Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 328-333 |
| Seitenumfang | 6 |
| Fachzeitschrift | Procedia CIRP |
| Jahrgang | 44 |
| Publikationsstatus | Veröffentlicht - 11 Mai 2016 |
| Veranstaltung | 6th CIRP Conference on Assembly Technologies and Systems, CATS 2016 - Gothenburg, Schweden Dauer: 16 Mai 2016 → 18 Mai 2016 |
Abstract
The disassembly of components with solidified assembly connections is often difficult to plan. A typical example can be found in the aviation industry, where turbine blades solidify in the turbine disc due to operational loads. The solidification of the joining partners has several causes such as thermal stress or high centrifugal forces so that the disassembly forces cannot be estimated exactly. The forces in manual disassembly, e.g. when striking the assembled part with a hammer, are often too high and thus difficult to control. An automated approach is investigated, in which a piezo stack actuator induces vibrations to the joined components and force amplitudes are reduced based on a simplified model of the solidification. For this purpose, simulations are presented to determine forms of excitation for the piezo actuator and to control the disassembly process.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Steuerungs- und Systemtechnik
- Ingenieurwesen (insg.)
- Wirtschaftsingenieurwesen und Fertigungstechnik
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in: Procedia CIRP, Jahrgang 44, 11.05.2016, S. 328-333.
Publikation: Beitrag in Fachzeitschrift › Konferenzaufsatz in Fachzeitschrift › Forschung › Peer-Review
}
TY - JOUR
T1 - Reduction of Disassembly Forces for Detaching Components with Solidified Assembly Connections
AU - Wolff, Julius
AU - Yan, Miping
AU - Schultz, Melf
AU - Raatz, Annika
PY - 2016/5/11
Y1 - 2016/5/11
N2 - The disassembly of components with solidified assembly connections is often difficult to plan. A typical example can be found in the aviation industry, where turbine blades solidify in the turbine disc due to operational loads. The solidification of the joining partners has several causes such as thermal stress or high centrifugal forces so that the disassembly forces cannot be estimated exactly. The forces in manual disassembly, e.g. when striking the assembled part with a hammer, are often too high and thus difficult to control. An automated approach is investigated, in which a piezo stack actuator induces vibrations to the joined components and force amplitudes are reduced based on a simplified model of the solidification. For this purpose, simulations are presented to determine forms of excitation for the piezo actuator and to control the disassembly process.
AB - The disassembly of components with solidified assembly connections is often difficult to plan. A typical example can be found in the aviation industry, where turbine blades solidify in the turbine disc due to operational loads. The solidification of the joining partners has several causes such as thermal stress or high centrifugal forces so that the disassembly forces cannot be estimated exactly. The forces in manual disassembly, e.g. when striking the assembled part with a hammer, are often too high and thus difficult to control. An automated approach is investigated, in which a piezo stack actuator induces vibrations to the joined components and force amplitudes are reduced based on a simplified model of the solidification. For this purpose, simulations are presented to determine forms of excitation for the piezo actuator and to control the disassembly process.
KW - Assembly Connections
KW - Automation
KW - Disassembly
KW - Dissambly Forces
KW - Turbine Blade
KW - Vibrations
UR - http://www.scopus.com/inward/record.url?scp=84994101824&partnerID=8YFLogxK
U2 - 10.1016/j.procir.2016.02.006
DO - 10.1016/j.procir.2016.02.006
M3 - Conference article
AN - SCOPUS:84994101824
VL - 44
SP - 328
EP - 333
JO - Procedia CIRP
JF - Procedia CIRP
SN - 2212-8271
T2 - 6th CIRP Conference on Assembly Technologies and Systems, CATS 2016
Y2 - 16 May 2016 through 18 May 2016
ER -