首页> 外国专利> Improvements in or relating to emergency oxygen valves for use with aviator's oxygen masks

Improvements in or relating to emergency oxygen valves for use with aviator's oxygen masks

机译:与飞行员的氧气面罩配合使用的紧急氧气阀或与之相关的改进

摘要

789,466. Respiratory appliances. ARO EQUIPMENT CORPORATION. June 14, 1955 [Dec. 13, 1954], No. 17068/55. Class 81 (2). [Also in Group XXIX] A valve connected between an aviator's breathing mask and an oxygen supply bottle carried by the aviator and which automatically opens in the event of a parachute jump, comprises a valve body 10 mounted on an oxygen bottle 14 and connected by a tube 23 to a breathing mask. The body houses a normally closed, spring-loaded valve member 24 which is operably associated with a toggle comprising levers 43, 44 mounted on a pivot pin 46 and over-centre springs 52. The toggle is connected by a link 55 to a reset stem 54 held in inoperative position by a shear-pin 55b and connected by a flexible cable 62 to a quick-release mechanism A. The quick-release mechanism comprises a hook member 86 connected to the aircraft structure and a spring-loaded pin 68 secured to the member 86 by means of indents 72 in the pin, balls 76 and a collar 74. On a jump being made the cable 62 is tautened, whence the stem 54 operates the toggle to unseat the valve member 24. The pin 68 is subsequently pulled downwardly against its spring so that the balls 76 are released and the pin 68 freed from the member 86. Prior to jumping, the aviator should remove the shear pin 55b but in the event of this being overlooked it will be sheared by the stem 54 when the cable 62 is tautened. A removable cap 60 per mits re-setting of the valve in its closed position and a check valve 102 protected by a removable cap 112 allows the bottle 14 to be recharged. The oxygen from the bottle passes through a filter 34 and a ceramic pin 36 to regulate the flow.
机译:789,466。呼吸器。 ARO设备公司。 1955年6月14日[十二月[1954年13月13日],第17068/55号。等级81(2)。 [也在第XXIX组中]连接在飞行员的呼吸面罩和由飞行员携带的供氧瓶之间的阀,该阀在跳伞时自动打开,该阀包括安装在氧瓶14上并通过阀门连接的阀体10。管23到呼吸面罩。主体容纳常闭的,弹簧加载的阀构件24,该阀构件24与肘节可操作地相关联,该肘节包括安装在枢轴销46上的杠杆43、44和偏心弹簧52。肘节通过连杆55连接至复位杆。 54通过剪切销55b保持在不工作位置,并通过柔性电缆62连接到快速释放机构A。快速释放机构包括连接到飞机结构的钩构件86和固定到飞机结构的弹簧加载销68。通过销,球76和套环74中的凹口72将部件86固定。在跳动时,拉紧电缆62,然后,杆54操作肘节使阀部件24松开。随后拉动销68。向下抵抗其弹簧,使球76松开,销子68从构件86上松开。在跳动之前,飞行员应卸下剪切销子55b,但如果忽略了该情况,则当杆54松开时,它将被杆54剪切。电缆62被拉紧。可移动盖60允许将阀重新设置在其关闭位置,并且由可移动盖112保护的止回阀102允许对瓶14进行再填充。来自瓶的氧气通过过滤器34和陶瓷销36以调节流量。

著录项

  • 公开/公告号GB789466A

    专利类型

  • 公开/公告日1958-01-22

    原文格式PDF

  • 申请/专利权人 THE ARO EQUIPMENT CORPORATION;

    申请/专利号GB19550017068

  • 发明设计人

    申请日1955-06-14

  • 分类号A62B7/14;B01D3/28;

  • 国家 GB

  • 入库时间 2022-08-23 20:26:07

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