;The first secondary damper (6a) is carried by the axle shaft (2) and comprises:an inertial mass (M); andconnection means (7a) between the inertial mass (M) and the axle shaft (2) damping movements of the inertial mass (M) along a first axis (X1) of movement of the inertial mass (M) relative to the axle shaft (2), said first axis of movement (X1) extending in a plane (P) perpendicular to said steering axis (Z)."/>
LANDING-GEAR ASSEMBLY FOR AN AIRCRAFT, THE LANDING-GEAR ASSEMBLY INCLUDING A SECONDARY SHIMMY DAMPER
首页>
外国专利>
LANDING-GEAR ASSEMBLY FOR AN AIRCRAFT, THE LANDING-GEAR ASSEMBLY INCLUDING A SECONDARY SHIMMY DAMPER
LANDING-GEAR ASSEMBLY FOR AN AIRCRAFT, THE LANDING-GEAR ASSEMBLY INCLUDING A SECONDARY SHIMMY DAMPER
展开▼
机译：飞机起落架总成，包括次要减震器的起落架总成
展开▼
页面导航
摘要
著录项
相似文献
摘要
A landing-gear assembly (1) for an aircraft, the landing-gear assembly comprising:an axle shaft (2);a leg (3) presenting a first portion (3a) carrying said axle shaft (2) and a second portion (3b) connected to a carrier structure of the aircraft;a main damper (5); anda first secondary damper (6a) distinct from the main damper (5).;The first secondary damper (6a) is carried by the axle shaft (2) and comprises:an inertial mass (M); andconnection means (7a) between the inertial mass (M) and the axle shaft (2) damping movements of the inertial mass (M) along a first axis (X1) of movement of the inertial mass (M) relative to the axle shaft (2), said first axis of movement (X1) extending in a plane (P) perpendicular to said steering axis (Z).展开▼
机译：用于飞机的起落架组件（ 1 ），该起落架组件包括：一根轴（ 2 ）; 一条腿（ 3 ）呈现出承载所述车轴（ 2 ）的第一部分（ 3 a ）和第二部分（ 3 b ）连接到飞机的航母结构; 主阻尼器（ 5 ） ;和 与主阻尼器（）不同的第一辅助阻尼器（ 6 a ） > 5 ）。 ;第一个辅助阻尼器（ 6 a ）由轴（ 2 ）包括：惯性质量（M）;和 惯性质量（M）与车轴之间的连接装置（ 7 a ）轴（ 2 ）沿惯性质量（M）相对于车轴（M）的第一轴线（X 1 ）的惯性质量（M）的阻尼运动。 2 ），所述第一运动轴（X 1 ）在垂直于所述转向轴（Z）的平面（P）中延伸。
展开▼
