变距旋翼飞行器机体结构振动设计

RESEARCH ON STRUCTURAL VIBRATION DESIGN OF VARIABLE-PITCH ROTORCRAFT

  • 摘要: 旋翼飞行器设计时,要考虑旋翼激励引起的机体结构振动问题,以往仅考虑一阶通过频率影响进行机体结构振动设计是不充分的。为此,基于频域响应理论,以变距旋翼的运转载荷为输入求解机体结构有阻尼状态的频率响应特性,根据分析结果评估高阶通过频率的影响。同时,利用时域响应理论计算机体结构的时间历程,对结构响应幅值进行定量分析。典型结构的分析结果表明,旋翼二阶通过频率对该结构的过载、扭矩影响显著,设计时必须予以考虑。研究内容为变距旋翼飞行器的机体结构振动设计提供了指导,后续类似结构设计时应进行充分的振动评估。

     

    Abstract: It is necessary to consider the structural vibration caused by the excitation of rotor operation during the design of rotorcraft. But the previous practice of only considering the influence of first-order pass frequency on the structural vibration design is insufficient. Based on the theory of frequency-domain response, the working loads of variable-pitch rotor were employed as external excitation to solve the frequency response of the structure in damped states, and the influence of high-order passing frequencies were evaluated based on the analysis. At the same time, the time-domain response analysis was used to calculate the response history of structures, so as to quantitatively analyze the response amplitude. Results of the typical structure indicate that the influence of second-order frequency on overload and torque is significant in this article, which must be considered in structural dynamic design. The research provides an effective method for guiding the structural dynamics design of variable-pitch rotorcraft, and sufficient vibration evaluation should be conducted in the subsequent design of similar structures.

     

/

返回文章
返回