Purgina S. Design and structural-technological decisions of energy-efficient shape-generating tool with required life time for aircraft composite structures curing

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U000879

Thesis Registration Form

0411U000879.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

18-03-2011

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object is a shape-generating tool for polymeric composite aircraft structures manufacturing; aim is energy consumption and costs reduction on manufacturing of composite aircraft structures with high accuracy of shape as a result of self-heated shape-generating tool with required life time application; methods are theory of elasticity, laminated materials mechanics, thermodynamics; novelty consists in proposed and implemented for the first time new approach for design of shape-generating tool for composite structures manufacturing that provide required service life, minimal heat sink and minimal manufacturing process cost; result is expenses reduction on aircraft composite structures manufacturing; field of application is aircrafts and spacecrafts manufacturing.

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Files

aref.doc

dis.doc

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