Notes on 'The electric control of large aeroplanes'

Thompson K.

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Notes on 'The electric control of large aeroplanes'

机译：关于“大型飞机的电气控制”的说明

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The author examines a proposal published by D.T. Glass-Hooper (see Flight, Dec. 21, 1916) for controlling an aircraft using solenoids. He than discusses the control systems used almost universally in aircraft through the end of WWII, and the gradual evolution to almost all-electrical flight control (the hydraulic actuator is the last major nonelectrical element). Laboratory testing of electric actuators is considered and the C-141 Aileron electric actuation system is presented. The High Technology Test Bed program, which was implemented to provide a research aircraft for the development and evaluation of aerodynamic, avionic, and flight control system concepts, is described.

机译：作者研究了D.T. Glass-Hooper发布的一项提案（请参阅1916年12月21日，航班），该提案使用螺线管控制飞机。然后，他讨论了到第二次世界大战结束时几乎在飞机上普遍使用的控制系统，以及逐步发展为几乎全电动的飞行控制（液压执行器是最后一个主要的非电动元件）。考虑了电动执行器的实验室测试，并介绍了C-141 Aileron电动执行系统。描述了高科技试验台计划，该计划的实施旨在为航空器，航空电子和飞行控制系统概念的开发和评估提供研究飞机。

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《IEEE Aerospace and Electronic Systems Magazine》 |1988年第12期|P.19-24|共6页
作者
Thompson K.;
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正文语种 eng
中图分类航空;
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Notes on 'The electric control of large aeroplanes'

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