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Sikorsky Aircraft Advanced Rotorcraft Transmission (ART) programThe objectives of the Advanced Rotorcraft Transmission program were to achieve a 25 percent weight reduction, a 10 dB noise reduction, and a 5,000 hour mean time between removals (MTBR). A three engine Army Cargo Aircraft (ACA) of 85,000 pounds gross weight was used as the baseline. Preliminary designs were conducted of split path and split torque transmissions to evaluate weight, reliability, and noise. A split path gearbox was determined to be 23 percent lighter, greater than 10 dB quieter, and almost four times more reliable than the baseline two stage planetary design. Detail design studies were conducted of the chosen split path configuration, and drawings were produced of a 1/2 size gearbox consisting of a single engine path of the split path section. Fabrication and testing was then conducted on the 1/2 size gearbox. The 1/2 size gearbox testing proved that the concept of the split path gearbox with high reduction ratio double helical output gear was sound. The improvements were attributed to extensive use of composites, spring clutches, advanced high hot hardness gear steels, the split path configuration itself, high reduction ratio, double helical gearing on the output stage, elastomeric load sharing devices, and elimination of accessory drives.
Document ID
19930018079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kish, Jules G.
(United Technologies Corp. Stratford, CT, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
ARL-CR-49
AD-A266406
NASA-CR-191079
NAS 1.26:191079
Report Number: ARL-CR-49
Report Number: AD-A266406
Report Number: NASA-CR-191079
Report Number: NAS 1.26:191079
Accession Number
93N27268
Funding Number(s)
CONTRACT_GRANT: NAS3-25423
PROJECT: RTOP 505-62-10
PROJECT: DA PROJ. 1L1-62211-A-47-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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