共查询到18条相似文献,搜索用时 156 毫秒
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一种涡轮叶尖间隙主动控制系统的建模与仿真 总被引:2,自引:0,他引:2
为了提高现代航空发动机的性能,通过机械装置来控制(减小)涡轮叶尖间隙成为现在和未来的一个研究热点。在分析研究了航空发动机在不同工况下涡轮叶尖间隙的变化规律的基础上,提出了一种双闭环主动快速控制系统。进而,设计了一种可以控制非均匀叶尖间隙变化的作动装置,并对其进行了深入的数学建模分析。最后,分别通过PID和模糊PID两种控制器工作方式,对所设计的涡轮叶尖间隙主动快速控制系统的控制效果进行了仿真验证,结果表明,在起飞时段,PID控制曲线与模糊自适应PID控制曲线基本重合;但是在巡航、迅速减速、迅速加速、再次巡航时段,模糊自适应PID的控制效果要明显优于PID控制。 相似文献
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航空发动机转子叶尖间隙测量 总被引:6,自引:0,他引:6
简述了航空发动机转子叶尖间隙控制的意义及作用,转子叶尖间隙设计选择的依据.以某型风扇和某型高压压气机转子叶尖间隙测量为例,具体分析了间隙对性能的影响作用和变化规律,论证了间隙测试技术作为一种指导和验证手段在工程应用中的重要作用. 相似文献
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动叶片的叶尖间隙参数直接决定航空发动机的工作效率和运行安全,随着发动机朝着质量更轻、运转效率更高的方向发展,碳纤维复合材料(CFRP)被广泛应用于大涵道比航空发动机风扇叶片的设计,然而材料导电性会影响间隙测量结果。提出了一种基于电容法的CFRP叶片叶尖间隙测量方法;利用显微观察和元素分析,获取了CFRP叶片导电性规律,建立了仅碳纤维层参与构成电容器极板的叶尖间隙测量模型;开展了金属叶片和CFRP叶片叶尖间隙测量的仿真和实验,结果表明,两种叶片在不同间隙值下的电容输出呈比例关系,CFRP叶片的叶尖间隙测量精度优于45μm;完成了某型大涵道比航空发动机的测量试验,验证了航空发动机CFRP风扇叶片叶尖间隙测量方法的可行性和可靠性。 相似文献
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开展基于主动防喘的航空发动机加速控制仿真研究。在建立航空发动机数学模型的基础上,设计了基本加速率控制、基于主动防喘的加速率控制、基于主动防喘的喘振裕度控制及基于喘振裕度估计的喘振裕度控制等4个发动机加速控制方案。仿真结果表明:①主动防喘控制可以在发动机稳定性恶化的情况下,通过较小的控制输出和性能损失实现无喘加速;②主动防喘控制与直接喘振裕度控制相结合可以简化发动机加速控制器设计,不需要额外的优化过程便能得到较优的加速性能;③主动防喘控制可以降低发动机设计点的喘振裕度,从整体上提高了发动机的性能。 相似文献
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动叶片与发动机机匣之间的叶尖间隙参数是反映航空发动机工作性能和运行安全的关键状态参数之一。提高叶尖间隙信号信噪比是实现高精度叶尖间隙测量的关键,为此提出基于自适应滑动均值和小波阈值的混合叶尖间隙信号实时降噪方法。首先根据叶片转速等信息,估算叶尖间隙信号带宽大小,然后通过动态改变滑动均值滤波的滑动点数来实现自适应低通滤波,最后结合小波阈值降噪时频分析能力,进一步降低噪声干扰。通过仿真实验确定采用对db5小波基函数进行6层小波阈值分解.仿真结果表明该方法在各项降噪评价指标方面全面优于现有的有限脉冲响应和固定点滑动均值滤波方法。1000rpm~4000rpm转速范围内实际测试表明,该方法最大测量误差为16μm,有效提高叶尖间隙测量精度。 相似文献
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基于奇异摄动的双连杆柔性臂模糊控制 总被引:3,自引:0,他引:3
讨论了双连杆柔性臂位置控制问题。应用拉格朗日-假设模态法建立系统的动力学方程,并用奇异摄动法将双连杆柔性臂系统分解为两个降阶的慢变子系统和快变子系统。针对柔性臂强非线性、强耦合性及不确定性等特点,给出一种慢变子系统在反馈线性化后采用模糊控制、快变子系统因呈线性系统而采用简单的最优控制的混合控制方法。其中,模糊控制是二维PD型控制器,其输入为关节角跟踪误差及其导数。最后进行了计算机仿真,结果表明,该方法不仅能实现柔性臂轨迹的快速、准确跟踪,有效的抑制弹性振动,并且对负载的变化具有强的鲁棒性。 相似文献
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A PI control strategy based on fuzzy set-point weighting following was proposed for the active damp- ing control of a hydraulic crane boom system (HCBS). Two valve-controlled PI controllers, which include a proportional feedforward controller based on fuzzy set-point weighting following and a limited semi-integrator(LSI), are designed re- spectively. LSI is used to limit output signal and to prevent wind up at the low frequency of the spectrum . By using a range camera and an electronic feedback control, the tip damping on the HCBS can be adjusted artificially. A collaborative control simulation technique of HOPSAN and MATLAB/SIMULINK is applied to the controller design. Simulation results show that the proposed PI control system has less overshoot as well as faster response. The tip damping on the HCBS during operation is improved. 相似文献
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A PI control strategy based on fuzzy set-point weighting following was proposed for the active damping control of a hydraulic crane boom system (HCBS). Two valve-controlled PI controllers, which include a proportional feedforward controller based on fuzzy set-point weighting following and a limited semi-integrator(LSI), are designed respectively. LSI is used to limit output signal and to prevent wind up at the low frequency of the spectrum. By using a range camera and an electronic feedback control, the tip damping on the HCBS can be adjusted artificially. A collaborative control simulation technique of HOPSAN and MATLAB/SIMULINK is applied to the controller design. Simulation results show that the proposed PI control system has less overshoot as well as faster response. The tip damping on the HCBS during operation is improved. 相似文献
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V. Feliu J. A. Somolinos A. García L. Sánchez 《Journal of Intelligent and Robotic Systems》2002,34(4):467-488
This article describes a comparative study of two control schemes designed for a new three-degree-of-freedom flexible arm. This arm has been built with light links, has most of its mass concentrated on the tip, and its special mechanical configuration uncouples tip motions in spherical coordinates. This special configuration simplifies the dynamic modeling and control of the arm. A compliance matrix is used to model the oscillations of the structure. A consequence of this simple dynamics is that minimum sensing effort is required (only direct motor and tip measurements), and the use of complex observers is avoided because the state of the system can be very easily obtained from these measurements; then its control becomes very simple. Two two-nested control loop schemes are used to control the tip position, by using a joint position and tip acceleration feedback, measured with accelerometers placed at the tip (first control scheme), or tip deflexions feedback, measured with strain gauges placed at the bars of the mechanism near the joints (second control scheme). Both control systems can be considered as equivalents when nominal payload is used for designing them. It can be proved that the use of strain gauges is more robust than the use of accelerometers as tip sensors if the tip mass differs from the nominal one. Simulated results are presented for both control schemes and different payload conditions. Comparative results between the controlled and non-controlled tip responses are also shown. 相似文献
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