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Load sensor for helicopter skid energy-absorbing landing gear

机译:直升机防滑吸能起落架的载荷传感器

摘要

The shear beam extends between installation tabs (32, 34) in which are defined holes for mounting the load sensor to the helicopter fuselage (18) by fasteners (64). An arcuate part of the beam is a load bearing area which senses the change in shear force exerted by the fuselage cross-tubes (16) under landing load. On either side of the shear beam, a pair of webs of reduced cross-thickness mounts a set of four steam gauges (5a,b,c,d) each with its grid lines disposed at forty five degrees of arc relative to the beam. A raised boss (60) sustains overloads as during a crash or heavy landing.
机译:剪切梁在安装凸片(32、34)之间延伸,安装凸片上有限定的孔,用于通过紧固件(64)将载荷传感器安装到直升机机身(18)上。梁的弧形部分是一个承载区域,该区域可感测着陆横梁(16)在着陆负载下施加的剪切力的变化。在剪切梁的任一侧,一对厚度减小的腹板安装了一组四个蒸汽计(5a,b,c,d),每个蒸汽计的网格线相对于梁成45度角。凸起的凸台(60)在碰撞或重着陆时承受过载。

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