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排序方式: 共有677条查询结果,搜索用时 421 毫秒
511.
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在5G高速发展的背景下,为实现机舱内部信息传输的无线化,设计了一款用于飞机设备舱内无线通信的毫米波微带阵列天线。结合串联馈电和并联馈电优点,采用串并联结合的方式对馈电网络进行设计。通过泰勒综合法实现阵元的同相位不等幅馈电,在保证高增益的情况下,有效地进行副瓣抑制。综合以上方法,设计出了一款中心频率为 48 GHz;在 47.3 ~48.7 GHz之间回波损耗小于-10 dB,工作带宽1.4 GHz;H 面上的半功率波束宽度小于 11°,副瓣抑制为-28 dB:E面上的半功率波束宽度小于 17°,副瓣抑制优于-21 dB 的4x8 微带天线阵,该阵列天线很好地实现了高增益/地旁瓣的特性。 相似文献
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514.
In recent years, the Active Flutter Suppression(AFS) employing Linear ParameterVarying(LPV) framework has become a hot spot in the research field. Nevertheless, the flutter suppression technique is facing two severe challenges. On the one hand, due to the fatal risk of flight test near critical airspeed, it is hard to obtain the accurate mathematical model of the aeroelastic system from the testing data. On the other hand, saturation of the actuator may degrade the closed-loop performance, which... 相似文献
515.
This paper aims to gain insight into the nonlinear modal characteristics and the possible influence of the modes on the responses for the practical dual-rotor system with rub-impact in aero-engine. The finite solid element method combined with a constraint stiffness model produced by rub-impact is introduced to build the governing equation of the complicated nonlinear dualrotor system. In order to deal with the efficiency and numerical divergence in the process of solving the nonlinear modes of ... 相似文献
516.
Cutting force and specific energy for rotary ultrasonic drilling based on kinematics analysis of vibration effectiveness 总被引:1,自引:1,他引:0
Rotary ultrasonic drilling(RUD) has become an effective approach for machining advanced composites which are widely using in the field of aeronautics. The cutting kinematics and the corresponding material removal mechanisms are distinct in different drilling areas during RUD. However, these fundamentals have not been fully considered in the existing studies. In this research, two distinct forms of interaction induced by ultrasonic vibration were considered as impact-separation and vibratory lapp... 相似文献
517.
《中国航空学报》2022,35(9):226-241
Space robotics has been used extensively in complex space missions. Rigid-manipulator space robots may suffer from rigid-body collisions with targets. This collision is likely to cause damage to the space robot and the target. To overcome such a problem, a novel Continuum-Manipulator Space Robot (CMSR) for performing on-orbit servicing missions is proposed in this paper. Compared with rigid-manipulator space robots, CMSRs are able to perform compliant operations and avoid rigid-body collisions with a target. The CMSR consists of two kinds of flexible components, including solar arrays and continuum manipulators. The elastic vibrations of these flexible components disturb the position and attitude of CMSRs. The beating phenomenon introduced by the energy transfer among these flexible components can cause damage to solar arrays. The complicated dynamic coupling poses enormous challenges in dynamic modeling and vibration analysis. The dynamic model for CMSRs is derived and the mechanism of the beating phenomenon is analyzed in this paper. Simulation results show that an obvious beating phenomenon occurs and the amplitude of the solar arrays increases significantly when the natural frequencies of two kinds of flexible components are close. A method is provided to avoid the beating phenomenon. 相似文献
518.
伺服作动器是飞控操纵系统的执行机构,为了保证飞行过程的安全性和可靠性,会对飞控作动系统进行液压余度备份;当采用通道并列的余度备份形式,各个通道控制回路之间的机械结构、信号传输和传感采集等环节的差异性,会导致作动筒输出的位移不一致,从而在舵面铰链之间产生力纷争现象;力纷争现象会影响系统的控制性能并对舵面结构造成疲劳损伤。从力纷争现象及其产生机理进行分析,对相关的研究进行了调研和汇总,阐述了针对不同构型的余度作动系统在力纷争抑制中尚需解决的问题和难点,在未来可能会与人工智能相结合对力纷争进行准确抑制。 相似文献
519.
《中国航空学报》2021,34(2):376-385
This paper proposes using a Nonlinear Energy Sink (NES) to suppress the nonlinear aeroelastic response of laminated composite panels in supersonic airflows. Relevant aeroelastic equations are established using Hamilton’s principle and a finite element approach, drawing upon Von Karman’s large deflection theory and first order piston theory. The idea of the NES suppression region is proposed and the effects of NES parameters on the NES suppression region are studied in detail. The results show that the nonlinear aeroelastic responses of the panel can be completely suppressed by the Transient Resonance Capture (TRC); the appropriate NES parameter values can increase the critical dynamic pressure for flutter and suppress the nonlinear aeroelastic response effectively. Increasing the mass ratio of the NES can improve the NES suppression region; the nonlinear stiffness coefficient and damping of the NES within a specific range can suppress the nonlinear aeroelastic response. The most effective installation position for a NES is in a specific region behind the center-line of the panel in the direction of the airflow. 相似文献
520.