Topology Optimization Study of Airplane Controls Console

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F26%3A00557995" target="_blank" >RIV/60162694:G43__/26:00557995 - isvavai.cz</a>

Výsledek na webu

<a href="https://ieeexplore.ieee.org/document/9746515" target="_blank" >https://ieeexplore.ieee.org/document/9746515</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/NTAD54074.2021.9746515" target="_blank" >10.1109/NTAD54074.2021.9746515</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Topology Optimization Study of Airplane Controls Console

Popis výsledku v původním jazyce

The article presents a study on topology optimization applied on an aluminium alloy airplane controls console to save the weight. The weight is one of the crucial factors of airplane structures affecting their efficiency, payload, performance, and costs. The article introduces to topology optimization as a SW tool to redistribute the part material yet enabling to carry the applied load. First, it is analysed the load acting on the console during airplane flight and ground operations as well. Next, the most crucial load is applied on the console under topology optimization procedure using the SW Ansys Workbench 2020. The differential influence of load cases is considered using the weight function reflecting the load occurrence. The optimized console shape is finally modified using the SW Autodesk Inventor to achieve the stiffness and strength of the origin console. Achieved reduction of the console weight is 11%. The final console shape is possible to produce using conventional or additive technologies. The article gives the recommendations for further development.

Název v anglickém jazyce

Topology Optimization Study of Airplane Controls Console

Popis výsledku anglicky

The article presents a study on topology optimization applied on an aluminium alloy airplane controls console to save the weight. The weight is one of the crucial factors of airplane structures affecting their efficiency, payload, performance, and costs. The article introduces to topology optimization as a SW tool to redistribute the part material yet enabling to carry the applied load. First, it is analysed the load acting on the console during airplane flight and ground operations as well. Next, the most crucial load is applied on the console under topology optimization procedure using the SW Ansys Workbench 2020. The differential influence of load cases is considered using the weight function reflecting the load occurrence. The optimized console shape is finally modified using the SW Autodesk Inventor to achieve the stiffness and strength of the origin console. Achieved reduction of the console weight is 11%. The final console shape is possible to produce using conventional or additive technologies. The article gives the recommendations for further development.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20304 - Aerospace engineering

Projekt

—

Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2021

Kód důvěrnosti údajů

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

Název statě ve sborníku

2021 New Trends in Aviation Development (NTAD)

ISBN

978-1-6654-1342-8

ISSN

—

e-ISSN

—

Počet stran výsledku

6

Strana od-do

53-58

Název nakladatele

IEEE

Místo vydání

Košice, Slovakia

Místo konání akce

Košice

Datum konání akce

25. 11. 2021

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

—