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

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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

Doctor of Engineering Science, professor

Russian Federation

M. K. Smyslova

Ufa’s state aircraft technical univercity

Email: alexey.dubin@rambler.ru

Candidate of Engineering Science

Russian Federation

A. I. Dubin

Ufa’s engine-building company

Email: alexey.dubin@rambler.ru

the manager of the laboratory

Russian Federation


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