首页> 外国专利> Installation for aircraft load transportation - comprises load rails with anchor points connected by rods to aircraft in displaceable support points in deformable structure and to structure parts maintaining their shape

Installation for aircraft load transportation - comprises load rails with anchor points connected by rods to aircraft in displaceable support points in deformable structure and to structure parts maintaining their shape

机译:飞机载荷运输装置-包括带有锚固点的载荷轨,锚固点通过杆连接到可变形结构中可移位支撑点中的飞机,并保持其形状

摘要

Loading rails (24) have anchor points (22) connected to the aircraft deformable structure (14,18) in displaceable support points (b,g,h) by support rods (28,30,32,34,36). The anchor points (22) are fixed along axes (OXYZ) by the support rods to parts of the aircraft structure which maintains its shape. A first connecting rod in the longitudinal direction (OX) connects the anchor point (22) to a support point in the deformable structure, fixed in the direction (OX). A second connecting rod (28) transverse to the aircraft connects the anchor point (22) to a second support point (b) in the deformable structure, in the direction (OY). Connecting rods (30,32,34) in a plane perpendicular to the longitudinal direction connect the anchor point (22) to support points (g,h) in the structure, capable of submitting simultaneously to a displacements in the transverse and vertical (OZ) directions. USE/ADVANTAGE - Supporting , without deformation, large dimension loads inside aircraft and not requiring the addition of a rigid support system which would increase the aircraft load.
机译:装载轨道(24)具有通过支撑杆(28、30、32、34、36)在可移位的支撑点(b,g,h)中连接至飞机可变形结构(14、18)的锚定点(22)。锚定点(22)通过支撑杆沿着轴线(OXYZ)固定在飞机结构的保持其形状的部分上。沿纵向(OX)的第一连杆将锚定点(22)连接至在可变形结构中沿方向(OX)固定的支撑点。横向于飞机的第二连杆(28)在方向(OY)上将锚定点(22)连接至可变形结构中的第二支撑点(b)。在垂直于纵向的平面上的连杆(30,32,34)将锚固点(22)连接到结构中的支撑点(g,h),能够同时承受横向和垂直方向的位移(OZ )路线。使用/优点-支撑飞机内部较大的载荷,且不变形,并且不需要添加会增加飞机载荷的刚性支撑系统。

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