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CN106643906A - Monitoring method and monitoring system for variable-pitch bearing - Google Patents

Monitoring method and monitoring system for variable-pitch bearing Download PDF

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Publication number
CN106643906A
CN106643906A CN201611260550.2A CN201611260550A CN106643906A CN 106643906 A CN106643906 A CN 106643906A CN 201611260550 A CN201611260550 A CN 201611260550A CN 106643906 A CN106643906 A CN 106643906A
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strain
parameters
bolt holes
bearing end
bearing
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CN106643906B (en
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聂峰
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Beijing Goldwind Science and Creation Windpower Equipment Co Ltd
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Beijing Goldwind Science and Creation Windpower Equipment Co Ltd
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D21/00Measuring or testing not otherwise provided for
    • G01D21/02Measuring two or more variables by means not covered by a single other subclass
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K11/00Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00
    • G01K11/32Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00 using changes in transmittance, scattering or luminescence in optical fibres
    • G01K11/3206Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00 using changes in transmittance, scattering or luminescence in optical fibres at discrete locations in the fibre, e.g. using Bragg scattering
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/24Measuring force or stress, in general by measuring variations of optical properties of material when it is stressed, e.g. by photoelastic stress analysis using infrared, visible light, ultraviolet
    • G01L1/242Measuring force or stress, in general by measuring variations of optical properties of material when it is stressed, e.g. by photoelastic stress analysis using infrared, visible light, ultraviolet the material being an optical fibre
    • G01L1/246Measuring force or stress, in general by measuring variations of optical properties of material when it is stressed, e.g. by photoelastic stress analysis using infrared, visible light, ultraviolet the material being an optical fibre using integrated gratings, e.g. Bragg gratings

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Optical Transform (AREA)

Abstract

The invention relates to a monitoring method and a monitoring system for a variable-pitch bearing. Pitch bearing (100) comprises a bearing end face (130, 140) and bolt holes (1-54) formed in the bearing end face (130, 140), and is characterized in that the monitoring method comprises the following steps: monitoring temperature parameters and strain parameters of the bearing end surfaces (130, 140) or the bolt holes (1-54) by using a fiber bragg grating sensing measurement system (500); and correcting the strain parameters of the bearing end surfaces (130, 140) or the bolt holes (1-54) by using the temperature parameters to obtain actual strain parameters.

Description

变桨轴承的监测方法和监测系统Monitoring method and monitoring system for pitch bearing

技术领域technical field

本发明涉及轴承的监测技术领域,特别是涉及变桨轴承的监测方法和监测系统。The invention relates to the technical field of monitoring bearings, in particular to a monitoring method and a monitoring system for variable pitch bearings.

背景技术Background technique

能源是社会经济和人类生活的主要物质基础,是社会发展的动力。然而,作为世界能源主要支柱的石油、煤炭、天然气等不可再生的能源的储量日趋减少,世界各个国家都在发展风力发电,风力发电作为新能源,已经形成了成熟的规模。Energy is the main material basis of social economy and human life, and the driving force of social development. However, the reserves of non-renewable energy such as petroleum, coal, and natural gas, which are the main pillars of energy in the world, are decreasing day by day. All countries in the world are developing wind power generation. As a new energy source, wind power generation has formed a mature scale.

风力发电机是将风能转换成电能的设备,在风力发电机中,变桨轴承作为叶片和轮毂的连接部件,在风力发电的变桨过程中起到了十分重要的作用。变桨是通过调整桨叶角度,改变气流对叶片的攻角,从而改变风电机组获取的空气动力,使风力发电机按照设计的输出功率输出。由于叶片重量和气动推力较大,变桨轴承要承受很大的载荷,尤其是变桨轴承的端面和用于连接的螺栓孔,可能会因为载荷过大而出现裂纹。而且,变桨轴承工作的环境恶劣,环境温度梯度大,变桨轴承也有可能会因为温度的变化影响油脂的润滑和材料的特性从而引起失效。由于变桨轴承结构应力复杂,工作温度场分布不均,为了提早预警,降低质量和安全事故,监测手段至关重要。A wind turbine is a device that converts wind energy into electrical energy. In a wind turbine, the pitch bearing, as the connecting part between the blade and the hub, plays a very important role in the pitch change process of wind power generation. Pitch adjustment is to change the angle of attack of the airflow on the blades by adjusting the angle of the blades, thereby changing the aerodynamic force obtained by the wind turbine, so that the wind turbine can output according to the designed output power. Due to the large weight and aerodynamic thrust of the blades, the pitch bearing is subject to a large load, especially the end face of the pitch bearing and the bolt holes used for connection, which may crack due to excessive load. Moreover, the working environment of the pitch bearing is harsh, and the ambient temperature gradient is large, and the pitch bearing may also cause failure due to changes in temperature affecting the lubrication of the grease and the characteristics of the material. Due to the complex structural stress of the pitch bearing and the uneven distribution of the working temperature field, monitoring means are very important in order to give early warning and reduce quality and safety accidents.

发明内容Contents of the invention

以往,监测轴承的技术手段不足,且无法全面考量轴承的受力特性。目前的手段是利用电阻应变片在可能的受力集中点进行安装测量,但是因为轴承本身应力集中区域安装空间和被测面较小,加上电阻应变片测量只是单点应力测量,如果要描述线应力和面应力需要安装大量的电阻应变片、引线和采集设备通道,成本较高,操作困难,使用寿命短,加上变桨轴承工作环境有强磁场对监测结果有较大的影响。另外,如果要测量整个轴承的温度场分布,需额外加装温度传感器、布线和采集设备。In the past, the technical means for monitoring bearings were insufficient, and the force characteristics of bearings could not be fully considered. The current method is to use the resistance strain gauge to install and measure the possible stress concentration points, but because the installation space of the stress concentration area of the bearing itself and the measured surface are small, and the resistance strain gauge measurement is only a single-point stress measurement, if you want to describe Linear stress and surface stress require the installation of a large number of resistance strain gauges, lead wires, and acquisition equipment channels, which are costly, difficult to operate, and have a short service life. In addition, the strong magnetic field in the working environment of the pitch bearing has a greater impact on the monitoring results. In addition, if the temperature field distribution of the entire bearing is to be measured, additional temperature sensors, wiring and acquisition equipment need to be installed.

本发明的目的在于提供一种变桨轴承的监测方法和监测系统,能够避免电磁干扰,延长使用寿命,安装和布线简单,并且能够降低变桨轴承的监测成本。The purpose of the present invention is to provide a monitoring method and monitoring system for a pitch bearing, which can avoid electromagnetic interference, prolong the service life, simplify installation and wiring, and reduce the monitoring cost of the pitch bearing.

本发明的一个方面提供了一种变桨轴承的监测方法,所述变桨轴承包括轴承端面和被开设在所述轴承端面上的螺栓孔,所述监测方法包括:利用光纤光栅传感测量系统对所述轴承端面或所述螺栓孔的温度参数和应变参数进行监测;以及利用所述温度参数对所述轴承端面或所述螺栓孔的应变参数进行校正,以获得实际应变参数。One aspect of the present invention provides a monitoring method for a pitch bearing, the pitch bearing includes a bearing end face and bolt holes opened on the bearing end face, the monitoring method includes: using a fiber grating sensing measurement system monitoring the temperature parameter and the strain parameter of the bearing end surface or the bolt hole; and using the temperature parameter to correct the strain parameter of the bearing end surface or the bolt hole to obtain an actual strain parameter.

本发明的另一个方面提供一种变桨轴承的监测系统,变桨轴承包括轴承端面和被开设在所述轴承端面上的螺栓孔,所述监测系统包括:光纤光栅传感测量系统,对所述轴承端面或所述螺栓孔的温度参数和应变参数进行监测;以及校正单元,利用所述温度参数对所述轴承端面或所述螺栓孔的应变参数进行校正,以获得实际应变参数。Another aspect of the present invention provides a monitoring system for a pitch bearing. The pitch bearing includes a bearing end face and bolt holes opened on the bearing end face. The monitoring system includes: an optical fiber grating sensing and measuring system for measuring monitoring the temperature parameters and strain parameters of the bearing end face or the bolt holes; and a correction unit, using the temperature parameters to correct the strain parameters of the bearing end face or the bolt holes to obtain actual strain parameters.

