Viscoelastic damping design: A novel approach for shape optimization of Constrained Layer Damping treatments at different ambient temperatures

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Autorschaft

  • Martin Gröhlich
  • Marc Böswald
  • Jörg Wallaschek

Externe Organisationen

  • Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
  • Technische Universität Braunschweig
  • Exzellenzcluster SE²A Sustainable and Energy-Efficient Aviation
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Aufsatznummer117703
FachzeitschriftJournal of sound and vibration
Jahrgang555
Frühes Online-Datum5 Apr. 2023
PublikationsstatusVeröffentlicht - 7 Juli 2023

Abstract

Passive damping plays an important role in the vibration mitigation of aeronautic structures. In contrast to active systems, passive damping systems do not require any energy supply. Thus, their readiness is independent, which reduces the failure probability compared to active systems. Constrained Layer Damping (CLD) has become an established treatment for damping bending vibrations. Unlike other passive systems such as shock-mounts, CLD can be compactly integrated into an existing structure as an add-on solution. However, the design scope is limited by mass constraints and the optimal design for maximum damping must be found by optimization. For this purpose, a novel optimization approach is presented. The layer widths of the core and face layers of a CLD structure are treated as design parameters. Compared to the strategy of placing CLD patches on vibration antinodes, the proposed approach provides up to 52 % higher damping. The optimal design of a generic beam structure is determined considering different modes, viscoelastic material stiffnesses and ambient temperatures. Furthermore, the simulated damping is experimentally verified for a shape-optimized beam. The analyses show that the optimal design depends significantly on the viscoelastic material stiffness and is therefore temperature dependent. As a consequence, a generalized design guideline for CLD treatments cannot be derived.

ASJC Scopus Sachgebiete

Zitieren

Viscoelastic damping design: A novel approach for shape optimization of Constrained Layer Damping treatments at different ambient temperatures. / Gröhlich, Martin; Böswald, Marc; Wallaschek, Jörg.
in: Journal of sound and vibration, Jahrgang 555, 117703, 07.07.2023.

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

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abstract = "Passive damping plays an important role in the vibration mitigation of aeronautic structures. In contrast to active systems, passive damping systems do not require any energy supply. Thus, their readiness is independent, which reduces the failure probability compared to active systems. Constrained Layer Damping (CLD) has become an established treatment for damping bending vibrations. Unlike other passive systems such as shock-mounts, CLD can be compactly integrated into an existing structure as an add-on solution. However, the design scope is limited by mass constraints and the optimal design for maximum damping must be found by optimization. For this purpose, a novel optimization approach is presented. The layer widths of the core and face layers of a CLD structure are treated as design parameters. Compared to the strategy of placing CLD patches on vibration antinodes, the proposed approach provides up to 52 % higher damping. The optimal design of a generic beam structure is determined considering different modes, viscoelastic material stiffnesses and ambient temperatures. Furthermore, the simulated damping is experimentally verified for a shape-optimized beam. The analyses show that the optimal design depends significantly on the viscoelastic material stiffness and is therefore temperature dependent. As a consequence, a generalized design guideline for CLD treatments cannot be derived.",
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AU - Gröhlich, Martin

AU - Böswald, Marc

AU - Wallaschek, Jörg

N1 - Funding Information: We would like to acknowledge the funding by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany's Excellence Strategy – EXC 2163/1 - Sustainable and Energy Efficient Aviation – Project-ID 390881007.

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