
We present the method of the choice of supports position of turbocompressor of gas turbine engine at the draft design stage with using decision support system. The formalization is achieved by using methodology of SADT. Program components of the information environment and interaction between them are considered.
Представлен метод выбора расположения опор турбокомпрессора ГТД на этапе эскизного проектирования с применением системы поддержки принятия решения. Формализация выполнена на основе методологии SADT, рассмотрены программные компоненты информационной среды и взаимодействие между ними.
АВТОМАТИЗАЦИЯ, ПРОЕКТИРОВАНИЕ, СХЕМА РАСПОЛОЖЕНИЯ ОПОР, КОНСТРУКТИВНО-СИЛОВАЯ СХЕМА ГТД
АВТОМАТИЗАЦИЯ, ПРОЕКТИРОВАНИЕ, СХЕМА РАСПОЛОЖЕНИЯ ОПОР, КОНСТРУКТИВНО-СИЛОВАЯ СХЕМА ГТД
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