Patents by Inventor Andreas Hubertus von Flotow

Andreas Hubertus von Flotow has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20120104169
    Abstract: Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include 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. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.
    Type: Application
    Filed: January 10, 2012
    Publication date: May 3, 2012
    Applicant: Insitu, Inc.
    Inventors: Andreas Hubertus von Flotow, Tyler Patrick Horton
  • Patent number: 8091833
    Abstract: Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include 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. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.
    Type: Grant
    Filed: February 20, 2009
    Date of Patent: January 10, 2012
    Assignee: Insitu, Inc.
    Inventors: Andreas Hubertus von Flotow, Tyler Patrick Horton
  • Publication number: 20090218447
    Abstract: Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include 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. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.
    Type: Application
    Filed: February 20, 2009
    Publication date: September 3, 2009
    Inventors: Andreas Hubertus von Flotow, Tyler Patrick Horton