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Experimental testing of prototype face gears for helicopter transmissionsAn experimental program to test the feasibility of using face gears in a high-speed and high-power environment was conducted. Four face gear sets were tested, two sets at a time, in a closed-loop test stand at pinion rotational speeds to 19,100 rpm and to 271 kW. The test gear sets were one-half scale of the helicopter design gear set. Testing the gears at one-eighth power, the test gear set had slightly increased bending and compressive stresses when compared to the full scale design. The tests were performed in the LeRC spiral bevel gear test facility. All four sets of gears successfully ran at 100 percent of design torque and speed for 30 million pinion cycles, and two sets successfully ran at 200 percent of torque for an additional 30 million pinion cycles. The results, although limited, demonstrated the feasibility of using face gears for high-speed, high-load applications.
Document ID
19920022105
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Handschuh, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Lewicki, D.
(NASA Lewis Research Center Cleveland, OH, United States)
Bossler, R.
(Lucas Western, Inc., City of Industry CA., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-105434
E-7084
AVSCOM-TR-92-C-008
AD-A257175
NAS 1.15:105434
Report Number: NASA-TM-105434
Report Number: E-7084
Report Number: AVSCOM-TR-92-C-008
Report Number: AD-A257175
Report Number: NAS 1.15:105434
Meeting Information
Meeting: Gearbox Configurations of the 1990''s
Location: Solihull
Start Date: October 28, 1992
Sponsors: Inst. of Mechanical Engineers
Accession Number
92N31349
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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