Patents by Inventor Victoria OTTO

Victoria OTTO 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).

  • Pitch control device for a ducted tail rotor of a rotorcraft
    Patent number: 10654559
    Abstract: A pitch control device for a ducted tail rotor of a rotorcraft. The pitch control device comprises a control input member with a disc-shaped central component and at least two connecting arms that extend radially from the disc-shaped central component, wherein the disc-shaped central component is provided for being mounted to an associated pitch control shaft of the ducted tail rotor, and a control transfer member with a ring-shaped connector and at least two push rods that extend axially from the ring-shaped connector, wherein each one of the at least two push rods is provided for being coupled to an associated pitch lever of a rotor blade of the ducted tail rotor.
    Type: Grant
    Filed: February 27, 2018
    Date of Patent: May 19, 2020
    Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Julius Vogl, Gerald Kuntze-Fechner, Victoria Otto
  • Multi-blade rotor for a rotary wing aircraft
    Patent number: 10518874
    Abstract: A multi-blade rotor for a rotary wing aircraft, comprising a plurality of rotor that is connected to an associated rotor head via a plurality of flexbeam elements, wherein at least one flexbeam element of the plurality of flexbeam elements comprises an asymmetrical flexbeam root that is mounted to the associated rotor head.
    Type: Grant
    Filed: May 17, 2017
    Date of Patent: December 31, 2019
    Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Gerald Kuntze-Fechner, Martin Ortner, Victoria Otto, Christeline Salmon, Eugen Rink, Rupert Pfaller
  • PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
    Publication number: 20180244368
    Abstract: A pitch control device for a ducted tail rotor of a rotorcraft. The pitch control device comprises a control input member with a disc-shaped central component and at least two connecting arms that extend radially from the disc-shaped central component, wherein the disc-shaped central component is provided for being mounted to an associated pitch control shaft of the ducted tail rotor, and a control transfer member with a ring-shaped connector and at least two push rods that extend axially from the ring-shaped connector, wherein each one of the at least two push rods is provided for being coupled to an associated pitch lever of a rotor blade of the ducted tail rotor.
    Type: Application
    Filed: February 27, 2018
    Publication date: August 30, 2018
    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Julius VOGL, Gerald KUNTZE-FECHNER, Victoria OTTO
  • MULTI-BLADE ROTOR FOR A ROTARY WING AIRCRAFT
    Publication number: 20170341742
    Abstract: A multi-blade rotor for a rotary wing aircraft, comprising a plurality of rotor that is connected to an associated rotor head via a plurality of flexbeam elements, wherein at least one flexbeam element of the plurality of flexbeam elements comprises an asymmetrical flexbeam root that is mounted to the associated rotor head.
    Type: Application
    Filed: May 17, 2017
    Publication date: November 30, 2017
    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
    Inventors: Gerald KUNTZE-FECHNER, Martin ORTNER, Victoria OTTO, Christeline SALMON, Eugen RINK, Rupert PFALLER