Voytenko S. Research of processes of the factors of a technological heredity formation at gas-turbine engines parts manufacturing from titanium alloys

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0407U004775

Thesis Registration Form

0407U004775.pdf

Applicant for

Specialization

  • 05.07.04 - Технологія виробництва літальних апаратів

26-10-2007

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Research of features of fatigue crack initiation and growth in gas turbine engines blades from titanic alloys. Calculation of residual stresses influence on fatigue resistance. Research of thermomechanical processing modes, operations of etching and ultrasonic hardening influence on characteristics of crack resistance and fatigue resistance. Is applied in Motor-Sich JSC (annual benefit - 46000 $).

Read more

Files

aref.doc

dis1.doc

dis2.doc

dis3.doc

dis4.doc

Similar theses

0407U000863

Polischuk Elena Alekseevna

Technology of inertial method of utilization of aviation ammunition taking into account safety criterion

0407U000449

Melnikov Sergij Mihailovich

Methods of technological tolerance standartization in honeycomb production for airspace production technique

0406U002975

Melnychuk Olexandr P

Modelling the Technological Processes of Hydrodynamic Trailing Edge Punching for Air System Pipelines in the Aircraft

0406U000121

Zamkovoy Vasyliy Evgeniovich

Improvement of procedures of forming internal cavities of cooled blades of gas turbine engine

0505U000251

Labur Tatyana Michaylovna

Technological fundamentals of providing the reliability of welded joints in structures of flying vehicles of plate aluminuim- lithium alloys.