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Psychoacoustic Testing of Modulated Blade Spacing for Main RotorsPsychoacoustic testing of simulated helicopter main rotor noise is described, and the subjective results are presented. The objective of these tests was to evaluate the potential acoustic benefits of main rotors with modulated (uneven) blade spacing. Sound simulations were prepared for six main rotor configurations. A baseline 4-blade main rotor with regular blade spacing was based on the Bell Model 427 helicopter. A 5-blade main rotor with regular spacing was designed to approximate the performance of the 427, but at reduced tipspeed. Four modulated rotors - one with "optimum" spacing and three alternate configurations - were derived from the 5 bladed regular spacing rotor. The sounds were played to 2 subjects at a time, with care being taken in the speaker selection and placement to ensure that the sounds were identical for each subject. A total of 40 subjects participated. For each rotor configuration, the listeners were asked to evaluate the sounds in terms of noisiness. The test results indicate little to no "annoyance" benefit for the modulated blade spacing. In general, the subjects preferred the sound of the 5-blade regular spaced rotor over any of the modulated ones. A conclusion is that modulated blade spacing is not a promising design feature to reduce the annoyance for helicopter main rotors.
Document ID
20020048532
Document Type
Contractor Report (CR)
Authors
Edwards, Bryan (Bell Helicopter Co. Fort Worth, TX United States)
Booth, Earl R., Jr.
Date Acquired
September 7, 2013
Publication Date
May 1, 2002
Subject Category
Acoustics
Report/Patent Number
Rept-699-099-536
NASA/CR-2002-211651
NAS 1.26:211651
Funding Number(s)
PROJECT: RTOP 727-03-15-10
CONTRACT_GRANT: NAS1-00091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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