Coordinatore | "University of Split, Faculty of Electrical Engineering, Mechanical Engineering and Naval Architecture"
Organization address
address: Rudjera Boskovica bb contact info |
Nazionalità Coordinatore | Croatia [HR] |
Totale costo | 45˙000 € |
EC contributo | 45˙000 € |
Programma | FP7-PEOPLE
Specific programme "People" implementing the Seventh Framework Programme of the European Community for research, technological development and demonstration activities (2007 to 2013) |
Code Call | FP7-PEOPLE-2010-RG |
Funding Scheme | MC-ERG |
Anno di inizio | 2011 |
Periodo (anno-mese-giorno) | 2011-03-01 - 2014-02-28 |
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1 |
"University of Split, Faculty of Electrical Engineering, Mechanical Engineering and Naval Architecture"
Organization address
address: Rudjera Boskovica bb contact info |
HR (Split) | coordinator | 45˙000.00 |
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
'Significant components of the interior noise in high speed vehicles are caused by the Turbulent Boundary Layer (TBL) disturbances which are inherently random and broadband. In fact, aircraft cabin noise during cruise is dominated by the TBL noise components. The noise is generated by the airflow over the fuselage surface and transmitted to the vehicle interior especially through vibration and sound radiation of panels of the aircraft fuselage. This problem is traditionally solved passively, by applying sound absorbing materials onto the panels. However, the low-frequency effectiveness of passive treatments is not sufficient. For this reason an interest has grown in using active noise transmission control. It can be implemented through smart panels with embedded sensor-actuator pairs which apply decentralised velocity feedback control. Such control generates active damping and thus significantly decreases the sound transmission at low frequencies, where it is dominated by resonances of fuselage panels. The major challenge in development of smart panels with decentralised velocity feedback control loops is the stability of practical systems, which limits the maximum feedback gain, and thus the maximum performance. Furthermore, due to the cross-talk between the control units, the increase in the number of feedback loops does not necessarily lead to the increase in global performance, as the maximum stable gain tends to decrease. In that case, there is a danger that unnecessary mass is added to the structure. Therefore the three objectives of the project SPRiNT are: to improve on the stability of the feedback loops, to investigate ways to reduce mass added to the structure by the active control system components, and finally, to optimize the number of control units per smart panel area. This will be done theoretically by numerical simulations and experimentally on prototype smart panels.'
EU-funded scientists have unveiled a novel active control system in a bid to mitigate aircraft cabin noise.
Turbulent airflow over the fuselage surface generates noise that is radiated by vibrating panels. Although absorbing materials are already used on panel surfaces, passive methods are unfortunately not effective against low-frequency noise components.
The EU-funded 'SPRiNT - Smart panels for the reduction of noise transmission' (http://marjan.fesb.hr/kk/SPRINT_abstract.html (SPRINT)) project focused on embedded sensor-actuator pairs evenly distributed on a smart panel surface. These control units generate active damping, significantly decreasing sound transmission at low frequencies.
Project members simulated sound transmission from a smart double-panel system. In addition to force actuators and velocity sensors, a mathematical model was extended to include frequency response from coil actuators and accelerometer sensors.
To achieve maximum performance, the stability of this decentralised velocity feedback control architecture was analysed. As an increase in the feedback loop number does not necessarily lead to performance improvement, project partners sought instead to optimise their number.
An electromechanical test rig was successfully built to test system control effectiveness, stability and noise abatement. Experimental validation on the rig should significantly increase knowledge regarding the effectiveness of the proposed active control method.
Further experimental work is highly likely to result in more publications in peer-reviewed journals. The final outcomes are expected to lead to a successful demonstration of a very interesting and novel active noise control technique.
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