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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Применить Всего найдено 2. Отображено 2.
14-07-2023 дата публикации

Offshore platform rocket transportation device

Номер: CN116424569A
Принадлежит:

The invention relates to the technical field of rocket transportation, in particular to an offshore platform rocket transportation device which comprises a frame, a telescopic cylinder active damping assembly is arranged on the frame, the telescopic cylinder active damping assembly comprises a telescopic cylinder, and an elastic piece passive damping assembly is further arranged on the frame. The elastic piece passive damping assembly comprises an elastic piece, the elastic piece and the telescopic cylinder are arranged up and down, and the elastic piece is used for elastically stretching out and drawing back when subjected to vibration acting force. A shock absorption system combining the telescopic cylinder active shock absorption assembly and the elastic piece passive shock absorption assembly is formed, the elastic piece passive shock absorption assembly has the good effects of absorbing sudden impact and high-frequency shock and reducing noise, then the telescopic cylinder active shock ...

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25-07-2023 дата публикации

Rocket erecting device for offshore platform

Номер: CN116481380A
Принадлежит:

The invention provides a rocket erecting device for an offshore platform, the rocket erecting device comprises a base and an erecting frame, the erecting frame is provided with a supporting structure used for supporting and placing a rocket and a locking mechanism used for fixing the rocket on the erecting frame in the erecting process, one end of the erecting frame is hinged to the base, and the other end of the erecting frame is hinged to the base. At least two telescopic cylinders are arranged between the supporting structure and the base, the telescopic cylinders are used for driving the erecting frame to erect, the telescopic cylinders are arranged on the two sides of the erecting frame in the width direction of the erecting frame, or the telescopic cylinders are arranged on the side, back to the supporting structure, of the erecting frame at intervals in the length direction of the erecting frame; the rocket erecting device further comprises a cross coupling controller and a sensor ...

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