Experimental and Numerical Investigation of Novel Acoustic Liners and Their Design for Aero-Engine Applications

被引:0
|
作者
Neubauer, Moritz [1 ]
Genssler, Julia [2 ]
Radmann, Vincent [3 ]
Kohlenberg, Fleming [2 ]
Pohl, Michael [4 ]
Boehme, Kurt [1 ]
Knobloch, Karsten [5 ]
Sarradj, Ennes [3 ]
Hoeschler, Klaus [4 ]
Modler, Niels [1 ]
Enghardt, Lars [2 ]
机构
[1] Tech Univ Dresden, Inst Lightweight Engn & Polymer Technol ILK, Holbeinstr 3, D-01307 Dresden, Germany
[2] Tech Univ Berlin, Inst Fluid Dynam & Engn Acoust, Muller Breslau Str 8, D-10623 Berlin, Germany
[3] Tech Univ Berlin, Inst Fluid Dynam & Engn Acoust, Einsteinufer 25, D-10587 Berlin, Germany
[4] Brandenburg Univ Technol Cottbus Senftenberg, Chair Aero Engine Design, Siemens Halske Ring 14, D-03046 Cottbus, Germany
[5] German Aerosp Ctr DLR, Inst Prop Technol, Engine Acoust, Muller Breslau Str 8, D-10623 Berlin, Germany
关键词
acoustic liner; plate resonator; Helmholtz resonator; broadband noise; honeycomb structure; model; curved design; HELMHOLTZ RESONATOR; NOISE-CONTROL; MECHANICAL-PROPERTIES; PLATE SILENCER; STRENGTH; OPTIMIZATION; REFLECTION; BEHAVIOR;
D O I
10.3390/aerospace10010005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a combined experimental and numerical investigation on a novel liner concept for enhanced low-frequency and broadband acoustic attenuation. In particular, two different realizations, derived from conventional Helmholtz resonators (HR) and plate resonators (PR) are investigated, which both deploy flexible materials with material inherent damping. In this context, a comprehensive experimental investigation was carried out focusing the identification and evaluation of various geometric parameters and material properties on the acoustics dissipation and related properties of various materials in a simplified setup of a single Helmholtz resonator with flexible walls (FHR concept). Furthermore, a parameter study based on analytical models was performed for both liner concepts, taking into account material as well as geometric parameters and their effects on transmission loss. In addition, design concepts that enable cylindrical or otherwise curved liner structures and the corresponding manufacturing technologies are presented, while considering essential structural features such as drainage. With respect to the potential application in jet engines, a structural-mechanical analysis considering the relevant load cases to compare and discuss the mechanical performance of a classical HR and the FHR concept liner is presented. Finally, both concepts are evaluated and possible challenges and potentials for further implementation are described.
引用
收藏
页数:24
相关论文
共 50 条
  • [31] Multidisciplinary Design Optimization on Conceptual Design of Aero-engine
    Zhang, Xiao-bo
    Wang, Zhan-xue
    Zhou, Li
    Liu, Zeng-wen
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 33 (02) : 195 - 208
  • [32] Experimental investigation on forced response of mistuned bladed disc rotor in an aero-engine
    Madhavan, S.
    Jain, Rajeev
    Sujatha, C.
    Sekhar, A. S.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (14) : 2572 - 2588
  • [33] NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF COMBUSTION INSTABILITY PHENOMENA IN GAS TURBINE BURNERS FOR HEAVY DUTY AND AERO-ENGINE APPLICATIONS
    Accornero, Daniele
    Caruggi, Mario
    Nilberto, Alessandro
    Pittaluga, Ferruccio
    PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 2, PTS A AND B, 2011, : 1193 - 1203
  • [34] Experimental Investigation of Oblique Laser Shock Processing on Aero-engine Fan Shaft
    Yu, Zhang Pei
    Cheng, Wang
    Yan, Chai
    PROCEEDINGS OF THE INTERNATIONAL SYMPOSIUM ON MECHANICAL ENGINEERING AND MATERIAL SCIENCE, 2016, 93 : 328 - 334
  • [35] Experimental investigation on ice accretion on a rotating aero-engine spinner with hydrophobic coating
    Zheng, Mei
    Guo, Zhiqiang
    Dong, Wei
    Guo, Xiaofeng
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 136 : 404 - 414
  • [36] EXPERIMENTAL INVESTIGATION INTO OIL FILM THICKNESS AND BEHAVIOUR NEAR AN AERO-ENGINE BEARING
    Sinha, Avick
    Hann, David
    Johnson, Kathy
    Walsh, Mike
    PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 8A, 2022,
  • [37] An integrated controller design for a small aero-engine
    Bai Jie
    Liu Shuai
    Wang Wei
    PROCEEDINGS OF THE 2019 31ST CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2019), 2019, : 3129 - 3133
  • [38] Managing uncertainties in aero-engine combustor design
    Cirillo, V.
    Izzo, A.
    Marulo, F.
    Palumbo, B.
    PROCEEDINGS OF ISMA2010 - INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING INCLUDING USD2010, 2010, : 4753 - 4760
  • [39] A Review of Design and Dynamics for the GTF Aero-engine
    Cao S.
    Hou L.
    Jixie Gongcheng Xuebao/Journal of Mechanical Engineering, 2019, 55 (13): : 53 - 63
  • [40] Research Progress in Numerical Zooming Technology of Aero-Engine
    Wang, Zhan-Xue
    Song, Fu
    Zhou, Li
    Zhang, Xiao-Bo
    Zhang, Ming-Yang
    Tuijin Jishu/Journal of Propulsion Technology, 2018, 39 (07): : 1441 - 1454