Details
| Translated title of the contribution | Methods for the simulation and compensation of residual stress-induced component distortion: Prevention of component distortion in aeronautical components by means of FEM simulation and adjusted processing |
|---|---|
| Original language | German |
| Pages (from-to) | 208-211 |
| Number of pages | 4 |
| Journal | Zeitschrift für wirtschaftlichen Fabrikbetrieb (ZWF) (online) |
| Volume | 108 |
| Issue number | 4 |
| Publication status | Published - 1 Apr 2013 |
Abstract
In the manufacturing of aerospace structural components distortions related to residual stress can occur despite proper machining. If these distortions cannot be corrected by a straightening process, the part cannot be assembled. This paper presents methods which allow the determination of the component distortion prior to machining. This allows an adjustment of the production, so that the manufactured part shows no distortion.
ASJC Scopus subject areas
- Engineering(all)
- General Engineering
- Business, Management and Accounting(all)
- Strategy and Management
- Decision Sciences(all)
- Management Science and Operations Research
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In: Zeitschrift für wirtschaftlichen Fabrikbetrieb (ZWF) (online), Vol. 108, No. 4, 01.04.2013, p. 208-211.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - Methoden zur Simulation und Kompensation von eigenspannungsbedingtem Bauteilverzug
T2 - Vermeidung von Bauteilverzug bei Luftfahrtbauteilen mittels FEM-Simulation und angepasster Bearbeitung
AU - Denkena, Berend
AU - Kaddour, Rabih
AU - Dreier, Steven
PY - 2013/4/1
Y1 - 2013/4/1
N2 - In the manufacturing of aerospace structural components distortions related to residual stress can occur despite proper machining. If these distortions cannot be corrected by a straightening process, the part cannot be assembled. This paper presents methods which allow the determination of the component distortion prior to machining. This allows an adjustment of the production, so that the manufactured part shows no distortion.
AB - In the manufacturing of aerospace structural components distortions related to residual stress can occur despite proper machining. If these distortions cannot be corrected by a straightening process, the part cannot be assembled. This paper presents methods which allow the determination of the component distortion prior to machining. This allows an adjustment of the production, so that the manufactured part shows no distortion.
UR - http://www.scopus.com/inward/record.url?scp=84878187769&partnerID=8YFLogxK
M3 - Artikel
AN - SCOPUS:84878187769
VL - 108
SP - 208
EP - 211
JO - Zeitschrift für wirtschaftlichen Fabrikbetrieb (ZWF) (online)
JF - Zeitschrift für wirtschaftlichen Fabrikbetrieb (ZWF) (online)
SN - 0947-0085
IS - 4
ER -