Investigation of a parallel active vibration isolation mount for mitigating N/Rev helicopter vibrations

DOIResolve DOI: http://doi.org/10.2514/6.2017-1441
AuthorSearch for: ; Search for: ; Search for: ; Search for:
TypeArticle
Proceedings title25th AIAA/AHS Adaptive Structures Conference
Conference25th AIAA/AHS Adaptive Structures Conference, 9-13 january 2017, Grapevine, TX, USA
ISBN978-1-62410-446-6
Pages# of pages: 13
AbstractThis paper presents an active isolation mount using a flexible passive support in parallel with a voice coil actuator. This active mount is designed to reduce the N/rev harmonic vibration of a helicopter at the local seat structure. The active mount is tested in a simple single degree of freedom mechanical system to reduce vibration at a payload mass representative of a 95th percentile pilot. The system is tested experimentally and also modeled in Simulink®. The results from the experiment are compared to those obtained numerically. The active mount was shown to be effective by reducing vibration representative of a Bell-412 helicopter by 11.96 dB (74.77 %).
Publication date
PublisherAmerican Institute of Aeronautics and Astronautics
LanguageEnglish
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number23002454
Export citationExport as RIS
Report a correctionReport a correction
Record identifier8a86d5e7-6dca-401e-82cc-14b29e426823
Record created2017-11-14
Record modified2017-11-14
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
  • Share this page with Delicious (Opens in a new window)