HIGH-FIDELITY SENSITIVITY ANALYSIS OF MODAL PROPERTIES OF MISTUNED BLADED DISKS REGARDING MATERIAL ANISOTROPY

被引:0
作者
Koscso, Adam [1 ]
Dhondt, Guido [2 ]
Petrov, E. P. [1 ]
机构
[1] Univ Sussex, Sch Engn & Informat, Brighton BN1 9QT, E Sussex, England
[2] MTU Aero Engines AG, Dachauer Str 665, D-80995 Munich, Germany
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 7C | 2018年
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A new method has been developed for sensitivity calculations of modal characteristics of bladed disks made of anisotropic materials. The method allows the determination of the sensitivity of the natural frequencies and mode shapes of mistuned bladed disks with respect to anisotropy angles that define the crystal orientation of the monocrystalline blades using full-scale finite element models. An enhanced method is proposed to provide high accuracy for the sensitivity analysis of mode shapes. An approach has also been developed for transforming the modal sensitivities to coordinate systems used in industry for description of the blade anisotropy orientations. The capabilities of the developed methods are demonstrated on examples of a single blade and a mistuned realistic bladed disk finite element models. The modal sensitivity of mistuned bladed disks to anisotropic material orientation is thoroughly studied.
引用
收藏
页数:13
相关论文
共 37 条
[21]   High-Fidelity Multidisciplinary Sensitivity Analysis and Design Optimization for Rotorcraft Applications [J].
Wang, Li ;
Diskin, Boris ;
Biedron, Robert T. ;
Nielsen, Eric J. ;
Bauchau, Olivier A. .
AIAA JOURNAL, 2019, 57 (08) :3117-3131
[22]   Uncertainty and global sensitivity analysis of bladed disk statics with material anisotropy and root geometry variations [J].
Rajasekharan, Rahul ;
Petrov, Evgeny .
ENGINEERING REPORTS, 2019, 1 (03)
[23]   ANALYSIS OF NONLINEAR MODAL DAMPING DUE TO FRICTION AT BLADE ROOTS USING HIGH-FIDELITY MODELLING [J].
Chen, Junjie ;
Zang, Chaoping ;
Zhou, Biao ;
Petrov, E. P. .
PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 7C, 2018,
[24]   Developing a numerical framework for high-fidelity simulation of contrails: sensitivity analysis for conventional contrails [J].
Ferreira, Tania S. C. ;
Alonsot, Juan J. ;
Gor, Catherine .
AIAA AVIATION FORUM AND ASCEND 2024, 2024,
[25]   Dimensionality Reduction of High-Fidelity Machine Tool Models by Using Global Sensitivity Analysis [J].
Ellinger, Johannes ;
Semm, Thomas ;
Zaeh, Michael F. .
JOURNAL OF MANUFACTURING SCIENCE AND ENGINEERING-TRANSACTIONS OF THE ASME, 2022, 144 (05)
[26]   Evaluation of High-Fidelity Multidisciplinary Sensitivity-Analysis Framework for Multipoint Rotorcraft Optimization [J].
Wang, Li ;
Diskin, Boris ;
Biedron, Robert T. ;
Nielsen, Eric J. ;
Bauchau, Olivier A. .
JOURNAL OF AIRCRAFT, 2020, 57 (05) :830-842
[27]   DEVELOPMENT AND APPLICATION OF A HIGH-FIDELITY NUMERICAL TOOL FOR DYNAMIC ANALYSIS OF BLADED DISC SYSTEMS WITH UNDERPLATFORM DAMPERS IN AIRCRAFT ENGINE TURBINES [J].
Tufekci, Mertol .
PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 10B, 2024,
[28]   Development of a high-fidelity and optimal model for magneto-rheological damper by parametric sensitivity analysis [J].
Adarsh, S. ;
Panda, Jagajyoti ;
Ray-Chaudhuri, Samit .
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2025, 177
[29]   A coupled-adjoint sensitivity analysis method for high-fidelity aero-structural design [J].
Martins, Joaquim R. R. A. ;
Alonso, Juan J. ;
Reuther, James J. .
OPTIMIZATION AND ENGINEERING, 2005, 6 (01) :33-62
[30]   A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design [J].
Joaquim R.R.A. Martins ;
Juan J. Alonso ;
James J. Reuther .
Optimization and Engineering, 2005, 6 :33-62