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Raisable landing gear for wide-body aircraft, of the type a vertical lifting

机译:可升降起落架,用于宽体飞机,垂直升降类型

摘要

The invention relates to a raisable landing gear for wide-body aircraft, of the type that are raised vertically, comprising a plurality of legs arranged one behind the other to form, in the undercarriage-down position, a row parallel to the median longitudinal plane of the aircraft, and at the end of each of which is mounted a pair of roues.conformément to the invention, each leg (101) comprises a tubular enclosure (102) is rigidly secured to a structure of the airplane, a balance (103) articulated on the lower end of this tubular strut, and a shock absorber (106) pivotally connecting an appendage (105) of the balance (103) to a device (110) mounted to slide axially inside the tubular enclosure (102), the sliding member (110) being connected to a manuevering jack (125) by a linkage associated (120, 123) mounted in the upper part of the tubular box so that said member is axially displaceable by the actuation of the operating ram (125) between two extreme positions, one of which corresponds to the undercarriage-down position and the other to the raised position.
机译:用于宽体飞机的可升降起落架技术领域本发明涉及一种用于垂直起升的宽体飞机的起落架,其包括多个腿,它们彼此并排布置,以在起落架下位置形成平行于中间纵向平面的行。根据本发明,每个支腿(101)包括管状外壳(102),刚性地固定到飞机的结构上,摆轮(103)固定在飞机的结构上。 )铰接在该管状支柱的下端上,并且减震器(106)将摆轮(103)的附件(105)可枢转地连接到设备(110),该设备安装成可在管状外壳(102)内轴向滑动,滑动构件(110)通过安装在管状箱体上部的相关联的联动装置(120、123)连接到操纵千斤顶(125),使得所述滑动构件(110)通过操作撞锤(125)的驱动可轴向移动。两个极端职位,其中之一则将其转到起落架降下位置,将另一个移至升高位置。

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