首页> 外国专利> ENERGY ABSORBING LANDING GEAR SYSTEM FOR A VERTICAL LANDING APPARATUS AND METHOD OF USING THE SAME

ENERGY ABSORBING LANDING GEAR SYSTEM FOR A VERTICAL LANDING APPARATUS AND METHOD OF USING THE SAME

机译:用于垂直着陆装置的能量吸收着陆齿轮系统及其使用方法

摘要

There is provided an energy absorbing landing gear system (10) for attachment to a vertical landing apparatus. The energy absorbing landing gear system (10) includes a linear damper assembly (12), and a load limiter assembly (14) coupled to the linear damper assembly (12), the load limiter assembly (14) having at least one deformable element (130) to enhance an energy absorption capability. When the energy absorbing landing gear system (10) is attached to the vertical landing apparatus, during a landing phase, the linear damper assembly (12) contacts a landing surface, and a piston assembly (74) of the linear damper assembly (12) moves a first compression distance toward the load limiter assembly (14), and when the linear damper assembly (12) reaches a maximum compression, the linear damper assembly (12) moves a second compression distance into the load limiter assembly (14), and the at least one deformable element (130) deforms.
机译:提供了一种能量吸收着陆齿轮系统(10),用于连接到垂直着陆装置。 能量吸收着陆齿轮系统(10)包括线性阻尼器组件(12),以及耦合到线性阻尼器组件(12)的负载限制器组件(14),所述负载限制器组件(14)具有至少一个可变形元件( 130)提高能量吸收能力。 当能量吸收着陆齿轮系统(10)附接到垂直着陆装置时,在着陆阶段期间,线性阻尼器组件(12)接触着线性阻尼器组件(12)的着陆表面和活塞组件(74) 将第一压缩距离朝向负载限制器组件(14)移动,并且当线性阻尼器组件(12)达到最大压缩时,线性阻尼器组件(12)将第二压缩距离移动到负载限制器组件(14)中, 至少一个可变形元件(130)变形。

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