根据上述的变桨轴承的监测方法和监测系统,使用光纤光栅传感测量系统代替了以往的电阻应变片。由于变桨轴承有时会处于高湿、烟雾、或雷电的工作环境中,光纤光栅传感器由光纤制得,光纤的绝缘性能好、耐腐蚀、化学性能稳定,无需电源驱动,且光纤光栅传感器中传递的光信号不受电磁干扰的影响,在高湿、烟雾、雷电或电磁干扰的工作环境中,均可稳定使用。因此,能够避免电磁干扰,延长了使用寿命,安装和布线都很简单。另外,光纤光栅传感器能够通过裸光栅覆盖、微型传感器熔接等方式,组成与变桨轴承外圈端面、内圈端面以及外圈圆周面或螺栓孔等选定部位相应的形状,因此安装难度和安装成本均较低。According to the above-mentioned monitoring method and monitoring system of the pitch bearing, the optical fiber grating sensing measurement system is used to replace the previous resistance strain gauge. Since pitch bearings are sometimes in high humidity, smog, or lightning working environments, the fiber grating sensor is made of optical fiber, which has good insulation performance, corrosion resistance, and stable chemical properties. The optical signal is not affected by electromagnetic interference, and can be used stably in the working environment of high humidity, smog, lightning or electromagnetic interference. Therefore, electromagnetic interference can be avoided, the service life is prolonged, and installation and wiring are simple. In addition, the optical fiber grating sensor can form the shape corresponding to the selected parts such as the end face of the pitch bearing outer ring, the end face of the inner ring, the circumferential surface of the outer ring or the bolt holes through bare grating covering, micro-sensor welding, etc., so the installation difficulty and installation The cost is lower.

根据上述的变桨轴承的监测方法和监测系统,使用光纤光栅传感测量系统对轴承端面的应变和温度进行监测,根据轴承端面的应变以及预先建立的轴承端面的应变与螺栓孔的应变的对应关系来获取螺栓孔的应变。即,只需要在变桨轴承的轴承端面上安装光纤光栅传感器,根据预定的变桨轴承的轴承端面的应变与变桨轴承的螺栓孔的应变的对应关系,就可得到变桨轴承的螺栓孔的应变,而不需要在变桨轴承的轴承端面和螺栓孔中都安装光纤光栅传感器,从而降低变桨轴承的轴承端面和螺栓孔的监测成本。另外,根据变桨轴承的轴承端面的应变以及预定的变桨轴承的轴承端面的应变与变桨轴承的螺栓孔的应变的对应关系,能够得到较准确的螺栓孔的应变,由此不需要在螺栓孔中安装传感器,螺栓孔中可以放置螺栓,保证了变桨轴承的使用寿命。因此,能够在确保变桨轴承的使用寿命的同时,得到较准确的螺栓孔内的应变的监测结果。或者,使用光纤光栅传感测量系统对螺栓孔的应变和温度进行监测,根据螺栓孔的应变以及预先建立的轴承端面的应变与螺栓孔的应变的对应关系来获取轴承端面的应变。即,同样地,只需要在变桨轴承的螺栓孔中安装光纤光栅传感器,根据预定的变桨轴承的轴承端面的应变与变桨轴承的螺栓孔的应变的对应关系,就可得到变桨轴承的端面和螺栓孔的应变,而不需要在变桨轴承的轴承端面和螺栓孔中都安装光纤光栅传感器,从而降低变桨轴承的轴承端面和螺栓孔的监测成本。According to the above-mentioned monitoring method and monitoring system of the pitch bearing, the strain and temperature of the bearing end face are monitored using the fiber grating sensing measurement system, and the strain and the temperature of the bearing end face are monitored according to the strain of the bearing end face and the pre-established strain of the bearing end face and the strain of the bolt hole. relation to obtain the strain in the bolt hole. That is, it is only necessary to install a fiber optic grating sensor on the bearing end surface of the pitch bearing, and according to the predetermined corresponding relationship between the strain of the bearing end surface of the pitch bearing and the strain of the bolt hole of the pitch bearing, the bolt hole of the pitch bearing can be obtained The strain of the pitch bearing does not need to install the fiber grating sensor in both the bearing end face and the bolt hole of the pitch bearing, thereby reducing the monitoring cost of the bearing end face and the bolt hole of the pitch bearing. In addition, according to the strain of the bearing end surface of the pitch bearing and the predetermined corresponding relationship between the strain of the bearing end surface of the pitch bearing and the strain of the bolt hole of the pitch bearing, a more accurate strain of the bolt hole can be obtained, thereby eliminating the need to The sensor is installed in the bolt hole, and the bolt can be placed in the bolt hole, which ensures the service life of the pitch bearing. Therefore, while ensuring the service life of the pitch bearing, more accurate monitoring results of the strain in the bolt holes can be obtained. Alternatively, the strain and temperature of the bolt holes are monitored using a fiber Bragg grating sensing measurement system, and the strain of the bearing end surface is obtained according to the strain of the bolt holes and the pre-established relationship between the strain of the bearing end surface and the strain of the bolt hole. That is, similarly, it is only necessary to install a fiber grating sensor in the bolt hole of the pitch bearing, and according to the predetermined corresponding relationship between the strain of the bearing end face of the pitch bearing and the strain of the bolt hole of the pitch bearing, the pitch bearing The strain of the end face and the bolt hole of the pitch bearing does not need to install the fiber grating sensor in both the bearing end face and the bolt hole of the pitch bearing, thereby reducing the monitoring cost of the bearing end face and the bolt hole of the pitch bearing.

根据上述的变桨轴承的监测方法和监测系统,在轴承端面圆周的0°、90°、180°和270°处安装光纤光栅传感器,即采用环形布置方式来布置光纤光栅传感器。通过上述光纤光栅传感器的布置,能够准确评估变桨轴承的线或面应力以及温度场,优化了设计参数,降低了故障概率。According to the above monitoring method and monitoring system for pitch bearings, fiber grating sensors are installed at 0°, 90°, 180° and 270° of the circumference of the bearing end face, that is, the fiber grating sensors are arranged in a ring arrangement. Through the above-mentioned arrangement of the fiber grating sensor, the line or surface stress and the temperature field of the pitch bearing can be accurately evaluated, the design parameters are optimized, and the failure probability is reduced.

根据上述的变桨轴承的监测方法和监测系统,在所述轴承端面圆周的0°和180°处设置多个测点安装所述光纤光栅传感器。由于在变桨轴承的轴承端面上的0°和180°处承载的载荷较大,在此处集中多点测量,从而能够更加准确测得此处的应力状态。According to the above-mentioned monitoring method and monitoring system for a pitch bearing, a plurality of measuring points are set at 0° and 180° of the circumference of the end face of the bearing to install the fiber grating sensor. Since the loads carried at 0° and 180° on the bearing end face of the pitch bearing are relatively large, multi-point measurements are concentrated here, so that the stress state here can be measured more accurately.

根据上述的变桨轴承的监测方法和监测系统,在所述螺栓孔的内壁沿轴向或径向安装所述光纤光栅传感器。由于变桨轴承的螺栓孔的内壁裂纹更容易沿轴向或径向发生损坏,因此沿着轴向或径向布置光纤光栅传感器,从而能够更加准确测得螺栓孔的应力状态。According to the above-mentioned monitoring method and monitoring system for a pitch bearing, the fiber grating sensor is installed axially or radially on the inner wall of the bolt hole. Since the inner wall cracks of the bolt holes of the pitch bearing are more likely to be damaged in the axial or radial direction, the fiber grating sensors are arranged in the axial or radial direction, so that the stress state of the bolt holes can be measured more accurately.

根据上述的变桨轴承的监测方法和监测系统,光纤光栅传感器通过光纤链路与光解调仪连接,光纤链路的两端分别与光解调仪连接。由此能够同步地采集数据,可做到通讯故障冗余设计,即使光路中间某处故障,也不会影响整个光路的通讯测试。According to the above-mentioned monitoring method and monitoring system for the pitch bearing, the fiber grating sensor is connected to the optical demodulator through the optical fiber link, and the two ends of the optical fiber link are respectively connected to the optical demodulator. In this way, data can be collected synchronously, and communication fault redundancy design can be achieved. Even if a fault occurs somewhere in the middle of the optical path, it will not affect the communication test of the entire optical path.

