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DSpace at Transilvania University >
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COMEC 2015 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/1900
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| Title: | THE 3D LIGHTWEIGHT OPTIMIZATION FOR HIGH LOADED PARTS – CASE STUDY |
| Authors: | DIMA, Gabriel. D.
DIACONU, Marius
BALCU, Ion
TEȘULĂ, Ionuț |
| Keywords: | lightweight
topology optimization
aerospace
design for manufacturing |
| Issue Date: | Oct-2015 |
| Publisher: | Transilvania University Press of Brasov |
| Citation: | Google Scholar |
| Series/Report no.: | ;134-139 |
| Abstract: | The 3D structural optimization is the most difficult optimization process, being used in aerospace industry only in few applications. In accordance with the efforts to set up a methodology to help to the implementation of extensive structural optimization in the development teams, within the paper a case study from a helicopter pilot seat is presented. The optimization of the fitting targeted lightweight, with respect to the constraints of a high loading environment and the manufacturing issues. Iterations of optimization, together with conclusions and lessons learned are presented. |
| URI: | http://hdl.handle.net/123456789/1900 |
| ISSN: | 2457-8541
L 2457-8541 |
| Appears in Collections: | COMEC 2015
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