Klimenko V. Structural and technological methods of increase of bolt joints of titanium elements fatigue life for aircraft design taking fretting corrosion into consideration.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0409U000199

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

19-12-2008

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Objective: Design of bolted joints with scheduled fatigue life; novelty: there have been created experiment-calculated relationships for prediction of fatigue life of titanium components of shear bolt joints of aircraft design taking fretting corrosion into consideration; there have been proposed and investigated structural and technological methods of increase of fatigue life of titanium components of shear bolt joints of aircraft design taking fretting corrosion into consideration.

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