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VIBRATION ISOLATION DEVICES AND ASSOCIATED SYSTEMS AND METHODS

  • US 20090218447A1
  • Filed: 02/20/2009
  • Published: 09/03/2009
  • Est. Priority Date: 02/29/2008
  • Status: Active Grant
First Claim
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1. An unmanned aircraft system, comprising:

  • a fuselage having a first fuselage section and a second fuselage section adjacent to and at least approximately longitudinally aligned with the first fuselage section; and

    at least one vibration isolation device coupling the first fuselage section to the second fuselage section, wherein the vibration isolation device istranslationally stiffer along a longitudinal axis than it is along a lateral axis and a vertical axis; and

    rotationally stiffer about a pitch axis and a yaw axis than it is about a roll axis.

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