Physics-based integrated vehicle health management system for predicting the remaining useful life of an aircraft planetary gear transmission

• Published in: International journal of structural integrity Vol. 8; no. 4; pp. 484 - 495
• Main Authors: Cubillo, Adrian, Vermeulen, Jeroen, Rodriguez de la Peña, Marcos, Collantes Casanova, Ignacio, Perinpanayagam, Suresh
• Format: Journal Article
• Language: English
• Published: Bingley Emerald Publishing Limited 01.01.2017; Emerald Group Publishing Limited
• Subjects: Aging aircraft; Aircraft; Computer simulation; Crack propagation; Decision making; Diagnostic systems; Failure analysis; Failure modes; Fatigue failure; Fault detection; Gear trains; Generators; Health; Life prediction; Maintenance management; Mechanical engineering; Metal fatigue; Monitoring systems; Neural networks; Physics; Real time; Signal processing; Fatigue; Metal-metal contact; Physics-based model; Stribeck curve; Aerospace industry; Integrated vehicle health management
• ISSN: 1757-9864; 1757-9872
• DOI: 10.1108/IJSI-01-2016-0003

Purpose Integrated vehicle health management has been developed for several years in different industries, to be able to provide the required inputs to determine the optimal maintenance operations depending on the actual health status of the system. The purpose of this paper is to demonstrate the potential of a physics-based model (PbM) for prognostics with a real case study, based on the detection of incipient faults and estimate the remaining useful life of a planetary transmission of an aircraft system. Design/methodology/approach Most of the research in the area of health assessment algorithms has been focused on data-driven approaches that are not based on the knowledge of the physics of the system, while PbM approaches rely on the understanding of the system and the degradation mechanisms. A physics-based modelling approach to represent metal-metal contact and fatigue in the gears of the planetary transmission of an aircraft system is applied. Findings Both the failure mode caused by metal-metal contact as caused by fatigue in the gears is described. Furthermore, the real-time application that retrieves the results from the simulations to assess the health of the system is described. Finally the decision making that can be executed during flight in the aircraft is incorporated. Originality/value The paper proposes an innovative prognostics health management system that assesses two important failure modes of the planetary transmission that regulates the speed of the generators of an aircraft. The results from the models have been integrated in an application that emulates a real system in the aircraft and computes the remaining useful life in real time.