3D Fabric Application on Glider Structures

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F05%3APU48119" target="_blank" >RIV/00216305:26210/05:PU48119 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

3D Fabric Application on Glider Structures

Original language description

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 aand 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.

Czech name

Aplikace 3D tkanin na kompozitní konstrukci kluzáku.

Czech description

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 aand 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.

Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2005

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

CD-Rom of Congress proceedings

ISBN

0 85825-732-7

ISSN

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e-ISSN

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Number of pages

100

Pages from-to

1-100

Publisher name

The Royal Aeronautical Society, Australia

Place of publication

Melbourne, Austálie

Event location

Melbourne

Event date

Mar 13, 2005

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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