首页> 外国专利> OBSERVATION HATCH IN OR FOR MILITARY EQUIPMENT

OBSERVATION HATCH IN OR FOR MILITARY EQUIPMENT

机译:军事装备或军事装备的观察舱

摘要

1409030 An observation hatch FRANCE ARMED FORCES MINISTER OF 28 Feb 1974 [8 March 1973] 9214/74 Heading F3C An observation hatch has an opening therein, a transparent dome 2, Fig. 1, for covering the opening and an armoured dome 3 for shielding the dome 2. Both domes are mounted for pivotal movements about a common axis 6 and means are provided to effect the opening and closing thereof. In an embodiment the hatch is mounted in the roof 1 of the turret of a military armoured land vehicle and is defined by a raised edge 5 of the roof. The transparent dome 2 is made of synthetic plastics material, may be hemispherical-shaped and has a supporting frame 4 attached thereto which makes a fluidtight connection with the edge 5 when the dome 2 is closed. The armoured dome 3 has its opening movement limited by a stop 8. A latch 10 is provided to releasably fasten the frame 4 to the edge 5 and a latch 9 is provided to releasably fasten the armoured dome 3 to the frame 4 of the transparent dome 2. The latch 9 comprises a slidable bolt 13, Figs. 5 and 6, which is mounted in a guide 14 carried by the frame 4, is urged by a spring 12 and has an inclined face 13a, and a keeper 11 carried by the armoured dome 3. Release of the latch 9 is effected by a handle 17 mounted on a rotatable rod 15 having a transverse finger 16 engageable in a slot in the bolt 13. The latch 10 comprises a support 18, Figs. 7 and 8, which is secured to the frame 4 and carries a two-armed member 19 having a pivot 20 with a catch 21 pivotally mounted thereon and urged by a spring 22 into engagement with the edge 5 of the roof 1. A lever 23 is pivotally mounted on a pivot 24 carried by the roof 1, is urged by a tension-spring 25, and is rotated in a clockwise direction to release the catch 21 and unfasten the transparent dome 2 from the edge 5. The latch 10 may be released externally of the hatch by a handle 28, Fig. 8, which is mounted on a rotatable spindle 26. The latter is supported by the frame 4 and has a finger 27 which is engageable with the catch 21 to release the transparent dome 2 from the hatch. The external operation of the latch 10 can be prevented by a screw 29, Figs. 9 and 10, which is carried by one arm of a bell crank lever 30 mounted on a pivot 31 supported by the member 19 and which blocks the movement of the finger 27 on the spindle 26. The means for opening and closing the armoured dome 3 from inside the hatch comprises a handle 33, Fig. 11, mounted on a rod 32 which passes through the roof 1 and carries a bevel gear 34. The latter meshes with a bevel gear 35 attached to the armoured dome 3.
机译:1409030观察舱1974年2月28日法国武装部队部长[1973年3月8日] 9214/74标题F3C观察舱中有一个开口,透明圆顶2(图1)用于遮盖该开口,装甲圆顶3用于屏蔽两个圆顶均安装成可绕着共同的轴线6作枢轴运动,并设有实现其打开和关闭的装置。在一个实施例中,舱口安装在军用装甲陆上车辆的炮塔的车顶1中,并由车顶的升高边缘5限定。透明圆顶2由合成塑料制成,可以是半球形,并具有附接到其上的支撑框架4,当封闭圆顶2时,该支撑框架与边缘5形成流体密封连接。装甲穹顶3的打开运动受到止挡件8的限​​制。提供了闩锁10以将框架4可释放地紧固到边缘5,并且提供了闩锁9以将装甲圆顶3可释放地紧固到透明穹顶的框架4。闩锁9包括可滑动的螺栓13,图1和2。如图5和图6所示,安装在由框架4支撑的导向件14中的弹簧5受到弹簧12的推动,并具有倾斜面13a,并且由铠装拱顶3支撑的保持器11由闩锁9释放。手柄17安装在可旋转的杆15上,该杆具有可接合在螺栓13上的槽中的横向指状件16。闩锁10包括支撑件18,如图1和2所示。如图7和图8所示,其固定在框架4上并带有两臂构件19,该两臂构件具有枢轴20,其上枢转地安装有钩子21,并由弹簧22推动以与屋顶1的边缘5接合。杠杆23闩锁10可枢转地安装在由屋顶1承载的枢轴24上,并由拉簧25推动,并沿顺时针方向旋转以释放卡子21并从边缘5松开透明圆顶2。闩锁10可以是通过安装在可旋转心轴26上的手柄28(图8)在舱口外部释放。该心轴由框架4支撑,并具有指状件27,该指状件可与with子21接合,以从中释放透明圆顶2舱口。闩锁10的外部操作可以通过螺钉29来防止,如图1和2所示。如图9和10所示,它由曲柄30的一个臂支撑,该曲柄30安装在由构件19支撑的枢轴31上,并阻止手指27在心轴26上的运动。用于打开和关闭铠装弹片3的装置从舱门的内部包括图11中的手柄33,手柄33安装在穿过屋顶1并带有锥齿轮34的杆32上。锥齿轮34与附接到铠装圆顶3上的锥齿轮35啮合。

著录项

  • 公开/公告号GB1409030A

    专利类型

  • 公开/公告日1975-10-08

    原文格式PDF

  • 申请/专利权人 FRANCE MINISTER OF ARMED FORCES;

    申请/专利号GB19740009214

  • 发明设计人

    申请日1974-02-28

  • 分类号E05B53/00;

  • 国家 GB

  • 入库时间 2022-08-23 03:37:13

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