首页> 外国专利> Mirror Tilting Mechanism for Artificial Satellite with the Fail-Safe Mechanism to Secure the Main Optical Path When Emergancy Mode

Mirror Tilting Mechanism for Artificial Satellite with the Fail-Safe Mechanism to Secure the Main Optical Path When Emergancy Mode

机译:人造卫星的反射镜倾斜机制,带有故障保护机制,可确保出现紧急模式时的主要光路

摘要

PURPOSE: A mirror driving apparatus for an artificial satellite with a safety device is provided to rotate a correction mirror by using a drive unit, thereby providing the infrared ray information to a correctable infrared ray detection unit. CONSTITUTION: A mirror driving apparatus for an artificial satellite with a safety device comprises a safety device. The safety device forcibly turns a correction mirror (201) to a first position separately from a mirror driving unit (204). The safety device comprises a restriction removal unit (207) and a static load spring (208). The restriction removal unit connects the end part of the other side of a mirror supporting frame (202) with a rotary shaft of the mirror driving unit, and separates the end part of the other side of a mirror supporting frame (202) from a rotary shaft of the mirror driving unit as occasion demands. The static load spring has one end which is mounted on a main frame (203) and the other end which is mounted to the mirror supporting frame, and provides a restoring force for the correction mirror to move from a second position to a first position.
机译:用途:具有安全装置的人造卫星的镜驱动装置被设置为通过使用驱动单元来旋转校正镜,从而将红外线信息提供给可校正的红外线检测单元。构成:具有安全装置的人造卫星镜驱动装置,包括安全装置。安全装置与镜驱动单元(204)分开地将校正镜(201)强制旋转到第一位置。该安全装置包括限制去除单元(207)和静态负载弹簧(208)。限制去除单元将镜支撑框架(202)的另一侧的端部与镜驱动单元的旋转轴连接,并且将镜支撑框架(202)的另一侧的端部与旋转体分开。视情况需要后视镜驱动单元的轴。静态负载弹簧的一端安装在主框架(203)上,另一端安装在反射镜支撑框架上,并为恢复镜提供从第二位置移动到第一位置的恢复力。

著录项

  • 公开/公告号KR101303091B1

    专利类型

  • 公开/公告日2013-09-06

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20120001189

  • 发明设计人 이경민;오현웅;

    申请日2012-01-04

  • 分类号B64G1/36;G02B7/182;G01J5/48;

  • 国家 KR

  • 入库时间 2022-08-21 16:24:31

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