International audienceThis paper deals with safety-critical, high-power actuation in aerospace applications. Using a system-level synthetic view, it identifies, explains and discusses the reasons why electrically supplied, or power-by-wire, solutions have not spread rapidly enough to become a generalized replacement of the conventional, hydraulically supplied ones. Once the actuation needs have been summarized, the drawbacks of conventional actuation and the merits of electrically supplied actuation are listed and analyzed. Then, the challenges to be met in order to mitigate the intrinsic disadvantages of power-by-wire are addressed in detail with a focus on the solutions under development or research. Numerous examples, numerical data and ...
In modern electric aircraft, many conventional systems are replaced with their electrical equivalent...
International audienceThis book is the first of a series of volumes that cover the topic of aerospac...
A power by wire aircraft is one in which all active functions other than propulsion are implemented ...
International audienceThis paper deals with safety-critical, high-power actuation in aerospace appli...
International audienceThe combination of electrics and hydraulics technology is addressed for aerosp...
The concept of More Electric Aircraft (MEA) aims to address the demand for efficiency, reliability a...
The power to move aircraft control surfaces has advanced from being manually generated (by the pilot...
An ever increasing number of actuation functions historically performed by hydraulics or pneumatics ...
This book presents recent results on fault diagnosis and condition monitoring of airborne electromec...
International audienceThe analysis of customer's requirements is addressed in the case of actuation ...
During the last two decades, the aerospace industry has experienced a significant research boom in t...
Electrical actuation systems have recently been introduced in aviation pursuing the concepts of More...
PBW actuation methods, particularly Electro-Mechanical Actuators (EMA) and Electro-Hyrdrostatic Actu...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
International audienceThe paper deals with the comparison of hydraulically and electrically powered ...
In modern electric aircraft, many conventional systems are replaced with their electrical equivalent...
International audienceThis book is the first of a series of volumes that cover the topic of aerospac...
A power by wire aircraft is one in which all active functions other than propulsion are implemented ...
International audienceThis paper deals with safety-critical, high-power actuation in aerospace appli...
International audienceThe combination of electrics and hydraulics technology is addressed for aerosp...
The concept of More Electric Aircraft (MEA) aims to address the demand for efficiency, reliability a...
The power to move aircraft control surfaces has advanced from being manually generated (by the pilot...
An ever increasing number of actuation functions historically performed by hydraulics or pneumatics ...
This book presents recent results on fault diagnosis and condition monitoring of airborne electromec...
International audienceThe analysis of customer's requirements is addressed in the case of actuation ...
During the last two decades, the aerospace industry has experienced a significant research boom in t...
Electrical actuation systems have recently been introduced in aviation pursuing the concepts of More...
PBW actuation methods, particularly Electro-Mechanical Actuators (EMA) and Electro-Hyrdrostatic Actu...
Development of reliable power-by-wire actuation systems for both aeronautical and space applications...
International audienceThe paper deals with the comparison of hydraulically and electrically powered ...
In modern electric aircraft, many conventional systems are replaced with their electrical equivalent...
International audienceThis book is the first of a series of volumes that cover the topic of aerospac...
A power by wire aircraft is one in which all active functions other than propulsion are implemented ...