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本文介绍了一种基于386微机的转速测量方法,该方法克服了一般数字式转速测量方法高、低速精度不等以及精度不高的缺陷,可实现宽转速范围的等精度测量,测量精度可达2.3×10~(-10)。 相似文献
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飞机发动机转速实时在线检测系统二次开发 总被引:1,自引:0,他引:1
介绍一种以AT89C52单片机为系统控制核心,用二相步进电机精确地驱动仪表指针,对飞机发动机转速实时在线检测系统进行研究与开发,实现机电一体化功能的智能仪表技术。 相似文献
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为了提高发动机故障分类的准确率和成功率,提出了基于角域信号特征统计量的发动机故障分类方法。包括:利用编码器进行发动机振动信号的等角度采样;采用小波包分析和相关系数法获取发动机角域信号的特征阶次;选取特征阶次信号的能量比、标准差比、谱能量比及谱均值比4组参数作为角域信号特征统计量来提取发动机故障特征;采用支持向量机法对发动机故障进行分类。连杆轴承配合间隙故障的台架试验结果证明:相比于传统的分类方法,该方法明显提高了发动机故障分类的准确率。 相似文献
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基于虚拟仪器的串激电机转速测量装置的实现 总被引:4,自引:0,他引:4
在工业测控系统中,电动机尤其是交流电动机转速的检测和控制占有很大比重。在以磁电或光电构成的测速系统中,常用的测量方法有3种,分别为T法、M/T法和M法。但对于电动机被封闭的场合则测速比较困难。文中介绍的是应用虚拟仪器技术的一种非接触式转速测量方法及装置,通过从串激电机在转动时感应出的信号中提取出与转速对应的信号,求其频率,然后根据推导出的公式使其转化为转速,从而得出结果。基于该方法的测量装置,速度与串激电机感应出的频率有一一对应关系,因而具有高效率、高精度、非接触测量,且可以及时反映物体的瞬时变化情况等优点。 相似文献
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This paper presents a method for determining the instantaneous angular speed and instantaneous angular acceleration of the crankshaft in a reciprocating engine and propeller dynamical system from electrical pulse signals generated by a magnetic encoder. The method is based on accurate determination of the measured global mean angular speed and precise values of times when leading edges of individual magnetic teeth pass through the magnetic sensor. Under a steady-state operating condition, a discrete deviation time vs. shaft rotational angle series of uniform interval is obtained and used for accurate determination of the crankshaft speed and acceleration. The proposed method for identifying sub- and super-harmonic oscillations in the instantaneous angular speeds and accelerations is new and efficient. Experiments were carried out on a three-cylinder four-stroke Saito 450R model aircraft engine and a Solo propeller in connection with a 64-teeth Admotec KL2202 magnetic encoder and an HS-4 data acquisition system. Comparisons with an independent data processing scheme indicate that the proposed method yields noise-free instantaneous angular speeds and is superior to the finite difference based methods commonly used in the literature. 相似文献
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AMT车辆换挡过程中发动机转速控制与试验研究 总被引:1,自引:0,他引:1
提出了换挡过程中通过控制断油电磁阀来调节发动机转速的新方法,分析了断油电磁阀对发动机工作特性的影响,制定了断油电磁阀的控制策略,并在装有AMT的某重型载货汽车上进行了试验。试验结果表明,换挡过程中通过控制断油电磁阀来调节发动机的转速,可减小离合器接合时主、被动部分的转速差,改善AMT的换挡品质。 相似文献
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提出了一种基于16位单片机MC9S12DG128的柴油机数字式电子调速系统,通过单片机对柴油机转速进行PID调节,克服了传统机械式调速系统的诸多缺点。试验结果表明:该控制系统能有效地提高柴油机调速系统的响应速度,改善数字式电子调速系统的动态性能。 相似文献
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Seong Man Choi Seong Ho Jang Dong Hun Lee Gyong Won You 《Journal of Mechanical Science and Technology》2010,24(2):551-558
In micro-turbojet engines with less than 350 kW power, it is not easy to find a suitable fuel injector with good spray quality.
