Experimental and Analytical Study of Aerospace Spiral Bevel Gear Tooth Fillet Stresses

[+] Author and Article Information
R. F. Handschuh

Army Research Laboratory, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, Ohio 44135

G. D. Bibel

University of North Dakota, Department of Mechanical Engineering, Grand Forks, North Dakota 58202-8359

J. Mech. Des 121(4), 565-572 (Dec 01, 1999) (8 pages) doi:10.1115/1.2829500 History: Received March 01, 1999; Revised July 01, 1999; Online December 11, 2007


An aerospace-quality spiral bevel gearset was analytically and experimentally rolled through mesh to investigate tooth bending stress. A nonlinear finite element model utilized multiple teeth from the pinion and gear to simulate three-dimensional multitooth contact. The results were compared to those obtained experimentally with strain gages. A total of five strain gages, mounted in the root/fillet region of three teeth, were used. Effects of changing speed and load were measured. Tests were conducted from static (slow roll) to 14,400 rpm at power levels up to 537 kW (720 hp).

Copyright © 1999 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.






Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In