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Blade-Tip Monitoring with Through-the-Case Eddy Current Sensors

机译:通过全程涡流传感器进行刀尖监控

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A new eddy current sensor can monitor turbine blade-tip timing and clearance through the housing, in the presence of contaminants, and at temperatures up to 1000°F. Augmented with a nonintrusive stress measurement system, the sensor can detect both synchronous and asynchronous vibrations as well as the onset of blade fatigue. Blade-tip sensors are widely used to monitor the behavior of bladed disks in rocket engine turbo pumps, gas turbine engines, and steam turbines. They can also diagnose problems and help predict how much more service life to expect from the rotor. The sensors are commonly integrated with a nonintrusive stress measurement system in the laboratory and in test cells to measure blade resonance (high-cycle fatigue), detect cracks in blades and disks (high- and low-cycle fatigue), detect damage from foreign objects, investigate rotating stall, and analyze blade flutter, along with other rotational anomalies. The equipment also has the potential to perform real-time monitoring of an engine during flight. The conventional practice has been to mount strain gauges on the blades or in the engine casing (usually by drilling holes through the case). Depending on the sensor target location on the blade, such measurement devices can protrude into the gas path. This article describes the development of a novel sensor that can make the same detailed measurements while mounted on the outside of the engine case. No holes, and no interruption in the gas path. The three leading candidate sensor technologies for blade vibration measurement at present are capacitance, optics, and eddy current. Capacitance works well when clear access to the blade tip is available and the dielectric of the fluid in the gap between sensor and blade is constant. But these sensors tend to be unreliable at medium-to-high temperatures, they cannot be used when oil contamination is present, and special materials are needed for operation at cryogenic temperatures. Optical devices also require clear access to the blade tip, and the fluid in the gap must be transparent. These sensors can be used at very high temperatures but not in the presence of contaminants. Eddy current sensors can be used whether access to the blade is available or not (i.e., they can "see through the case"), and are unaffected by the presence of oil and other contaminants. Hood Technology's eddy current sensors (see Figure 1) can operate at up to 1000°F, and recent tests in a liquid nitrogen bath have shown that the signal is not affected by cryogenic temperatures. They can measure both tip timing and tip clearance of each blade in real time at very high resolution. There are, however, limits to the thickness and material of the case that these sensors can see through.
机译:一个新的涡流传感器可以监视涡轮机叶片的正时和通过壳体的间隙,是否存在污染物以及温度高达1000°F。借助非侵入式应力测量系统,该传感器可以检测同步和异步振动以及叶片疲劳的发作。叶片尖端传感器广泛用于监视火箭发动机涡轮泵,燃气涡轮发动机和蒸汽涡轮中叶片盘的行为。他们还可以诊断问题并帮助预测转子的预期使用寿命。传感器通常在实验室和测试单元中与非侵入式应力测量系统集成在一起,以测量叶片共振(高周疲劳),检测叶片和磁盘上的裂纹(高周疲劳和低周疲劳),检测异物损坏,调查旋转失速并分析叶片颤动以及其他旋转异常。该设备还具有在飞行过程中对发动机进行实时监控的潜力。常规做法是将应变仪安装在叶片上或发动机壳体上(通常通过在壳体上钻孔)。根据传感器在叶片上的目标位置,此类测量设备可能会伸入气路。本文介绍了一种新型传感器的开发,该传感器可以在安装在发动机壳体外部时进行相同的详细测量。没有孔,气路也没有中断。目前,用于叶片振动测量的三种领先的候选传感器技术是电容,光学器件和涡流。当可以清楚地接触到刀片尖端并且传感器与刀片之间的间隙中的流体介电常数恒定时,电容效果很好。但是这些传感器在中至高温下往往不可靠,在存在油污的情况下不能使用它们,并且在低温下运行需要特殊的材料。光学设备还需要通向刀片尖端的通道,间隙中的流体必须透明。这些传感器可以在很高的温度下使用,但不能在有污染物的情况下使用。无论是否有刀片可用,都可以使用涡流传感器(即,它们可以“透视外壳”),并且不受油和其他污染物的影响。 Hood Technology的涡流传感器(见图1)可以在高达1000°F的温度下运行,最近在液氮浴中进行的测试表明,该信号不受低温影响。他们可以非常高分辨率地实时测量每个刀片的叶尖正时和叶尖间隙。但是,这些传感器可以透视的外壳的厚度和材料受到限制。

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