首页> 外国专利> Improvements in or relating to safety harness for aeronauts and the like

Improvements in or relating to safety harness for aeronauts and the like

机译:改进或相关于航空航天员等的安全带

摘要

360,605. Safety harness for aviators. MILLS EQUIPMENT CO., Ltd. and LETHERN, A. A., 56, Victoria Street, London. Oct. 10, 1930, No. 30337. [Class 141.] Safety harness for retaining an aviator in his seat comprises shoulder straps adapted to pass from one or more anchors over the aviator's shoulders and to have their ends detachably secured by fastenings on each side of the breast, and thighanchoring straps adapted to be detachably connected to fastenings on the aviator's thighs, each thigh-anchoring strap being so interconnected with a shoulder strap that the release of the shoulder straps automatically slackens the thigh-anchoring straps so that these can then slide through their anchors and permit the aviator to rise. When the safety harness is used in conjunction with parachute harness, Fig. 1, the ends of the shoulder straps G are fastened to parts A1 of the parachute harness lying on the pilot's breast by quick-release devices comprising interengaging metal loops G1, G2 attached to the parts G, A1, respectively, which are locked by a fabric-enshrouded spring steel strip J. The thigh-anchoring straps D are connected to the thigh straps A of the parachute harness by similar fastenings adapted to be automatically released when the pilot rises, after releasing the shoulder straps G. Each thigh-anchoring strap D is coupled through an adjusting buckle D1 to a strap E which passes through a side-anchor F on the floor of the cockpit to a similar centrally-disposed rear anchor F1 thence upwardly through an aperture in the back of the pilot's seat to constitute the shoulder straps G, which are interconnected by a tie behind the pilot's neck. Anchorage of the shoulders to the seat is effected by a strap H, which is looped through a rear anchor F3 and passes through loops secured to the shoulder straps G and thence downwardly on each side through an adjusting buckle H1 to the side anchors F. The buckle H1 includes a loop H2 ; by pulling on this, the pilot may lengthen the strap H enabling him to lean forward and can tighten the strap again by pulling on the free end thereof. Each locking strip J is provided with a releasing strap J1 which, when pulled, flexes the strip J and withdraws it from the loop G2, whereupon the two loops G1, G2 disengage. The straps Jl of the shoulder straps are connected together by press fasteners J3 so that they may be released simultaneously by the pilot. The straps J1 of the thigh attachments are connected by lanyards J2 to the seat. These lanyards are tensioned as the pilot rises after releasing his shoulder straps and thus disconnect the thigh-anchoring straps from the harness. In a modification, for use when no parachute harness is worn, a body harness is provided comprising chest straps K, Fig. 5, the lower ends of which are connected to each other and to the ends of a thigh strap K1, similar in form to