The failure monitoring in laminate structures during loading

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F13%3APU103784" target="_blank" >RIV/00216305:26210/13:PU103784 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

The failure monitoring in laminate structures during loading

Popis výsledku v původním jazyce

Laminate structures are increasingly widespread and it is necessary to monitor the condition of the structure during static and fatigue tests. There are many NDT methods that can be used to detect the range of internal damage. Individual methods have their advantages, disadvantages and specific use. These methods include acoustic emissions. This method is not very widespread for testing laminate aircraft structures, thus providing space for finding the appropriate use and application of this method. Appropriate placement of sensors can monitor large areas and determines the method for application to test larger structures, such as fuselage sections or wing. A specific feature of this method is that it can detect only failures that occur during loading.Other failure such as manufacturing defects that occur in the structure cannot be located, until they are forced by external influence to spread.

Název v anglickém jazyce

The failure monitoring in laminate structures during loading

Popis výsledku anglicky

Laminate structures are increasingly widespread and it is necessary to monitor the condition of the structure during static and fatigue tests. There are many NDT methods that can be used to detect the range of internal damage. Individual methods have their advantages, disadvantages and specific use. These methods include acoustic emissions. This method is not very widespread for testing laminate aircraft structures, thus providing space for finding the appropriate use and application of this method. Appropriate placement of sensors can monitor large areas and determines the method for application to test larger structures, such as fuselage sections or wing. A specific feature of this method is that it can detect only failures that occur during loading.Other failure such as manufacturing defects that occur in the structure cannot be located, until they are forced by external influence to spread.

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/ED0002%2F01%2F01" target="_blank" >ED0002/01/01: NETME Centre (Nové technologie pro strojírenství)</a><br>

Návaznosti

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

Rok uplatnění

2013

Kód důvěrnosti údajů

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

Název statě ve sborníku

POLYMER COMPOSITES 2013

ISBN

978-80-261-0213-7

ISSN

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e-ISSN

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Počet stran výsledku

7

Strana od-do

1-7

Název nakladatele

Copydigital s.r.o.

Místo vydání

Plzeň

Místo konání akce

Plzeň

Datum konání akce

28. 5. 2013

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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