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Landing gear with skids and anti-tilting method of a rotorcraft provided with such a landing gear

机译:带有起落架的起落架和具有这种起落架的旋翼飞机的防倾斜方法

摘要

The gear (1) has bases (11, 12) connected together by front and rear cross-pieces (8, 2), and provided with a longitudinal support part and another longitudinal support part (120), respectively. A sliding unit (15) includes one surface (41) e.g. curved plane plate, and another surface (42) that are fixed on contact areas (51, 52) partially covering front parts (20, 30) of one of the bases, respectively. Each support part includes a tube with given diameter. One of the surfaces includes a contact strip with the ground contact width of value between 120 to 140 percent of the diameter. An independent claim is also included for a method for limiting risk of tilting, and preventing the tilting toward the front or on a side of a rotocraft during landing.
机译:齿轮(1)具有通过前,后横档(8、2)连接在一起的基部(11、12),并且分别设有纵向支撑部分和另一个纵向支撑部分(120)。滑动单元(15)包括一个表面(41),例如表面。弯曲的平板以及固定在接触区域(51、52)上的另一表面(42)分别部分地覆盖其中一个基座的前部(20、30)。每个支撑部分包括具有给定直径的管。其中一个表面包括一个接触条,其接地宽度的值在直径的120%到140%之间。还包括一种独立权利要求,该方法用于限制倾斜的风险,并防止在着陆期间朝着旋翼机的前部或侧面倾斜。

著录项

  • 公开/公告号PL2420444T3

    专利类型

  • 公开/公告日2013-02-28

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号PL20110006446T

  • 发明设计人 PRUDHOMME-LACROIX PIERRE;

    申请日2011-08-05

  • 分类号B64C25/52;

  • 国家 PL

  • 入库时间 2022-08-21 16:40:15

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