Effect of different weightage of Enovav® IC3100 silica aerogel on aluminium alloy composites in ISO2685 aviation standard fire-test

被引:2
作者
Abu Talib, Abd. Rahim [1 ,2 ]
Mohammed, Ibrahim [1 ,3 ]
Rujhan, Wahiduddeen [1 ]
Bheekhun, Nadiir Ibrahim [4 ]
机构
[1] Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
[2] Univ Putra Malaysia, Fac Engn, Aerosp Malaysia Res Ctr, Serdang 43400, Selangor, Malaysia
[3] Hassan Usman Katsina Polytech, Coll Engn, Dept Mech Engn, Katsina 2052, Nigeria
[4] Management & Sci Univ, Fac Informat Sci & Engn, Aerosp & Commun Technol Res Grp, Shah Alam 40100, Selangor, Malaysia
关键词
aluminium alloy; composite; Enova (R) IC3100; flax fibre; ISO2685; standard; MECHANICAL-PROPERTIES; FIBER;
D O I
10.1504/IJSA.2019.099923
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The study presents the use of Enova (R) IC3100 and hardener/epoxy resin on the metal alloy and a hybrid composite of metal with natural fibre (flax) with the percentage of aerogel, for use in aircraft high-temperature region. The main objective of the study is to determine the percentage amount of Enova (R) IC3100 and epoxy resin/hardener on the hybrid composite. The composites were fabricated using different percentage of aerogel in an epoxy. The composites undergo a fire test using ISO2685 propane-air burner. The results obtained indicate that a less layered aluminium alloy coated with greener and lighter substance mix with epoxy resin/hardener can be used in a high-temperature aircraft application. The hybrid composite with flax fibre presents 5-10% greater than the other composite in terms of fire resistance. The study shows that the composite of aluminium alloy 2024-T3 coated with silica aerogel possesses good properties that resist high-temperature in an aircraft component.
引用
收藏
页码:43 / 53
页数:11
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