Optimal design of multi-direction composite flywheel rotors

被引:20
作者
Gowayed, Y [1 ]
Abel-Hady, F
Flowers, GT
Trudell, JJ
机构
[1] Auburn Univ, Dept Text Engn, Auburn, AL 36849 USA
[2] Auburn Univ, Dept Mech Engn, Auburn, AL 36849 USA
[3] NASA, Glenn Res Ctr, Cleveland, OH 44135 USA
关键词
D O I
10.1002/pc.10445
中图分类号
TB33 [复合材料];
学科分类号
摘要
Design of composite flywheels made with reinforcement in the hoop and radial directions (Multiple Direction Composites MDC) involves a large multitude of parameters such as those related to the flywheel operation, flywheel geometry, material characteristics, material layup, and stress spatial distribution and values. The problem is further complicated because most design parameters are interactive and because one parameter cannot be optimized independent of the other parameters. Optimum structural design of MDC flywheels using nonlinear optimization via a sequential quadratic programming approach and parametric finite element analysis are used to address this problem. Numerical examples are solved to compare the efficacy of the two approaches.
引用
收藏
页码:433 / 441
页数:9
相关论文
共 35 条
[1]  
ASHLEY S, 1993, MECH ENG, V115, P42
[2]  
COPPA A, 1984, CP NATL AERONAUTICS, V2346
[3]  
DETERESA S, 1999, MRS B, V51
[4]  
EDWARDS K, 1994, DESIGN MANUFACTURING, V64, P237
[5]   OPTIMUM DESIGN OF COMPOSITE STRUCTURES FOR SHAPE, LAYER ANGLE AND LAYER THICKNESS DISTRIBUTIONS [J].
FUKUNAGA, H ;
SEKINE, H .
JOURNAL OF COMPOSITE MATERIALS, 1993, 27 (15) :1479-1492
[6]  
GABRYS C, 1997, J REINFORCED PLASTIC, V16
[7]  
GENDREAU J, 1997, FLYWH WORKSH NASA LE
[8]  
Genta G., 1985, KINETIC ENERGY STORA
[9]  
GOWAYED Y, 1999, FLYWH WORKSH NASA GL
[10]  
HERBST J, 1998, P SOC AUT ENG