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Imaging Ultrasonic Sensor System SWISS Completed 60.000 Simulated Flight Hours to Check Structural Integrity of Aircraft Subcomponent

机译:成像超声波传感器系统瑞士完成了60.000个模拟飞行时间,检查飞机子组件的结构完整性

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Many military platforms such as fighter aircraft are nowadays operated for several decades under sometimes varying missions. Additional requirements resulting from more severe fatigue spectra or extended life for these platforms may require additional means of ensuring structural integrity. It is then important to gain the maximum usage (fatigue life) of aircraft components most efficiently still ensuring structural integrity at all times. Conventional structural health monitoring systems are typically based on loads and usage monitoring. Together with modern non destructive damage detection techniques it could be possible to safely operate even aged platforms. This goal is achieved by periodic examinations in order to ensure that a structural item is free of damage. However, the dismantling of structures for the purpose of non destructive testing can be very costly, time intensive and sometimes harmful to the surrounding structure itself. Therefore integrated, reliable and affordable damage detection techniques are needed to avoid disassembly where economically or technically justified. Especially for well known hot spots an integrated damage sensor could provide an alternative solution to conventional procedures. SWISS (Smart Wide area Imaging Sensor System) is an ultrasonic imaging approach. A small sensor is permanently surface mounted on the component that is to be monitored. Typically the sensor is activated on ground and interrogated via cables that are built into the platform. These sensors facilitate the examination of the internal structure of a subcomponent. The ultrasonic beam is electronically controlled in order to scan the most critical areas from a fixed position. Functionality aspects as well as practicability issues of such a technology had to be addressed and solved. As a result of this study, simulated fatigue tests on a real complex fitting structure have proven the reliability of the imaging ultrasonic sensor under laboratory conditions for more than 60000 simulated flight hours without problems and that the high volume coverage proved to be beneficial for detecting even unexpected damages.
机译:如今,许多军用平台如战斗机,在有时不同的任务下运行了数十年。由更严重的疲劳光谱或延长这些平台的寿命产生的额外要求可能需要额外的方法来确保结构完整性。然后,重要的是为了获得飞机组分的最大用法(疲劳寿命)最有效地始终确保结构完整性。传统的结构健康监测系统通常基于负载和使用监控。与现代的非破坏性损坏检测技术一起,可以安全地操作甚至是老化平台。通过定期检查实现这一目标,以确保结构项目没有损坏。然而,为非破坏性测试的目的拆除结构可能是非常昂贵的,时间密集且有时对周围结构本身有害。因此,需要集成,可靠和实惠的损坏检测技术,以避免在经济或技术上辩护的地方拆卸。特别是众所周知的热点集成损伤传感器可以向常规程序提供替代解决方案。瑞士(智能宽面积成像传感器系统)是超声波成像方法。小型传感器永久地安装在要监视的部件上。通常,传感器在地面上激活并通过电缆询问,该电缆内置在平台中。这些传感器有助于检查子组件的内部结构。超声波束被电子控制,以便从固定位置扫描最关键的区域。功能方面以及这种技术的实用性问题必须得到解决和解决。由于本研究,实际复合拟合结构上的模拟疲劳试验在实验室条件下证明了成像超声波传感器的可靠性超过60000模拟的飞行时间而没有问题,并且高容量覆盖率证明是有益的检测意外损害。

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