附图说明Description of drawings

下面将参考附图来描述本发明示例性实施例的特征、优点和技术效果。The features, advantages, and technical effects of exemplary embodiments of the present invention will be described below with reference to the accompanying drawings.

图1是示出本发明涉及的变桨轴承的结构的主视图;FIG. 1 is a front view showing the structure of a pitch bearing according to the present invention;

图2是示出本发明涉及的光纤光栅传感测量系统的构成图;Fig. 2 is a structural diagram showing the fiber grating sensing measurement system involved in the present invention;

图3是示出本发明涉及的变桨轴承的监测方法之一的流程图;Fig. 3 is a flow chart showing one of the monitoring methods of the pitch bearing involved in the present invention;

图4是示出本发明涉及的变桨轴承的监测方法之二的流程图;Fig. 4 is a flow chart showing the second monitoring method of the pitch bearing involved in the present invention;

图5例示出变桨轴承的外圈端面的应变与螺栓孔的应变的对应关系;Fig. 5 exemplifies the corresponding relationship between the strain of the end surface of the outer ring of the pitch bearing and the strain of the bolt hole;

图6是示出本发明涉及的变桨轴承的监测系统的构成图。Fig. 6 is a configuration diagram showing a monitoring system of a pitch bearing according to the present invention.

在附图中,相同的部件使用相同的附图标记。附图并未按照实际的比例绘制。In the figures, the same parts are given the same reference numerals. The figures are not drawn to scale.

标号说明Label description

100变桨轴承;110轴承外圈;120轴承内圈;130外圈端面;140内圈端面;1~54螺栓孔;200光纤光栅应变和温度传感器;300光纤链路;400光解调仪;500光纤光栅传感测量系统;500a校正单元;600获取单元;700预警单元;800监测系统100 pitch bearing; 110 bearing outer ring; 120 bearing inner ring; 130 outer ring end face; 140 inner ring end face; 1~54 bolt holes; 200 fiber grating strain and temperature sensor; 300 optical fiber link; 500 fiber grating sensing measurement system; 500a correction unit; 600 acquisition unit; 700 early warning unit; 800 monitoring system

具体实施方式detailed description

下面结合附图和实施例对本发明的实施方式作进一步详细描述。以下实施例的详细描述和附图用于示例性地说明本发明的原理,但不能用来限制本发明的范围,即本发明不限于所描述的实施例。Embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings and examples. The detailed description and drawings of the following embodiments are used to illustrate the principle of the present invention, but not to limit the scope of the present invention, that is, the present invention is not limited to the described embodiments.

在本发明的描述中,需要说明的是,除非另有说明,“若干”的含义是一个或者一个以上;“多个”的含义是两个或两个以上;术语“上”、“下”、“左”、“右”、“内”、“外”、“前端”、“后端”、“头部”、“尾部”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。In the description of the present invention, it should be noted that unless otherwise specified, the meaning of "several" is one or more; the meaning of "plurality" is two or more; the terms "upper" and "lower" , "Left", "Right", "Inner", "Outer", "Front", "Rear", "Head", "Tail" and other indicated directions or positional relationships are based on the directions shown in the drawings or The positional relationship is only for the convenience of describing the present invention and simplifying the description, but does not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.

变桨轴承作为叶片和轮毂的连接部件是风力发电机的变桨系统中的重要组成部分,其结构形式分为内齿型和外齿型两种。所谓内齿型是指轴承内圈带齿与驱动电机小齿轮啮合,其连接方式则是内圈通过螺栓与叶片连接,外圈通过螺栓与轮毂连接;外齿型是指轴承外圈带齿与驱动电机小齿轮啮合,其连接方式则是外圈通过螺栓与叶片连接,内圈通过螺栓与轮毂连接。以下,本实施例以外齿型变桨轴承为例进行说明。As the connecting part between the blade and the hub, the pitch bearing is an important part of the pitch system of the wind turbine, and its structure is divided into two types: internal tooth type and external tooth type. The so-called internal tooth type refers to the meshing of the inner ring of the bearing with teeth and the pinion of the drive motor. The connection method is that the inner ring is connected to the blade through bolts, and the outer ring is connected to the hub through bolts; The drive motor pinion meshes, and the connection method is that the outer ring is connected to the blade through bolts, and the inner ring is connected to the hub through bolts. Hereinafter, the present embodiment will be described as an example of an external gear pitch bearing.

图1是示出本发明涉及的变桨轴承的结构的主视图。如图1所示,变桨轴承100包括轴承外圈110、轴承内圈120以及被开设在外圈端面130和内圈端面140上的用于连接叶片和轮毂的螺栓孔,在图1中例示了54个螺栓孔,并分别以序号1、2、3…54按照顺时针方向进行了标注。轴承外圈110通过螺栓与叶片(未图示)相连,轴承内圈120通过螺栓与轮毂(未图示)相连。轴承外圈110能够相对于轴承内圈120转动,从而改变叶片的迎风角度,使叶片保持为最佳的迎风状态。变桨轴承的内部结构形式包括双排球轴承等,变桨轴承不仅可以承受径向载荷,而且对于轴向载荷也有一定的承受能力。FIG. 1 is a front view showing the structure of a pitch bearing according to the present invention. As shown in Figure 1, the pitch bearing 100 includes a bearing outer ring 110, a bearing inner ring 120, and bolt holes for connecting the blades and the hub that are opened on the end face 130 of the outer ring and the end face 140 of the inner ring. 54 bolt holes are marked clockwise with numbers 1, 2, 3...54. The bearing outer ring 110 is connected to the blade (not shown) through bolts, and the bearing inner ring 120 is connected to the hub (not shown) through bolts. The bearing outer ring 110 can rotate relative to the bearing inner ring 120, thereby changing the windward angle of the blade and keeping the blade in an optimal windward state. The internal structure of the pitch bearing includes double-row ball bearings, etc. The pitch bearing can not only bear radial loads, but also has a certain bearing capacity for axial loads.

如上所述,在风力发电机中,变桨轴承在风力发电的变桨过程中起到了十分重要的作用。变桨是通过调整桨叶角度,改变气流对叶片的攻角,从而改变风电机组获取的空气动力,使风力发电机按照设计的输出功率输出。由于叶片重量和气动推力较大,变桨轴承要承受很大的载荷,尤其是变桨轴承的端面和用于连接的螺栓孔,可能会因为载荷过大而出现裂纹。而且,变桨轴承工作的环境恶劣,环境温度梯度大,变桨轴承也有可能会因为温度的变化影响油脂的润滑和材料的特性从而引起失效。由于变桨轴承结构应力复杂,工作温度场分布不均,为了提早预警,降低质量和安全事故,监测手段至关重要。As mentioned above, in the wind power generator, the pitch bearing plays a very important role in the pitching process of wind power generation. Pitch adjustment is to change the angle of attack of the airflow on the blades by adjusting the angle of the blades, thereby changing the aerodynamic force obtained by the wind turbine, so that the wind turbine can output according to the designed output power. Due to the large weight and aerodynamic thrust of the blades, the pitch bearing is subject to a large load, especially the end face of the pitch bearing and the bolt holes used for connection, which may crack due to excessive load. Moreover, the working environment of the pitch bearing is harsh, and the ambient temperature gradient is large, and the pitch bearing may also cause failure due to changes in temperature affecting the lubrication of the grease and the characteristics of the material. Due to the complex structural stress of the pitch bearing and the uneven distribution of the working temperature field, monitoring means are very important in order to give early warning and reduce quality and safety accidents.

