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Fiber Metal Laminates Based on Aluminum–Lithium Alloy Sheets in New-Generation Aircraft

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Abstract

Fiber metal laminates based on aluminum–lithium alloy sheets are considered. The basic characteristics of such materials are considered as a function of their laminar structure. Tests show that laminar hybrids are preferable to traditional aluminum-alloy structures.

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Authors and Affiliations

  1. Russian Institute of Aviation Materials, Moscow, Russia

    E. N. Kablov, V. V. Antipov, R. I. Girsh, N. Yu. Serebrennikova & A. N. Konovalov

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  1. E. N. Kablov
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  2. V. V. Antipov
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  3. R. I. Girsh
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  4. N. Yu. Serebrennikova
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  5. A. N. Konovalov
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Correspondence to E. N. Kablov.

Additional information

Translated by B. Gilbert

This research was conducted as part of the program on strategic trends in materials processing up to 2030 (with particular attention to high-strength, crack-resistant laminar metallic materials) [1].

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Kablov, E.N., Antipov, V.V., Girsh, R.I. et al. Fiber Metal Laminates Based on Aluminum–Lithium Alloy Sheets in New-Generation Aircraft. Russ. Engin. Res. 41, 215–221 (2021). https://doi.org/10.3103/S1068798X21030060

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  • DOI: https://doi.org/10.3103/S1068798X21030060

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