Surface Hardening in Hydraulic Cylinders for Airplane Engines

L. V. Denisov; A. G. Boitsov; M. V. Siluyanova

doi:10.3103/S1068798X18120237

Surface Hardening in Hydraulic Cylinders for Airplane Engines

Authors: Denisov L.V.¹, Boitsov A.G.¹, Siluyanova M.V.¹
Affiliations:
1. Moscow Aviation Institute
Issue: Vol 38, No 12 (2018)
Pages: 1080-1083
Section: Article
URL: https://journals.rcsi.science/1068-798X/article/view/227612
DOI: https://doi.org/10.3103/S1068798X18120237
ID: 227612

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Abstract
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Abstract

Means of increasing the reliability and durability of hydraulic cylinders for airplane engines are considered. The wear of their working surfaces may be decreased by applying a carbide–oxide coating and subsequent smoothing.

Keywords

carbide–oxide coating, smoothing, titanium alloy, hydraulic cylinder

About the authors

L. V. Denisov

Moscow Aviation Institute

Author for correspondence.
Email: x700fl@mail.ru
Russian Federation, Moscow

A. G. Boitsov

Moscow Aviation Institute

Author for correspondence.
Email: agboytsov@mail.ru
Russian Federation, Moscow

M. V. Siluyanova

Moscow Aviation Institute

Author for correspondence.
Email: dc2mati@yandex.ru
Russian Federation, Moscow

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