为此,本发明的发明人潜心研究了一种监测手段,在变桨轴承的变桨轴承外圈端面、内圈端面、轴承外圈圆周面或螺栓孔中分别安装光纤光栅传感器代替以往的电阻应变片来监测变桨轴承的变桨轴承外圈端面、内圈端面、轴承外圈圆周面或螺栓孔的例如应变、温度参数等,根据变桨轴承的变桨轴承外圈端面、内圈端面、轴承外圈圆周面和螺栓孔的应变参数来进行预警,防止变桨轴承在运行过程中损坏。即,本发明的监测对象是变桨轴承外圈端面、内圈端面以及轴承外圈圆周面及连接螺栓的螺栓孔的内孔壁,从而覆盖了轴承各个区域,以下,为了方便说明,在不必区分的情况下,有时将变桨轴承外圈端面、内圈端面以及轴承外圈圆周面统称为变桨轴承的轴承端面。由于变桨轴承的轴承端面与螺栓孔的应变参数之间具有一定联系,可以预先建立变桨轴承的轴承端面的应变参数和螺栓孔的应变参数的对应关系,详细情况后面叙述。For this reason, the inventors of the present invention have devoted themselves to researching a monitoring method, installing optical fiber grating sensors on the pitch bearing outer ring end face, inner ring end face, bearing outer ring circumferential surface or bolt holes to replace the previous resistors. Strain gauges are used to monitor the pitch bearing outer ring end face, inner ring end face, bearing outer ring circumferential surface or bolt holes such as strain, temperature parameters, etc., according to the pitch bearing outer ring end face, inner ring end face of the pitch bearing , the strain parameters of the outer ring circumference of the bearing and the bolt holes to give an early warning to prevent the pitch bearing from being damaged during operation. That is, the monitoring objects of the present invention are the end face of the pitch bearing outer ring, the end face of the inner ring, the circumferential surface of the outer ring of the bearing and the inner wall of the bolt hole of the connecting bolt, thus covering all areas of the bearing. In the case of distinction, sometimes the end face of the outer ring of the pitch bearing, the end face of the inner ring, and the circumferential surface of the outer ring of the bearing are collectively referred to as the bearing end face of the pitch bearing. Since there is a certain connection between the bearing end surface of the pitch bearing and the strain parameters of the bolt holes, the corresponding relationship between the strain parameters of the bearing end surface of the pitch bearing and the strain parameters of the bolt holes can be established in advance, and the details will be described later.

如图1所示,在变桨轴承100的外圈端面130上设置光纤光栅应变和温度传感器200,光纤光栅应变和温度传感器200采集变桨轴承100的外圈端面130的例如应变、温度参数等的光信号。具体地说,在变桨轴承100的外圈端面130上的0°、90°、180°和270°处各设置一个测点安装光纤光栅应变和温度传感器200,用于采集变桨轴承100的外圈端面130的应变和温度的光信号。在图1中,根据叶片的形状,外圈端面130的0°为叶片的后缘位置,外圈端面130的180°为叶片的前缘位置。进一步地,由于变桨轴承100的外圈端面130上的0°和180°处承载的载荷较大,因此可以在变桨轴承100的外圈端面130上的0°和180°处设置多个测点集中来安装光纤光栅应变和温度传感器200,比如,在0°处设置6个测点安装光纤光栅应变和温度传感器200。光纤光栅应变和温度传感器200通过裸光栅覆盖、微型传感器熔接等方式,组成与变桨轴承外圈端面等选定部位相应的形状。As shown in Figure 1, a fiber grating strain and temperature sensor 200 is arranged on the outer ring end face 130 of the pitch bearing 100, and the fiber grating strain and temperature sensor 200 collects such as strain and temperature parameters of the outer ring end face 130 of the pitch bearing 100 light signal. Specifically, a measuring point is installed at 0°, 90°, 180° and 270° on the outer ring end face 130 of the pitch bearing 100 to install a fiber grating strain and temperature sensor 200 for collecting the temperature of the pitch bearing 100. Optical signals of strain and temperature of the outer ring end face 130 . In FIG. 1 , according to the shape of the blade, 0° of the outer ring end surface 130 is the trailing edge position of the blade, and 180° of the outer ring end surface 130 is the leading edge position of the blade. Further, since the 0° and 180° positions on the outer ring end surface 130 of the pitch bearing 100 carry relatively large loads, multiple The measuring points are concentrated to install the FBG strain and temperature sensors 200, for example, 6 measuring points are set at 0° to install the FBG strain and temperature sensors 200. The optical fiber grating strain and temperature sensor 200 forms a shape corresponding to selected parts such as the end face of the pitch bearing outer ring by covering the bare grating and welding the micro sensor.

图2是示出本发明涉及的光纤光栅传感测量系统500的构成图。如图2所示,光纤光栅应变和温度传感器200通过光纤链路300与光解调仪400连接,光纤链路300的两端分别与光解调仪400连接。光解调仪400对由光纤光栅应变和温度传感器200采集的光信号进行分析,测得变桨轴承100的外圈端面130的应变和温度。光纤光栅应变和温度传感器200、光纤链路300和光解调仪400构成光纤光栅传感测量系统500。FIG. 2 is a configuration diagram showing a fiber grating sensing measurement system 500 according to the present invention. As shown in FIG. 2 , the fiber grating strain and temperature sensor 200 is connected to the optical demodulator 400 through the optical fiber link 300 , and the two ends of the optical fiber link 300 are respectively connected to the optical demodulator 400 . The optical demodulator 400 analyzes the optical signal collected by the FBG strain and temperature sensor 200 to measure the strain and temperature of the end face 130 of the outer ring of the pitch bearing 100 . The fiber grating strain and temperature sensor 200 , the fiber link 300 and the optical demodulator 400 constitute a fiber grating sensing measurement system 500 .

由于光纤光栅应变传感器的测试结果受到温度影响较大,需要进行温度补偿。Since the test results of fiber grating strain sensors are greatly affected by temperature, temperature compensation is required.

应变及温度补偿计算方法如下所述。The strain and temperature compensation calculation methods are as follows.

以其中一个光纤光栅应变传感器为例计算其应变,传感器初始中心波长:λ0(nm)(室温下测定,传感器自由状态时);Take one of the fiber grating strain sensors as an example to calculate its strain, the initial center wavelength of the sensor: λ0 (nm) (measured at room temperature, when the sensor is in a free state);

预装在外圈端面130上后校正波长:λS0(单位nm,25℃下测定),传感器安装在外圈端面130上后传感器的中心波长发生了变化,传感器在安装完成后,可在现场测量温度T1和波长λ1后再通过表达式After pre-installed on the end face 130 of the outer ring, the wavelength is calibrated: λS0 (in nm, measured at 25°C). After the sensor is installed on the end face 130 of the outer ring, the central wavelength of the sensor changes. After the sensor is installed, the temperature T1 can be measured on site and wavelength λ1 and then through the expression

λS0=λ1-(T1-25)*CS得到,λS0=λ1-(T1-25)*C S is obtained,

产生应变后实际测量时读取波长:λS1(nm)(室温下测定)Read wavelength during actual measurement after strain generation: λ S1 (nm) (measured at room temperature)

波长变化:Δλ=λs1-λs0Wavelength change: Δλ=λ s1 -λs0

光纤光栅应变传感器应变灵敏度:FS(με/pm)Fiber Bragg grating strain sensor strain sensitivity: F S (με/pm)

光纤光栅应变传感器的温度系数:CS(℃/pm)Temperature Coefficient of Fiber Bragg Grating Strain Sensor: C S (°C/pm)

工作时产生的应变(με)计算公式:Calculation formula of strain (με) generated during work:

Δε=(Δλ-ΔT*CS)*FS Δε=(Δλ-ΔT*C S )*F S

其中,in,

ΔT可通过光纤光栅温度传感器测量出来,其计算表达式为:ΔT can be measured by a fiber grating temperature sensor, and its calculation expression is:

ΔT=(λT1T0)/CT ΔT=(λ T1T0 )/C T

光纤光栅温度传感器实际测量时读取波长:λT1(nm)The reading wavelength of the fiber grating temperature sensor in actual measurement: λ T1 (nm)

光纤光栅温度传感器初始波长:λT0(nm,室温下测定)Fiber Bragg Grating temperature sensor initial wavelength: λ T0 (nm, measured at room temperature)

光纤光栅温度传感器的灵敏度系数:CT Sensitivity coefficient of fiber grating temperature sensor: C T

应力计算方法:Stress calculation method:

应力σ的计算表达式为:The calculation expression of stress σ is:

σ=Δε*Eσ=Δε*E

其中△ε为应变变化量,E为变桨轴承外圈的材料的弹性模量。Where △ε is the amount of strain change, and E is the elastic modulus of the material of the pitch bearing outer ring.

