'MORE ELECTRIC' CONTROL SURFACE ACTUATION: A STANDARD FOR THE NEXT GENERATION OF TRANSPORT AIRCRAFT

机译：“更多电”控制表面致动：下一代运输飞机的标准

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For a long time the control surfaces of transport airplanes above a certain weight have been hydraulically powered. The most recent generation of in-service commercial transports is showing generalization of the electrical signaling of the hydraulic flight control actuators, known as Fly By Wire systems. The very new aircraft generation, presently under development, now features a mixed flight control actuation power source distribution, associating electrically powered actuators with conventional FBW hydraulic servocontrols. The intent of this paper is to highlight the drivers for this evolution, to discuss the presently selected electrical actuator technology and the future of this "More Electric" configuration.

机译：长期以来，一定重量以上的运输飞机的控制面都采用液压驱动。最新一代的在役商业运输工具显示了液压飞行控制执行器的电子信号的一般化，这被称为Fly By Wire系统。目前正在开发中的新一代飞机，现在具有混合飞行控制致动电源分配，将电动致动器与常规FBW液压伺服控制器相关联。本文的目的是强调这一发展的驱动力，讨论当前选择的电动执行器技术以及这种“更多电动”配置的未来。

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《Power Electronics Intelligent Motion Power Quality》|2005年|31-37|共7页
会议地点 Nurnberg(DE)
作者
Dominique van den Bossche;
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作者单位

Primary Flight Control Actuation Hydraulics AIRBUS 316 Route de Bayonne, 31060 Toulouse Cedex 03, France;

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会议组织
原文格式 PDF
正文语种 eng
中图分类输配电工程、电力网及电力系统;
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专利

1. Control of flying flexible aircraft using control surfaces and dispersed piezoelectric actuators [J] . Tuzcu H, Meirovitch L Smart Materials & Structures . 2006,第4期

机译：使用控制面和分散的压电执行器控制柔性飞机的飞行
2. Aurora to replace control surfaces on electric aircraft with actuators or effectors [J] . John Keller Military & Aerospace Electronics . 2021,第8期

机译：Aurora用致动器或效应替换电机上的控制表面
3. Fault Tolerant Control of Aircraft Actuating Surfaces using Generalized DI and Integral SM Control [J] . Abdulrahman H. Bajodah, Hamayun M. Tariq, Kumar Pakki. Bharani Chandra, Journal of Intelligent & Robotic Systems: Theory & Application . 2013,第1a4期

机译：使用广义DI和集成SM控制的飞机操纵面容错控制
4. MORE ELECTRIC CONTROL SURFACE ACTUATION A STANDARD FOR THE NEXT GENERATION OF TRANSPORT AIRCRAFT [C] . Dominique van den Bossche Europ Official of the International Conference on Power ELectronics Intelligent Motion Power Quality . 2006

机译：更多的电控表面致动下一代运输飞机的标准
5. Fault-tolerant control design for an electrohydraulic actuator with application to positioning of aircraft flight control surfaces. [D] . Karpenko, Mark. 2002

机译：电动液压执行器的容错控制设计，应用于飞机飞行控制表面的定位。
6. Linear Extended State Observer-Based Motion Synchronization Control for Hybrid Actuation System of More Electric Aircraft [O] . Xingjian Wang, Rui Liao, Cun Shi, 2017

机译：基于线性扩展状态观测器的混合动力电动飞机运动同步控制
7. Experimental Development of a Health Monitoring Method for Electro-Mechanical Actuators of Flight Control Primary Surfaces in More Electric Aircrafts [O] . Mirko Mazzoleni, Fabio Previdi, Matteo Scandella, 2019

机译：更多电气飞机飞行控制主要表面的机电致动器健康监测方法的实验开发
8. Research and Development of Aircraft Control Actuation Systems. The Development of a Flight Control System Simulator,Research on a Control Surface Flutter Suppression Technique and High Temperature Testing of Mil-H-83282. [R] . jenney, gavin d. 1975

机译：飞机控制驱动系统的研究与开发。飞控系统模拟器的研制，控制面颤振抑制技术及mil-H-83282高温测试研究。

'MORE ELECTRIC' CONTROL SURFACE ACTUATION: A STANDARD FOR THE NEXT GENERATION OF TRANSPORT AIRCRAFT

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