Perceived discomfort for typical helicopter vertical sine vibrations for seated participants
Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort. Fifty-three participants, seated on a helicopter seat fixed to a vibration test bench, evaluated the discomfort of vertical sinusoidal vibrations...
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Published in | Journal of Low Frequency Noise, Vibration and Active Control Vol. 40; no. 3; pp. 1661 - 1667 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
London, England
SAGE Publications
01.09.2021
Sage Publications Ltd Sage SAGE Publishing |
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Abstract | Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort. Fifty-three participants, seated on a helicopter seat fixed to a vibration test bench, evaluated the discomfort of vertical sinusoidal vibrations using a magnitude estimation procedure. Stimuli had a frequency between 15 and 30 Hz and a level between 0.32 and 3.16 m/s2. The average discomfort was shown related to vibration velocity using Steven’s power law, without any frequency dependence. The exponent depended on velocity and was 1.18 for higher velocities (approx. above 0.008 m/s) and 0.65 for velocities below that limit. |
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AbstractList | Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort. Fifty-three participants, seated on a helicopter seat fixed to a vibration test bench, evaluated the discomfort of vertical sinusoidal vibrations using a magnitude estimation procedure. Stimuli had a frequency between 15 and 30 Hz and a level between 0.32 and 3.16 m/s 2 . The average discomfort was shown related to vibration velocity using Steven’s power law, without any frequency dependence. The exponent depended on velocity and was 1.18 for higher velocities (approx. above 0.008 m/s) and 0.65 for velocities below that limit. Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort. Fifty-three participants, seated on a helicopter seat fixed to a vibration test bench, evaluated the discomfort of vertical sinusoidal vibrations using a magnitude estimation procedure. Stimuli had a frequency between 15 and 30 Hz and a level between 0.32 and 3.16 m/s2. The average discomfort was shown related to vibration velocity using Steven’s power law, without any frequency dependence. The exponent depended on velocity and was 1.18 for higher velocities (approx. above 0.008 m/s) and 0.65 for velocities below that limit. |
Author | Laurianne Delcor Etienne Parizet Julie Ganivet-Ouzeneau Julien Caillet |
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Cites_doi | 10.1016/S0169-8141(98)00017-1 10.1007/978-1-4419-6712-1_3 10.4050/JAHS.29.11 10.1080/00140139.2012.678390 10.1016/j.apergo.2012.10.006 10.1037/h0046162 10.2486/indhealth.6.1 10.1016/j.jsv.2006.06.011 10.1080/00140139.2018.1533145 |
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Contributor | Laboratoire Vibrations Acoustique (LVA) ; Institut National des Sciences Appliquées de Lyon (INSA Lyon) ; Université de Lyon-Institut National des Sciences Appliquées (INSA)-Université de Lyon-Institut National des Sciences Appliquées (INSA) Airbus Helicopters ; Aeroport International de Marseille-Provence ANR-11-IDEX-0007,Avenir L.S.E.,PROJET AVENIR LYON SAINT-ETIENNE |
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References | Miwa 1968; 6 Basri, Griffin 2013; 44 Basri, Griffin 2012; 55 Stevens 1957; 64 Morioka, Griffin 2006; 298 Han, Song, Kwahk 1999; 23 Huang, Zhang 2019; 62 Leatherwood, Dempsey 1976 bibr11-1461348420979759 Leatherwood JD (bibr6-1461348420979759) 1976 NF EN ISO 1683:2008 (bibr13-1461348420979759) 2008 bibr3-1461348420979759 bibr14-1461348420979759 Griffin M. (bibr7-1461348420979759) 1990 bibr9-1461348420979759 bibr5-1461348420979759 bibr10-1461348420979759 bibr12-1461348420979759 bibr1-1461348420979759 bibr8-1461348420979759 bibr2-1461348420979759 bibr15-1461348420979759 bibr4-1461348420979759 |
References_xml | – year: 1976 article-title: Psychophysical relationships characterizing human response to whole body sinusoidal vertical vibrations publication-title: NASA TN D-8188 – volume: 55 start-page: 909 year: 2012 end-page: 922 article-title: Equivalent comfort contours for vertical seat vibration: effect of vibration magnitude and backrest inclination publication-title: Ergonomics – volume: 44 start-page: 423 year: 2013 end-page: 434 article-title: Predicting discomfort from whole-body vertical vibration when sitting with an inclined backrest publication-title: Appl Ergon – volume: 298 start-page: 755 year: 2006 end-page: 772 article-title: Magnitude-dependence of equivalent comfort contours for fore-and-aft, lateral and vertical whole body vibration publication-title: J Sound Vib – volume: 6 start-page: 1 year: 1968 end-page: 10 article-title: Evaluation methods for vibration effect. Part 4. Measurements of vibration greatness for whole body and hand in vertical and horizontal vibrations publication-title: Indus Health – volume: 64 start-page: 153 year: 1957 end-page: 181 article-title: On the psychophysical law publication-title: Psychol Rev – volume: 23 start-page: 513 year: 1999 end-page: 524 article-title: A systematic method for analysing magnitude estimation data publication-title: Int J Indus Ergonom – volume: 62 start-page: 420 year: 2019 end-page: 430 article-title: Subjective discomfort caused by vertical whole-body vibration in the frequency range 2–100 Hz publication-title: Ergonomics – ident: bibr12-1461348420979759 doi: 10.1016/S0169-8141(98)00017-1 – ident: bibr11-1461348420979759 doi: 10.1007/978-1-4419-6712-1_3 – year: 1976 ident: bibr6-1461348420979759 publication-title: NASA TN D-8188 – ident: bibr2-1461348420979759 doi: 10.4050/JAHS.29.11 – ident: bibr9-1461348420979759 doi: 10.1080/00140139.2012.678390 – ident: bibr1-1461348420979759 – ident: bibr14-1461348420979759 doi: 10.1016/j.apergo.2012.10.006 – ident: bibr5-1461348420979759 doi: 10.1037/h0046162 – volume-title: Acoustics – preferred reference values for acoustical and vibratory levels year: 2008 ident: bibr13-1461348420979759 – ident: bibr4-1461348420979759 – ident: bibr15-1461348420979759 doi: 10.2486/indhealth.6.1 – ident: bibr8-1461348420979759 doi: 10.1016/j.jsv.2006.06.011 – ident: bibr10-1461348420979759 doi: 10.1080/00140139.2018.1533145 – volume-title: Handbook of human vibration year: 1990 ident: bibr7-1461348420979759 – ident: bibr3-1461348420979759 |
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Snippet | Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort.... Vibrations contribute to helicopter's ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort.... |
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SubjectTerms | [SPI.MECA.VIBR]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Vibrations [physics.class-ph] Acoustics. Sound Control engineering systems. Automatic machinery (General) Discomfort Engineering Sciences Helicopters Mechanics Passenger comfort Perception QC221-246 Seats TJ212-225 Vibration tests Vibrations |
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Title | Perceived discomfort for typical helicopter vertical sine vibrations for seated participants |
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