同理,其他光纤光栅应变传感器测得的应力均可以通过以上的方法获取。通过以上的温度补偿,能够获取变桨轴承的外圈端面130的实际的应力状态。Similarly, the stress measured by other FBG strain sensors can be obtained by the above method. Through the above temperature compensation, the actual stress state of the outer ring end surface 130 of the pitch bearing can be obtained.

如上所述,由于变桨轴承的轴承端面与螺栓孔的应变参数之间具有一定联系,因此可以预先建立变桨轴承的轴承端面的应变参数和螺栓孔的应变参数的对应关系。这里,可以预先根据实验来得到变桨轴承的外圈端面的应变参数与螺栓孔的应变参数的对应关系。图5例示出变桨轴承的外圈端面的应变与螺栓孔的应变的对应关系。其中,X轴表示变桨轴承100的外圈端面130的应变,Y轴为螺栓孔的应变,R2是相关系数,越接近1表示两者的相关性越高。这里,由于在变桨轴承100的外圈端面130上的0°、90°、180°和270°处各设置了一个测点,与此对应的螺栓孔的序号为1、14、28、41。As mentioned above, since there is a certain relationship between the bearing end surface of the pitch bearing and the strain parameters of the bolt holes, the corresponding relationship between the strain parameters of the bearing end surface of the pitch bearing and the strain parameters of the bolt holes can be established in advance. Here, the corresponding relationship between the strain parameters of the end surface of the outer ring of the pitch bearing and the strain parameters of the bolt holes can be obtained in advance according to experiments. FIG. 5 shows an example of the correspondence relationship between the strain on the end surface of the outer ring of the pitch bearing and the strain on the bolt holes. Wherein, the X-axis represents the strain of the outer ring end surface 130 of the pitch bearing 100, the Y-axis represents the strain of the bolt hole, and R2 is a correlation coefficient, and the closer to 1, the higher the correlation between the two . Here, since a measuring point is set at 0°, 90°, 180° and 270° on the end surface 130 of the outer ring of the pitch bearing 100, the serial numbers of the corresponding bolt holes are 1, 14, 28, 41 .

接着,具体地说明本发明涉及的变桨轴承的监测方法。图3是示出本发明涉及的变桨轴承的监测方法之一的流程图。在步骤101中,预先根据实验来得到变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系。在步骤102中,使用光纤光栅应变和温度传感器200采集变桨轴承100的外圈端面130的温度和应变的光信号,由光解调仪400对由光纤光栅应变和温度传感器200采集的光信号进行分析,测得变桨轴承100的外圈端面130的温度和应变。在步骤103中,利用外圈端面130的温度对外圈端面130的应变进行校正,以获得外圈端面130的实际应变。在步骤104中,根据外圈端面130的实际应变以及变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系来获取螺栓孔的应变。在步骤105中,将如上得到的变桨轴承100的外圈端面130的应变和螺栓孔的应变与预设的故障应变阈值进行比较,根据比较结果发出预警。Next, the monitoring method of the pitch bearing according to the present invention will be specifically described. FIG. 3 is a flowchart showing one of the monitoring methods of the pitch bearing according to the present invention. In step 101 , the corresponding relationship between the strain of the outer ring end surface 130 of the pitch bearing 100 and the strain of the bolt holes is obtained in advance according to experiments. In step 102, the optical signals of temperature and strain of the outer ring end face 130 of the pitch bearing 100 are collected using the optical fiber grating strain and temperature sensor 200, and the optical signals collected by the optical fiber grating strain and temperature sensor 200 are analyzed by the optical demodulator 400 For analysis, the temperature and strain of the outer ring end surface 130 of the pitch bearing 100 are measured. In step 103 , the temperature of the end surface 130 of the outer ring is used to correct the strain of the end surface 130 of the outer ring to obtain the actual strain of the end surface 130 of the outer ring. In step 104, the strain of the bolt hole is obtained according to the actual strain of the end surface 130 of the outer ring and the corresponding relationship between the strain of the end surface 130 of the outer ring of the pitch bearing 100 and the strain of the bolt hole. In step 105, the strain of the end surface 130 of the outer ring of the pitch bearing 100 and the strain of the bolt holes obtained above are compared with a preset fault strain threshold, and an early warning is issued according to the comparison result.

在以上的监测方法中,使用光纤光栅传感测量系统500测得变桨轴承的外圈端面130的应变和温度,根据测得的外圈端面130的应变以及变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系来获取螺栓孔的应变,但是本发明涉及的监测方法不限于此,也可以使用光纤光栅传感测量系统500测得螺栓孔的应变和温度,根据测得的螺栓孔的应变以及变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系来获取变桨轴承100的外圈端面130的应变。In the above monitoring method, the strain and temperature of the outer ring end face 130 of the pitch bearing 100 are measured by using the fiber Bragg grating sensing measurement system 500. According to the measured strain and the outer ring end face 130 of the pitch bearing 100 The strain of the bolt hole can be obtained by the corresponding relationship between the strain of the bolt hole and the strain of the bolt hole, but the monitoring method involved in the present invention is not limited thereto, and the strain and temperature of the bolt hole can also be measured using the fiber grating sensing measurement system 500, according to the measured The strain of the bolt holes and the corresponding relationship between the strain of the outer ring end surface 130 of the pitch bearing 100 and the strain of the bolt holes are used to obtain the strain of the outer ring end surface 130 of the pitch bearing 100 .

具体地说,在变桨轴承100的0°、90°、180°和270°处的螺栓孔1、14、28、41中各设置一个测点安装光纤光栅应变和温度传感器200,并在螺栓孔1、14、28、41的内壁沿轴向或径向安装光纤光栅应变和温度传感器200。图4是示出本发明涉及的变桨轴承的监测方法之二的流程图。在步骤201中,预先根据实验来得到变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系。在步骤202中,使用光纤光栅应变和温度传感器200采集变桨轴承130的螺栓孔的应变和温度的光信号,由光解调仪400对由光纤光栅应变和温度传感器200采集的光信号进行分析,测得变桨轴承的螺栓孔的应变和温度。在步骤203中,利用螺栓孔的温度对螺栓孔的应变进行校正,以获得螺栓孔的实际应变。在步骤204中,根据螺栓孔的实际应变以及变桨轴承100的外圈端面130的应变与螺栓孔的应变的对应关系来获取变桨轴承100的外圈端面130的应变。在步骤205中,将如上得到的变桨轴承100的螺栓孔的应变和外圈端面130的应变与预设的故障应变阈值进行比较,根据比较结果发出预警。Specifically, in the bolt holes 1, 14, 28, and 41 at 0°, 90°, 180°, and 270° of the pitch bearing 100, a measuring point is installed to install a fiber grating strain and temperature sensor 200, and The inner walls of the holes 1, 14, 28, 41 are installed with fiber grating strain and temperature sensors 200 axially or radially. Fig. 4 is a flow chart showing the second monitoring method of the pitch bearing involved in the present invention. In step 201 , the corresponding relationship between the strain of the outer ring end surface 130 of the pitch bearing 100 and the strain of the bolt holes is obtained in advance according to experiments. In step 202, the strain and temperature optical signals of the bolt holes of the pitch bearing 130 are collected using the optical fiber grating strain and temperature sensor 200, and the optical signals collected by the optical fiber grating strain and temperature sensor 200 are analyzed by the optical demodulator 400 , the strain and temperature of the bolt holes of the pitch bearing are measured. In step 203, the temperature of the bolt hole is used to correct the strain of the bolt hole to obtain the actual strain of the bolt hole. In step 204 , the strain of the outer ring end surface 130 of the pitch bearing 100 is obtained according to the actual strain of the bolt hole and the corresponding relationship between the strain of the outer ring end surface 130 of the pitch bearing 100 and the strain of the bolt hole. In step 205, the strain of the bolt holes of the pitch bearing 100 obtained above and the strain of the end face 130 of the outer ring are compared with a preset fault strain threshold, and an early warning is issued according to the comparison result.

