Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | ASME Turbo Expo 2002: Power for Land, Sea, and Air |
| Seiten | 991-1002 |
| Seitenumfang | 12 |
| Publikationsstatus | Veröffentlicht - 2002 |
| Veranstaltung | ASME TURBO EXPO 2002: Ceramics Industrial and Cogeneration Structures and Dynamics - Amsterdam, Niederlande Dauer: 3 Juni 2002 → 6 Juni 2002 |
Abstract
Optimization of the..... A computation method which analyzes bladed disk assemblies with different types of underplatform dampers and a general formulation of the contact conditions that includes a spatial contact mdoel consisting of a number of discrete point contact elements that include tangential as well as normal relative displacements to study spatial blade vibrations was made. Thus, the analysis of a tuned system consisting of 16 identical blades showed the effectiveness of the different damper types for different spatial vibration modes under varying excitation amplitudes and engine orders. It was shown that the cylindrical damper works very well in the case of sufficient relative displacements within the friction contacts.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Allgemeiner Maschinenbau
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ASME Turbo Expo 2002: Power for Land, Sea, and Air . 2002. S. 991-1002.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Optimization of the contact geometry between turbine blades and underplatform dampers with respect to friction damping
AU - Panning, Lars
AU - Sextro, Walter
AU - Popp, Karl
PY - 2002
Y1 - 2002
N2 - Optimization of the..... A computation method which analyzes bladed disk assemblies with different types of underplatform dampers and a general formulation of the contact conditions that includes a spatial contact mdoel consisting of a number of discrete point contact elements that include tangential as well as normal relative displacements to study spatial blade vibrations was made. Thus, the analysis of a tuned system consisting of 16 identical blades showed the effectiveness of the different damper types for different spatial vibration modes under varying excitation amplitudes and engine orders. It was shown that the cylindrical damper works very well in the case of sufficient relative displacements within the friction contacts.
AB - Optimization of the..... A computation method which analyzes bladed disk assemblies with different types of underplatform dampers and a general formulation of the contact conditions that includes a spatial contact mdoel consisting of a number of discrete point contact elements that include tangential as well as normal relative displacements to study spatial blade vibrations was made. Thus, the analysis of a tuned system consisting of 16 identical blades showed the effectiveness of the different damper types for different spatial vibration modes under varying excitation amplitudes and engine orders. It was shown that the cylindrical damper works very well in the case of sufficient relative displacements within the friction contacts.
UR - http://www.scopus.com/inward/record.url?scp=0036994308&partnerID=8YFLogxK
U2 - 10.1115/GT2002-30429
DO - 10.1115/GT2002-30429
M3 - Conference contribution
AN - SCOPUS:0036994308
SN - 0-7918-3609-6
SP - 991
EP - 1002
BT - ASME Turbo Expo 2002: Power for Land, Sea, and Air
T2 - ASME TURBO EXPO 2002: Ceramics Industrial and Cogeneration Structures and Dynamics
Y2 - 3 June 2002 through 6 June 2002
ER -