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Aerospace - Testing of Electromechanical Actuators, General Guidelines For 航空航天.机电作动器的试验.一般指南
发布日期: 2013-10-04
本文件概述了机电执行器(EMA)特有的测试以及与测试相关的问题。测试和记录的问题不一定包括所有内容。本文件讨论了适用于EMA的测试以及实现测试目标的测试方法。EMA可用于多种应用,如公用事业、二次飞行控制和一次飞行控制,在多种市场,包括载人和无人民用和军用飞机、小型导弹鳍和推力矢量控制应用,直至高功率公用事业和飞行控制。EMA也可以有旋转或线性输出,由伺服控制,或使用简单的开环点对点或其他控制拓扑。因此,本文件涵盖了广泛的潜在应用,任何给定测试要求的应用由应用程序和用户决定。本文件试图为各种应用中应考虑哪些测试提供基本指导。 本文件还列出了并非EMA独有的测试,但仍适用于EMA。在这些情况下,本文件不包含对此类试验的讨论,如适用,读者可参考文本中所示的适当文件。虽然许多EMA配置包括数字动力驱动电子设备(PDE),但电子硬件、软件或固件所需的特定测试不在本文档的范围内。
This document provides an overview of the tests, and issues related to testing, that are unique to Electromechanical Actuators (EMAs). The tests, and issues documented, are not necessarily all-inclusive. This document discusses both the tests applicable to EMAs and the test methodologies to accomplish the test objectives. EMAs may be used in a wide variety of applications such as utility, secondary flight controls and primary flight controls, in a wide variety of markets including manned and unmanned civil and military aircraft, small missile fin and thrust vector control applications up to high powered utility and flight controls. EMAs may also have either a rotary or a linear output, be servo controlled or use simple open loop point-to-point or other control topologies. As such this document covers a wide range of potential applications, the application of any given test requirement is determined by the application and the user. This document attempts to provide basic guidance on which tests should be considered for various applications. This document also lists tests that are not unique to EMAs, but are still applicable to EMAs. In these instances a discussion of such tests is not contained in this document, and as applicable, the reader may reference the appropriate documents as indicated in the text. While many EMA configurations include digital power drive electronics (PDE), the specific tests required for the electronic hardware, software, or firmware are outside the scope of this document.
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