Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft

Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft

For this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufacturing scheme for low-curvature panels helped to...

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Bibliographic Details
Main Authors: Evgeny Dubovikov, Danil Fomin, Natalia Guseva, Ivan Kondakov, Evgeny Kruychkov, Ivan Mareskin, Alexander Shanygin
Format: Article
Language:English
Published: MDPI AG 2019-02-01
Series:Aerospace
Subjects:
manufacturing
low-curvature panels
pressurized fuselage
blended wing-body aircraft
Online Access:https://www.mdpi.com/2226-4310/6/2/18
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spelling doaj-8e008806931f4a8bb7e858f0b427b5352020-11-25T02:20:58ZengMDPI AGAerospace2226-43102019-02-01621810.3390/aerospace6020018aerospace6020018Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil AircraftEvgeny Dubovikov0Danil Fomin1Natalia Guseva2Ivan Kondakov3Evgeny Kruychkov4Ivan Mareskin5Alexander Shanygin6Central Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaCentral Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky St., Zhukovsky, Moscow Region 140180, RussiaFor this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufacturing scheme for low-curvature panels helped to achieve high strength characteristics of the composite details as well as decreased the labor input necessary for manufacturing and assembling. The beneficial features of the proposed structure are that the panels have a low weight, incur low manufacturing costs, and satisfy the demands of repairability.https://www.mdpi.com/2226-4310/6/2/18manufacturinglow-curvature panelspressurized fuselageblended wing-body aircraft
collection DOAJ
language English
format Article
sources DOAJ
author Evgeny Dubovikov
Danil Fomin
Natalia Guseva
Ivan Kondakov
Evgeny Kruychkov
Ivan Mareskin
Alexander Shanygin
spellingShingle Evgeny Dubovikov
Danil Fomin
Natalia Guseva
Ivan Kondakov
Evgeny Kruychkov
Ivan Mareskin
Alexander Shanygin
Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
Aerospace
manufacturing
low-curvature panels
pressurized fuselage
blended wing-body aircraft
author_facet Evgeny Dubovikov
Danil Fomin
Natalia Guseva
Ivan Kondakov
Evgeny Kruychkov
Ivan Mareskin
Alexander Shanygin
author_sort Evgeny Dubovikov
title Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
title_short Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
title_full Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
title_fullStr Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
title_full_unstemmed Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
title_sort manufacturing aspects of creating low-curvature panels for prospective civil aircraft
publisher MDPI AG
series Aerospace
issn 2226-4310
publishDate 2019-02-01
description For this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufacturing scheme for low-curvature panels helped to achieve high strength characteristics of the composite details as well as decreased the labor input necessary for manufacturing and assembling. The beneficial features of the proposed structure are that the panels have a low weight, incur low manufacturing costs, and satisfy the demands of repairability.
topic manufacturing
low-curvature panels
pressurized fuselage
blended wing-body aircraft
url https://www.mdpi.com/2226-4310/6/2/18
work_keys_str_mv AT evgenydubovikov manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT danilfomin manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT nataliaguseva manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT ivankondakov manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT evgenykruychkov manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT ivanmareskin manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
AT alexandershanygin manufacturingaspectsofcreatinglowcurvaturepanelsforprospectivecivilaircraft
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