A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear
學年 104
學期 1
出版（發表）日期 2015-11-23
作品名稱 A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear
作品名稱（其他語言）
著者 P. W. Chen; W. T. Huang
單位
出版者
著錄名稱、卷期、頁數 Materials Research Innovations 19(sup.9), p.142-147
摘要 This study uses finite element analysis software to conduct simulations and compares the fatigue behaviour of the aluminium alloy and glass fibre-reinforced composite that is used in light aircraft landing gear. The maximum stress, maximum strain and deformation of landing gear of different shapes (plate and tube shapes) are also determined. The results show that the composite landing gear weighs 45% less than an aluminium equivalent. Of the samples tested, plate-shaped glass fibre-reinforced composite landing gear exhibits the lowest maximum stress under a static load. Regardless of whether the landing gear is plate- or tube-shaped, the maximum strain and deformation for the composite landing gear are more than four times those for the aluminium alloy landing gear. The results for dynamic load show that plate-shaped glass fibre-reinforced composite and tube-shaped aluminium landing gear have similar maximum alternating stress under cyclic loading.
關鍵字 Light aircraft;Landing gear;Glass fibre-reinforced composites;Fatigue;Finite element analysis
語言 en
ISSN 1432-8917;1433-075X
期刊性質 國外
收錄於 EI
產學合作
通訊作者 Pu-Woei Chen
審稿制度 是
國別 GBR
公開徵稿
出版型式 ,電子版,紙本
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機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/106060 )

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