the thigh strap A of Fig. 1, by a central quick-release device K2 of the pin-and-cotter type. The safety harness is the same as in Fig. 1 but no releasing straps are provided on the locking strips J, release being obtained from both body and safety harness by withdrawing the cotter of the quick-release device K2. According to a further modification, Figs. 7 and 8, the pilot is provided with a strap element comprising a thigh strap L and upwardlyextending chest straps L1 connected permanently at L2. The ends of straps L, L1 are connected by means similar to those of Fig. 1 to the ends of a thigh-anchoring strap D and shoulder straps M, respectively. A strap N is looped through the rear anchor F3, Fig. 8, through loops M1 at the rear ends of the shoulder straps M, down the pilot's back and through a rear anchor F1, and thence through one of two side anchors F, where it is coupled by an adjusting buckle D1 to the thighanchoring strap D. This safety harness may be used with the parachute harness shown in Fig. 1, or with the harness of Fig. 5, in which case the releasing tabs J1 are omitted. Alternatively, the harness shown in Fig. 1 may be employed with the chest and thigh strap element shown in Fig. 7. According to a still further modification, the safety harness may be employed in conjunction with fastening devices attached to or mounted on the wearer's clothing. The method of guiding the straps E and the positions of the anchorages F, F1, F3 may be varied.
机译:360,605。飞行员安全带。 MILLS EQUIPMENT CO。,Ltd.和LETHERN,A. A.,伦敦维多利亚街56号。 1930年10月10日,编号30337。[等级141]。用于将飞行员固定在其座位上的安全带包括肩带,该肩带适合从一个或多个锚定点穿过飞行员的肩膀,并通过分别固定在每个驾驶员的两端来固定其末端。胸部侧面,大腿固定带适于可拆卸地连接到飞行员大腿上的固定装置,每个大腿固定带与肩带相互连接,以至于肩带的松开会自动放松大腿固定带,以便于然后滑过他们的锚点,让飞行员升起。当安全线束与降落伞线束一起使用(图1)时,肩带G的端部通过包括相互啮合的金属环G的快速释放装置固定在降落伞线束位于飞行员胸部上的A <1>部分上<1>,G <2>分别附着在由织物包裹的弹簧钢带J锁定的部件G,A <1>上。大腿固定带D连接到降落伞的大腿带A通过释放飞行员肩带G后,飞行员升起时会自动释放的类似紧固装置,固定大腿。每个大腿固定带D通过调节扣D <1>耦合至穿过侧面固定器F的带E。驾驶舱的地板通过一个类似的居中后锚F <1>向上穿过飞行员座椅后部的一个孔,以构成肩带G,这些肩带通过飞行员脖子后面的领带相互连接。肩带固定在座椅上的是皮带H,该皮带穿过后锚F <3>并穿过固定在肩带G上的环,然后通过调节扣H <1>在每一侧向下穿过搭扣H <1>包括环H <2>;搭扣H <1>包括环H <2>。通过拉动,飞行员可以拉长皮带H,使其向前倾斜,并可以通过拉动皮带的自由端再次拉紧皮带。每个锁定条带J设置有释放带J <1>,释放带J <1>在被拉动时弯曲条带J并将其从环G2抽出,于是两个环G <1>,G <2>脱离。肩带的带J1通过压紧紧固件J3连接在一起,使得飞行员可以同时释放它们。大腿附件的带子J <1>通过挂绳J <2>连接到座椅。飞行员在松开肩带后升起时,这些挂绳会张紧,从而从安全带上断开大腿固定带。在一种变型中,为了在不佩戴降落伞背带的情况下使用,提供了包括胸带K的人体安全带,图5,胸带K的下端彼此连接并且与大腿带K 1的端部连接。在形式上类似于图1的大腿带A,是通过销钉式的中央快速释放装置K 2来实现的。安全带与图1中的安全带相同,但是在锁定条J上未提供释放带,通过撤回快速释放装置K 2的开口可从车体和安全带获得释放。根据进一步的修改,图1至图4示出了图1至图4。参照图7和图8,飞行员配备有带子元件,该带子元件包括大腿带L和在L 2上永久连接的向上延伸的胸带L 1。带子L,L 1的端部通过类似于图1的方式分别连接到大腿固定带D和肩带M的端部。一条带子N穿过图8中的后锚F <3>,穿过肩带M后端的环M <1>,沿着飞行员的背部向下,并经过后锚F <1>,因此通过两个侧面锚F中的一个,通过调节扣D <1>连接到大腿固定带D。此安全带可与图1所示的降落伞线束或图5所示的线束一起使用。 (在这种情况下,释放标签J <1>被忽略了)。可替代地,图1所示的安全带可以与图7所示的胸部和大腿带元件一起使用。根据又一变型,安全带可以与连接到或安装在穿戴者的安全带上的紧固装置结合使用。服装。引导带子E的方法和锚固件F,F 1,F3的位置可以改变。

著录项

  • 公开/公告号GB360605A

    专利类型

  • 公开/公告日1931-11-12

    原文格式PDF

  • 申请/专利号GB19300030337

  • 发明设计人

    申请日1930-10-10

  • 分类号B64D17/22;B64D25/06;

  • 国家 GB

  • 入库时间 2022-08-24 07:52:59

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号