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On dynamic loads in parallel shaft transmissions. 2: Parameter studySolutions to the governing equations of a spur gear transmission model, developed in NASA TM-100180 (AVSCOM TM-87-C-2), are presented. Factors affecting the dynamic load are identified. It is found that the dynamic load increases with operating speed up to a system natural frequency. At operating speeds beyond the natural frequency the dynamic load decreases dramatically. Also. it is found that the applied load and shaft inertia have little effect on the dynamic load. Damping and friction decrease the dynamic load. Finally, tooth stiffness has a significant effect on dynamic loading; the higher the stiffness, the lower the dynamic loading. Also, the higher the stiffness the higher the rotating speed required for dynamic response.
Document ID
19880003416
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lin, Edward Hsiang-Hsi
(Memphis State Univ. TN., United States)
Huston, Ronald L.
(Cincinnati Univ. OH., United States)
Coy, John J.
(Army Aviation Research and Development Command Cleveland, Ohio., United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1987
Subject Category
Mechanical Engineering
Report/Patent Number
AD-A189109
NAS 1.15:100181
AVSCOM-TM-87-C-3
NASA-TM-100181
E-3756
Report Number: AD-A189109
Report Number: NAS 1.15:100181
Report Number: AVSCOM-TM-87-C-3
Report Number: NASA-TM-100181
Report Number: E-3756
Accession Number
88N12798
Funding Number(s)
PROJECT: RTOP 505-63-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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