Koltun S. Quality improvement of gas-turbine engine compressor rotor blades made of titanium alloys based on complex forming technology.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U002508

Thesis Registration Form

0411U002508.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

13-05-2011

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object - working compressor blades, and complex technology of their manufacturing; aim - ensuring a high level of quality parameters of a turbine engine compressor blades, methods of research - carried out research based on the general equations of continuum mechanics and fundamentals of the theory of plastic flow of metals novelty - , a new solution applied scientific and technical problems of technological options to ensure a high level of compressor blades of a turbine engine by developing a comprehensive formative technology. A mathematical model of cold rolling blade.

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Files

aref.pdf

dis.pdf

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