Aircraft side wall with improved low-frequency sound insulation using a lining panel with Helmholtz resonators
Aircraft side wall with improved low-frequency sound insulation using a lining panel with Helmholtz resonators
The continuous development of aircraft engines aims to reduce fuel consumption by increasing the bypass ratio. However, an increased bypass ratio changes the sound emission of the engine, such that the sound spectrum inside the cabin can be dominated by low frequency tones with high sound pressure levels, penetrating more efficiently the current cabin wall than sound of higher frequencies. Thus, the comfort level of the passengers could be adversely affected. This contribution presents a new side wall panel design that is capable to significantly increase the transmission loss of low frequency tones. The rear side of the lining is fully covered by a resonator system of a cantilever integrated into a Helmholtz resonator. With this approach, the lining with resonators can be tuned with respect to two resonance frequencies to improve the sound transmission loss of the cabin wall. A transfer matrix for the Helmholtz resonator panel is derived and the transmission loss of the proposed side wall design is determined. The analytically calculated transmission loss is compared to numerical and experimental results obtained under diffuse field conditions
Bandwidth, Double wall, Helmholtz resonators, Transmission loss, Vibration resonators
Canadian Acoustical Association
Hoppen, Hannah
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Langfeldt, Felix
2bf86877-f2cd-4c35-be0f-e38a718a915c
Gleine, Wolfgang
6b99025f-b44a-46a8-b699-ec25962c7e75
Von Estorff, Otto
7b2f7283-9bab-49e4-9ac8-baaa061e769d
2019
Hoppen, Hannah
f609ed2b-6b7a-4a2e-89c9-45fd11ee50a0
Langfeldt, Felix
2bf86877-f2cd-4c35-be0f-e38a718a915c
Gleine, Wolfgang
6b99025f-b44a-46a8-b699-ec25962c7e75
Von Estorff, Otto
7b2f7283-9bab-49e4-9ac8-baaa061e769d
Hoppen, Hannah, Langfeldt, Felix, Gleine, Wolfgang and Von Estorff, Otto
(2019)
Aircraft side wall with improved low-frequency sound insulation using a lining panel with Helmholtz resonators.
In Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019.
Canadian Acoustical Association..
Record type:
Conference or Workshop Item
(Paper)
Abstract
The continuous development of aircraft engines aims to reduce fuel consumption by increasing the bypass ratio. However, an increased bypass ratio changes the sound emission of the engine, such that the sound spectrum inside the cabin can be dominated by low frequency tones with high sound pressure levels, penetrating more efficiently the current cabin wall than sound of higher frequencies. Thus, the comfort level of the passengers could be adversely affected. This contribution presents a new side wall panel design that is capable to significantly increase the transmission loss of low frequency tones. The rear side of the lining is fully covered by a resonator system of a cantilever integrated into a Helmholtz resonator. With this approach, the lining with resonators can be tuned with respect to two resonance frequencies to improve the sound transmission loss of the cabin wall. A transfer matrix for the Helmholtz resonator panel is derived and the transmission loss of the proposed side wall design is determined. The analytically calculated transmission loss is compared to numerical and experimental results obtained under diffuse field conditions
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More information
Published date: 2019
Additional Information:
Funding Information:
This work has been funded by the Federal Ministry for Economic Affairs and Energy, under the frame-work of the research project Flight-LAB (grand number: 20K1511D). The financial support is gratefully acknowledged. Furthermore, the authors would like to thank Evonik for providing the foam.
Publisher Copyright:
© Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019. All rights reserved.
Venue - Dates:
26th International Congress on Sound and Vibration, ICSV 2019, , Montreal, Canada, 2019-07-07 - 2019-07-11
Keywords:
Bandwidth, Double wall, Helmholtz resonators, Transmission loss, Vibration resonators
Identifiers
Local EPrints ID: 469335
URI: http://eprints.soton.ac.uk/id/eprint/469335
PURE UUID: d6e8a6a8-1078-4019-b74b-406d7a0bd99d
Catalogue record
Date deposited: 13 Sep 2022 16:47
Last modified: 18 Mar 2024 04:05
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Contributors
Author:
Hannah Hoppen
Author:
Wolfgang Gleine
Author:
Otto Von Estorff
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