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Обычная версия сайта

Центральный институт авиационного
моторостроения имени П.И. Баранова

Версия для слабовидящих

Противодействие коррупции

Rus

Array
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            [LINK] => /research/engines/
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                (
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        (
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            [LINK] => /research/strength-reliability/structural-strength-metal-alloys/
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            [DEPTH_LEVEL] => 2
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    [16] => Array
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            [LINK] => /research/strength-reliability/composite-materials/
            [SELECTED] => 
            [PERMISSION] => R
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            [IS_PARENT] => 
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        (
            [TEXT] => Динамика ГТД
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                (
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            [IS_PARENT] => 
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            [SELECTED] => 
            [PERMISSION] => R
            [ADDITIONAL_LINKS] => Array
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                    [1] => Двигатели в эксплуатации
                )

            [DEPTH_LEVEL] => 2
            [IS_PARENT] => 
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    [22] => Array
        (
            [TEXT] => Сертификация
            [LINK] => /research/strength-reliability/certification/
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            [ADDITIONAL_LINKS] => Array
                (
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            [DEPTH_LEVEL] => 2
            [IS_PARENT] => 
        )

    [23] => Array
        (
            [TEXT] => Газовая динамика и горение
            [LINK] => /research/gas-dynamics/
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                (
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            [LINK] => /research/kinetika/
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            [ADDITIONAL_LINKS] => Array
                (
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            [DEPTH_LEVEL] => 1
            [IS_PARENT] => 
        )

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            [LINK] => /research/aviation-chemmotology/
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)

Узлы авиационных двигателей

узлы_компрессора 2.jpg

Даже самая прогрессивная схема авиационного двигателя (АД) сама по себе не является гарантом создания эффективной силовой установки без тщательной проработки ее отдельных элементов. При этом каждый из этих элементов столь сложен и специфичен, что требует особой квалификации и опыта разработки именно этого узла.
В ТРДД выделяют четыре конструктивных блока, по которым в ЦИАМ сформировались отдельные направления исследовательской работы:

вентиляторы и компрессоры;
турбины;
камеры сгорания;
сопла и воздухозаборники.