Shmyreff V. Design of Aircraft Air Load Distribution System Subject to Gasdynamic Performance and Service Life

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0402U001568

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

17-05-2002

Specialized Academic Board

Д 64. 062.03

Essay

The aim оf the thesis is to develop procedure of aircraft air load (distribution system, (AALDS) composed of airways of air conditioning system (AIR CONU), air preparation system (AIR PREP), wing protection system (WING ANTI-ICE) and tens of others. The systems mentioned are essential components or modem airplane, and they exert Influence upon airplane competitive ability.The technique la developed to determine airways critical design factors such as material, geometric dimensions, manufacturing procedures depend upon of specified (air parameters fair consumption, pressure, temperature) and specified life time of air load d!9!nbutian system. The system of design-manufacturing measures is constituted to maintain specified aerodynamics and life time of AALDS at airplane manufacturing, operation, renewal and design,The basic outcomes are applied at design of An-74, An-70 and An-140 modern airliners.

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