Investigation of Mechanical Properties Achieved by Additive Manufacturing

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F21%3A00557440" target="_blank" >RIV/60162694:G43__/21:00557440 - isvavai.cz</a>

Výsledek na webu

<a href="http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=9502737" target="_blank" >http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=9502737</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/ICMT52455.2021.9502797" target="_blank" >10.1109/ICMT52455.2021.9502797</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Investigation of Mechanical Properties Achieved by Additive Manufacturing

Popis výsledku v původním jazyce

The development of additive manufacturing in the past decade greatly increased the applicability of such methods for manufacturing components, which would be otherwise expensive or impossible to manufacture by more conventional methods. Additive manufacturing is being slowly introduced even into the aviation industry, which requires rigorous testing of each component. The variety of production parameters, process defects and often complex design require even more component-specific testing. The paper presents a selected aircraft component, which has been manufactured and tested for bending strength under varying conditions. The results of the test were then compared to the FEM analysis of the selected component.

Název v anglickém jazyce

Investigation of Mechanical Properties Achieved by Additive Manufacturing

Popis výsledku anglicky

The development of additive manufacturing in the past decade greatly increased the applicability of such methods for manufacturing components, which would be otherwise expensive or impossible to manufacture by more conventional methods. Additive manufacturing is being slowly introduced even into the aviation industry, which requires rigorous testing of each component. The variety of production parameters, process defects and often complex design require even more component-specific testing. The paper presents a selected aircraft component, which has been manufactured and tested for bending strength under varying conditions. The results of the test were then compared to the FEM analysis of the selected component.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20301 - Mechanical engineering

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2021

Kód důvěrnosti údajů

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

Název statě ve sborníku

2021 8th International Conference on Military Technologies, ICMT 2021 - Proceedings

ISBN

978-1-6654-3724-0

ISSN

—

e-ISSN

—

Počet stran výsledku

5

Strana od-do

—

Název nakladatele

Institute of Electrical and Electronics Engineers Inc.

Místo vydání

Piscataway, USA

Místo konání akce

Brno, the Czech Republic

Datum konání akce

8. 6. 2021

Typ akce podle státní příslušnosti

CST - Celostátní akce

Kód UT WoS článku

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