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Airplane engine maintaining working ladder
The invention provides an airplane engine maintaining working ladder. The airplane engine maintaining working ladder comprises a steel structure bottom frame and a main ladder, wherein the bottom frame comprises a horizontal truss and a perpendicular truss fixed to one end of the horizontal truss; the outer end of the horizontal truss and the outer end of the perpendicular truss are provided withsupporting legs which extend downwards and are provided with universal wheels on bottoms; the main ladder is the perpendicular truss with a convex platform on top; the main ladder is mounted in the perpendicular truss of the bottom frame; the bulged part of the convex platform faces towards the other end of the horizontal truss; the periphery of the main ladder is limited in movement in the horizontal direction through 8 V-shaped guide wheels; a lifting drive mechanism is arranged between the main ladder and the bottom frame for realizing up-down movement of the main ladder; the outer end of the perpendicular truss of the bottom frame is further fixedly provided with an inclined climbing ladder which faces towards the convex platform of the main ladder; the position, which corresponds to the side surface of the inclined climbing ladder, on the main ladder is fixedly provided with a straight climbing ladder until the convex platform; and two auxiliary lifting platforms are further arranged on the horizontal truss of the bottom frame. The maintaining working ladder provided by the invention is adjustable in height, and can be applied to airplanes of various airplane types.
本发明提供一种飞机发动机维修工作梯,包括:一钢结构的底架,包括水平桁架及固定于其一端的垂直桁架,水平桁架及垂直桁架的外端设有下伸且底部带万向轮的支腿;一主梯,其为一顶部设有凸字型平台的垂直桁架;主梯安装在底架的垂直桁架内,凸字型平台的凸出部朝向水平桁架的另一端,主梯的四周通过8个V型导轮限制其水平方向的移动;主梯与底架之间设有升降驱动机构实现主梯的上下移动;底架的垂直桁架的外端还固定设有朝向主梯凸字型平台的斜爬梯,主梯上、对应于斜爬梯的侧面固定设有直爬梯至凸字型平台;底架的水平桁架上,还设有两个辅助升降平台。本发明维修工作梯,高度可调能够应用于多个机型的飞机。
Airplane engine maintaining working ladder
The invention provides an airplane engine maintaining working ladder. The airplane engine maintaining working ladder comprises a steel structure bottom frame and a main ladder, wherein the bottom frame comprises a horizontal truss and a perpendicular truss fixed to one end of the horizontal truss; the outer end of the horizontal truss and the outer end of the perpendicular truss are provided withsupporting legs which extend downwards and are provided with universal wheels on bottoms; the main ladder is the perpendicular truss with a convex platform on top; the main ladder is mounted in the perpendicular truss of the bottom frame; the bulged part of the convex platform faces towards the other end of the horizontal truss; the periphery of the main ladder is limited in movement in the horizontal direction through 8 V-shaped guide wheels; a lifting drive mechanism is arranged between the main ladder and the bottom frame for realizing up-down movement of the main ladder; the outer end of the perpendicular truss of the bottom frame is further fixedly provided with an inclined climbing ladder which faces towards the convex platform of the main ladder; the position, which corresponds to the side surface of the inclined climbing ladder, on the main ladder is fixedly provided with a straight climbing ladder until the convex platform; and two auxiliary lifting platforms are further arranged on the horizontal truss of the bottom frame. The maintaining working ladder provided by the invention is adjustable in height, and can be applied to airplanes of various airplane types.
本发明提供一种飞机发动机维修工作梯,包括:一钢结构的底架,包括水平桁架及固定于其一端的垂直桁架,水平桁架及垂直桁架的外端设有下伸且底部带万向轮的支腿;一主梯,其为一顶部设有凸字型平台的垂直桁架;主梯安装在底架的垂直桁架内,凸字型平台的凸出部朝向水平桁架的另一端,主梯的四周通过8个V型导轮限制其水平方向的移动;主梯与底架之间设有升降驱动机构实现主梯的上下移动;底架的垂直桁架的外端还固定设有朝向主梯凸字型平台的斜爬梯,主梯上、对应于斜爬梯的侧面固定设有直爬梯至凸字型平台;底架的水平桁架上,还设有两个辅助升降平台。本发明维修工作梯,高度可调能够应用于多个机型的飞机。
Airplane engine maintaining working ladder
一种飞机发动机维修工作梯
LIANG JIANBO (Autor:in) / WU HUI (Autor:in) / HUANG ZHIKUN (Autor:in) / GAO ZHIYANG (Autor:in)
07.08.2020
Patent
Elektronische Ressource
Chinesisch
IPC:
E06C
LADDERS
,
Leitern
Combined type working ladder for airplane engine maintenance
Europäisches Patentamt | 2020
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