Reliable electro-mechanical actuators in aircraft

  • A. Garcia*
  • , J. Cusidó
  • , J. A. Rosero
  • , J. A. Ortega
  • , L. Romeral
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

156 Citations (Scopus)

Abstract

There is a general trend in the aerospace industry toward increasing the use of electrically-powered equipment. This trend is usually referred to as "Power-by-Wire" in the "More Electric Aircraft" (MEA) concept and it leads, among others, to the substitution of hydraulic actuators by Electro-Mechanical Actuators (EMA). Its benefits are a decrease in maintenance effort and weight, and an increase in efficiency. However, jamming case obstacles stop the massive use of EMAs in flight-control actuators. The aim herein is to introduce the safety needs of electro-mechanical actuators in aircraft applications, and its major goal is to present the suitability and reliability of such actuator systems, including electric motors and power converters.

Original languageEnglish
Article number4607895
Pages (from-to)19-25
Number of pages7
JournalIEEE Aerospace and Electronic Systems Magazine
Volume23
Issue number8
DOIs
Publication statusPublished - Aug 2008
Externally publishedYes

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