Devising a concept of integrated design and modeling of aircraft

The analysis of aircraft design methods reported here has revealed that building a competitive aircraft necessitates devising a scientifically based concept of integrated aircraft design employing CAD/CAM/CAE/PLM software suites. A generalized concept of integrated design and three-dimensional com...

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Autores principales:	Oleksandr Grebenikov, Andrii Humennyi, Oleksandr Dveirin, Oleksandr Soboliev, Lilia Buival
Formato:	article
Lenguaje:	EN RU UK
Publicado:	PC Technology Center 2021
Materias:	integrated aircraft design master geometry concept three-dimensional parametric modeling takeoff mass Technology (General) T1-995 Industry HD2321-4730.9
Acceso en línea:	https://doaj.org/article/ff97ff874f404951b55d39dd9d216624
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id	oai:doaj.org-article:ff97ff874f404951b55d39dd9d216624
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spelling	oai:doaj.org-article:ff97ff874f404951b55d39dd9d2166242021-11-04T14:05:20ZDevising a concept of integrated design and modeling of aircraft1729-37741729-406110.15587/1729-4061.2021.240108https://doaj.org/article/ff97ff874f404951b55d39dd9d2166242021-10-01T00:00:00Zhttp://journals.uran.ua/eejet/article/view/240108https://doaj.org/toc/1729-3774https://doaj.org/toc/1729-4061The analysis of aircraft design methods reported here has revealed that building a competitive aircraft necessitates devising a scientifically based concept of integrated aircraft design employing CAD/CAM/CAE/PLM software suites. A generalized concept of integrated design and three-dimensional computer modeling of aircraft involving the CAD/CAM/CAE/PLM systems has been developed. Based on the proposed concept, the principles of integrated design of aircraft were devised. The features of designing the training and training-combat aircraft, transport-category aircraft, light civilian aircraft have been described. A method for determining the take-off weight, design parameters, and formation of the general appearance of aircraft has been improved. The method is intended to form the appearance of the aircraft at the stages of preliminary design, the purpose of which is reduced to determining the permissible version of the aircraft project. The project must meet the predefined requirements and restrictions in the selected aircraft scheme and the assigned set of parameters that characterize its airframe and power plant. A method of parametric modeling of aircraft has been improved, which includes the stages of creating a master geometry of the aircraft and a model of space distribution. Parametric models of master geometry and models of space distribution, training and training-combat aircraft, transport-category aircraft, light civilian aircraft have been constructed. Methods of integrated design of aircraft main units have been devised and theoretically substantiated. Parametric models of master geometry of the wing for a training aircraft, the wings, appendage, and fuselage of a light civilian aircraft were built, taking into consideration the design features of aircraft units of various categoriesOleksandr GrebenikovAndrii HumennyiOleksandr DveirinOleksandr SobolievLilia BuivalPC Technology Centerarticleintegrated aircraft designmaster geometryconceptthree-dimensional parametric modelingtakeoff massTechnology (General)T1-995IndustryHD2321-4730.9ENRUUKEastern-European Journal of Enterprise Technologies, Vol 5, Iss 1(113), Pp 15-23 (2021)
institution	DOAJ
collection	DOAJ
language	EN RU UK
topic	integrated aircraft design master geometry concept three-dimensional parametric modeling takeoff mass Technology (General) T1-995 Industry HD2321-4730.9
spellingShingle	integrated aircraft design master geometry concept three-dimensional parametric modeling takeoff mass Technology (General) T1-995 Industry HD2321-4730.9 Oleksandr Grebenikov Andrii Humennyi Oleksandr Dveirin Oleksandr Soboliev Lilia Buival Devising a concept of integrated design and modeling of aircraft
description	The analysis of aircraft design methods reported here has revealed that building a competitive aircraft necessitates devising a scientifically based concept of integrated aircraft design employing CAD/CAM/CAE/PLM software suites. A generalized concept of integrated design and three-dimensional computer modeling of aircraft involving the CAD/CAM/CAE/PLM systems has been developed. Based on the proposed concept, the principles of integrated design of aircraft were devised. The features of designing the training and training-combat aircraft, transport-category aircraft, light civilian aircraft have been described. A method for determining the take-off weight, design parameters, and formation of the general appearance of aircraft has been improved. The method is intended to form the appearance of the aircraft at the stages of preliminary design, the purpose of which is reduced to determining the permissible version of the aircraft project. The project must meet the predefined requirements and restrictions in the selected aircraft scheme and the assigned set of parameters that characterize its airframe and power plant. A method of parametric modeling of aircraft has been improved, which includes the stages of creating a master geometry of the aircraft and a model of space distribution. Parametric models of master geometry and models of space distribution, training and training-combat aircraft, transport-category aircraft, light civilian aircraft have been constructed. Methods of integrated design of aircraft main units have been devised and theoretically substantiated. Parametric models of master geometry of the wing for a training aircraft, the wings, appendage, and fuselage of a light civilian aircraft were built, taking into consideration the design features of aircraft units of various categories
format	article
author	Oleksandr Grebenikov Andrii Humennyi Oleksandr Dveirin Oleksandr Soboliev Lilia Buival
author_facet	Oleksandr Grebenikov Andrii Humennyi Oleksandr Dveirin Oleksandr Soboliev Lilia Buival
author_sort	Oleksandr Grebenikov
title	Devising a concept of integrated design and modeling of aircraft
title_short	Devising a concept of integrated design and modeling of aircraft
title_full	Devising a concept of integrated design and modeling of aircraft
title_fullStr	Devising a concept of integrated design and modeling of aircraft
title_full_unstemmed	Devising a concept of integrated design and modeling of aircraft
title_sort	devising a concept of integrated design and modeling of aircraft
publisher	PC Technology Center
publishDate	2021
url	https://doaj.org/article/ff97ff874f404951b55d39dd9d216624
work_keys_str_mv	AT oleksandrgrebenikov devisingaconceptofintegrateddesignandmodelingofaircraft AT andriihumennyi devisingaconceptofintegrateddesignandmodelingofaircraft AT oleksandrdveirin devisingaconceptofintegrateddesignandmodelingofaircraft AT oleksandrsoboliev devisingaconceptofintegrateddesignandmodelingofaircraft AT liliabuival devisingaconceptofintegrateddesignandmodelingofaircraft
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Devising a concept of integrated design and modeling of aircraft

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