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Adaptable System for Vehicle Health and Usage MonitoringAircraft and other vehicles are often kept in service beyond their original design lives. As they age, they become susceptible to system malfunctions and fatigue. Unlike future aircraft that will include health-monitoring capabilities as integral parts in their designs, older aircraft have not been so equipped. The Adaptable Vehicle Health and Usage Monitoring System is designed to be retrofitted into a preexisting fleet of military and commercial aircraft, ships, or ground vehicles to provide them with state-of-the-art health- and usage-monitoring capabilities. The monitoring system is self-contained, and the integration of it into existing systems entails limited intrusion. In essence, it has bolt-on/ bolt-off simplicity that makes it easy to install on any preexisting vehicle or structure. Because the system is completely independent of the vehicle, it can be certified for airworthiness as an independent system. The purpose served by the health-monitoring system is to reduce vehicle operating costs and to increase safety and reliability. The monitoring system is a means to identify damage to, or deterioration of, vehicle subsystems, before such damage or deterioration becomes costly and/or disastrous. Frequent monitoring of a vehicle enables identification of the embryonic stages of damage or deterioration. The knowledge thus gained can be used to correct anomalies while they are still somewhat minor. Maintenance can be performed as needed, instead of having the need for maintenance identified during cyclic inspections that take vehicles off duty even when there are no maintenance problems. Measurements and analyses acquired by the health-monitoring system also can be used to analyze mishaps. Overall, vehicles can be made more reliable and kept on duty for longer times. Figure 1 schematically depicts the system as applied to a fleet of n vehicles. The system has three operational levels. All communication between system components is by use of wireless transceivers operating at frequencies near 433 MHz. Electromagnetic-interference tests have demonstrated that the radio-frequency emissions from the transceivers do not influence civilian aircraft communication and navigation systems.
Document ID
20110014934
Acquisition Source
Langley Research Center
Document Type
Other - NASA Tech Brief
Authors
Woodart, Stanley E.
(NASA Langley Research Center Hampton, VA, United States)
Woodman, Keith L.
(NASA Langley Research Center Hampton, VA, United States)
Coffey, Neil C.
(NASA Langley Research Center Hampton, VA, United States)
Taylor, Bryant D.
(Swales Aerospace Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
June 1, 2005
Publication Information
Publication: NASA Tech Briefs, June 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LAR-16516
Distribution Limits
Public
Copyright
Public Use Permitted.
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