Tools for Prognostics and Health-Monitoring of Aircraft Power Systems

Posted by on Oct 22, 2009 in Distributed Heterogeneous Simulation, Eric A. Walters, Generator, Prognostics and Health Management, Publications, Tommy Baudendistel | 0 comments

T. Baudendistel, PC Krause and Associates, Inc; Steve Pekarek, Mario Rotea, Purdue University; E. A. Walters, PC Krause and Associates, Inc; Steve Peecher, Smiths Aerospace; Sean A. Field, Nathan E. Kumbar, Naval Air Systems Command In this presentation, a cadre of recently developed hardware and software tools for the prognostics and health-monitoring of electric generators, motors, power electronic components, and electric power systems will be presented. One of the tools is a vibration sensor that is low cost, durable, and relatively straightforward to implement in a drive system or power electronic module. This sensor has been used to detect torque-ripple-induced vibration created by electric machines. It provides a convenient means to detect faults of both electrical and mechanical components of electric drive systems and also facilitates feedback-based control to mitigate the vibration source through control of the excitation to a machine. In addition to providing vibration feedback, it has also been shown to be effective as a back-up position sensor. Specifically, in applications where fault tolerance is critical, the sensor has been used to determine the position of the rotor of the machine when in-line or Hall-effect sensors fail. A second tool is a thermal-based health monitor for electric machines that effectively predicts the thermal behavior of stator, rotor, and winding structures based upon input from a minimal number of thermocouples and stator current sensors. This observer has been tested on a 3.7 kW generator and is presently being used to evaluate the short- and long-term effects of pulsed loading of electric machines. A third tool is a method of Distributed Heterogeneous Simulation (DHS) that provides a means to simulate the healthy and faulted behavior of large-scale systems at a speed and level of detail heretofore unachievable. Specifically, DHS enables the synchronized interconnection of any number of dynamic subsystem simulations, developed using any combination of a variety of programs/languages, and implemented on a single computer/workstation/supercomputer, a local area network (Intranet), a distributed, and any combination thereof. Theoretically, using an M-computer network, DHS can approach an 3M gain in computational speed over single computer, single numerical algorithm implementation. It is shown that through coupling of these three tools, a comprehensive prognostic and health management system (PHM) for aircraft generators and associated electrical systems can be developed. Specifically, using DHS, component and system-level simulations of aircraft generator systems under nominal and failure modes can be performed efficiently. Using the simulation results obtained, the vibration sensor and thermal-condition monitor concepts are coupled to establish a multi-physics approach that can effectively detect component degradation and predict time-to-failure, and to develop feedback-based strategies for operation of generator electrical systems under component degradation or failure. Hence, maintaining the warfighting capabilities by extending the life of the generator electrical system. 2007 ISHM Conference, August 2007. Contact information:...

Read More

Noninvasive Approach to Health Management of Aircraft Power Systems Using Torque Ripple

Posted by on Oct 22, 2009 in Aircraft, Distributed Heterogeneous Optimization, Eric A. Walters, Prognostics and Health Management, Publications, Tommy Baudendistel | 0 comments

T. Baudendistel, PC Krause and Associates, inc;  S. Pekarek, Purdue University;  Steve Peecher, GE Aerospace; Sean Field, Nathan Kumbar, Naval Air Systems Command; E. A. Walters, PC Krause and Associates, inc. In this presentation, a recently developed hardware and software tool for the health management of electric generators, motors, power electronic components, and electric power systems will be presented. This tool enables higher fidelity health management prognostics. The hardware component of this tool is a vibration sensor that is low cost, durable, and relatively straightforward to implement in a drive system or power electronic module. The sensor has been used to detect torque-ripple-induced vibration created by electric machines. It provides a convenient means to detect faults of both electrical and mechanical components of electric drive systems and also facilitates feedback-based control to mitigate the vibration source through control of the excitation to a machine. The first software tool analyzes the raw data acquired by the vibration sensor.  This software utilizes both signal processing and statistical algorithms to reduce the acquired data into a user friendly pareto chart format.  This format allows vehicle level PHM systems to cost-effectively analyze and store pertinent data relating to the health of the power system.  This format also allows ground maintenance teams to quickly assess the health changes between flights without adding to “information overload”. The second software tool is a method of Distributed Heterogeneous Simulation (DHS) that provides a means to simulate the healthy and faulted behavior of large-scale systems at a speed and level of detail heretofore unachievable. Specifically, DHS enables the synchronized interconnection of any number of dynamic subsystem simulations, developed using any combination of a variety of programs/languages, and implemented on a single computer/workstation/supercomputer, a local area network (Intranet), a distributed, and any combination thereof. Theoretically, using an -computer network, DHS can approach an  gain in computational speed over single computer, single numerical algorithm implementation. It is shown that through coupling of these tools, a comprehensive prognostics and health management system (PHM) for aircraft generators and associated electrical systems can be developed. Specifically, using DHS, component and system-level simulations of aircraft generator systems under nominal and failure modes can be performed efficiently. Using the simulation results obtained, the vibration sensor, unique monitoring concepts and advanced signal conditioning are coupled to establish an approach that can effectively detect component degradation and predict time-to-failure, and to develop feedback-based strategies for operation of generator electrical systems under component degradation or failure. Hence, maintaining the war fighting capabilities by extending the life of the aircraft electrical systems. Contact information:...

