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GUN BORESIGHTING CONTROL APPARATUS OF AIRCRAFT

机译:飞机的炮检控制装置

摘要

PURPOSE: A gun bore sighting adjusting apparatus of an aircraft is provided to install many fuel tanks in a bay of a bulkhead, and to prevent mixture of remaining or fuel gas and pressure oil in firing by mounting a manual gun bore sighting adjuster in the limit space close to the fuel tanks. CONSTITUTION: A gun bore sighting adjusting device of an aircraft is composed of an outer eccentric cam inserted in the inner periphery of a through hole in the front of a bulkhead(10); an inner eccentric cam inserted to the outer eccentric cam with fitting the end of a gun system; an index plate(60) assembled with the front of the outer eccentric cam, and rotated in adjusting the gun bore sighting with forming an index groove; and a fixing member(70) fastened in the bulkhead, and inserted to the index groove to fix the index plate. Many fuel tanks are mounted in the bay by installing the manual gun bore sighting adjuster in the limit space of the bulkhead.
机译:目的:提供一种飞机的枪孔瞄准调整装置,以便在舱壁的舱内安装许多燃油箱,并通过在极限位置安装手动枪孔瞄准调整器来防止射击时残留的或燃料气体和压力油混合靠近油箱的空间。组成:飞机的枪孔瞄准调整装置,由一个外部偏心凸轮组成,该偏心凸轮插入在隔板前面的通孔的内周面(10);内偏心凸轮插入外偏心凸轮中,并与喷枪系统的末端相配合;分度板(60)与外偏心凸轮的前部组装在一起,并旋转以调整枪孔瞄准点并形成分度槽。固定构件(70)固定在隔板上,并插入到分度槽中以固定分度板。通过在隔板的极限空间中安装手动枪孔瞄准调节器,可将许多燃油箱安装在机架中。

著录项

  • 公开/公告号KR20020073830A

    专利类型

  • 公开/公告日2002-09-28

    原文格式PDF

  • 申请/专利权人 KOREA AEROSPACE INDUSTRIES LTD.;

    申请/专利号KR20010013698

  • 发明设计人 KIM BYEONG GU;PARK SEO SIN;

    申请日2001-03-16

  • 分类号B64C1/00;

  • 国家 KR

  • 入库时间 2022-08-22 00:30:20

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