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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

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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Форма поиска

Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 4. Отображено 4.
25-07-2023 дата публикации

Automatic assembling machine for tool handle tail pin

Номер: CN116475721A
Автор: OUYANG ZHONG, CHEN WEIJUN
Принадлежит:

The invention provides an automatic assembling machine for a tool handle tail pin, which is characterized by comprising a rack and an intermittently moving segmentation turntable, the segmentation turntable is rotatably connected to the rack, a tool positioning seat is arranged on the segmentation turntable, and a handle tail pin press-fitting device is arranged on the periphery of the segmentation turntable. In the working process, a tool which is sleeved with a tail shell and is to be provided with a tail pin serves as a workpiece to be loaded on the tool positioning base and positioned on the tool positioning base, the workpiece rotates along with the dividing rotary disc, the workpiece is conveyed to different positions and pauses intermittently, and the two working procedures of tail pin penetrating and tail pin press fitting are conducted during intermittent pause. And finally, finished product form output of handle tail pin assembly is completed. The automatic degree of assembling ...

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07-04-2023 дата публикации

Full-automatic slipper assembling machine

Номер: CN115919033A
Принадлежит:

The invention relates to a full-automatic slipper assembling machine which is characterized in that a turntable is arranged on a rack, shoe mold stations are arranged on the turntable in the rotating direction of the turntable, and an unlocking mechanism, a vamp shaping mechanism, a laminating mechanism, a screw driving mechanism and a finished product discharging mechanism which are electrically connected with a control mechanism are arranged around the turntable; the unlocking mechanism is arranged on the lower side of the rotary table, and the pair of push rods is controlled by the unlocking mechanism to unlock the shoe mold tensioning clamp and position the shoe sole on the shoe mold; the vamp shaping mechanism shapes the flat vamp into an inverted-U-shaped vamp through a male die and a female die, and the inverted-U-shaped vamp is adsorbed through a grabbing device and moved to a sole on a shoe die; the attaching mechanism is used for positioning the inverted-U-shaped vamp downwards ...

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25-07-2023 дата публикации

Anti-releasing hook

Номер: CN116477464A
Автор: OUYANG ZHONG, CHEN WEIJUN
Принадлежит:

The invention provides an anti-tripping hook which comprises a hook body and an outer sealing shell, the outer sealing shell comprises a pair of buckled shells, the hook body is packaged in the outer sealing shell, the middle of the hook body is exposed out of the outer sealing shell, the two shells are connected through a buckle structure, the buckle structure comprises a buckle arranged on one shell and a bayonet arranged on the other shell, and the buckle is connected with the buckle. And the buckles are correspondingly clamped with the bayonets. When the anti-tripping hook is used, the assembly of the outer sealing shell and the sealing of the opening of the hook body can be quickly completed only through simple buckling operation, and the unlocking and tripping between the buckle and the bayonet can be completed by one key only by pressing the main unlocking piece when the shell is disassembled, so that the disassembly and assembly efficiency of a tool on the anti-tripping hook is ...

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12-05-2023 дата публикации

Terminal guided rocket projectile

Номер: CN116105554A
Принадлежит:

The terminal guided rocket projectile comprises a head cover, a seeker, a control cabin, a warhead and a rocket engine which are sequentially arranged from the head to the tail, and a falling-off socket is arranged on the control cabin; the test socket is in signal connection with the control cabin through a CAN bus; and the test socket and the drop-off socket are symmetrically arranged by taking the central axis of the control cabin as a symmetry axis. As the test socket is additionally provided with the transmission node, original data can be directly obtained, and the transmission speed is high, so that the launching preparation time is short, the test can be quickly completed before launching, and the launching efficiency can be improved. Besides, the test socket and the drop-off socket are symmetrically arranged by taking the central axis of the control cabin as a symmetry axis, so that asymmetric aerodynamic torque can be eliminated, and the rocket projectile can fly more stably; ...

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