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Robust Hydraulic Filter Rated Using Dynamic Efficiency Test Method Will Increase Aircraft Reliability and Safety

机译:使用动态效率测试方法对坚固的液压滤清器进行评级,将提高飞机的可靠性和安全性

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Hydraulic contamination is a major contributor to flight control anomalies, binding, and leakage of hydraulic components Typically, filters are rated using Beta Ratio/Efficiency at certain micron sizes per standard lab tests such as ISO 16889 or MM-F-8815D (Ref 1, 2). These are all steady flow tests at 100°F Unfortunately, during normal aircraft operations, hydraulic filters are exposed to a wide range of operating conditions such as high oil temperatures, vibration due to pressure pulsations and flight maneuvers, cyclic flow and thermal excursions. The current hydraulic filters used on Army helicopters tend to shed particles during cyclic flow and vibration which can cause close clearance spools to lock-up in servo controls. This may result in un-commanded flight control inputs. This can also result in low Mean Time Between Failures (MTBF) on pumps and actuators The US Army has developed new hydraulic filter specifications which require dynamic test procedures using more realistic conditions. This has resulted in the development of more robust media filters, which have been shown during on-aircraft demonstrations to increase fluid cleanliness and decrease maintenance costs.
机译:液压污染是导致飞行控制异常,粘结和液压元件泄漏的主要因素。通常,按照ISO 16889或MM-F-8815D等标准实验室测试,使用某些特定微米尺寸的Beta比率/效率来对过滤器进行评级(参考资料1, 2)。这些都是在100°F下进行的稳定流量测试。不幸的是,在飞机正常运行期间,液压滤清器要承受广泛的运行条件,例如油温高,压力脉动和飞行操纵引起的振动,循环流和热偏移。当前在陆军直升机上使用的液压过滤器在循环流动和振动过程中往往会掉落颗粒,这可能导致紧密的线轴在伺服控制中锁定。这可能会导致不受控的飞行控制输入。这也可能导致泵和执行器的平均故障间隔时间(MTBF)降低。美国陆军开发了新的液压过滤器规格,该规格要求使用更实际的条件进行动态测试程序。这导致了更坚固的介质过滤器的开发,在飞机上的演示过程中已经证明了这种过滤器可以提高流体清洁度并降低维护成本。

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