Test bench for helicopter electro mechanical actuation system validation: Design and validation of dedicated test bench for aeronautical electromechanical actuators

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

9 Citations (Scopus)

Abstract

The introduction of a new product in the aeronautical sector implies conducting characterization tests in an automated, safe and sustainable way. This paper describes a dedicated test bench design and validation that allows characterizing a swashplate Helicopter Electro Mechanical Actuation System (HEMAS). The test bench replicates the operating conditions that the actuator will encounter in service simulating the aerodynamic force by a hydraulic counter load system. The results obtained in validation tests show the ability of the test bench to replicate specified test cases. The validation was performed using a hydraulic cylinder to replicate the motion profile that will be followed by the actuator. The test campaign with the actuator will be performed during 2015.

Original languageEnglish
Title of host publication2015 IEEE International Conference on Industrial Technology, ICIT 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages517-523
Number of pages7
EditionJune
ISBN (Electronic)9781479978007
DOIs
Publication statusPublished - 16 Jun 2015
Event2015 IEEE International Conference on Industrial Technology, ICIT 2015 - Seville, Spain
Duration: 17 Mar 201519 Mar 2015

Publication series

NameProceedings of the IEEE International Conference on Industrial Technology
NumberJune
Volume2015-June

Conference

Conference2015 IEEE International Conference on Industrial Technology, ICIT 2015
Country/TerritorySpain
CitySeville
Period17/03/1519/03/15

Keywords

  • Actuators
  • Design
  • Electro mechanical
  • EMA
  • HEMAS
  • Simulation
  • Test bench
  • Test rig

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