Application of improved hybrid interface substructural component modal synthesis method in vibration characteristics of mistuned blisk

The large and complex structures are divided into hundreds of thousands or millions degrees of freedom(DOF) when they are calculated which will spend a lot of time and the efficiency will be extremely low. The classical component modal synthesis method (CMSM) are used extensively, but for many structures in the engineering of high-rise buildings, aerospace systemic engineerings, marine oil platforms etc, a large amount of calculation is still needed. An improved hybrid interface substructural component modal synthesis method(HISCMSM) is proposed. The parametric model of the mistuned blisk is built by the improved HISCMSM. The double coordinating conditions of the displacement and the force are introduced to ensure the computational accuracy. Compared with the overall structure finite element model method(FEMM), the computational time is shortened by 23.86%–31.56% and the modal deviation is 0.002%–0.157% which meets the requirement of the computational accuracy. It is faster 4.46%–10.57% than the classical HISCMSM. So the improved HISCMSM is better than the classical HISCMSM and the overall structure FEMM. Meanwhile, the frequency and the modal shape are researched, considering the factors including rotational speed, gas temperature and geometry size. The strong localization phenomenon of the modal shape’s the maximum displacement and the maximum stress is observed in the second frequency band and it is the most sensitive in the frequency veering. But the localization phenomenon is relatively weak in 1st and the 3d frequency band. The localization of the modal shape is more serious under the condition of the geometric dimensioning mistuned. An improved HISCMSM is proposed, the computational efficiency of the mistuned blisk can be increased observably by this method.

[1]  Jun Wu,et al.  Stiffness influential factors-based dynamic modeling and its parameter identification method of fixed joints in machine tools , 2010 .

[2]  Zhiqin Cui Parametric modeling and modal analysis for the complex mechanical structure , 2008 .

[3]  Chandramouli Padmanabhan,et al.  A fixed–free interface component mode synthesis method for rotordynamic analysis , 2006 .

[4]  Guangchen Bai,et al.  Distributed collaborative response surface method for mechanical dynamic assembly reliability design , 2013 .

[5]  Christophe Pierre,et al.  Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks—Part I: Theoretical Models , 2001 .

[6]  Alok Sinha,et al.  Reduced Order Modeling of a Bladed Rotor With Geometric Mistuning Via Estimated Deviations in Mass and Stiffness Matrices , 2013 .

[7]  Alan Palazzolo,et al.  An Efficient Algorithm for Blade Loss Simulations Using a High Fidelity Ball Bearing and Damper Model , 2003 .

[8]  Bogdan I. Epureanu,et al.  Detection of Cracks in Mistuned Bladed Disks Using Reduced-Order Models and Vibration Data , 2012 .

[9]  O. G. McGee,et al.  Three-Dimensional Tailored Vibration Response and Flutter Control of High-Bypass Shroudless Aeroengine Fans , 2013 .

[10]  Christophe Pierre,et al.  Predicting blade stress levels directly from reduced-order vibration models of mistuned bladed disks , 2006 .

[11]  Chorng-Shyan Lin,et al.  Joint stiffness identification using FRF measurements , 2003 .

[12]  Carlos Martel,et al.  Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response , 2009 .

[13]  Akira Saito,et al.  Reduced-Order Modeling for Nonlinear Analysis of Cracked Mistuned Multistage Bladed-Disk Systems , 2012 .

[14]  Christophe Pierre,et al.  Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced-Order Modeling , 2002 .

[15]  Denis Laxalde,et al.  Dynamics of Multistage Bladed Disks Systems , 2007 .

[16]  Marc P. Mignolet,et al.  Maximum Amplification of Blade Response due to Mistuning: Localization and Mode Shape Aspects of the Worst Disks , 2003 .

[17]  J. H. Griffin,et al.  Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model-Part I: Theory (2003-GT-38952) , 2004 .

[18]  Alan Palazzolo,et al.  Long duration blade loss simulations including thermal growths for dual-rotor gas turbine engine , 2008 .

[19]  G. T. Zheng,et al.  Improved Component-Mode Synthesis for Nonclassically Damped Systems , 2008 .

[20]  Bogdan I. Epureanu,et al.  Reduced Order Models of Mistuned Cracked Bladed Disks , 2011 .

[21]  Joseph A. Beck,et al.  Probabilistic Mistuning Assessment Using Nominal and Geometry Based Mistuning Methods , 2013 .

[22]  J. H. Griffin,et al.  Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model-Part II: Application (2003-GT-38953) , 2004 .