Konstanzer et al., 2006 - Google Patents
Aircraft interior noise reduction through a piezo tunable vibration absorber systemKonstanzer et al., 2006
View PDF- Document ID
- 6305458879515381863
- Author
- Konstanzer P
- Grunewald M
- Janker P
- Storm S
- Publication year
- Publication venue
- Proceedings of the 25th international congress of the aeronautical sciences (ICAS 2006)
External Links
Snippet
Turboprop aircrafts, such as Airbus A400M, are challenged amongst others by high interior noise levels due to tonal propeller-induced vibrations of the aircraft structure. One approach for interior noise reduction is the reduction of fuselage vibrations by vibration absorbers. In …
- 239000006096 absorbing agent 0 title abstract description 29
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