Features of integration management tools in the aviation industry

Vieira, Darli Rodrigues; Vieira, Raimundo Kennedy; Chain, Milena Chang; Vieira, Adalena Kennedy

doi:10.1504/ijplm.2019.104355

Cited by 1 publication

(2 citation statements)

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Aviation technical documentation was compiled by drawing geometry methods and was submitted for the production of aircraft on paper. The structure was adjusted on design plazas, which did not always make it possible to identify errors caused by the imperfection of the design method and embedded in the design documentation [7].…”

Section: Literature Review and Problem Statementmentioning

confidence: 99%

See 1 more Smart Citation

Devising a concept of integrated design and modeling of aircraft

Grebenikov

Humennyi

Dveirin³

et al. 2021

EEJET

View full text Add to dashboard Cite

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

show abstract

Section: Literature Review and Problem Statementmentioning

confidence: 99%

“…The methods of integrated design should be based on the development of three-dimensional analytical standards of the aircraft surface, its assembly units, prefabricated components and systems [7,16,17].…”

Section: Literature Review and Problem Statementmentioning

confidence: 99%