Scott A. Billington
Georgia Institute of Technology
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Tribology Transactions | 1999
Yawei Li; Scott A. Billington; Cheng Zhang; Thomas R. Kurfess; Steven Danyluk; Steven Y. Liang
Rolling element bearing failure is a major factor in the failure of rotating machinery. Current methods of bearing condition monitoring focus on determining any existing fault presence on a bearing as early as possible. Although a defect can be detected when it is well below the industry standard of a fatal size of 6.25 mm2 (0.01 in2), the remaining life of a bearing (the time it takes to reach the final failure size) from the point where a defect can be detected can vary substantially. As a fatal defect is detected, it is common to shut down machinery as soon as possible to avoid catastrophic consequences. Performing such an action, which usually occurs at inconvenient times, typically results in substantial time and economics losses. It is, therefore, important that the bearings remaining life be more precisely forecasted, in a prognostic rather than diagnostic manner, so that maintenance can be optimally scheduled. Unfortunately, current bearing remaining life prediction methods have not been well dev...
Archive | 2006
Thomas R. Kurfess; Scott A. Billington; Steven Y. Liang
Bearing failure is one of the foremost causes of breakdown in rotating machine, resulting in costly systems downtime. This chapter presents an overview of current state-of-the-art monitoring approaches for rolling element bearings. Issues related to sensors, signal processing as well as diagnostics and prognostics are discussed. This chapter also presents a brief discussion related to the typical failure modes of bearings. Such failures are more and more common on advanced, high speed, ultra precision production systems as higher spindle speeds are employed for increased accuracy, productivity and machining satiability. Models for rolling element bearing behavior are presented as well as mechanistic models for damage propagation. Examples are also presented from test systems to demonstrate the various approaches discussed in this chapter.
Volume 3: Controls, Diagnostics and Instrumentation; Education; Electric Power; Microturbines and Small Turbomachinery; Solar Brayton and Rankine Cycle | 2011
Michaël A. Hafner; Thomas Holst; Scott A. Billington
A microwave tip clearance sensor capable of measuring the hottest stages of industrial and aero gas turbines has been developed. This new microwave sensor has been integrated into a commercial package for online real-time monitoring of machine data. However, data analysis of large numbers of tip clearance probes makes standard industry graphic techniques cluttered. A method has been developed to reduce this data and visualize it in order to provide intuitive representations of the data from which a user can quickly draw the right conclusions about machine behavior. The main motivation for the development of a 3D graphical user interface is the density of information that can be shown to the user at one time. Tip clearance measurement is very data-rich, as every individual blade for each sensor mounted around the engine case is available. The result is that it may be difficult to find slight changes within hundreds of clearance trends. Only specialists with long experience in tip clearance measurement can synthesize all the data quickly enough using standard 2D plots. The 3D graphical user interface brings all of this data together to calculate the aggregated blade pattern, rotor positioning, and estimated case shape. All of these measurements are available to the user in a single visualization. Colors indicating alarm or clearance scale quickly draw attention to the most important data such as the minimum clearance point around the engine case where a rub may be likely to occur. This method is based about a case shape fitting algorithm that combines data from multiple sensors to make a case shape estimate based on fitting of a non-uniform rational B-spline (NURB). The scaling is also distorted in order to accentuate the graphics in a way that provides an intuitive understanding of the machine state. The method of applying this data accentuation is important so as to not be misleading. This innovative navigation interface presented in this paper capitalizes on modern advances in computer graphics to aid engineers and operators in understanding, access, monitoring, and analysis of tip clearance and air-gap measurements.© 2011 ASME
Mechanical Systems and Signal Processing | 1999
Yawei Li; Scott A. Billington; Cheng Zhang; Thomas R. Kurfess; Steven Danyluk; Steven Y. Liang
Mechanical Systems and Signal Processing | 2001
T. Williams; X. Ribadeneira; Scott A. Billington; Thomas R. Kurfess
Archive | 2006
Jonathan L. Geisheimer; Scott A. Billington; David W. Burgess; Glenn Hopkins
Archive | 2007
Scott A. Billington; Jonathan L. Geisheimer; Thomas Holst
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit | 2005
Thomas Holst; Thomas R. Kurfess; Scott A. Billington; Jonathan L. Geisheimer
Procedia Engineering | 2014
Steven Y. Liang; Yawei Li; Scott A. Billington; Chen Zhang; Jason Shiroishi; Thomas R. Kurfess; Steve Danyluk
Archive | 2007
Scott A. Billington; Jonathan L. Geisheimer; Phillip Moore