The Royal Aeronautical Society, Australia

Místo

Melbourne, Austálie

ISBN

0-85825-732-7

Kniha

CD-Rom of Congress proceedings

Počet stran

100

BIBTEX


@inproceedings{BUT16865,
  author="Jaroslav {Juračka},
  title="3D Fabric Application on Glider Structures",
  booktitle="CD-Rom of Congress proceedings",
  year="2005",
  month="March",
  publisher="The Royal Aeronautical Society, Australia",
  address="Melbourne, Austálie",
  isbn="0-85825-732-7"
}