Numerical Simulation and Analysis of the forming process of an airplane frame part

DOI

10.2991/icmse-15.2015.249How to use a DOI?

Keywords

Airplane frame parts; Drop hammer forming; Transition mould; Simulation

Abstract

Airplane frame parts can form by the method of increasing the transition mould. The main purpose of the transitional surface design is to change the material flow state, and make the material flow is uniform. Mainly studied forming process to a typical frame sheet metal part, analyzed the forming characteristics, as well as the advantages and disadvantages of drop hammer forming, studied the transitional surface design, analyzed the wrinkling and rupture caused by a variety of reasons, finally designed a reasonable transition mould. The forming process of product has carried on the simulation by PAM-STAMP software, optimize the process parameters, verified the method is feasible.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Ling -Yun Zhang
AU  - Wen –Yuan Wang
PY  - 2015/12
DA  - 2015/12
TI  - Numerical Simulation and Analysis of the forming process of an airplane frame part
BT  - Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
PB  - Atlantis Press
SP  - 1374
EP  - 1378
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmse-15.2015.249
DO  - 10.2991/icmse-15.2015.249
ID  - Zhang2015/12
ER  -