Evaluation of carburized and ground face gears

Citation
Dg. Lewicki et al., Evaluation of carburized and ground face gears, J AMER HELI, 45(2), 2000, pp. 118-124
Citations number
17
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY
ISSN journal
00028711 → ACNP
Volume
45
Issue
2
Year of publication
2000
Pages
118 - 124
Database
ISI
SICI code
0002-8711(200004)45:2<118:EOCAGF>2.0.ZU;2-C
Abstract
Experimental durability tests were performed on carburized and ground AISI 9310 steel face gears. The tests were in support of a Defense Advanced Rese arch Projects Agency (DARPA) Technology Reinvestment Program (TRP) to enhan ce face-gear technology. The tests were conducted in the NASA Glenn spiral- bevel-gear/face-gear test facility, Tests were run at 2300 rpm face gear sp eed and at loads of 64, 76, 88, 100, and 112-percent of the design torque o f 377 N-m (3340 in.-lb.). The carburized and ground face gears demonstrated the required durability when run for ten-million cycles at each of the app lied loads. proper installation was critical for the successful operation o f the spur pinions and face gears. A large amount of backlash produced toot h contact patterns that approached the inner-diameter edge of the fate-gear tooth. Low backlash produced tooth contact patterns that approached the ou ter-diameter edge of the face-gear tooth. Measured backlashes in the range of 0.178 to 0.254 mm (0.007 to 0.010 in.) produced acceptable tooth contact patterns.