About relaxational resistance of the compressor’s blades from titanium alloys

Abstract


The questions of fatigue strength and surface parameters of the compressor’s blades gas-turbine’s engine (GTE) from titanium alloy VT6 investigation are considered. The complex vacuum-plasma treatment of the surface (CVPT) comparing with serial (base) technology is described. Recommendations for practice use of CVPT technology are given.


About the authors

A. M. Smyslov

Ufa’s state aircraft technical univercity

Author for correspondence.
Email: alexey.dubin@rambler.ru

Russian Federation

Doctor of Engineering Science, professor

M. K. Smyslova

Ufa’s state aircraft technical univercity

Email: alexey.dubin@rambler.ru

Russian Federation

Candidate of Engineering Science

A. I. Dubin

Ufa’s engine-building company

Email: alexey.dubin@rambler.ru

Russian Federation

the manager of the laboratory

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