Multi Objective Optimization of Drilling Parameters Using Genetic Algorithm

被引：19

作者：

Saravanan, M. ^{[1
]}

Ramalingam, D. ^{[2
]}

Manikandan, G. ^{[3
]}

Kaarthikeyen, R. Rinu ^{[4
]}

机构：

[1] VPV Coll Engn, Periyakulam, Tamil Nadu, India

[2] Einstein Coll Engn, Mech Engn, Tirunelyeli, India

[3] Sri Vidya Coll Engn & Technol, Virudunagar, India

[4] PSG Inst Technol, AUG Mech, Coimbatore, Tamil Nadu, India

来源：

INTERNATIONAL CONFERENCE ON MODELLING OPTIMIZATION AND COMPUTING | 2012年 / 38卷

关键词：

CFRP Laminate Composite Materials; Drilling; Eccentricity; Feed Rate; Finite Element Formulation; Genetic Algorithm; Multi Objective Optimization; Material Removal Rate; DELAMINATION; DAMAGE;

D O I：

10.1016/j.proeng.2012.06.027

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Drilling operation on the aircraft and unmanned ariel vehicle made of composite materials is considered as a precarious and highly sensitive operation. Due to the problem of delamination and eccentricity of drilled hole which leads to loosening of rivets in joining various structures is challenging. Hence in modern research of manufacturing process the multi objective optimization of drilling parameters has become an embryonic topic. In this paper the feed rate and the torque of drilling tool has been selected as input parameters and the multi objective optimization of drilled hole has been carried out. The optimization parameters considered are the hole eccentricity and material removal rate. Carbon fibre reinforced plastic composite material has been chosen for investigation. The maximum and minimum eccentricity limits have been computed by Finite element formation. Genetic Algorithm optimization technique has been formulated. Experimental investigation has been carried out and compared with numerical method and soft computing techniques. (c) 2012 Published by Elsevier Ltd. Selection and/or peer-review under responsibility of Noorul Islam Centre for Higher Education

引用

页码：197 / 207

页数：11

共 18 条

[11] Delamination analysis in drilling process of glass fiber reinforced plastic (GFRP) composite materials [J].

Mohan, N. S. ;

Kulkarni, S. M. ;

Ramachandra, A. .

JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 2007, 186 (1-3) :265-271

[12] Experimental analysis of drilling damage in thin carbon/epoxy plate using special drills [J].

Piquet, R ;

Ferret, B ;

Lachaud, F ;

Swider, P .

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (10) :1107-1115

[13]

SADAT AB, 1992, ASME J E RES TECHNOL, V114, P139

[14] Multi-objective optimization of cutting parameters for drilling laminate composite materials by using genetic algorithms [J].

Sardinas, Ramon Quiza ;

Reis, Pedro ;

Davim, J. Paulo .

COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (15) :3083-3088

[15] CALCULATION OF MAIN CUTTING EDGE FORCES AND TORQUE FOR DRILLS WITH ARBITRARY POINT GEOMETRIES [J].

STEPHENSON, DA ;

AGAPIOU, JS .

INTERNATIONAL JOURNAL OF MACHINE TOOLS & MANUFACTURE, 1992, 32 (04) :521-538

[16] Taguchi analysis of delamination associated with various drill bits in drilling of composite material [J].

Tsao, CC ;

Hocheng, H .

INTERNATIONAL JOURNAL OF MACHINE TOOLS & MANUFACTURE, 2004, 44 (10) :1085-1090

[17] The effect of chisel length and associated pilot hole on delamination when drilling composite materials [J].

Tsao, CC ;

Hocheng, H .

INTERNATIONAL JOURNAL OF MACHINE TOOLS & MANUFACTURE, 2003, 43 (11) :1087-1092

[18] Assessment of the exit defects in carbon fibre-reinforced plastic plates caused by drilling [J].

Zhang, HJ ;

Chen, WY ;

Chen, DC ;

Zhang, LC .

PRECISION MACHINING OF ADVANCED MATERIALS, 2001, 196 :43-52

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