Electromechanical Actuator Test Stand Coupling Design to Support Actuator Prognostic Model Development

Uncertainty assessment and management is becoming an increasingly essential aspect of good prognostic design for engineering complex systems. Uncertainty surrounding diagnostics, loads, and fault progression models is very real and propagating this uncertainty from component-level health estimates to the system-level remains difficult at best. In this work, a test stand is used to conduct real-time failure experiments aboard various aircraft platforms to collect failure response data, expanding the actuator knowledge base that forms the foundation of component health estimations. The research takes a step towards standardizing a test stand design to produce comparable and scalable failure data sets, fostering uncertainty reduction within the electromechanical actuator prognostic model. This paper specifically presents a method to optimize the actuator coupling for a commercially available actuator where a model was built to minimize the coupling deflection and estimate the coupling life. Using this model, researchers can rapidly develop their own electromechanical actuator test stands.Copyright © 2011 by ASME

[1]  Sankalita Saha,et al.  Evaluating prognostics performance for algorithms incorporating uncertainty estimates , 2010, 2010 IEEE Aerospace Conference.

[2]  Richard C. Millar,et al.  Defining requirements for advanced PHM technologies for optimal reliability centered maintenance , 2009, 2009 IEEE Aerospace conference.

[3]  K. Goebel,et al.  Real-time Probabilistic Forecasting of Wear Degradation using a Macro-scale Physical Model , 2008, 2008 IEEE Aerospace Conference.

[4]  Abhinav Saxena,et al.  A diagnostic approach for electro-mechanical actuators in aerospace systems , 2009, 2009 IEEE Aerospace conference.

[5]  Pradeep Shetty,et al.  A Hybrid Prognostic Model Formulation and Health Estimation of Auxiliary Power Units , 2008 .

[6]  Delbert Tesar,et al.  Intelligent Electromechanical Actuators to Modernize Ship Operations , 2008 .

[7]  Abhinav Saxena,et al.  Airborne Electro-Mechanical Actuator Test Stand for Development of Prognostic Health Management Systems , 2010 .

[8]  K. Goebel,et al.  Standardizing research methods for prognostics , 2008, 2008 International Conference on Prognostics and Health Management.

[9]  Irem Y. Tumer,et al.  Reliability Based Design Recommendations for an Electromechanical Actuator Test Stand , 2010 .

[10]  Frank L. Lewis,et al.  Intelligent Fault Diagnosis and Prognosis for Engineering Systems , 2006 .

[11]  Bhaskar Saha,et al.  Prognostics Methods for Battery Health Monitoring Using a Bayesian Framework , 2009, IEEE Transactions on Instrumentation and Measurement.

[12]  Ellen Ullman The Bug , 2003 .

[13]  S. C. Jensen,et al.  Flight test experience with an electromechanical actuator on the F-18 Systems Research Aircraft , 2000, 19th DASC. 19th Digital Avionics Systems Conference. Proceedings (Cat. No.00CH37126).

[14]  Irem Y. Tumer,et al.  An Analysis of Maneuvering Effects on Transmission Vibrations in an AH-1 Cobra Helicopter , 2002 .

[15]  E.R. Brown,et al.  Prognostics and Health Management A Data-Driven Approach to Supporting the F-35 Lightning II , 2007, 2007 IEEE Aerospace Conference.

[16]  George Vachtsevanos,et al.  Filtering and prediction techniques for model-based prognosis and uncertainty management , 2010, 2010 Prognostics and System Health Management Conference.

[17]  B. Saha,et al.  Uncertainty Management for Diagnostics and Prognostics of Batteries using Bayesian Techniques , 2008, 2008 IEEE Aerospace Conference.

[18]  Kls Bernhardt,et al.  Quantifying Uncertainty in Bridge Condition Assessment Data , 2000 .

[19]  David Draper,et al.  Assessment and Propagation of Model Uncertainty , 2011 .

[20]  George Vachtsevanos,et al.  Methodologies for uncertainty management in prognostics , 2009, 2009 IEEE Aerospace conference.

[21]  D.S. Bodden,et al.  Seeded Failure Testing and Analysis of an Electro-Mechanical Actuator , 2007, 2007 IEEE Aerospace Conference.

[22]  Carl S. Byington,et al.  Experimental Data Collection and Modeling for Nominal and Fault Conditions on Electro-Mechanical Actuators , 2009 .

[23]  Irem Y. Tumer,et al.  Function-Based Analysis and Redesign of a Flyable Electromechanical Actuator Test Stand , 2010 .