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
19920066314
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Krantz, T. L. (U.S. Army, Propulsion Directorate; NASA, Lewis Research Center Cleveland, OH, United States)
Kish, J. G. (Sikorsky Aircraft Stratford, CT, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 92-3365Report Number: AIAA PAPER 92-3365