Identification and evaluation of the potentials of Prognostics and Health Management in future civil aircraft

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Published Jul 8, 2014
Sebastian Torhorst Nico B. Hölzel Volker Gollnick

Abstract

After the stepwise implementation of health management systems in form of diagnostic on-board maintenance sys-tems in the latest generation of aircraft (e.g. AiRTHM (Air-bus Real-Time Health Monitoring) – Airbus, AIMS (Air-plane Information Management System) – Boeing, AHEAD (Aircraft Health Analysis and Diagnosis) – Embraer) and other technical equipment such as jet engines (Engine Con-dition Monitoring – MTU, Performance Based Logistics – GE) or trains (Remote Condition Monitoring – Future Rail-way), the pressure is high for an evolution of this technolo-gy. Integrated Vehicle Health Management (IVHM) repre-sents a set of capabilities that enable sustainable and safe operation of components and subsystems within aerospace platforms. [Rajamani, 2013]. The next step in IVHM is the ability to give prognoses on the Remaining Useful Life (RUL) of a system or component and the structure of the aircraft. This approach is covered in the term “Prognostics and Health Management” (PHM). PHM in this context consists of Integrated Systems Health Management (ISHM) and Structural Health Monitoring (SHM). To put that step into practice in an industrial environment, it is inevitable to weigh up costs vs. benefits in a Cost-Benefit Analysis (CBA). This trade-off is subject of the following investiga-tion. A methodology is presented with which it is possible to evaluate PHM on aircraft level and examples are given to show its applicability. The study shows that, under the as-sumptions made, a PHM system can benefit the design and operation of future civil aircraft. The dimensioning of struc-tures can be modified, maintenance processes adjusted, system reliability, aircraft availability and safety increased. With the help of the results presented herein and further in-depth studies of the aircraft structures/systems of interest, a sufficiently well-founded evaluation of the possible costs and benefits of the implementation of this advanced ap-proach on the PHM technology can be performed.

How to Cite

Torhorst, S., Hölzel, N. B., & Gollnick, V. (2014). Identification and evaluation of the potentials of Prognostics and Health Management in future civil aircraft. PHM Society European Conference, 2(1). https://doi.org/10.36001/phme.2014.v2i1.1457
Abstract 44023 | PDF Downloads 2481

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Keywords

structural health management, Condition Based Maintenance, Integrated Vehicle Health Management, aircraft systems, Cost Benefit Analysis

References
Assler, H., Telgkamp, J. (2004), Design of aircraft struc-tures under consideration of NDT, WCNDT-World Conference of Non-Destructive Testing, Montreal, Canada, October 2004
Banks, J., Reichard, E., Crow, E., Nickell, E. (2005), How
Engineers Can Conduct Cost-Benefit Analysis for PHM
Systems, IEEE Aerospace Conference, paper #1363, 2005, 0-7803-8870-4/05
Curran, R., Raghunathan, S., Price, M. (2004), Review of aerospace engineering cost modelling: The genetic causal approach, Progress in Aerospace Sciences 40 82004) 487-534, doi: 10.1016/j.paerosci.2004.10.001
Goebel, K., Bonanni, P., Eklund, N. (2005), Towards an Integrated Reasoner for Bearings Prognostics, Pro-ceedings of 2005 IEEE Aerospace Conference, paper #1309, 2005, 0-7803-8870-4/05/
Goebel, K. (2010), Prognostics, Presentation of the NASA Prognostics Center of Excellence, NASA Ames Re-search Center, Moffett Field CA94035, April 2010
Guo, F. (2013), Fleet Performance Management - CAAC A320 Fleet Performance Seminar, Airbus China, Shen-yang, July 2013
Hölzel, N., Pape, O., Schilling, T. (2013), Internal presenta-tion on IVHM, DLR/Hamburg, September 2013
Lammering, T., Franz, K., Risse, K. et al. (2012), Aircraft Cost Model for Preliminary Design Synthesis, 50th AI-AA Aerospace Sciences Meeting, January 2012, Nash-ville, Tennessee
MacConnell, J.H. (2007), ISHM & Design: A review of the benefits of the ideal ISHM system, IEEEAC Paper #1596, 2007, 1-4244-0525-4/07
Rajamani, R., Saxena, A., Kramer, F., Augustin, M. et al. (2013), Developing IVHM Requirements for Aerospace Systems, SAE Technical Paper 2013-01-2333, 2013
Speckmann, H., Roesner, H. (2006), Structural Health Mon-itoring: A contribution to the Intelligent Aircraft Struc-ture, ECNDT-European Conference of Non-Destructive Testing, September 2006, Berlin, Germany
Speckmann, H., Henrich, R. (2008), Structural Health Mon-itoring (SHM) - Overview on technologies under devel-opment, Airbus, Bremen, Germany
Teske/Schmidt (1999), Guidelines for the damage tolerant design of aircraft structures, Handbuch Struktur Berechnung, 62200-01, Issue B
Weiss, M. (2007), Ein Vorschlag zur Berücksichtigung der Schallemission bei der Betriebskostenbewertung im Vorentwurf von Verkehrsflugzeugen und dessen An-wendung an einer neuartigen lärmarmen Konfigurati-on, Forschungsberichte aus den Ingenieurwissenschaf-ten, Verlag: Mensch & Buch; 1. Auflage, ISBN-13: 978-3866642911
Wheeler, K. R., Kurtoglu, T., Poll, S. D. (2010), A survey of Health Management user objectives in aerospace sys-tems related to Diagnostic and Prognostic metrics, In-ternational Journal of Prognostics and Health Manage-ment, ISSN 2153-2648.
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