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Crack Detection for Aerospace Quality Spur GearsHealth and Usage Monitoring System research and development involves analysis of the vibration signals produced by a gearbox throughout its life. There are two major advantages of knowing the actual lifetime of a gearbox component: safety and cost. In this report, a technique is proposed to help extract the critical data and present it in a manner that can be easy to understand. The key feature of the technique is to make it independent of speed, torque and prior history for localized, single tooth damage such as gear cracks. This extraction technique is demonstrated on two sets of digitized vibration data from cracked spur gears. Standard vibration diagnostic parameters are calculated and presented for comparison. Several new detection algorithms are also presented. The results of this study indicate that crack detection methods examined are not robust or repeatable. The proposed techniques provide a limited improvement to existing diagnostic parameters. Current techniques show that the cracks progressed at a much faster rate than anticipated which reduced available time for detection.
Document ID
20020061785
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Decker, Harry J.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
August 29, 2013
Publication Date
April 1, 2002
Subject Category
Mechanical Engineering
Report/Patent Number
NASA/TM-2002-211492
NAS 1.15:211492
ARL-TR-2682
E-13260
Report Number: NASA/TM-2002-211492
Report Number: NAS 1.15:211492
Report Number: ARL-TR-2682
Report Number: E-13260
Meeting Information
Meeting: International 58th Annual Forum and Technology Display
Location: Montreal, Quebec
Country: Canada
Start Date: June 11, 2002
End Date: June 13, 2002
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
PROJECT: DA Proj. 1L1-61102-AH-45
PROJECT: RTOP 708-90-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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