Vibration and optimum design of rotating laminated blades

The vibration and optimum design of a rotating laminated blade subject to constraints on the dynamic behavior are investigated. Restrictions on multiple natural frequencies as well as the maximum dynamic deflections of rotating laminated blades are considered as constraints on the dynamic behavior of the system. Aerodynamic forces acting on the blade are simulated as harmonic excitations. The optimality criterion method and the modified method of feasible directions have been successfully developed for optimizing the weight of the rotating laminated blade. Effects of radius of the disk, aspect ratio, and rotating speed on the system dynamic behaviors and/or the optimum design are also studied. The vibration analysis shows that most of the bending modes can be significantly affected by the rotating speed and the radius of the disk. Results also show that the optimum weight with constraints on the dynamic response is higher than that with frequency constraints. Moreover, results show that the weight of the rotating laminated blade can be greatly reduced at the optimum design stage.

[1]  K. M. Ragsdell,et al.  The Generalized Reduced Gradient Method: A Reliable Tool for Optimal Design , 1977 .

[2]  E. Crawley,et al.  Frequency Determination Techniques for Cantilevered Plates with Bending-Torsion Coupling. , 1984 .

[3]  S. Timoshenko,et al.  THEORY OF PLATES AND SHELLS , 1959 .

[4]  S. Rawtani,et al.  Vibration analysis of rotating cantilever plates , 1971 .

[5]  Garret N. Vanderplaats,et al.  Numerical Optimization Techniques for Engineering Design: With Applications , 1984 .

[6]  Ting Nung Shiau,et al.  Optimization of Rotating Blades with Dynamic-Behavior Constraints , 1991 .

[7]  O. Mahrenholtz,et al.  Vibration of rotating rectangular plates , 1987 .

[8]  E. A. Sadek An optimality criterion method for dynamic optimization of structures , 1989 .

[9]  E. F. Crawley,et al.  Frequency determination and non-dimensionalization for composite cantilever plates , 1980 .

[10]  J. K. Lee,et al.  Vibrations of Blades With Variable Thickness and Curvature by Shell Theory , 1984 .

[11]  Khyruddin Akbar Ansari On the Importance of Shear Deformation, Rotatory Inertia, and Coriolis Forces in Turbine Blade Vibrations , 1986 .

[12]  Jaan Kiusalaas,et al.  An algorithm for optimal structural design with frequency constraints , 1978 .

[13]  M. W. Dobbs,et al.  Application of optimality criteria to automated structural design , 1976 .

[14]  Arthur W. Leissa,et al.  Rotating Blade Vibration Analysis Using Shells , 1982 .

[15]  Robert E. Kielb,et al.  Effects of Warping and Pretwist on Torsional Vibration of Rotating Beams , 1984 .

[16]  V Ramamurti,et al.  Coriolis effect on the vibration of flat rotating low aspect ratio cantilever plates , 1981 .

[17]  M. Lalanne,et al.  Vibration Analysis of Rotating Compressor Blades , 1974 .

[18]  H. Saunders,et al.  Finite element procedures in engineering analysis , 1982 .

[19]  Chien-Chang Lin,et al.  Optimum weight design of composite laminated plates , 1991 .

[20]  G. Zoutendijk,et al.  Methods of Feasible Directions , 1962, The Mathematical Gazette.

[21]  Edward F. Crawley,et al.  The Natural Modes of Graphite/Epoxy Cantilever Plates and Shells , 1979 .

[22]  S. Putter,et al.  Natural frequencies of radial rotating beams , 1978 .

[23]  R. D. Mindlin,et al.  Influence of rotary inertia and shear on flexural motions of isotropic, elastic plates , 1951 .