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Izvorni znanstveni članak
https://doi.org/10.17818/NM/2016/SI11

The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry

Dalibor Kužma ; Technical University of Košice Slovakia
Peter Korba ; Technical University of Košice Slovakia
Michal Hovanec ; Faculty of Aeronautics Technical University of Košice Slovakia
Ľuboslav Dulina ; Faculty of Mechanical Engineering Univerzity of Žilina

Puni tekst: engleski, pdf (3 MB) str. 134-139 preuzimanja: 166* citiraj
APA 6th Edition
Kužma, D., Korba, P., Hovanec, M. i Dulina, Ľ. (2016). The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry. NAŠE MORE, 63 (3 Special Issue), 134-139. https://doi.org/10.17818/NM/2016/SI11
MLA 8th Edition
Kužma, Dalibor, et al. "The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry." NAŠE MORE, vol. 63, br. 3 Special Issue, 2016, str. 134-139. https://doi.org/10.17818/NM/2016/SI11. Citirano 10.12.2019.
Chicago 17th Edition
Kužma, Dalibor, Peter Korba, Michal Hovanec i Ľuboslav Dulina. "The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry." NAŠE MORE 63, br. 3 Special Issue (2016): 134-139. https://doi.org/10.17818/NM/2016/SI11
Harvard
Kužma, D., et al. (2016). 'The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry', NAŠE MORE, 63(3 Special Issue), str. 134-139. https://doi.org/10.17818/NM/2016/SI11
Vancouver
Kužma D, Korba P, Hovanec M, Dulina Ľ. The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry. NAŠE MORE [Internet]. 2016 [pristupljeno 10.12.2019.];63(3 Special Issue):134-139. https://doi.org/10.17818/NM/2016/SI11
IEEE
D. Kužma, P. Korba, M. Hovanec i Ľ. Dulina, "The Use of CAX Systems as a Tool for Modeling Construction Element in the Aviation Industry", NAŠE MORE, vol.63, br. 3 Special Issue, str. 134-139, 2016. [Online]. https://doi.org/10.17818/NM/2016/SI11

Sažetak
The article deals with the adjustment of the wing selected part of the plane Viper SD-4 from slovak producer with using environment of software Siemens NX9. The adjustment is carried out after consultation with the test pilots of this plane and tries to take into account the observations made during the test flights. The first part of the article is focused on the current construction of the wings and its parts. The second part describes how digitalize the real wing by using reverse engineering. The last section describes adjustment of the design and its 3D model in a virtual environment. The model is created in the environment Modeling and Aero Sheet Metal in software Siemens NX. When modelling was also used part of the drawing documentation from the manufacturer. This article deals with the wing treatment on the theoretical base.

Ključne riječi
3D model; flap; wing adjustment

Hrčak ID: 162580

URI
https://hrcak.srce.hr/162580

Posjeta: 239 *