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Maximum life spiral bevel reduction designOptimization is applied to the design of a spiral bevel gear reduction for maximum life at a given size. A modified feasible directions search algorithm permits a wide variety of inequality constraints and exact design requirements to be met with low sensitivity to initial values. Gear tooth bending strength and minimum contact ratio under load are included in the active constraints. The optimal design of the spiral bevel gear reduction includes the selection of bearing and shaft proportions in addition to gear mesh parameters. System life is maximized subject to a fixed back-cone distance of the spiral bevel gear set for a specified speed ratio, shaft angle, input torque, and power. Significant parameters in the design are: the spiral angle, the pressure angle, the numbers of teeth on the pinion and gear, and the location and size of the four support bearings. Interpolated polynomials expand the discrete bearing properties and proportions into continuous variables for gradient optimization. After finding the continuous optimum, a designer can analyze near optimal designs for comparison and selection. Design examples show the influence of the bearing lives on the gear parameters in the optimal configurations. For a fixed back-cone distance, optimal designs with larger shaft angles have larger service lives.
Document ID
19930001794
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Savage, M.
(Akron Univ. OH., United States)
Prasanna, M. G.
(Akron Univ. OH., United States)
Coe, H. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-105790
NAS 1.15:105790
E-7220
AD-A259242
AVSCOM-TR-92-C-004
Report Number: NASA-TM-105790
Report Number: NAS 1.15:105790
Report Number: E-7220
Report Number: AD-A259242
Report Number: AVSCOM-TR-92-C-004
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Huntsville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: ASME, ASEE, SAE, AIAA
Accession Number
93N10982
Funding Number(s)
PROJECT: DA PROJ. 1L1-62211-A-47-A
PROJECT: RTOP 505-63-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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