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Low-frequency air- and structure-borne sound insulation challenges for a counter-rotating open-rotor aircraft

Low-frequency air- and structure-borne sound insulation challenges for a counter-rotating open-rotor aircraft
Low-frequency air- and structure-borne sound insulation challenges for a counter-rotating open-rotor aircraft

The increasing demand for environmentally friendly aircraft requires the use of more fuel efficient engine technologies, such as the counter-rotating open-rotor (CROR). Despite of their good emission performance, CROR-engines exhibit a significant drawback regarding the high-amplitude low-frequency noise, generated by the propellers. The challenge of dealing with that problem implies measures, which attenuate structure- and air-borne low-frequency sound, caused by the engines. In this paper, two major approaches for such measures are discussed. The first approach aims at the reduction of structure-borne sound transmission between two adjacent fuselage sections. In this context, a modification of the traditional fuselage section interconnection has been investigated numerically and compared with the conventional design. Models with increasing complexity were created in order to observe the structure-borne sound transmission performance of the newly proposed design: A beam model for analytical pre-evaluation, succeeded by plate and fuselage models for the numerical investigations. The second approach is concerned with the shielding of exterior noise. For this purpose, a noise shield mounted at the fuselage has been considered. Membrane type metamaterials were used as a middle layer of a double panel structure to improve low-frequency sound attenuation. Based on that concept, panels with different geometries, involving a framed single membrane structure as well as layered and multi-celled arrays have been investigated and the influence of the arrangement on the sound transmission behavior observed. The related numerical and analytical results are discussed and validated via experiments.

343-350
International Institute of Acoustics and Vibration
Marinova, Polina
9351444e-1709-41df-9889-42ecc0b7911c
Von Estorff, Otto
7b2f7283-9bab-49e4-9ac8-baaa061e769d
Lippert, Stephan
7c38b599-24ad-454a-9e8b-6339a336e810
Langfeldt, Felix
2bf86877-f2cd-4c35-be0f-e38a718a915c
Gleine, Wolfgang
6b99025f-b44a-46a8-b699-ec25962c7e75
Marinova, Polina
9351444e-1709-41df-9889-42ecc0b7911c
Von Estorff, Otto
7b2f7283-9bab-49e4-9ac8-baaa061e769d
Lippert, Stephan
7c38b599-24ad-454a-9e8b-6339a336e810
Langfeldt, Felix
2bf86877-f2cd-4c35-be0f-e38a718a915c
Gleine, Wolfgang
6b99025f-b44a-46a8-b699-ec25962c7e75

Marinova, Polina, Von Estorff, Otto, Lippert, Stephan, Langfeldt, Felix and Gleine, Wolfgang (2014) Low-frequency air- and structure-borne sound insulation challenges for a counter-rotating open-rotor aircraft. In 21st International Congress on Sound and Vibration 2014, ICSV 2014. International Institute of Acoustics and Vibration. pp. 343-350 .

Record type: Conference or Workshop Item (Paper)

Abstract

The increasing demand for environmentally friendly aircraft requires the use of more fuel efficient engine technologies, such as the counter-rotating open-rotor (CROR). Despite of their good emission performance, CROR-engines exhibit a significant drawback regarding the high-amplitude low-frequency noise, generated by the propellers. The challenge of dealing with that problem implies measures, which attenuate structure- and air-borne low-frequency sound, caused by the engines. In this paper, two major approaches for such measures are discussed. The first approach aims at the reduction of structure-borne sound transmission between two adjacent fuselage sections. In this context, a modification of the traditional fuselage section interconnection has been investigated numerically and compared with the conventional design. Models with increasing complexity were created in order to observe the structure-borne sound transmission performance of the newly proposed design: A beam model for analytical pre-evaluation, succeeded by plate and fuselage models for the numerical investigations. The second approach is concerned with the shielding of exterior noise. For this purpose, a noise shield mounted at the fuselage has been considered. Membrane type metamaterials were used as a middle layer of a double panel structure to improve low-frequency sound attenuation. Based on that concept, panels with different geometries, involving a framed single membrane structure as well as layered and multi-celled arrays have been investigated and the influence of the arrangement on the sound transmission behavior observed. The related numerical and analytical results are discussed and validated via experiments.

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More information

Published date: 2014
Venue - Dates: 21st International Congress on Sound and Vibration 2014, ICSV 2014, , Beijing, China, 2014-07-13 - 2014-07-17

Identifiers

Local EPrints ID: 467634
URI: http://eprints.soton.ac.uk/id/eprint/467634
PURE UUID: f3c3772f-8232-405b-ab75-991386c0ca84
ORCID for Felix Langfeldt: ORCID iD orcid.org/0000-0003-2380-2746

Catalogue record

Date deposited: 15 Jul 2022 20:18
Last modified: 07 Mar 2024 03:05

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Contributors

Author: Polina Marinova
Author: Otto Von Estorff
Author: Stephan Lippert
Author: Felix Langfeldt ORCID iD
Author: Wolfgang Gleine

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