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contributor authorH. W. Brown
date accessioned2017-05-08T23:07:09Z
date available2017-05-08T23:07:09Z
date copyrightNovember, 1979
date issued1979
identifier issn1087-1357
identifier otherJMSEFK-27681#421_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92364
description abstractInvolute spline couplings are commonly used in aircraft to transmit power to gearboxes, generators, pumps, and other engine driven accessories. Spline driven accessories which are cantilever mounted on an aircraft engine are of special concern to the user as these interface splines characteristically exhibit extremely poor reliability. To compound the problem, replacement of splines is difficult and costly due to their inaccessibility. Whereas the engine driven accessory may demonstrate a mean time between failures (MTBF) of 2000 hr., the spline coupling typically fails within 500 hr. Consequently, the degree of maintenance demanded by spline wear conflicts with the operational requirements of military or commercial aircraft. Failures can also compromise flight safety. This paper reviews recent spline research directed at understanding the characteristics and problems of conventional involute splines. It also discusses the design, development, and application of the circular spline coupling (MS14169) which was developed to solve spline wear problems being experienced in military aircraft.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Reliable Spline Coupling
typeJournal Paper
journal volume101
journal issue4
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3439531
journal fristpage421
journal lastpage426
identifier eissn1528-8935
keywordsSplines
keywordsAircraft
keywordsWear
keywordsEngines
keywordsFailure
keywordsGenerators
keywordsMilitary aircraft
keywordsMilitary systems
keywordsFlight
keywordsAircraft engines
keywordsReliability
keywordsMaintenance
keywordsSafety
keywordsCantilevers
keywordsCouplings
keywordsDesign AND Pumps
treeJournal of Manufacturing Science and Engineering:;1979:;volume( 101 ):;issue: 004
contenttypeFulltext


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