首页> 外国专利> Inflatable escape chute for aircraft - has central rib to give two slide paths and sliding surface overlays with varying friction

Inflatable escape chute for aircraft - has central rib to give two slide paths and sliding surface overlays with varying friction

机译:飞机充气逃生斜槽-具有中央肋,可提供两条滑动路径和滑动表面覆盖层,且摩擦力各不相同

摘要

The inflatable escape chute for aircraft has a main, generally rectangular, inflated track portion with transverse ribs, also inflatable, tensioning a stretching-web. The track comprises five longitudinal tubes: two (72, 74) of large dia. along the edges, two (78, 80) of smaller dia. inside these and a central one which increases in dia. from the smaller to the larger over the upper half-length of the chute. The slid-over surfaces have an overlay (82, 84) whose coefficient of friction may vary along its length.
机译:用于飞机的可充气逃生斜槽具有一个主要的,通常为矩形的,充气的轨道部分,该部分具有横向肋,该肋也为可充气的,张紧了张紧腹板。轨道包括五个纵向管:两个(72、74)大直径。沿着边缘,两个(78,80)较小的直径。在这些和一个中央的直径增加。在滑道的上半部从小到大。滑动表面具有覆盖物(82、84),其摩擦系数可沿其长度变化。

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