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MODELING AND DYNAMIC CHARACTERISTICS OF PLANETARY GEAR TRANSMISSION IN NON-INERTIAL SYSTEM OF AEROSPACE ENVIRONMENT

机译:航空环境非惯性系统中行星齿轮传动的建模与动力特性

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The traditional research on the dynamics of planetary gear transmission system is based on the assumption that the support is on the ground. However, the planetary gear transmission system inside the aircraft is spatially moved along with the airframe, which is not only subject to gravity, but also to convected inertia force and Coriolis inertia force, as well as gyroscopic moment. These loads affect the dynamic characteristics of the planetary gear transmission system. In order to investigate the dynamic behavior of planetary gear transmission system in non-inertial system of aerospace environment, the kinematic equations of the central component and planetary gear in arbitrary spatial motion state of the airframe are deduced with the influence of internal non-inertial system and external non-inertial system. Subsequently, the coupling dynamic model of planetary gear transmission system is established, which is in non-inertial system of aerospace environment. The motion variation law of planetary gear transmission system in the non-inertial system and the dynamic behavior of each component in different non-inertial conditions are researched based on the hovering motion of the airframe. The results indicate that the radial equilibrium position of the planetary gear has great offset due to the influence of non-inertial system inside the planetary gear train when the airframe has no spatial motion. Moreover, the gravity on each component will generate radial force, which and additional inertial force will vary with the external non-inertia conditions when the airframe is in the state of spatial motion. In addition, different non-inertial conditions have significant influence on the motion trajectory, bearing force and acceleration of each component, and have different influence rides on the central component and planetary gear.
机译:关于行星齿轮传动系统动力学的传统研究是基于这样的假设,即支撑物是在地面上的。然而,飞机内部的行星齿轮传动系统与机身一起在空间上移动,这不仅受到重力的影响,而且还受到对流惯性力和科里奥利惯性力以及陀螺力矩的影响。这些载荷影响行星齿轮传动系统的动态特性。为了研究航空航天环境非惯性系统中行星齿轮传动系统的动力学行为,在内部非惯性系统的影响下,推导出机身在任意空间运动状态下的中心分量和行星齿轮的运动方程。和外部非惯性系统。随后,建立了航天环境非惯性系统中行星齿轮传动系统的耦合动力学模型。基于机身的悬停运动,研究了非惯性系统中行星齿轮传动系统的运动变化规律以及不同惯性条件下各部件的动力学行为。结果表明,当机身无空间运动时,由于行星齿轮系内部非惯性系统的影响,行星齿轮的径向平衡位置有较大的偏移。而且,当机身处于空间运动状态时,每个组件上的重力将产生径向力,该径向力和附加的惯性力将随着外部非惯性条件而变化。另外,不同的非惯性条件对每个部件的运动轨迹,轴承力和加速度具有显着影响,并且对中央部件和行星齿轮具有不同的影响。

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