首页> 外国专利> BUFFER DEVICE FOR CAPTURING HIGH-TEMPERATURE FLYING-OFF SAMPLE IN SUPERGRAVITY ENVIRONMENT

BUFFER DEVICE FOR CAPTURING HIGH-TEMPERATURE FLYING-OFF SAMPLE IN SUPERGRAVITY ENVIRONMENT

机译:用于捕获高温飞行级别的高温飞行样品的缓冲装置

摘要

A buffer device for capturing a high-temperature flying-off sample in a supergravity environment. An outer flange at the bottom of a lower support body (9) is fixed on a test device base; an upper support body (3) is fixed at the top of the lower support body; a buffer body (5) is arranged in a through hole groove of the lower support body and a vertical channel of the upper support body; a poke rod (2) is assembled in an upper special-shaped groove (3-3) formed in the upper support body; a locking shaft (4) is hinged in a hinging hole (3-4) of the upper special-shaped groove; the poke rod passes through the upper special-shaped groove of the upper support body and a lower special-shaped groove (5-2) of the buffer body extend into a vertical through hole of the buffer body; a buffer structure (10) is assembled on a lower-layer partition plate (11); the upper support body (3) is provided with four grooves (3-2), each groove is provided with a guide groove (3-1) and provided with a blocking piece (6), and blocking piece guide bars (6-2) are embedded in the guide grooves and move along the guide grooves; and after the poke rod penetrates a limiting groove (6-1) of the blocking piece upwards, a journal of the poke rod is in contact connection with an outer side face of the blocking piece. The present buffer device can be assembled simply and used conveniently, can quickly capture and isolate a high-temperature flying-off sample, and can effectively solve the problem of the high-temperature flying-off sample damaging a test cabin under supergravity.
机译:用于捕获超级度环境中的高温飞出样品的缓冲装置。下支撑体(9)底部的外凸缘固定在测试装置基座上;上支撑体(3)固定在下支撑体的顶部;缓冲体(5)布置在下支撑体的通孔槽中和上支撑体的垂直通道;戳杆(2)组装在形成在上支撑体中的上部特殊形状的凹槽(3-3)中;锁定轴(4)在上部特殊形状槽的铰接孔(3-4)中铰接;戳杆穿过上支撑体的上部特殊形状凹槽,缓冲体的下部特殊形状的凹槽(5-2)延伸到缓冲体的垂直通孔中;缓冲结构(10)组装在下层隔板(11)上;上支撑体(3)设置有四个凹槽(3-2),每个凹槽设置有引导槽(3-1)并设置有阻挡件(6)和阻挡件引导杆(6-2 )嵌入引导槽中并沿着引导槽移动;在戳杆渗透到阻挡件的限制槽(6-1)之后,戳杆的轴颈与阻挡件的外侧面接触。本缓冲装置可以简单地组装并方便地使用,可以快速捕获和分离高温飞行样品,并可以有效地解决高温飞行样本损坏超级级测试舱的问题。

著录项

  • 公开/公告号WO2020206715A8

    专利类型

  • 公开/公告日2021-09-16

    原文格式PDF

  • 申请/专利权人 ZHEJIANG UNIVERSITY;

    申请/专利号WO2019CN83492

  • 发明设计人 WEI HUA;LIN WEIAN;CHEN YUNMIN;ZHANG ZE;

    申请日2019-04-19

  • 分类号G01N3/02;G01N3/08;G01N3/18;

  • 国家 CN

  • 入库时间 2024-06-14 22:05:17

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