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Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp facilityA helicopter transmission that was being considered for the Army's Utility Tactical Transport Attack System (UTTAS) was tested in the NASA Lewis 2240-kW (3000-hp) test facility to obtain the transmission's operational data. The results will form a vibration and efficiency data base for evaluation similar-class helicopter transmissions. The transmission's mechanical efficiency was determined to be 98.7 percent at its rated power level of 2080 kW (2792 hp). At power levels up to 113 percent of rated the transmission displayed 56 percent higher vibration acceleration levels on the right input than on the left input. Both vibration signature analysis and final visual inspection indicated that the right input spiral-bevel gear had poor contact patterns. The highest vibration meter level was 52 g's rms at the accessory gear, which had free-wheeling gearsets. At 113 percent power and 100 percent rated speed the vibration meter levels generally ranged from 3 to 25 g's rms.
Document ID
19860015521
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Mitchell, A. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Oswald, F. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Schuller, F. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.60:2538
E-2801
NASA-TP-2538
Report Number: NAS 1.60:2538
Report Number: E-2801
Report Number: NASA-TP-2538
Accession Number
86N24992
Funding Number(s)
PROJECT: RTOP 505-62-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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