在本实施例涉及的变桨轴承100的监测方法中,使用光纤光栅传感测量系统500代替了以往的电阻应变片。由于变桨轴承有时会处于高湿、烟雾、或雷电的工作环境中,光纤光栅传感器由光纤制得,光纤的绝缘性能好、耐腐蚀、化学性能稳定,无需电源驱动,且光纤光栅传感器中传递的光信号不受电磁干扰的影响,在高湿、烟雾、雷电或电磁干扰的工作环境中,均可稳定使用。因此,能够避免电磁干扰,延长了使用寿命,安装和布线都很简单。另外,光纤光栅传感器能够通过裸光栅覆盖、微型传感器熔接等方式,组成与变桨轴承外圈端面、内圈端面以及外圈圆周面或螺栓孔等选定部位相应的形状,因此安装难度和安装成本均较低。In the monitoring method of the pitch bearing 100 involved in this embodiment, the optical fiber grating sensing measurement system 500 is used instead of the conventional resistance strain gauge. Since pitch bearings are sometimes in high humidity, smog, or lightning working environments, the fiber grating sensor is made of optical fiber, which has good insulation performance, corrosion resistance, and stable chemical properties. The optical signal is not affected by electromagnetic interference, and can be used stably in the working environment of high humidity, smog, lightning or electromagnetic interference. Therefore, electromagnetic interference can be avoided, the service life is prolonged, and installation and wiring are simple. In addition, the optical fiber grating sensor can form the shape corresponding to the selected parts such as the end face of the pitch bearing outer ring, the end face of the inner ring, the circumferential surface of the outer ring or the bolt holes through bare grating covering, micro-sensor welding, etc., so the installation difficulty and installation The cost is lower.

另外,若要监测螺栓孔的应变,需要在螺栓孔内安装传感器。为了保证传感器不被损坏,安装传感器的螺栓孔内不能够放置螺栓,但不放置螺栓的螺栓孔在变桨轴承运行过程中,会比较容易因为载荷较大而发生损坏,从而降低变桨轴承的使用寿命。若想得到较准确的螺栓孔的应变,则需要在多个螺栓孔中安装传感器,但由于安装传感器的螺栓孔中不能放置螺栓,因此会带来风机运行安全隐患。若想要保证机组运行安全,就无法得到较准确的螺栓孔的应变。鉴于上述情况,在本实施例涉及的变桨轴承100的监测方法中,使用光纤光栅传感测量系统500对轴承外圈端面130的应变和温度进行监测,根据外圈端面130的应变以及预先建立的外圈端面130的应变与螺栓孔的应变的对应关系来获取螺栓孔的应变。即,只需要在变桨轴承100的轴承外圈端面130上安装光纤光栅应变和温度传感器200,根据预定的变桨轴承的轴承外圈端面130的应变与变桨轴承的螺栓孔的应变的对应关系,就可得到变桨轴承100的螺栓孔的应变,而不需要在变桨轴承100的轴承外圈端面130和螺栓孔中都安装光纤光栅应变和温度传感器200,从而降低变桨轴承100的轴承外圈端面130和螺栓孔的监测成本。另外,根据测得的变桨轴承100的轴承外圈端面130的应变以及预定的变桨轴承100的轴承外圈端面130的应变与变桨轴承100的螺栓孔的应变的对应关系,能够得到较准确的螺栓孔的应变,由此不需要在螺栓孔中安装传感器,螺栓孔中可以放置螺栓,保证了变桨轴承100的使用寿命。因此,能够在确保变桨轴承100的使用寿命的同时,得到较准确的螺栓孔内的应变的监测结果。In addition, to monitor the strain in the bolt hole, a sensor needs to be installed in the bolt hole. In order to ensure that the sensor is not damaged, no bolts can be placed in the bolt holes where the sensors are installed, but the bolt holes without bolts will be easily damaged due to the large load during the operation of the pitch bearing, thereby reducing the pitch bearing. service life. If you want to get a more accurate strain of the bolt holes, you need to install sensors in multiple bolt holes, but since no bolts can be placed in the bolt holes where the sensors are installed, it will bring hidden dangers to the safety of the fan operation. If you want to ensure the safe operation of the unit, you cannot get a more accurate strain of the bolt hole. In view of the above, in the monitoring method of the pitch bearing 100 involved in this embodiment, the strain and temperature of the end face 130 of the bearing outer ring are monitored using the fiber grating sensing measurement system 500, and according to the strain of the end face 130 of the outer ring and the pre-established The strain of the bolt hole is obtained by the corresponding relationship between the strain of the outer ring end face 130 and the strain of the bolt hole. That is, it is only necessary to install the fiber grating strain and temperature sensor 200 on the end surface 130 of the bearing outer ring of the pitch bearing 100, and according to the predetermined correspondence between the strain of the end surface 130 of the bearing outer ring of the pitch bearing and the strain of the bolt hole of the pitch bearing relationship, the strain of the bolt hole of the pitch bearing 100 can be obtained without installing the fiber grating strain and temperature sensor 200 in both the end face 130 of the bearing outer ring of the pitch bearing 100 and the bolt hole, thereby reducing the strain of the pitch bearing 100 The cost of monitoring the bearing outer ring face 130 and bolt holes. In addition, according to the measured strain of the end surface 130 of the bearing outer ring of the pitch bearing 100 and the predetermined corresponding relationship between the strain of the end surface 130 of the bearing outer ring of the pitch bearing 100 and the strain of the bolt holes of the pitch bearing 100, a comparative The strain of the bolt hole is accurate, so there is no need to install a sensor in the bolt hole, and bolts can be placed in the bolt hole, which ensures the service life of the pitch bearing 100 . Therefore, while ensuring the service life of the pitch bearing 100 , more accurate monitoring results of the strain in the bolt holes can be obtained.

或者,在本实施例涉及的变桨轴承的监测方法中,使用光纤光栅传感测量系统500对螺栓孔的应变和温度进行监测,根据螺栓孔的应变以及预先建立的轴承外圈端面130的应变与螺栓孔的应变的对应关系来获取轴承外圈端面130的应变。即,同样地,只需要在变桨轴承100的螺栓孔中安装光纤光栅应变和温度传感器200,根据预定的变桨轴承100的轴承外圈端面130的应变与变桨轴承100的螺栓孔的应变的对应关系,就可得到变桨轴承100的外圈端面130的应变,而不需要在变桨轴承100的轴承外圈端面130和螺栓孔中都安装光纤光栅应变和温度传感器200,从而降低变桨轴承100的轴承外圈端面130和螺栓孔的监测成本。Alternatively, in the monitoring method of the pitch bearing involved in this embodiment, the strain and temperature of the bolt holes are monitored using the fiber grating sensing measurement system 500, and according to the strain of the bolt holes and the pre-established strain of the end surface 130 of the bearing outer ring The strain of the end face 130 of the bearing outer ring is obtained from the corresponding relationship with the strain of the bolt hole. That is, similarly, it is only necessary to install the fiber grating strain and temperature sensor 200 in the bolt hole of the pitch bearing 100, according to the strain of the end surface 130 of the bearing outer ring of the pitch bearing 100 and the strain of the bolt hole of the pitch bearing 100 Corresponding relationship, the strain of the outer ring end surface 130 of the pitch bearing 100 can be obtained, without the need to install fiber grating strain and temperature sensors 200 in both the bearing outer ring end surface 130 and the bolt holes of the pitch bearing 100, thereby reducing the strain The cost of monitoring the bearing outer ring end face 130 and the bolt holes of the paddle bearing 100 .

另外,在本实施例涉及的变桨轴承100的监测方法中,在轴承外圈端面130圆周的0°、90°、180°和270°处安装光纤光栅应变和温度传感器200,即采用环形布置方式来布置光纤光栅应变和温度传感器200。通过上述光纤光栅应变和温度传感器200的布置,能够准确评估变桨轴承100的线或面应力以及温度场,优化了设计参数,降低了故障概率。此外,光纤光栅应变和温度传感器200的布置点不限于此,也可以在轴承外圈端面130圆周的0°、45°、90°、135°、180°、225°和270°处安装光纤光栅应变和温度传感器200,由此能够更准确地评估变桨轴承100的线或面应力以及温度场。In addition, in the monitoring method of the pitch bearing 100 involved in this embodiment, fiber grating strain and temperature sensors 200 are installed at 0°, 90°, 180° and 270° of the circumference of the end face 130 of the bearing outer ring, that is, a ring arrangement is adopted The fiber grating strain and temperature sensor 200 is arranged in a different manner. Through the above-mentioned arrangement of the fiber grating strain and temperature sensors 200, the line or surface stress and the temperature field of the pitch bearing 100 can be accurately evaluated, the design parameters are optimized, and the failure probability is reduced. In addition, the arrangement point of the fiber grating strain and temperature sensor 200 is not limited to this, and the fiber grating can also be installed at 0°, 45°, 90°, 135°, 180°, 225° and 270° of the end face 130 of the bearing outer ring Strain and temperature sensors 200 , thereby enabling a more accurate assessment of the linear or surface stress and temperature field of the pitch bearing 100 .

