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Lubrication System Failure Baseline Testing on an Aerospace Quality Gear MeshAerospace drive systems are required to survive a loss-of-lubrication test for qualification. In many cases emergency lubrication systems need to be designed and utilized to permit the drive system to pass this difficult requirement. The weight of emergency systems can adversely affect the mission capabilities of the aircraft. The possibility to reduce the emergency system weight through the use of mist lubrication will be described. Mist lubrication involves the delivery of a minute amount of an organic liquid as a vapor or fine mist in flowing compressed air to rubbing surfaces. At the rubbing surface, the vapor or mist reacts to form a solid lubricating film. The aim of this study was to establish a baseline for gear behavior under oil depleted conditions. A reactive vapor-mist lubrication method is described and proposed as a candidate emergency lubrication system.
Document ID
20000053474
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Handschuh, Robert F.
(Army Research Lab. Cleveland, OH United States)
Morales, Wilfredo
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2000
Subject Category
Mechanical Engineering
Report/Patent Number
ARL-TR-2214
NASA/TM-2000-209954
NAS 1.15:209954
E-12211
Report Number: ARL-TR-2214
Report Number: NASA/TM-2000-209954
Report Number: NAS 1.15:209954
Report Number: E-12211
Meeting Information
Meeting: Computers and Information in Engineering
Location: Baltimore, MD
Country: United States
Start Date: September 10, 2000
End Date: September 13, 2000
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
PROJECT: DA Proj. 1L1-62211-A-47-A
PROJECT: RTOP 581-30-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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