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ROTORCRAFT VIBRATION SUPPRESSION SYSTEM IN A FOUR CORNER PYLON MOUNT CONFIGURATION

  • US 20130270415A1
  • Filed: 01/08/2013
  • Published: 10/17/2013
  • Est. Priority Date: 01/10/2012
  • Status: Active Grant
First Claim
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1. A vibration suppression system for an aircraft, comprising:

  • a pylon mount structural assembly configured to control pitch and roll dynamics of a vibrating body within the aircraft, the pylon mount structural assembly having a pylon structure configured to support the vibrating body at a point of coupling; and

    a vibration isolator located at each end of the pylon structure to control the transmission of vibrations through the aircraft, the vibration isolator being spaced away from the vibrating body.

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