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EMC Failures Happen

机译:发生EMC故障

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摘要

EMC testing for components and subsystems has evolved greatly over the last 40 years since MIL-STD-461/461A was released. This design and test-procedures document was a credible attempt at standardizing EMC tests and has formed the basis for many other government and industrial procedures for equipment and subsystem tests. Unfortunately, it was not designed for system-level testing, and any attempt to use the procedure for in situ operational tests is futile. Unfortunately, duplicating the operational EME is impossible. Even coming close is very expensive because of the continually worsening adverse RF and physical environment such as shock and vibration, ESD, lightning, salt fog, or rain. These changing environmental conditions directly affect the performance of the EUT device. Since the EME is continually evolving, it is not possible to guarantee future performance of a new EUT based on the performance of the same or similar devices that may have been fielded in the past. This is especially true if an EMCSM was not established. Without previous EMCSM data or current EMC test data that provides the susceptibility profile, it can only be assumed that the equipment is at the threshold of failure with respect to the original EMC test environment. If the EMC test standard used was MIL-STD-461C, that standard defines a 20-year-old environment that is not adequate to protect today's equipment. Equipment often fails in its operational environment, and manufacturers chalk it up to unknown causes when, in many cases, the problem is an EMC susceptibility problem. All such failures should be investigated and a post-mortem reporting procedure developed to determine the cause of the failure so future systems won't have the same problem. When it's not possible to test like you fly and provide reasonable assurance that the system will work in an adverse environment, use a modern standard tailored to the most flight-like conditions possible and determine an EMCSM during the performance of the test. The recommended minimum EMCSM is 6 dB, but 12 dB would be better.
机译:自MIL-STD-461 / 461A发布以来,在过去40年中,针对组件和子系统的EMC测试有了很大的发展。此设计和测试过程文档是对EMC测试进行标准化的可靠尝试,并且已成为许多其他政府和工业程序用于设备和子系统测试的基础。不幸的是,它不是为系统级测试而设计的,任何尝试将该程序用于现场操作测试都是徒劳的。不幸的是,不可能复制可操作的EME。由于不利的RF和物理环境(例如冲击和振动,ESD,雷电,盐雾或雨水)持续恶化,即使接近也很昂贵。这些不断变化的环境条件直接影响EUT设备的性能。由于EME不断发展,因此不可能基于过去可能使用过的相同或相似设备的性能来保证新EUT的未来性能。如果未建立EMCSM,则尤其如此。如果没有以前的EMCSM数据或提供易感性配置文件的当前EMC测试数据,则只能假定设备相对于原始EMC测试环境而言处于故障阈值。如果使用的EMC测试标准是MIL-STD-461C,则该标准定义了一个已有20年历史的环境,不足以保护当今的设备。设备通常会在其运行环境中发生故障,并且在许多情况下,问题是EMC易感性问题时,制造商会将其归因于未知原因。应该调查所有此类故障,并开发事后报告程序以确定故障原因,以便将来的系统不会出现相同的问题。如果无法像飞机一样进行测试并提供合理的保证,以确保系统可以在不利的环境下运行,请使用适合于最可能出现类似飞行情况的现代标准,并在测试过程中确定EMCSM。建议的最小EMCSM为6 dB,但是12 dB更好。

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