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VEHICLE CRASHWORTHY SEAT.

机译:车辆创意座椅。

摘要

anti crash seat for a member of crew of a helicopter comprises a tub (12) connected by a support structure (18) by an energy attenuateur reglable (44) of a bending type cable.the attenuateur (46) provides a framework for the basin, three parallel vertical steel cables (68, 70, 72) connected to the end part of the opposite attenuateur.a carriage assembly and a fixed (74) on the support structure containing three sets of three rollers (86, 88, 90) rotating around three axes, horizontal vertical spaces.around which the cables are bent and deplies three when the bucket is a crash down in a crash of the helicopter.the two lower rollers of the two sets of three rollers are deplacables along their axes between a position and a position reached by going a cable associated with thethe rolls.these rollers are deplacables connect has a mechanism for adjustment of the operating manual attenuateur (126) with a maximum control on which all rollers are engaged with their cableswith an intermediate control, that only two of the three sets of three rollers are engaged with their associated cables.a control cable is only a minimum of the set of three rollers, which is not connected to the adjustment mechanism.by selecting a control limit, a control mechanism and a minimum of adjustment through adjustment of the weight of the occupant of the seat.the maximum distance of collision is reduced without adversely affecting the protection provided in the seat against the dangerous forces of acceleration.
机译:用于直升机机组人员的防撞座椅,其包括桶(12),桶(12)通过弯曲型电缆的可调节能量衰减器(44)通过支撑结构(18)连接。衰减器(46)提供了盆架。 ,三个平行的垂直钢缆(68、70、72)连接到相对的衰减器的末端部分。一个滑架组件和一个固定在支撑结构上的固定件(74),该支撑结构包含三组可旋转的三组三个滚轮(86、88、90)围绕三个轴,水平的垂直空间。当铲斗在直升机坠毁中坠落时,电缆会弯曲并弯曲成三个。两组三个滚轮中的两个下滚轮可沿其轴线在一个位置之间移动这些辊是可移动的,其连接装置具有用于调节手动衰减器(126)的机构,该机构具有最大程度的控制,所有辊都通过中间联轴器与其电缆接合。 ntrol,三个滚轮的三套中只有两个与其相关的电缆啮合。控制缆线是三个滚轮的最小组,未连接到调节机构。通过选择控制极限,控制通过调整座椅乘员的重量来实现最小的调节机构。最大的碰撞距离被减小,而不会不利地影响座椅上的保护装置免受加速危险。

著录项

  • 公开/公告号EP0065982A4

    专利类型

  • 公开/公告日1984-04-17

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP19820900240

  • 发明设计人 CAMPBELL RICHARD F.;

    申请日1981-12-07

  • 分类号B60R21/10;

  • 国家 EP

  • 入库时间 2022-08-22 08:59:43

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