Experimental Panel of Pressurized Passenger Door of New Design Conception
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F22%3AN0000030" target="_blank" >RIV/00010669:_____/22:N0000030 - isvavai.cz</a>
Výsledek na webu
<a href="http://www.ithec.de" target="_blank" >http://www.ithec.de</a>
DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Experimental Panel of Pressurized Passenger Door of New Design Conception
Popis výsledku v původním jazyce
The reinforced thermoplastic gives chance to achieve lower labor costs of the composite passenger door of the aircraft. The paper describes the new design conception with the variable shape of stiffeners, which enables to reduce of manufacturing costs. The goal of the work was to confirm the new architecture and sizing of the PAX door. The intention was to design the composite parts with a maximal level of integration to minimize the number of pieces in assembly. So that the shapes of parts are on the edge of thermoforming feasibility. All ones are manufactured by thermoforming excluding the skin. The biggest innovation is the design of the Omega beam, which provides optimal bending stiffness according to bending moment along of span and effective introduction of reaction forces on the ends of the beam. Numerical simulations of FEM were used to determine the load of the real structure, optimize the design of critical parts, and define representative load distribution into the newly designed door panel. The panel was impacted in the specified points and subsequently tested under static and fatigue mechanical loading with non-destructive inspection, deformation, and strain measurements, and residual static strength evaluation.
Název v anglickém jazyce
Experimental Panel of Pressurized Passenger Door of New Design Conception
Popis výsledku anglicky
The reinforced thermoplastic gives chance to achieve lower labor costs of the composite passenger door of the aircraft. The paper describes the new design conception with the variable shape of stiffeners, which enables to reduce of manufacturing costs. The goal of the work was to confirm the new architecture and sizing of the PAX door. The intention was to design the composite parts with a maximal level of integration to minimize the number of pieces in assembly. So that the shapes of parts are on the edge of thermoforming feasibility. All ones are manufactured by thermoforming excluding the skin. The biggest innovation is the design of the Omega beam, which provides optimal bending stiffness according to bending moment along of span and effective introduction of reaction forces on the ends of the beam. Numerical simulations of FEM were used to determine the load of the real structure, optimize the design of critical parts, and define representative load distribution into the newly designed door panel. The panel was impacted in the specified points and subsequently tested under static and fatigue mechanical loading with non-destructive inspection, deformation, and strain measurements, and residual static strength evaluation.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
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OECD FORD obor
20304 - Aerospace engineering
Návaznosti výsledku
Projekt
<a href="/cs/project/FV30033" target="_blank" >FV30033: Konstrukční a technologický vývoj primárních leteckých dílů pokročilých tvarů z kompozitu s termoplastovou matricí</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2022
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
ITHEC ‐ 6th International Conference & Exhibition on Thermoplastic Composites
ISBN
9783933339331
ISSN
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e-ISSN
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Počet stran výsledku
3
Strana od-do
185-187
Název nakladatele
Congress Bremen & Mess Bremen, M3B GmbH, Bremen, Germany
Místo vydání
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Místo konání akce
Bremen
Datum konání akce
12. 10. 2022
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
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