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Integrating Condition Indicators and Usage Parameters for Improved Spiral Bevel Gear Health MonitoringThe objective of this study was to illustrate the importance of combining Health Usage Monitoring Systems (HUMS) data with usage monitoring system data when detecting rotorcraft transmission health. Six gear sets were tested in the NASA Glenn Spiral Bevel Gear Fatigue Rig. Damage was initiated and progressed on the gear and pinion teeth. Damage progression was measured by debris generation and documented with inspection photos at varying torque values. A contact fatigue analysis was applied to the gear design indicating the effect temperature, load and reliability had on gear life. Results of this study illustrated the benefits of combining HUMS data and actual usage data to indicate progression of damage for spiral bevel gears.
Document ID
20130013528
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Dempsey, Paula J.
(NASA Glenn Research Center Cleveland, OH, United States)
Handschuh, Robert F.
(NASA Glenn Research Center Cleveland, OH, United States)
Delgado, Irebert R.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 27, 2013
Publication Date
May 21, 2013
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18665
Meeting Information
Meeting: American Helicopter Society 69th Annual Forum
Location: Phoenix, AZ
Country: United States
Start Date: May 21, 2013
End Date: May 23, 2013
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 380046.02.03.02.02.03
Distribution Limits
Public
Copyright
Other

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