Fire behavioural and mechanical properties of carbon fibre reinforced aluminium laminate composites for aero-engine

Mohammed, Ibrahim; Talib, Ahmad; Sultan, Mohamed Thariq Hameed; Sadoon, Syamimi

doi:10.14419/ijet.v7i4.13.21323

Cited by 4 publications

(3 citation statements)

References 30 publications

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“…Inflammability-sensitive parts are suitable. Fire cannot penetrate FML's interior layers because of its high fibre (glass fibre) melting point 1,12,22,37) .…”

Section: Fire Resistancementioning

confidence: 99%

A Review on Mechanical Properties and Response of Fibre Metal Laminate under Impact Loading (Experiment)

Awi¹,

Abdullah²

2023

Evergreen

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Fibre metal laminate (FMLs) are hybrid composite materials which consisted of metallic layers and fibre-reinforced polymer. Currently, FMLs are becoming increasingly utilized in a wide range of applications, such as aircraft, automotive, marine, sporting goods and medical due to their specific mechanical properties like superior impact resistance and fatigue resistance. ARALL (Aramid-Reinforced Aluminium Laminate), which is based on aramid fibres, GLARE (Glass Reinforced Aluminium Laminate), which is based on high-strength glass fibres and CARALL (Carbon Reinforced Aluminium Laminate), which is based on carbon fibres, are the most commercial products FMLs. This article analyzes pertinent literature associated with experimental work on FMLs and their constituent materials subjected to impact loading. It reviewed the mechanical properties, impact performance indices, crushing behavior, failure modes, and failure mechanisms of various FML structures with different variables (impact energy, fibre orientation, layup configuration, stacking sequence, metal arrangement, direction and type of reinforcement, laminate thickness, metal thickness) under impact conditions (lateral and axial impacts). Overall, the literature on the response of FML flat plate structures to axial impact loads is unreported, and the most current research focusing on the axial crushing of FML tubes. Hence, further studies are required to increase the applicability of FMLs in applications that may be impacted under axial loading.

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“…Inflammability-sensitive parts are suitable. Fire cannot penetrate FML's interior layers because of its high fibre (glass fibre) melting point 1,12,22,37) .…”

Section: Fire Resistancementioning

confidence: 99%

A Review on Mechanical Properties and Response of Fibre Metal Laminate under Impact Loading (Experiment)

Awi¹,

Abdullah²

2023

Evergreen

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“…fire resistance [204][205][206], • resistance to electric (atmospheric) discharge [207], • impact strength [114,208,209], and • corrosion resistance [204,210,211].…”

Section: Fabrication Of Fmlsmentioning

confidence: 99%

New Advances and Future Possibilities in Forming Technology of Hybrid Metal–Polymer Composites Used in Aerospace Applications

et al. 2021

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Fibre metal laminates, hybrid composite materials built up from interlaced layers of thin metals and fibre reinforced adhesives, are future-proof materials used in the production of passenger aircraft, yachts, sailplanes, racing cars, and sports equipment. The most commercially available fibre–metal laminates are carbon reinforced aluminium laminates, aramid reinforced aluminium laminates, and glass reinforced aluminium laminates. This review emphasises the developing technologies for forming hybrid metal–polymer composites (HMPC). New advances and future possibilities in the forming technology for this group of materials is discussed. A brief classification of the currently available types of FMLs and details of their methods of fabrication are also presented. Particular emphasis was placed on the methods of shaping FMLs using plastic working techniques, i.e., incremental sheet forming, shot peening forming, press brake bending, electro-magnetic forming, hydroforming, and stamping. Current progress and the future directions of research on HMPCs are summarised and presented.

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“…The use of aluminum alloys with reinforced fiber has been gradually increased in several different industrial applications due to its lightweight structure. Among others, it finds several applications in structural design such as in aircraft, light rail, marine crafts and also bridge deck [1]- [2]. Aluminum alloy is a strain-hardened alloy material that primarily depends on the grain refinement for the strengthening mechanism due to its micro structure.…”

Section: Introductionmentioning

confidence: 99%

Burn-Through Responses of Aero-Engine Nacelle using Fiber Metal Composites by ISO2685 Propane-Air Burner

Mohammed*,

Talib

2019

IJRTE

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The paper presents experimental investigation on the behavior and burn through responses of a flat plate composite of fiber-metal laminates composites of aluminum alloy 2024-T3 with carbon and natural fibers subjected to environmental conditions in fire designated zone of an aircraft engine exposed to fire. The main purpose of this study is to know the different burn through time responses of different forms of aluminum alloy with synthetic and natural fibers. The composites were designed and developed to improve the flame fire resistance in a fire designated zone of an aircraft engine in near future for prolonged burning through time that will at least withstand the fire flame for 15 minutes according to the ISO 2685 standard. The composites are fabricated by hand lay-up method in a mold of 300 mm x 300 mm and compressed by compression machine. Based on the obtained results, some of the composites are indicated to be fireproof while some others are fire resistant. It is shown that the carbon fiber reinforced aluminum alloy laminate with only aluminum at top and bottom (CF+AA) of the composites can resist more flame temperature than the carbon fiber reinforced aluminum alloy laminate with alternate layers of aluminum and carbon fiber (CARALL) with 7.86%, the sandwich of carbon fiber with flax with 18.2% and the sandwich of carbon fiber with kenaf with 23.43%. In conclusion, the study reveals that aluminum alloy 2024-T3 with carbon fiber and some types of natural fibers composites possess good properties of resisting high temperature of fire designated zone of an aircraft engine nacelle.

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Fire behavioural and mechanical properties of carbon fibre reinforced aluminium laminate composites for aero-engine

Cited by 4 publications

References 30 publications

A Review on Mechanical Properties and Response of Fibre Metal Laminate under Impact Loading (Experiment)

A Review on Mechanical Properties and Response of Fibre Metal Laminate under Impact Loading (Experiment)

New Advances and Future Possibilities in Forming Technology of Hybrid Metal–Polymer Composites Used in Aerospace Applications

Burn-Through Responses of Aero-Engine Nacelle using Fiber Metal Composites by ISO2685 Propane-Air Burner

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