另外,在本实施例涉及的变桨轴承100的监测方法中,在轴承外圈端面130圆周的0°和180°处设置多个测点安装光纤光栅应变和温度传感器200。由于在变桨轴承100的轴承外圈端面130上的0°和180°处承载的载荷较大,在此处集中多点测量,从而能够更加准确测得此处的应力状态。In addition, in the monitoring method of the pitch bearing 100 involved in this embodiment, a plurality of measuring points are installed at 0° and 180° of the end face 130 of the bearing outer ring to install the fiber grating strain and temperature sensors 200 . Since the loads carried at 0° and 180° on the end surface 130 of the bearing outer ring of the pitch bearing 100 are relatively large, multi-point measurements are concentrated here, so that the stress state here can be measured more accurately.

另外,在本实施例涉及的变桨轴承100的监测方法中,在所述螺栓孔的内壁沿轴向或径向安装光纤光栅应变和温度传感器200。由于变桨轴承100的螺栓孔的内壁裂纹更容易沿轴向或径向发生损坏,因此沿着轴向或径向布置光纤光栅应变和温度传感器200,从而能够更加准确测得螺栓孔的应力状态。In addition, in the monitoring method of the pitch bearing 100 involved in this embodiment, the fiber grating strain and temperature sensor 200 is installed axially or radially on the inner wall of the bolt hole. Since cracks on the inner wall of the bolt holes of the pitch bearing 100 are more likely to be damaged axially or radially, the fiber grating strain and temperature sensors 200 are arranged axially or radially, so that the stress state of the bolt holes can be measured more accurately .

另外,在本实施例涉及的变桨轴承100的监测方法中,光纤光栅应变和温度传感器200通过光纤链路300与光解调仪400连接,光纤链路300的两端分别与光解调仪400连接。由此能够同步地采集数据,可做到通讯故障冗余设计,即使光路中间某处故障,也不会影响整个光路的通讯测试。In addition, in the monitoring method of the pitch bearing 100 involved in this embodiment, the fiber grating strain and temperature sensor 200 is connected to the optical demodulator 400 through the optical fiber link 300, and the two ends of the optical fiber link 300 are connected to the optical demodulator 400 respectively. 400 connections. In this way, data can be collected synchronously, and communication fault redundancy design can be achieved. Even if a fault occurs somewhere in the middle of the optical path, it will not affect the communication test of the entire optical path.

以上,通过变桨轴承的监测方法实现了本发明的技术方案,但是也可以通过变桨轴承的监测系统实现本发明的技术方案。图6是示出本发明涉及的变桨轴承的监测系统的构成图。如图6所示,本发明涉及的变桨轴承的监测系统800包括:光纤光栅传感测量系统500,所述光纤光栅传感测量系统500对所述轴承端面或所述螺栓孔的温度参数和应变参数进行监测;校正单元500a,利用所述温度参数对所述轴承端面或所述螺栓孔的应变参数进行校正,以获得实际应变参数;获取单元600,所述获取单元600预先建立所述轴承端面的应变参数与所述螺栓孔的应变参数的对应关系,并根据所述轴承端面的实际应变参数或者所述螺栓孔的实际应变参数以及预先建立的所述轴承端面的应变参数与所述螺栓孔的应变参数的对应关系来获取所述螺栓孔的应变参数或者所述轴承端面的应变参数;预警单元700,所述预警单元700将所述应变参数与预定的故障应变参数阈值进行比较,根据比较结果发出预警。由此,采用上述变桨轴承的监测系统800同样能够得到上述的技术效果。Above, the technical solution of the present invention is realized through the monitoring method of the pitch bearing, but the technical solution of the present invention can also be realized through the monitoring system of the pitch bearing. Fig. 6 is a configuration diagram showing a monitoring system of a pitch bearing according to the present invention. As shown in FIG. 6 , the monitoring system 800 of the pitch bearing involved in the present invention includes: an optical fiber grating sensing and measuring system 500, and the optical fiber grating sensing and measuring system 500 measures the temperature parameters and Strain parameters are monitored; the correction unit 500a uses the temperature parameters to correct the strain parameters of the bearing end surface or the bolt holes to obtain actual strain parameters; the acquisition unit 600, the acquisition unit 600 pre-establishes the bearing The corresponding relationship between the strain parameter of the end surface and the strain parameter of the bolt hole, and according to the actual strain parameter of the bearing end surface or the actual strain parameter of the bolt hole and the pre-established strain parameter of the bearing end surface and the bolt The strain parameter of the bolt hole or the strain parameter of the bearing end surface is obtained through the corresponding relationship of the strain parameter of the hole; the early warning unit 700, the early warning unit 700 compares the strain parameter with a predetermined fault strain parameter threshold, according to The comparison results are alerted. Therefore, the monitoring system 800 adopting the above-mentioned pitch bearing can also obtain the above-mentioned technical effect.

虽然已经参考优选实施例对本发明进行了描述,但在不脱离本发明的范围的情况下,可以对其进行各种改进并且可以用等效物替换其中的部件。尤其是,只要不存在结构冲突,各个实施例中所提到的各项技术特征均可以任意方式组合起来。本发明并不局限于文中公开的特定实施例,而是包括落入权利要求的范围内的所有技术方案。While the invention has been described with reference to a preferred embodiment, various modifications may be made and equivalents may be substituted for parts thereof without departing from the scope of the invention. In particular, as long as there is no structural conflict, the technical features mentioned in the various embodiments can be combined in any manner. The present invention is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims (11)