However, the rotating fuel injection system can potentially provide high atomization quality without the high-pressure fuel
pump through the centrifugal forces of the engine shaft. With this motivation, a very small rotating fuel injector with 40
mm diameter is designed for the micro-turbo jet engine. It is directly linked to a high-speed rotational spindle capable of
a speed up to 100,000 rpm. The droplet size, velocity, and spray distribution from the PDPA (Phase Doppler Particle Analyzer)
system are measured. The spray is also visualized by a high-speed camera. The test results show that the length of liquid
column from injection orifice is controlled by the rotational speeds and that SMD (Sauter Mean Diameter) is decreased with
increasing rotational speeds. At a rotational speed of 73.3 m/s (35,000 rpm), SMD is lower than 60 μm at the entirety of the
measuring space in the case of Type 2 (injection orifice diameter of 1.5 mm) and Type 3 (injection orifice diameter of 2.2
mm). Therefore, conceptually, it is possible to apply this small rotating fuel injection system to the micro-turbojet engine
combustor. 相似文献
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某型运载火箭发动机机架为大直径桁架式结构,具有刚度弱、焊接变形大的特点。作为连接发动机和箭体传递推力的过渡结构,其上下端面对接孔具有高精度、一致性的协调要求。针对此,提出了一种精密孔协调方案,其利用预拟合和二次拟合法协调底孔包络,采用销孔定位协调二次基准,实现精密孔的整体协调;同时,提出了基于BP神经网络的同轴度预测模型以预测加工后对接孔位置度。经过实际加工验证,该方法能够实现5 m级桁架式结构对接孔的整体协调,保证了对接孔的高精度要求,且该算法能够有效预测并辅助验证位置度检验结果,提高了检验可靠性,为航天大型产品加工整体协调提供了一种思路。 相似文献
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S.F. Lee P. Lovenitti M.K. Lam S.H. Masood 《The International Journal of Advanced Manufacturing Technology》2002,20(3):180-189
This paper describes the design and development of a precision calliper system to measure the surface profile of an outboard
marine engine propeller blade. Several instruments that are commonly used for measuring the surface profile of a propeller
blade are reviewed in this paper. These include the pitch meter, the profilometer and the computer numerical control coordinate-measuring
machine (CNC-CMM). However, the operating practices and availability of different facilities in industry necessitate a more
cost-effective approach. An alternative method using a precision calliper system is therefore proposed. Details of the design
criteria, principles of operation and the testing and verification of the system are presented. The paper concludes that the
precision calliper system is a cost-effective method for measuring the surface profile of a propeller. 相似文献
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Compensation of rotor imbalance for precision rotation of a planar magnetic bearing rotor 总被引:2,自引:0,他引:2
Magnetic bearings provide an alternative for achieving precision rotation. But the rotational accuracy is sensitive to rotor imbalance. The system we study is a planar rotor supported by aerostatic suspension and positioned by a radial magnetic bearing of nanometer precision. We present compensation designs and experiment results for precision rotation about the geometric center and the mass center, respectively. In the former case, the base harmonic component at each sensor output is removed by explicit trigonometric compensation signals that are constructed in real time. In the latter case, a new double-loop compensation design is given. Each compensation loop is similar to that in the former case. The compensation, aided by a variable rotational speed that is changed up and down repeatedly, is shown to push the rotational center to approach the mass center. Once the mass center is reached, the rotor remains to rotate about the mass center at variable rotational speed without transient. Compared with the existing methods, which find the mass center or inertial axis at a fixed rotational speed and rely on exact values of plant parameters, our method may locate the mass center more accurately. Experiment data indicate that the mass center is located with an error of tens of nanometers. 相似文献
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柴油机状态监测信号众多且多为非平稳信号,相互干扰较大且具有非线性和复杂耦合的特征,导致基于向量模式的故障诊断方法难以准确诊断其工作状态。提出一种张量模式下的柴油机智能诊断方法。首先,结合线性支持高阶张量机的学习框架和在线随机梯度下降法的思想,设计带核函数的快速在线支持张量机算法。然后,构建“信号类别×曲轴转角×转速”的三阶张量形式的柴油机状态样本,分别以在线支持向量机、线性支持高阶张量机和快速在线支持张量机三种算法,对某柴油机的失火样本进行故障诊断,以“测试精度”“学习时间”“存储空间”作为评价指标对三种算法进行对比分析。分析结果表明,所设计的快速在线支持张量机算法测试精度较高,学习时间显著降低,所需存储空间很小,解决了超大样本、非线性和高维数据的分类问题,满足了柴油机智能故障诊断的工程应用要求。 相似文献
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电机转矩转速测量方法的分析 总被引:11,自引:1,他引:11
电机的转矩和转速是最重要的两个参数,对它们的测量必须准确.根据用户提出的测量航空电机具体要求,本文分析了转矩和转速的测量原理,指出了采用应变式和光电式传感器构成测量仪更适合测量大转矩、高转速电机.虽然与传统的测量方法一致,但经过理论分析,得出了这种测量方式机械结构影响测量稳定性的原因,即传动轴受减速器齿轮啮合力作用产生的弯曲应变和结构谐振对测量精度影响最大.本文通过精确的计算,充分地考虑了机械结构对测量稳定性的影响,提出了选择转矩传感器及转速传感器的基本原理与方法.据此,在所研制的电机测量仪中,大大地提高了测量精度,并有效地减小了测量仪的体积和重量,适合航空工业应用. 相似文献