The invention is related to a vibration dampening structure 7 for dampening vibrations occurring during operation of a rotary wing aircraft 1, comprising: a floating body 8; and a floating body support structure 9 that supports the floating body 8. The floating body support structure 9 comprises a mounting device 10 that is rigidly mountable to the rotary wing aircraft 1; and a pneumatic shock absorber system 29 that couples the floating body 8 to the mounting device 10. The pneumatic shock absorber system 29 dampens the vibrations occurring during operation of the rotary wing aircraft 1 for stabilizing the floating body 8 relative to the mounting device 10.
A VIBRATION DAMPENING STRUCTURE FOR A ROTARY WING AIRCRAFT
VIBRATIONSDÄMPFUNGSSTRUKTUR FÜR EIN DREHFLÜGELFLUGZEUG
STRUCTURE D'AMORTISSEMENT DE VIBRATIONS POUR UN AÉRONEF À VOILURE TOURNANTE
2021-12-15
Patent
Electronic Resource
English
Rotary-Wing Aircraft Outlook - Rotary-Wing Aircraft Table
Online Contents | 2009
VIBRATION AND VIBRATION MEASUREMENT DEVICE USING ROTARY-WING AIRCRAFT
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