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0019.937638
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006m     o  d f      
007cr |n|||||||||
008240501t20242024onca    o    f000 0 eng d
020 |a9780660716992
040 |aCaOODSP|beng|erda|cCaOODSP
043 |an-cn---
0861 |aNR74-12/2024E-PDF
24500|aActive seat mount system for rotorcraft.
264 1|a[Ottawa] : |bNational Research Council Canada = Conseil national de recherches Canada, |c2024.
264 4|c©2024
300 |a1 online resource (2 unnumbered pages) : |billustrations
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
500 |aIssued also in French under title: Système de suspension active du siège de giravion.
520 |a"During helicopter flight operations, rotorcraft floor vibration is generated by the periodical rotor blade aerodynamic and inertial loads. This unwanted vibration is transmitted through the helicopter seat, exposing the aircrew to health-related issues caused by whole-body vibration (WBV)"--page [1].
650 0|aHelicopters|xSeats.
650 0|aRotors|xVibration.
7102 |aNational Research Council Canada, |eissuing body.
77508|tSystème de suspension active du siège de giravion.|w(CaOODSP)9.937640
7760#|tActive seat mount system for rotorcraft.|w(CaOODSP)9.937639
85640|qPDF|s1.38 MB|uhttps://publications.gc.ca/collections/collection_2025/cnrc-nrc/NR74-12-2024-eng.pdf