Simulation and evaluation of noise and vibration reduction techniques in a helicopter cabin using SEA

被引:0
作者
Perazzolo, A. [1 ]
Cenedese, F. [1 ]
机构
[1] Agusta WEstland Acoust & Vibrat Dept, I-21017 Cascina Costa, Italy
来源
Proceedings of ISMA2006: International Conference on Noise and Vibration Engineering, Vols 1-8 | 2006年
关键词
D O I
暂无
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Increasing acoustic comfort inside the helicopter is demanded especially by VIP customer. Noise reduction is a big challenge, due to the high acoustic levels generated by the main sources (gearbox, engines, rotors, hydraulic and oil pumps) and requires the synergy of all available technologies. A mock-up built using a real helicopter is used like test-bench in order to apply and to validate noise and vibration reduction systems. In parallel, a SEA analytical model has been developed to reproduce the test results both in term of noise transfer path and of acoustic levels in running condition. The validated digital mock-up in "bare" configuration will be then used to compare several trimmed configurations to select only the most promising to be tested, saving time and costs required by experimental tests.
引用
收藏
页码:1489 / 1495
页数:7
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