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Thermal analysis of a planetary transmission with spherical roller bearings operating after complete loss of oilPlanetsys and Spherbean, two computer programs developed for the analysis of rolling element bearings, were used to simulate the thermal performance of an OH-58 helicopter main rotor transmission. A steady state and a transient thermal analysis were made and temperatures thus calculated were compared with experimental data obtained from a transmission that was operated to destruction, which occurred about 30 min after all the oil was drained from the transmission. Temperatures predicted by Spherbean were within 3% of the corresponding measured values at 15 min elapsed time and within 9% at 25 min. Spherbean also indicates a potential for high bearing cage temperatures with misalignment and outer ring rotation.
Document ID
19840024753
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Coe, H. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
E-2008
NAS 1.60:2367
NASA-TP-2367
Report Number: E-2008
Report Number: NAS 1.60:2367
Report Number: NASA-TP-2367
Accession Number
84N32824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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