Integrated Compact Electrically Powered and Signaled Actuation Systems

I. Tsun Wang, Dmitry Ignatyev, Gokhan Inalhan, Andrew Collins, Szuyu Cheng, Shirley Stephen

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

Abstract

One of the key challenges in enabling More Electric Aircraft is the development of electrically powered servos that meet or exceed the performance, packaging, weight, and cost of a hydraulic fly-by-wire servo. This paper introduces an innovative Electro-Hydrostatic Actuator that outperforms the existing solutions in terms of mass, size and energy efficiency. The innovative design features hydraulic regeneration when the commanded movement is aligned with the direction of external force. This new feature helps to decrease energy consumption. The high efficiency of the actuator prototype is confirmed by simulation with a verified MATLAB/Simulink model. Simulations also manifest that the proposed actuator has improved phase and gain margins as compared to existing solutions.

Original languageEnglish
Title of host publicationAIAA AVIATION 2022 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106354
DOIs
Publication statusPublished - 2022
Externally publishedYes
EventAIAA AVIATION 2022 Forum - Chicago, United States
Duration: 27 Jun 20221 Jul 2022

Publication series

NameAIAA AVIATION 2022 Forum

Conference

ConferenceAIAA AVIATION 2022 Forum
Country/TerritoryUnited States
CityChicago
Period27/06/221/07/22

Bibliographical note

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Funding

This work has been done as a cooperation between Cranfield University and Domin Fluid Power Limited. This research is funded by the Innovate UK in the scope of project INCEPSION: Integrated Compact Electrically Powered & Signalled Actuation Systems (project No 74303).

FundersFunder number
Domin Fluid Power Limited
Cranfield University
Innovate UK74303

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