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Bell Helicopter Advanced Rotocraft Transmission (ART) programFuture rotorcraft transmissions require key emerging material and component technologies using advanced and innovative design practices in order to meet the requirements for a reduced weight to power ratio, a decreased noise level, and a substantially increased reliability. The specific goals for the future rotorcraft transmission when compared with a current state-of-the-art transmission (SOAT) are: (1) a 25 percent weight reduction; (2) a 10 dB reduction in the transmitted noise level; and (3) a system reliability of 5000 hours mean-time-between-removal (MTBR) for the transmission. This report summarizes the work conducted by Bell Helicopter Textron, Inc. to achieve these goals under the Advanced Rotorcraft Transmission (ART) program from 1988 to 1995. The reference aircraft selected by BHTI for the ART program was the Tactical Tiltrotor which is a 17,000 lb gross weight aircraft. A tradeoff study was conducted comparing the ART with a Selected SOAT. The results showed the ART to be 29 percent lighter and up to 13 dB quieter with a calculated MTBR in excess of 5000 hours. The results of the following high risk component and material tests are also presented: (1) sequential meshing high contact ratio planetary with cantilevered support posts; (2) thin dense chrome plated M50 NiL double row spherical roller planetary bearings; (3) reduced kinematic error and increased bending strength spiral bevel gears; (4) high temperature WE43 magnesium housing evaluation and coupon corrosion tests; (5) flexure fatigue tests of precision forged coupons simulating precision forged gear teeth; and (6) flexure fatigue tests of plasma carburized coupons simulating plasma carburized gear teeth.
Document ID
19950023117
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Henry, Zachary S.
(Textron Bell Helicopter Fort Worth, TX, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1995
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-195479
E-9708
ARL-CR-238
NAS 1.26:195479
Report Number: NASA-CR-195479
Report Number: E-9708
Report Number: ARL-CR-238
Report Number: NAS 1.26:195479
Accession Number
95N29538
Funding Number(s)
CONTRACT_GRANT: NAS3-25455
PROJECT: DA PROJ. 1L1-6221-A-47-A
PROJECT: RTOP 505-62-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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