Optimum design of hybrid composite multi-ring flywheel rotor based on displacement method

被引:26
作者
Wen, Shaobo [1 ,2 ]
Jiang, Shuyun [1 ]
机构
[1] Southeast Univ, Sch Mech Engn, Nanjing 211189, Peoples R China
[2] Nanjing Inst Technol, Dept Vehicle Engn, Nanjing 211167, Peoples R China
基金
美国国家科学基金会;
关键词
Hybrid composites; Laminate; Strength; Modelling; Residual stress; ENERGY; TECHNOLOGY; SYSTEMS; STORAGE;
D O I
10.1016/j.compscitech.2012.03.007
中图分类号
TB33 [复合材料];
学科分类号
摘要
A structure optimum design based on the displacement method has been performed to maximize the energy storage capacity of a hybrid composite multi-ring flywheel rotor. In the process of optimal design, the preload stress generated by interference assembly, the fiber material failure and the delamination between two adjacent rings under high speed rotation are all considered. Four types of the optimal schemes of energy storage capacity, energy per unit mass (EPM), energy per unit volume (EPV), energy per unit cost (EPC) and energy per unit mass and cost (EPMC) are proposed to satisfy the needs of different applications and optimal designs are carried out by using a sequential quadratic programming (SQP). The optimal results show that all composed rings of the hybrid flywheel rotor can nearly reach the limits of strength in both radial and circumferential directions, and simultaneously the rotor is at the critical state of delamination. The radius parameters and the maximum allowed rotational speed of the hybrid composite flywheel are closely related to the optimal schemes. Considering the effects of angular acceleration and gravity on the delamination will result in the decreasing of energy storage capacities for four typical applications. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:982 / 988
页数:7
相关论文
共 22 条
[1]  
[Anonymous], 1970, Theory of elasticity (3rd Edition)
[2]   Deformation and life analysis of composite flywheel disk systems [J].
Arnold, SM ;
Saleeb, AF ;
Al-Zoubi, NR .
COMPOSITES PART B-ENGINEERING, 2002, 33 (06) :433-459
[3]   Optimal design of press-fitted filament wound composite flywheel rotors [J].
Arvin, AC ;
Bakis, CE .
COMPOSITE STRUCTURES, 2006, 72 (01) :47-57
[4]  
Behrang M., 2008, COMPUT CHEM ENG, V32, P1447
[5]   Flywheel technology - Past, present, and 21st century projections [J].
Bitterly, JG .
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 1998, 13 (08) :13-16
[6]   Flywheel energy and power storage systems [J].
Bolund, Bjorn ;
Bernhoff, Hans ;
Leijon, Mats .
RENEWABLE & SUSTAINABLE ENERGY REVIEWS, 2007, 11 (02) :235-258
[7]   Flywheel technology development program for aerospace applications [J].
Christopher, DA ;
Beach, R .
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 1998, 13 (06) :9-14
[8]  
Corbin CK, 2004, ENGINEERING, CONSTRUCTION AND OPERATIONS IN CHALLENGING ENVIRONMENTS: EARTH AND SPACE 2004, P890
[9]   ADVANCED COMPOSITE FLYWHEEL STRUCTURAL DESIGN FOR A PULSED DISK ALTERNATOR [J].
CURTISS, DH ;
MONGEAU, PP ;
PUTERBAUGH, RL .
IEEE TRANSACTIONS ON MAGNETICS, 1995, 31 (01) :26-31
[10]   Review of failure criteria of fibrous composite materials [J].
Echaabi, J ;
Trochu, F ;
Gauvin, R .
POLYMER COMPOSITES, 1996, 17 (06) :786-798