Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators

Electro-Hydraulic Servo-Actuators (EHSA) are currently the most used actuation technology for primary flight control systems of civil and military aircrafts. Although some alternatives have emerged in the last decade, such as electromechanical or electro-hydrostatic solutions, electrohydraulic syste...

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Main Authors: Sylvain Autin, Andrea De Martin Giovanni Jacazio, Jérôme Socheleau, George Vachtsevanos
Format: Article
Language:English
Published: The Prognostics and Health Management Society 2021-03-01
Series:International Journal of Prognostics and Health Management
Subjects:
Online Access:https://papers.phmsociety.org/index.php/ijphm/article/view/2935
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spelling doaj-82f2e480c6b049ac8a4708325f5be91b2021-07-02T21:15:08ZengThe Prognostics and Health Management SocietyInternational Journal of Prognostics and Health Management2153-26482153-26482021-03-01123doi:10.36001/ijphm.2021.v12i3.2935Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control ActuatorsSylvain Autin0Andrea De Martin Giovanni Jacazio1Jérôme Socheleau2George Vachtsevanos3Collins AerospacePolitecnico di Torino – Department of Mechanical and Aerospace EngineeringCollins AerospaceGeorgia Institute of TechnologyElectro-Hydraulic Servo-Actuators (EHSA) are currently the most used actuation technology for primary flight control systems of civil and military aircrafts. Although some alternatives have emerged in the last decade, such as electromechanical or electro-hydrostatic solutions, electrohydraulic systems are still considered the most effective technology in flight-critical application of new commercial aircrafts. Moreover, the vast majority of aircraft currently in service are equipped with this technology. Considering the number of actuators typically employed in a primary flight control system and the expected service life of a commercial aircraft, the development of an effective PHM system could provide significant benefits to fleet operators and aircraft maintenance. This paper presents the results of a feasibility study of such a system for electro-hydraulic actuators used in fly-by-wire primary flight control systems, considering the actuator of a wide body commercial aircraft as use case. Aim of the research is the implementation of a PHM system without the addition of dedicated sensors, solution which would allow for the application of the proposed prognostic solution on both new and existing platforms. This paper describes the methodology and the results of the feasibility study through simulation and experimental activities, which shows how the novel PHM technologies proposed for a PHM system for the EHSAs of primary flight control actuators can allow the migration from scheduled to condition-based maintenance.https://papers.phmsociety.org/index.php/ijphm/article/view/2935failure prognosticselectro-hydraulic actuatorsflight control actuators
collection DOAJ
language English
format Article
sources DOAJ
author Sylvain Autin
Andrea De Martin Giovanni Jacazio
Jérôme Socheleau
George Vachtsevanos
spellingShingle Sylvain Autin
Andrea De Martin Giovanni Jacazio
Jérôme Socheleau
George Vachtsevanos
Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
International Journal of Prognostics and Health Management
failure prognostics
electro-hydraulic actuators
flight control actuators
author_facet Sylvain Autin
Andrea De Martin Giovanni Jacazio
Jérôme Socheleau
George Vachtsevanos
author_sort Sylvain Autin
title Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
title_short Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
title_full Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
title_fullStr Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
title_full_unstemmed Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
title_sort results of a feasibility study of a prognostic system for electro-hydraulic flight control actuators
publisher The Prognostics and Health Management Society
series International Journal of Prognostics and Health Management
issn 2153-2648
2153-2648
publishDate 2021-03-01
description Electro-Hydraulic Servo-Actuators (EHSA) are currently the most used actuation technology for primary flight control systems of civil and military aircrafts. Although some alternatives have emerged in the last decade, such as electromechanical or electro-hydrostatic solutions, electrohydraulic systems are still considered the most effective technology in flight-critical application of new commercial aircrafts. Moreover, the vast majority of aircraft currently in service are equipped with this technology. Considering the number of actuators typically employed in a primary flight control system and the expected service life of a commercial aircraft, the development of an effective PHM system could provide significant benefits to fleet operators and aircraft maintenance. This paper presents the results of a feasibility study of such a system for electro-hydraulic actuators used in fly-by-wire primary flight control systems, considering the actuator of a wide body commercial aircraft as use case. Aim of the research is the implementation of a PHM system without the addition of dedicated sensors, solution which would allow for the application of the proposed prognostic solution on both new and existing platforms. This paper describes the methodology and the results of the feasibility study through simulation and experimental activities, which shows how the novel PHM technologies proposed for a PHM system for the EHSAs of primary flight control actuators can allow the migration from scheduled to condition-based maintenance.
topic failure prognostics
electro-hydraulic actuators
flight control actuators
url https://papers.phmsociety.org/index.php/ijphm/article/view/2935
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AT jeromesocheleau resultsofafeasibilitystudyofaprognosticsystemforelectrohydraulicflightcontrolactuators
AT georgevachtsevanos resultsofafeasibilitystudyofaprognosticsystemforelectrohydraulicflightcontrolactuators
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