Tribological studies of aircraft engine parts made by selective laser melting

Authors

  • Sergey Dmitrievich Seliverstov Moskovskiy aviacionnyy institut (nacionalnyy issledovatelskiy universitet)
  • Ilya Alekseevich Nikolaev Moskovskiy aviacionnyy institut (nacionalnyy issledovatelskiy universitet)
  • Oksana Anatolevna Bycenko Moskovskiy aviacionnyy institut (nacionalnyy issledovatelskiy universitet)

Keywords:

selective laser melting; microstructure; fretting; blade; gas turbine engine.

Abstract

This paper presents the results of comparative tribological tests to assess the resistance of additive metal parts to fretting wear. The microstructure of the products made by selective laser melting is studied. Tribological tests were carried out on a friction machine. It is experimentally shown that the tribological properties of products printed from metal, regardless of the printing angle in the construction chamber, differ from products made using traditional technology within 7%.

Published

2021-12-10

Issue

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY