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Studying Crack Resistance and Destruction Mechanism of Steel Aluminum Composite Material

  • MATERIALS MECHANICS: STRENGTH, DURABILITY, SAFETY
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Inorganic Materials Aims and scope

Abstract

Steel aluminum composite materials are widely used in engineering owing to excellent weight efficiency in combination with good mechanical properties. They are used, for instance, in the aerospace industry for production of rocket body structures, fuel tanks, and aircraft armor elements. This work is devoted to analysis of the crack resistance and the mechanism of destruction of aluminum-steel (20 vol %) composite material with the density of 2.85 g/cm3. The composite material was produced using very fine PAP-2 aluminum powder for formation of its matrix component. The reinforcing component was made of steel mesh woven from austenitic steel rope (08Kh17N13M2). The strength of the produced material upon transverse bending (550–600 MPa) was calculated by the maximum load corresponding to the first step of crack originating in the matrix. Its crack resistance at the stage of fracture initiation estimated by the parameter K1c was from 15 to 30 MPa m1/2. The crack resistance of the composite material at the stage of development of fracture was described by means of specific effective fracture work YF = 2 × 104—8 × 104 J/m2. For this composite material YF is an order of magnitude higher than for St3 steel, D16T aluminum alloy, and VT-5 titanium alloy, which is an advantage of the developed material. The high value of parameter YF is attributed to the mechanism of energy intensive destruction. It is provided by the increased energy consumption for the destruction of the bridges between the matrix aluminum layers by their shearing by the rope as a result of the action of shear stresses, for overriding of friction forces of rope drawing from the matrix, and for shearing of laminated packets inside the matrix formed by diffusion bonded scaly particles. The properties of the produced steel-aluminum composite material allow its use as a material for light structural elements operated under conditions of mechanical loading.

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Funding

This work was supported by state contract no. 11.7568.2017/B4 using the core facilities Aerospace Materials and Technologies, Moscow Aviation Institute.

Microscopic analysis was performed at the Joint Institute for High Temperatures, Russian Academy of Sciences, in accordance with the state contract of the Russian Academy of Sciences for basic research, project GR no. АААА-А-16-116051810082-7.

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Correspondence to D. A. Ivanov.

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Translated by I. Moshkin

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Ivanov, D.A., Shlyapin, S.D., Valiano, G.E. et al. Studying Crack Resistance and Destruction Mechanism of Steel Aluminum Composite Material. Inorg Mater 57, 1535–1540 (2021). https://doi.org/10.1134/S0020168521150097

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  • DOI: https://doi.org/10.1134/S0020168521150097

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