Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | International Council of the Aeronautical Sciences |
| Untertitel | 25th Congress of the International Council of the Aeronautical Sciences 2006 - Congress proceedings |
| Erscheinungsort | Edinburgh |
| Seiten | 2558-2564 |
| Seitenumfang | 7 |
| Band | 4.6.4 |
| Publikationsstatus | Veröffentlicht - 2006 |
| Veranstaltung | 25th Congress of the International Council of the Aeronautical Sciences 2006 - Hamburg, Deutschland Dauer: 3 Sept. 2006 → 8 Sept. 2006 |
Abstract
Machining operations on aluminum structural parts are typically carried out under high performance cutting conditions, which comprise high feeds, depths of cut and cutting speeds. These machining conditions exert thermal and mechanical loads on the workpiece, which lead to changes in the subsurface material. Residual stress is a manifestation of these machining induced changes. Its economical importance is considerable, since it can lead to high rejection rates as a consequence of part distortion. Therefore, it is important to know the influence of the machining process on residual stress. This paper presents the results of investigations about the influence of the cutting speed and feed per tooth on part distortion of workpieces made out of forged aluminum alloys.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
- Ingenieurwesen (insg.)
- Steuerungs- und Systemtechnik
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
- Werkstoffwissenschaften (insg.)
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- BibTex
- RIS
International Council of the Aeronautical Sciences: 25th Congress of the International Council of the Aeronautical Sciences 2006 - Congress proceedings. Band 4.6.4 Edinburgh, 2006. S. 2558-2564.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Influence of high performance cutting operations on the residual stresses of aluminum structural workpieces
AU - Denkena, B.
AU - de León-García, L.
AU - Köhler, J.
PY - 2006
Y1 - 2006
N2 - Machining operations on aluminum structural parts are typically carried out under high performance cutting conditions, which comprise high feeds, depths of cut and cutting speeds. These machining conditions exert thermal and mechanical loads on the workpiece, which lead to changes in the subsurface material. Residual stress is a manifestation of these machining induced changes. Its economical importance is considerable, since it can lead to high rejection rates as a consequence of part distortion. Therefore, it is important to know the influence of the machining process on residual stress. This paper presents the results of investigations about the influence of the cutting speed and feed per tooth on part distortion of workpieces made out of forged aluminum alloys.
AB - Machining operations on aluminum structural parts are typically carried out under high performance cutting conditions, which comprise high feeds, depths of cut and cutting speeds. These machining conditions exert thermal and mechanical loads on the workpiece, which lead to changes in the subsurface material. Residual stress is a manifestation of these machining induced changes. Its economical importance is considerable, since it can lead to high rejection rates as a consequence of part distortion. Therefore, it is important to know the influence of the machining process on residual stress. This paper presents the results of investigations about the influence of the cutting speed and feed per tooth on part distortion of workpieces made out of forged aluminum alloys.
KW - Aluminum
KW - High performance cutting
KW - Milling
KW - Part distortion
KW - Residual stress
UR - http://www.scopus.com/inward/record.url?scp=84878522629&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84878522629
SN - 9781604232271
VL - 4.6.4
SP - 2558
EP - 2564
BT - International Council of the Aeronautical Sciences
CY - Edinburgh
T2 - 25th Congress of the International Council of the Aeronautical Sciences 2006
Y2 - 3 September 2006 through 8 September 2006
ER -