Optimization and experiment of composite marine propellers

被引:51
作者
Lin, Ching-Chieh [2 ]
Lee, Ya-Jung [1 ]
Hung, Chu-Sung [3 ]
机构
[1] Natl Taiwan Univ, Dept Engn Sci & Ocean Engn, Taipei 106, Taiwan
[2] Ind Technol Res Inst, Mat Res Labs, Taipei 114, Taiwan
[3] Atech Composites Co Ltd, Kaohsiung, Taiwan
关键词
Fiber-reinforced plastic; FRP; Propeller; Optimization; Genetic algorithm; GENETIC ALGORITHM; WINGS;
D O I
10.1016/j.compstruct.2008.07.020
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper demonstrates the experimental result of changeable pitch propellers in composite material. The use of this composite material is to apply its characteristic of bend-twist coupling; this characteristic is applied to better performance design requirements of the propeller. Two stacking sequences are considered: the first one is a quasi isotropic sequence, while the second one is an optimum sequence obtained using a genetic algorithm. Experiments are designed considering two original propellers manufactured by the first and the second stacking sequence, respectively, and a pre-deformed propeller with the second sequence. Experimental results correspond to the same trend as the calculations and confirm the method of optimization. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:206 / 215
页数:10
相关论文
共 12 条
[1]  
ABDUL MK, 2000, MECH COMPOS MATER ST, V7, P383
[2]  
[Anonymous], 1982, SNAME T
[3]  
Jones R.M., 1999, MECH COMPOSITE MAT
[4]  
KERWIN JE, 1978, T SOC NAVAL ARCHITEC, V86, P218
[5]   Optimization of a composite rotor blade using a genetic algorithm with local search [J].
Lee, YJ ;
Lin, CC ;
Ji, JC ;
Chen, JS .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2005, 24 (16) :1759-1769
[6]   Optimized design of composite propeller [J].
Lee, YJ ;
Lin, CC .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2004, 11 (01) :17-30
[7]   Regression of the response surface of laminated composite structures [J].
Lee, YJ ;
Lin, CC .
COMPOSITE STRUCTURES, 2003, 62 (01) :91-105
[8]   Stacking sequence optimization of laminated composite structures using genetic algorithm with local improvement [J].
Lin, CC ;
Lee, YJ .
COMPOSITE STRUCTURES, 2004, 63 (3-4) :339-345
[9]  
NELKA JJ, 1974, 4113 DTNSRDC
[10]   AEROELASTIC TAILORING OF FORWARD SWEPT COMPOSITE WINGS [J].
WEISSHAAR, TA .
JOURNAL OF AIRCRAFT, 1981, 18 (08) :669-676