Smovziuk L. Design-technological solutions for damaged aircraft panelling load-carrying ability restoration by composite patch adhesive bonding

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U000358

Thesis Registration Form

0411U000358.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

28-01-2011

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object is a process of paneling repair by composite patch adhesive bonding; aim is restoration of damaged aeronautic panels load-carrying ability with minimal expenses by composite patch adhesive bonding; methods are theory of elasticity, laminated materials mechanics; novelty consists in proposed for the first time comprehensive approach for structural and technological parameters of panel's load-carrying ability restoration process by patch placement and developed for this purpose theoretical method; result is expenses reduction on aeronautic damaged panels load-carrying ability restoration; field of application is aircrafts and spacecrafts manufacturing.

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Files

aref.doc

dis.doc

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