Effect of different weightage of Enovav® IC3100 silica aerogel on aluminium alloy composites in ISO2685 aviation standard fire-test
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作者:
Abu Talib, Abd. Rahim
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Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
Univ Putra Malaysia, Fac Engn, Aerosp Malaysia Res Ctr, Serdang 43400, Selangor, MalaysiaUniv Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
Abu Talib, Abd. Rahim
[1
,2
]
Mohammed, Ibrahim
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Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
Hassan Usman Katsina Polytech, Coll Engn, Dept Mech Engn, Katsina 2052, NigeriaUniv Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
Mohammed, Ibrahim
[1
,3
]
Rujhan, Wahiduddeen
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Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, MalaysiaUniv Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
Rujhan, Wahiduddeen
[1
]
Bheekhun, Nadiir Ibrahim
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Management & Sci Univ, Fac Informat Sci & Engn, Aerosp & Commun Technol Res Grp, Shah Alam 40100, Selangor, MalaysiaUniv Putra Malaysia, Fac Engn, Dept Aerosp Engn, Aerodynam Heat Transfer & Prop AHTP Grp, Serdang 43400, Selangor, Malaysia
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
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.
机构:
Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea
Kim, Chang-Yeoul
Lee, Jong-Kyu
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Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea
Lee, Jong-Kyu
Kim, Byung-Ik
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机构:
Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea
机构:
Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea
Kim, Chang-Yeoul
Lee, Jong-Kyu
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机构:
Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea
Lee, Jong-Kyu
Kim, Byung-Ik
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机构:
Korea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South KoreaKorea Inst Ceram Engn & Technol, Glass & Display Team, Seoul 153801, South Korea