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The Alternative Low Noise FanA 106 bladed fan with a design takeoff tip speed of 1100 ft/sec was hypothesized as reducing perceived noise because of the shift of the blade passing harmonics to frequencies beyond the perceived noise rating range. A 22 in. model of this Alternative Low Noise Fan, ALNF, was tested in the NASA Glenn 9x 15 Wind Tunnel. 'Me fan was tested with a 7 vane long chord stator assembly and a 70 vane conventional stator assembly in both hard and acoustically treated configurations. In addition a partially treated 7 vane configuration was tested wherein the acoustic material between the 7 long chord stators was made inactive. The noise data from the 106 bladed fan with 7 long chord stators in a hard configuration was shown to be around 4 EPNdB quieter than a low tip speed Allison fan at takeoff and around 5 EPNdB quieter at approach. Although the tone noise behaved as hypothesized, the majority of this noise reduction was from reduced broadband noise related to the large number of rotor blades. This 106 bladed ALNF is a research fan designed to push the technology limits and as such is probably not a practical device with present materials technology. However, a low tip speed fan with around 50 blades would be a practical device and calculations indicate that it could be 2 to 3 EPNdB quieter at takeoff and 3 to 4 EPNdB quieter at approach than the Allison fan. 7 vane data compared with 70 vane data indicated that the tone noise was controlled by rotor wake-stator interaction but that the broadband noise is probably controlled by the interaction of the rotor with incoming flows. A possible multiple pure tone noise reduction technique for a fan/acoustic treatment system was identified. The data from the fully treated configuration showed significant noise reductions over a large frequency range thereby providing a real tribute to this bulk absorber treatment design. The tone noise data with the partially treated 7 vane configuration indicated that acoustic material in the source noise generation region may be more effective than similar material outside of the generation region.
Document ID
20010018723
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dittmar, James H.
(NASA Glenn Research Center Cleveland, OH United States)
Elliott, David M.
(NASA Glenn Research Center Cleveland, OH United States)
Jeracki, Robert J.
(NASA Glenn Research Center Cleveland, OH United States)
Moore, Royce D.
(NASA Glenn Research Center Cleveland, OH United States)
Parrott, Tony L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2000
Subject Category
Acoustics
Report/Patent Number
NASA/TM-2000-209916
E-12153
NAS 1.26:209916
Report Number: NASA/TM-2000-209916
Report Number: E-12153
Report Number: NAS 1.26:209916
Funding Number(s)
PROJECT: RTOP 522-81-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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