New types of materials in aircraft structure

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F17%3A00311605" target="_blank" >RIV/68407700:21260/17:00311605 - isvavai.cz</a>

Výsledek na webu

<a href="http://itpb.eu/index.php/ct-menu-item-3/14-engineering/424-12-cislo-1-clanok" target="_blank" >http://itpb.eu/index.php/ct-menu-item-3/14-engineering/424-12-cislo-1-clanok</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

New types of materials in aircraft structure

Popis výsledku v původním jazyce

Especially in aviation new trends push materials development and technologies forward and it is absolutely normal when half of aircraft construction is made by composite material. This kind of material is used in extreme conditions and can resist heavy loads. It is very light which is in aviation very important and needed. Main problem appears in setting save lifetime for this material or how to deal with damages during operations. This paper shows some kinds of degradation processes in materials such as delamination in composites used in construction aiming to special types of fibers. Increasing of costs in aircraft production despite efficiency improvements in technologies and manufacturing operations, can be attributed primarily to the increased use of more expensive materials and structural parts and assemblies. The tendency in aircraft production has been a growing use of high-cost composites, titanium parts and advanced materials to maximize weight efficiency. Aircraft composite material is in expanding usage continuously. Fiber reinforced composites find their utilization in the rapidly broadening field of applications. Some composite types can be considered as structural materials for usage at elevated temperatures. Ideally they should be lightweight, chemically and thermally stable, possessing good mechanical properties and cheap.

Název v anglickém jazyce

New types of materials in aircraft structure

Popis výsledku anglicky

Especially in aviation new trends push materials development and technologies forward and it is absolutely normal when half of aircraft construction is made by composite material. This kind of material is used in extreme conditions and can resist heavy loads. It is very light which is in aviation very important and needed. Main problem appears in setting save lifetime for this material or how to deal with damages during operations. This paper shows some kinds of degradation processes in materials such as delamination in composites used in construction aiming to special types of fibers. Increasing of costs in aircraft production despite efficiency improvements in technologies and manufacturing operations, can be attributed primarily to the increased use of more expensive materials and structural parts and assemblies. The tendency in aircraft production has been a growing use of high-cost composites, titanium parts and advanced materials to maximize weight efficiency. Aircraft composite material is in expanding usage continuously. Fiber reinforced composites find their utilization in the rapidly broadening field of applications. Some composite types can be considered as structural materials for usage at elevated temperatures. Ideally they should be lightweight, chemically and thermally stable, possessing good mechanical properties and cheap.

Druh

J_ost - Ostatní články v recenzovaných periodicích

CEP obor

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OECD FORD obor

20505 - Composites (including laminates, reinforced plastics, cermets, combined natural and synthetic fibre fabrics; filled composites)

Projekt

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2017

Kód důvěrnosti údajů

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

Název periodika

Interdisciplinarity in Theory and Practice

ISSN

2344-2409

e-ISSN

2344-2409

Svazek periodika

2017

Číslo periodika v rámci svazku

12

Stát vydavatele periodika

RO - Rumunsko

Počet stran výsledku

6

Strana od-do

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Kód UT WoS článku

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EID výsledku v databázi Scopus

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