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A Procedure for 3-D Contact Stress Analysis of Spiral Bevel GearsContact stress distribution of spiral bevel gears using nonlinear finite element static analysis is presented. Procedures have been developed to solve the nonlinear equations that identify the gear and pinion surface coordinates based on the kinematics of the cutting process and orientate the pinion and the gear in space to mesh with each other. Contact is simulated by connecting GAP elements along the intersection of a line from each pinion point (parallel to the normal at the contact point) with the gear surface. A three dimensional model with four gear teeth and three pinion teeth is used to determine the contact stresses at two different contact positions in a spiral bevel gearset. A summary of the elliptical contact stress distribution is given. This information will be helpful to helicopter and aircraft transmission designers who need to minimize weight of the transmission and maximize reliability.
Document ID
19940028423
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kumar, A.
(Akron Univ. Akron, OH, United States)
Bibel, G.
(Akron Univ. Akron, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1994
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-194472
E-8613
NAS 1.26:194472
ARL-CR-72
Report Number: NASA-CR-194472
Report Number: E-8613
Report Number: NAS 1.26:194472
Report Number: ARL-CR-72
Accession Number
94N32929
Funding Number(s)
CONTRACT_GRANT: NAG3-1476
PROJECT: DA PROJ. 1L1-62211-A-47-A
PROJECT: RTOP 505-62-10
Distribution Limits
Public
Copyright
Public Use Permitted.
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