1.一种变桨轴承(100)的监测方法,所述变桨轴承(100)包括轴承端面(130,140)和被开设在所述轴承端面(130,140)上的螺栓孔(1~54),其特征在于,所述监测方法包括:1. A monitoring method for a pitch bearing (100), the pitch bearing (100) comprising a bearing end face (130, 140) and bolt holes (1-140) provided on the bearing end face (130, 140) 54), it is characterized in that, described monitoring method comprises: 利用光纤光栅传感测量系统(500)对所述轴承端面(130,140)或所述螺栓孔(1~54)的温度参数和应变参数进行监测;以及monitoring temperature parameters and strain parameters of the bearing end faces (130, 140) or the bolt holes (1-54) by using a fiber Bragg grating sensing measurement system (500); and 利用所述温度参数对所述轴承端面(130,140)或所述螺栓孔(1~54)的应变参数进行校正,以获得实际应变参数。The temperature parameters are used to correct the strain parameters of the bearing end surfaces (130, 140) or the bolt holes (1-54), so as to obtain actual strain parameters. 2.根据权利要求1所述的监测方法,其特征在于,所述监测方法具体包括:2. The monitoring method according to claim 1, wherein the monitoring method specifically comprises: 预先建立所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系,利用所述光纤光栅传感测量系统(500)对所述轴承端面(130,140)的温度参数和应变参数进行监测;The corresponding relationship between the strain parameters of the bearing end faces (130, 140) and the strain parameters of the bolt holes (1-54) is established in advance, and the fiber grating sensing and measuring system (500) is used to measure the bearing end faces (130 , 140) temperature parameters and strain parameters are monitored; 利用所述轴承端面(130,140)的温度参数对所述轴承端面(130,140)的应变参数进行校正,以获得所述轴承端面(130,140)的实际应变参数;correcting the strain parameter of the bearing end face (130, 140) by using the temperature parameter of the bearing end face (130, 140), so as to obtain the actual strain parameter of the bearing end face (130, 140); 根据所述轴承端面(130,140)的实际应变参数以及预先建立的所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系来获取所述螺栓孔(1~54)的应变参数。According to the actual strain parameters of the bearing end surfaces (130, 140) and the pre-established corresponding relationship between the strain parameters of the bearing end surfaces (130, 140) and the strain parameters of the bolt holes (1-54), the said The strain parameter of the bolt hole (1~54). 3.根据权利要求1所述的监测方法,其特征在于,所述监测方法具体包括:3. The monitoring method according to claim 1, wherein the monitoring method specifically comprises: 预先建立所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系,The corresponding relationship between the strain parameters of the bearing end faces (130, 140) and the strain parameters of the bolt holes (1-54) is established in advance, 利用所述光纤光栅传感测量系统(500)对所述螺栓孔(1~54)的温度参数和应变参数进行监测;Monitoring temperature parameters and strain parameters of the bolt holes (1-54) by using the fiber Bragg grating sensing measurement system (500); 利用所述螺栓孔(1~54)的温度参数对所述螺栓孔(1~54)的应变参数进行校正,以获得所述螺栓孔(1~54)的实际应变参数;correcting the strain parameters of the bolt holes (1-54) by using the temperature parameters of the bolt holes (1-54), so as to obtain the actual strain parameters of the bolt holes (1-54); 根据所述螺栓孔(1~54)的实际应变参数以及预先建立的所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系来获取所述轴承端面(130,140)的应变参数。According to the actual strain parameters of the bolt holes (1-54) and the pre-established correspondence between the strain parameters of the bearing end surfaces (130, 140) and the strain parameters of the bolt holes (1-54), the said Strain parameters of the bearing end faces (130, 140). 4.一种变桨轴承(100)的监测系统(800),所述变桨轴承(100)包括轴承端面(130,140)和被开设在所述轴承端面(130,140)上的螺栓孔(1~54),其特征在于,所述监测系统(800)包括:4. A monitoring system (800) for a pitch bearing (100), the pitch bearing (100) comprising a bearing end face (130, 140) and bolt holes opened on the bearing end face (130, 140) (1-54), characterized in that the monitoring system (800) includes: 光纤光栅传感测量系统(500),对所述轴承端面(130,140)或所述螺栓孔(1~54)的温度参数和应变参数进行监测;以及An optical fiber grating sensing and measuring system (500), which monitors temperature parameters and strain parameters of the bearing end faces (130, 140) or the bolt holes (1-54); and 校正单元(500a),利用所述温度参数对所述轴承端面(130,140)或所述螺栓孔(1~54)的应变参数进行校正,以获得实际应变参数。The correction unit (500a) uses the temperature parameters to correct the strain parameters of the bearing end surfaces (130, 140) or the bolt holes (1-54), so as to obtain actual strain parameters. 5.根据权利要求4所述的监测系统(800),其特征在于,5. The monitoring system (800) according to claim 4, characterized in that, 所述光纤光栅传感测量系统(500)对所述轴承端面(130,140)的温度参数和应变参数进行监测,The fiber grating sensing and measuring system (500) monitors temperature parameters and strain parameters of the bearing end faces (130, 140), 所述校正单元(500a)利用所述轴承端面(130,140)的温度参数对所述轴承端面(130,140)的应变参数进行校正,以获得所述轴承端面(130,140)的实际应变参数,The correction unit (500a) corrects the strain parameter of the bearing end surface (130, 140) by using the temperature parameter of the bearing end surface (130, 140), so as to obtain the actual strain of the bearing end surface (130, 140) parameter, 所述监测系统(800)还包括获取单元(600),所述获取单元(600)预先建立所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系,并根据所述轴承端面(130,140)的实际应变参数以及预先建立的所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系来获取所述螺栓孔(1~54)的应变参数。The monitoring system (800) further includes an acquisition unit (600), and the acquisition unit (600) pre-establishes the relationship between the strain parameters of the bearing end faces (130, 140) and the strain parameters of the bolt holes (1-54). Corresponding relationship, and according to the actual strain parameters of the bearing end surface (130, 140) and the pre-established corresponding relationship between the strain parameters of the bearing end surface (130, 140) and the strain parameters of the bolt holes (1-54) to obtain the strain parameters of the bolt holes (1-54). 6.根据权利要求4所述的监测系统(800),其特征在于,6. The monitoring system (800) according to claim 4, characterized in that, 所述光纤光栅传感测量系统(500)对所述螺栓孔(1~54)的温度参数和应变参数进行监测,The fiber grating sensing measurement system (500) monitors the temperature parameters and strain parameters of the bolt holes (1-54), 所述校正单元(500a)利用所述螺栓孔(1~54)的温度参数对所述螺栓孔(1~54)的应变参数进行校正,以获得所述螺栓孔(1~54)的实际应变参数,The correction unit (500a) uses the temperature parameters of the bolt holes (1-54) to correct the strain parameters of the bolt holes (1-54), so as to obtain the actual strain of the bolt holes (1-54) parameter, 所述监测系统(800)还包括获取单元(600),所述获取单元(600)预先建立所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系,并根据所述螺栓孔(1~54)的实际应变参数以及预先建立的所述轴承端面(130,140)的应变参数与所述螺栓孔(1~54)的应变参数的对应关系来获取所述轴承端面(130,140)的应变参数。The monitoring system (800) further includes an acquisition unit (600), and the acquisition unit (600) pre-establishes the relationship between the strain parameters of the bearing end faces (130, 140) and the strain parameters of the bolt holes (1-54). Corresponding relationship, and according to the actual strain parameters of the bolt holes (1-54) and the pre-established corresponding relationship between the strain parameters of the bearing end surface (130, 140) and the strain parameters of the bolt holes (1-54) to obtain the strain parameter of the bearing end surface (130, 140). 7.根据权利要求5或6所述的监测系统(800),其特征在于,所述光纤光栅传感测量系统(500)包括对所述轴承端面(130,140)和所述螺栓孔(1~54)的温度参数和应变参数的光信号进行采集的光纤光栅传感器(200),所述光纤光栅传感器(200)分别设置在所述轴承端面圆周的0°、90°、180°和270°处。7. The monitoring system (800) according to claim 5 or 6, characterized in that, the fiber grating sensing measurement system (500) includes a pair of the bearing end face (130, 140) and the bolt hole (1 ~54) the fiber grating sensor (200) that collects the optical signal of temperature parameter and strain parameter, and described fiber grating sensor (200) is respectively arranged at 0 °, 90 °, 180 ° and 270 ° of the circumference of described bearing end face place. 8.根据权利要求7所述的监测系统(800),其特征在于,所述光纤光栅传感器(200)还设置在所述变桨轴承(100)的0°、90°、180°和270°处的所述螺栓孔(1,14,28,41)中。8. The monitoring system (800) according to claim 7, characterized in that, the fiber grating sensor (200) is also arranged at 0°, 90°, 180° and 270° of the pitch bearing (100) in the said bolt holes (1,14,28,41). 9.根据权利要求7所述的监测系统(800),其特征在于,所述光纤光栅传感器(200)在所述轴承端面圆周的0°和180°处被设置多个。9. The monitoring system (800) according to claim 7, characterized in that, multiple fiber grating sensors (200) are arranged at 0° and 180° of the circumference of the bearing end face. 10.根据权利要求8所述的监测系统(800),其特征在于,所述光纤光栅传感器(200)在所述螺栓孔(1,14,28,41)的内壁沿轴向或径向被安装。10. The monitoring system (800) according to claim 8, characterized in that, the fiber grating sensor (200) is axially or radially mounted on the inner wall of the bolt hole (1, 14, 28, 41) Install. 11.根据权利要求4至10中任一项所述的监测系统(800),其特征在于,所述光纤光栅传感测量系统(500)还包括对由所述光纤光栅传感器(200)采集到的光信号进行分析的光解调仪(400),所述光纤光栅传感器(200)通过光纤链路(300)与所述光解调仪(400)连接,所述光纤链路(300)的两端分别与所述光解调仪(400)连接。11. according to the monitoring system (800) described in any one in claim 4 to 10, it is characterized in that, described optical fiber grating sensing measurement system (500) also comprises to collect by described optical fiber grating sensor (200) An optical demodulator (400) for analyzing the optical signal, the fiber grating sensor (200) is connected with the optical demodulator (400) through an optical fiber link (300), and the optical fiber link (300) The two ends are respectively connected with the optical demodulator (400).
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