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Testing of UH-60A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facilityThe U.S. Army's UH-60A Black Hawk 2240-kW (3000-hp) class, twin-engine helicopter transmission was tested at the NASA Lewis Research Center. The vibration and efficiency test results will be used to enhance the data base for similar-class helicopters. Most of the data were obtained for a matrix of test conditions of 50 to 100 percent of rated rotor speed and 20 to 100 percent of rated input power. The transmission's mechanical efficiency at 100 percent of rated power was 97.3 and 97.5 percent with its inlet oil maintained at 355 and 372 K (180 and 210 F), respectively. The highest vibration reading was 72 g's rms at the upper housing side wall. Other vibration levels measured near the gear meshes are reported.
Document ID
19870000958
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)
Coe, H. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
E-2941
NASA-TP-2626
NAS 1.60:2626
Report Number: E-2941
Report Number: NASA-TP-2626
Report Number: NAS 1.60:2626
Accession Number
87N10391
Funding Number(s)
PROJECT: RTOP 505-62-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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