Read More

Simulation of a Zonal Electric Distribution System for Shipboard Applications

Posted by on Oct 22, 2009 in Automated State Model Generator, Eric A. Walters, Naval, Oleg Wasynczuk, Power Systems, Publications | 0 comments

O. Wasynczuk, E. A. Walters, PC Krause and Associates, Inc; H. J. Hegner, Naval Surface Warfare Center A new approach of automatically generating state-space models of power circuits and systems is presented. In this approach, the composite system state equations are established algorithmically given the standard node incidence matrix and elementary branch data (e.g. resistances, inductances, back emf’s). The resulting state equations can be solved using a variety of numerical techniques or commercially available computer simulation programs. An example system consisting of a three-phase generator and rectifier load is used to illustrate this approach. Experimental verification is also provided. Proceedings 32nd Intersociety Energy Conversion Engineering Conference, vol. 1, July 1997, pp....

Read More

An Automated State Model Generation Algorithm for Simulation/Analysis of Power Systems with Power Electronic Components

Posted by on Oct 21, 2009 in Aircraft, Automated State Model Generator, Electronics, Eric A. Walters, Generator, Oleg Wasynczuk, Power Systems, Publications | 0 comments

S. D. Pekarek, E. A. Walters, T. L. Skvarenina, O. Wasynczuk, PC Krause and Associates, Inc. In this paper, a recently developed algorithmic method of deriving the state equations of power systems containing power electronic components is described. Therein the system is described by the pertinent branch parameters and the circuit topology; however, unlike circuit-based algorithms, the difference equations are not implemented at the branch level. Instead, the composite system state equations are established. A demonstration of the computer implementation of this algorithm to model a variable-speed, constant-frequency aircraft generation system is described. Because of the large number of states and complexity of the system, particular attention is placed on the development of a model structure which provides optimal simulation efficiency. SAE Transactions Journal of Aerospace, sec. 1, vol. 107, Month 1998, pp....

Read More

Continuous State-Space Modeling of Switched Electric Networks

Posted by on Oct 21, 2009 in Automated State Model Generator, Charles Eric Lucas, Electronics, Eric A. Walters, Oleg Wasynczuk, Power Systems, Publications | 0 comments

J. Jatskevich, O. Wasynczuk, E. A. Walters, C. E. Lucas, PC Krause and Associates, Inc. An Automated State Model Generator (ASMG) is a tool for modeling and analysis of lumped-parameter power-electronic-based systems. In this modeling approach, the minimal state-space representation of the overall system is generated automatically and updated dynamically based upon the topological state of the system. However, due to the changing topology, simulation of a switched circuit using the ASMG requires the concatenation of solutions to the initial value problems (IVPs) corresponding to the time intervals between commutations. In this paper, a transformation of state variables is derived such that the states are continuous throughout the simulation process. This feature eliminates the need to re-initialize the ODE solver. The continuous state algorithm is verified on a high-pulse-count power supply and sets the stage for state-space averaging and system-level analysis of switched circuits. Proceedings IEEE International Conference on Control Applications, vol. 1, September 2000, pp....

Read More

A Distributed Heterogeneous Simulation of a Representative Aircraft Power System

Posted by on Oct 21, 2009 in Aircraft, Charles Eric Lucas, Distributed Heterogeneous Simulation, Eric A. Walters, Oleg Wasynczuk, Power Systems, Publications | 0 comments

C. E. Lucas, E. A. Walters, J. Jatskevich, O. Wasynczuk, PC Krause and Associates, Inc; P. T. Lamm, U.S. Air Force Research Laboratory In this paper, a new technique useful for the numerical simulation of large-scale systems is presented. This approach enables the overall system simulation to be formed by the dynamic interconnection of the various interdependent simulations, each representing a specific component or subsystem such as electrical, mechanical, hydraulic, or thermal. Each simulation may be developed separately using possibly different commercial-off-the shelf simulation programs thereby allowing the most suitable language or tool to be used based on the design/analysis needs. For the purpose of demonstration, this technique is applied to a detailed simulation of a representative aircraft power system. This system is comprised of ten component models each developed using MATLAB/SimulinkTM, EASY5TM, or ACSLTM. When the ten component simulations were distributed across just four personal computers (PCs), a greater than 15-fold improvement in simulation speed (compared to the single-computer implementation) was achieved. 2002 SAE Power Systems Conference, October 29-31, 2002, Coral Spring, FL. Paper...

Read More