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Advanced Rotorcraft Transmission (ART) program summaryThe Advanced Rotorcraft Transmission (ART) Program was initiated to advance the state of the art for rotorcraft transmissions. The goal of the ART Program was to develop and demonstrate the technologies needed to reduce transmission weight by 25 pct. and reduce noise by 10 dB while obtaining a 5000 hr 'mean time between failure'. The research done under the ART Program is summarized. A split path design was selected as best able to meet the program goals. Key part technologies needed for this design were identified, studied, and developed. Two of these technologies are discussed in detail: the load sharing of split path designs including the use of a compliant elastomeric torque splitter and the application of a high ratio, low pitch line velocity gear mesh. Development of an angular contact spherical roller bearing, transmission error analysis, and fretting fatigue testing are discussed. The technologies for a light weight, quiet, and reliable rotorcraft transmission were demonstrated.
Document ID
19920015741
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Krantz, T. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Kish, J. G.
(Sikorsky Aircraft Stratford, CT., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
E-7027
NASA-TM-105665
AIAA PAPER 92-3365
NAS 1.15:105665
AD-A252379
AVSCOM-TR-92-C-011
Report Number: E-7027
Report Number: NASA-TM-105665
Report Number: AIAA PAPER 92-3365
Report Number: NAS 1.15:105665
Report Number: AD-A252379
Report Number: AVSCOM-TR-92-C-011
Meeting Information
Meeting: Joint Propulsion Conference
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: SAE, ASME, AIAA, ASEE
Accession Number
92N24984
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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