OPTIMUM WEIGHT DESIGN OF A ROTOR BEARING SYSTEM WITH DYNAMIC BEHAVIOR CONSTRAINTS

被引:17
作者
SHIAU, TN
HWANG, JL
机构
[1] National Cheng Kung University, Institute of Aeronautics and Astronautics, Tainan
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 1990年 / 112卷 / 04期
关键词
D O I
10.1115/1.2906189
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An efficient design algorithm for optimum weight design of a rotor bearing system with dynamic behavior constraints is investigated. The constraints include restrictions on stresses, unbalance response, and/or critical speeds. The system dynamic behaviors are analyzed by the finite element method. The exterior penalty function method is used as the optimization technique to minimize the system weight. The system design variables are the cross-sectional areas of the shaft and the stiffnesses of the bearings. The sensitivity analysis of the system parameters is also in vestigated. The example of a single spool rotor bearing system is employed to demonstrate the merits of the design algorithm with different combinations of dynamic behavior constraints. At the optimum stage, it is shown that the weight of the rotor system can be significantly reduced. Moreover, the optimum design weights are quite different for various combinations of dynamic behavior constraints. © 1990 ASME.
引用
收藏
页码:454 / 462
页数:9
相关论文
共 21 条
[1]  
CHILDS DW, 1982, ASME, V104, P412
[2]   SHEAR COEFFICIENT IN TIMOSHENKOS BEAM THEORY [J].
COWPER, GR .
JOURNAL OF APPLIED MECHANICS, 1966, 33 (02) :335-&
[3]  
DWORSKI J, 1964, ASME, V86, P149
[4]   RATES OF CHANGE EIGENVALUES AND EIGENVECTORS [J].
FOX, RL ;
KAPOOR, MP .
AIAA JOURNAL, 1968, 6 (12) :2426-&
[5]  
FRITZEN CP, 1982, NASA C PUBLICATION, V2250, P284
[6]  
GUNTER EJ, 1970, ASME, V92, P59
[7]  
Haug E. J. Jr., 1972, International Journal for Numerical Methods in Engineering, V5, P171, DOI 10.1002/nme.1620050204
[8]  
Kane TR., 1985, DYNAMICS THEORY APPL
[9]  
LUND JW, 1962, ASME, V84, P491
[10]  
LUND JW, 1979, ASME, V102, P115