alternativeАльтернативная энергетика и экология (ISJAEE)Alternative Energy and Ecology (ISJAEE)1608-8298Международный издательский дом научной периодики "Спейс10.15518/isjaee.2024.02.182-197alternative-2364Research ArticleТРАНСПОРТНЫЕ ЭКОЛОГИЧЕСКИЕ СРЕДСТВА. МУЛЬТИРЕЖИМНЫЕ ТРАНСПОРТНЫЕ СРЕДСТВАENVIRONMENTAL VEHICLES. MULTY MODE VEHICLESАнализ создания пускового момента трехкаскадного синхронного генератора для новой электростартерной системы на базе водородных топливных элементовAnalysis of the creation of the starting torque of a three-stage generator for a new electric starter system based on hydrogen fuel cellsЖарковМ. А.ZharkovM. A.

Жарков Максим Андреевич, кандидат техн. наук, доцент кафедры Электроники и Электротехники, заместитель директора Института силовой электроники

630073, Новосибирск, пр. Карла Маркса, 20

Zharkov Maksim Andreevich, candidate of Technical Sciences, Associate Professor of the Department of EE, Deputy Director of the Institute of Power Electronics

630073, Novosibirsk, Karl Marx Ave., 20

maks.zharkoff@yandex.ruСарахановаР. Ю.SarakhanovaR. Yu.

Сараханова Регина Юрьевна, младший научный сотрудник

630073, Новосибирск, пр. Карла Маркса, 20

Sarakhanova Regina Yurievna, engineer, Institute of power electronics

630073, Novosibirsk, Karl Marx Ave., 20

sarakhanova_nstu@mail.ruХаритоновС. А.KharitonovS. A.

Харитонов Сергей Александрович, доктор технических наук, профессор, заведующий кафедрой Электроники и Электротехники, директор Института силовой электроники

630073, Новосибирск, пр. Карла Маркса, 20

Kharitonov Sergey Aleksandrovich, Doctor of Science, Professor, Head Department of Electronics and Electrical Engineering, Director of Institute of Power Electronics

630073, Novosibirsk, Karl Marx Ave., 20

kharit1@yandex.ruНовосибирский Государственный Технический УниверситетРоссияNovosibirsk State Technical UniversityRussian Federation20241505202402182197Copyright © Международный издательский дом научной периодики "Спейс, 20232023Международный издательский дом научной периодики "СпейсМеждународный издательский дом научной периодики "Спейсhttps://www.isjaee.com/jour/about/submissions#copyrightNoticehttps://www.isjaee.com/jour/article/view/2364

Современные тенденции в отраслях, связанных с автономными, подвижными объектами, такими как авиастроение, направлены на увеличение доли электрификации или на полную замену всех агрегатов в пользу электрических. Замена узлов и агрегатов на полностью электрические соответствует концепции полностью электрического самолета, основой которого являются новые источники питания и источники электродвижения, такие как – литий-ионные аккумуляторы, водородные элементы питания, источники на основе возобновляемой энергетики. В то же время повышаются требования к энергоэффективности и массогабаритным показателям узлов и агрегатов. Эти потребности могут быть учтены за счет многоцелевого использования оборудования, а также с помощью новых систем, сочетающих в себе ряд функций. В статье рассматривается использование авиационного трёхкаскадного синхронного генератора в качестве пускового устройства для газотурбинного двигателя. Проанализированы проблемы, связанные с использованием трёхкаскадного генератора, и предложен способ их решения. В статье представлен способ создания пускового момента с использованием реактивной составляющей электромагнитного момента для синхронного явнополюсного генератора. Анализ проведен с точки зрения формирования электромагнитного момента в авиационном генераторе с помощью инвертора напряжения. Получено обобщенное выражение для момента, регулируемое и управляемое электрическими параметрами преобразователя частоты.

Current trends in industries related to autonomous, mobile objects, such as aircraft manufacturing, are aimed at increasing the share of electrification or completely replacing all units in favor of electric ones. Replacing components and assemblies with fully electric ones corresponds to the concept of a fully electric aircraft, which is based on new power sources and sources of electric propulsion, such as lithium-ion batteries, hydrogen batteries, and sources based on renewable energy. At the same time, the requirements for energy efficiency and weight and size parameters of components and assemblies are increasing. These needs can be met through the multi-purpose use of equipment, as well as through new systems that combine a number of functions. The article discusses the use of an aircraft three-stage synchronous generator as a starting device for a gas turbine engine. The problems associated with the use of a three-stage generator are analyzed and a method for solving them is proposed. The article presents a method for creating a starting torque using the reactive component of the electromagnetic torque for a synchronous salient pole generator. The analysis was carried out from the point of view of the formation of electromagnetic torque in an aircraft generator using a voltage inverter. A generalized expression for the torque is obtained, regulated and controlled by the electrical parameters of the frequency converter.

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The authors declare that there are no conflicts of interest present.