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Titanium Alloy Fasteners for Aerospace Engineering

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Abstract

A new production technology is proposed for VT16 alloy fasteners. The destructive loads in fracture and shear are considerably greater than those of comparable mass-produced fasteners. The technological parameters and weight of the fasteners produced meet the requirements of aerospace engineering.

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REFERENCES

  1. Volodin, V.A., Vorob’ev, I.A., and Kolachev, B.A., Tekhnologiya izgotovleniya titanovykh detalei krepleniya (Manufacturing Technology for Titanium Fastener Parts), Moscow: Metallurgiya, 1996.

  2. Kolachev, B.A. and Glazunov, S.G., Metallografiya titanovykh splavov (Metallography of Titanium Alloys), Moscow: Metallurgiya, 1980.

  3. Glazunov, S.G. and Kolachev, B.A., Metallovedenie titana i ego splavov (Metallurgy of Titanium and Its Alloys), Moscow: Metallurgiya, 1982.

  4. Glazunov, S.G. and Moiseev, V.N., Konstruktsionnye titanovye splavy (Construction Titanium Alloys), Moscow: Metallurgiya, 1974.

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Correspondence to I. A. Vorob’ev or T. Sh. Galiakhmetov.

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The authors declare that they have no conflicts of interest.

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Translated by B. Gilbert

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Vorob’ev, I.A., Galiakhmetov, T.S. Titanium Alloy Fasteners for Aerospace Engineering. Russ. Engin. Res. 43, 771–776 (2023). https://doi.org/10.3103/S1068798X23070389

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  • DOI: https://doi.org/10.3103/S1068798X23070389

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