DocumentCode
1428195
Title
The “Intelligent” Valve: A Diagnostic Framework for Integrated System-Health Management of a Rocket-Engine Test Stand
Author
Russell, Michael J. ; Lecakes, George D., Jr. ; Mandayam, Shreekanth ; Jensen, Scott
Author_Institution
Electr. & Comput. Eng. Dept., Rowan Univ., Glassboro, NJ, USA
Volume
60
Issue
4
fYear
2011
fDate
4/1/2011 12:00:00 AM
Firstpage
1489
Lastpage
1497
Abstract
Valves play a critical role in rocket-engine test stands because they are essential for the cryogen transport mechanisms that are vital to test operations. Sensors that are placed on valves monitor the pressure, temperature, flow rate, valve position, and any other features that are required for diagnosing their functionality. Integrated system-health management (ISHM) algorithms have been used to identify and evaluate anomalous operating conditions of systems and subsystems (e.g., valves and valve components) on complex structures, such as rocket test stands. In order for such algorithms to be useful, there is a need to develop realistic models for the most common and problem-prone elements. Furthermore, the user needs to be provided with efficient tools to explore the nature of the anomaly and its possible effects on the element, as well as its relationship to the overall system state. This paper presents the development of an intelligent-valve framework that is capable of tracking and visualizing events of the large linear actuator valve (LLAV) in order to detect anomalous conditions. The framework employs a combination of technologies, including a dynamic data exchange data-transfer protocol, autoassociative neural networks, empirical and physical models, and virtual-reality environments. The diagnostic procedure that is developed has the ability to be integrated into existing ISHM systems and can be used for assessing the integrity of rocket-engine test-stand components.
Keywords
aerospace computing; aerospace engineering; aerospace testing; computerised monitoring; condition monitoring; fault diagnosis; neural nets; protocols; rocket engines; valves; virtual reality; anomalous operating condition detection; autoassociative neural networks; cryogen transport mechanism; diagnostic framework; dynamic data exchange data-transfer protocol; empirical model; integrated system-health management algorithm; intelligent valve monitoring system; large linear actuator valve; physical model; rocket-engine test stand; virtual-reality environment; Automated test and diagnostic systems; human–computer interface; virtual measurement systems;
fLanguage
English
Journal_Title
Instrumentation and Measurement, IEEE Transactions on
Publisher
ieee
ISSN
0018-9456
Type
jour
DOI
10.1109/TIM.2010.2101350
Filename
5688453
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