Patents by Inventor Carlos Miralles

Carlos Miralles 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: 20210371081
    Abstract: Various embodiments are described of an unmanned aerial vehicle having a wing. The unmanned aerial vehicle includes a first body of the wing with a first end proximate a body of the vehicle. A second end is opposite the first end. A first joint is on the first end of the first main body of the wing. The joint rotatably couples the wing to the vehicle. A second joint is on the second end of the vehicle. A second body of the wing is rotatably coupled to the first body via the second joint.
    Type: Application
    Filed: March 11, 2021
    Publication date: December 2, 2021
    Inventors: Ken Finklea, Carlos Miralles, Guan Hua Su
  • Patent number: 10974809
    Abstract: In one embodiment, a wing for an unmanned aerial vehicle is described. The unmanned aerial vehicle includes a first body of the wing with a first end proximate a body of the vehicle. A second end is opposite the first end. A first joint is on the first end of the first main body of the wing. The joint rotatably couples the wing to the vehicle. A second joint is on the second end of the vehicle. A second body of the wing is rotatably coupled to the first body via the second joint.
    Type: Grant
    Filed: May 30, 2017
    Date of Patent: April 13, 2021
    Assignee: Sierra Nevada Corporation
    Inventors: Ken Finklea, Carlos Miralles, Guan Hua Su
  • Publication number: 20170369150
    Abstract: In one embodiment, a wing for an unmanned aerial vehicle is described. The unmanned aerial vehicle includes a first body of the wing with a first end proximate a body of the vehicle. A second end is opposite the first end. A first joint is on the first end of the first main body of the wing. The joint rotatably couples the wing to the vehicle. A second joint is on the second end of the vehicle. A second body of the wing is rotatably coupled to the first body via the second joint.
    Type: Application
    Filed: May 30, 2017
    Publication date: December 28, 2017
    Applicant: SIERRA NEVADA CORPORATION
    Inventors: Ken FINKLEA, Carlos MIRALLES
  • Publication number: 20160298635
    Abstract: There is provided a portable, electrically powered debris blower that includes a noise reducing and energy efficient design. The debris blower includes a blower that is powered by a portable power supply, such as electrochemical battery cells. The blower includes an air intake, a curved blower housing that acts as an air inlet guide tube, an axial fan, and an air exhaust. To reduce noise and vibration output from the blower, the blower further includes a noise and vibration reducing material covering the inside walls of the blower, vibration and noise isolating mounts supporting the axial fan within the blower, and the air inlet is angled towards the ground with respect to the axis of the axial fan.
    Type: Application
    Filed: September 15, 2015
    Publication date: October 13, 2016
    Inventors: GUAN SU, CARLOS MIRALLES, DAVID KOPLOW
  • Patent number: 9211947
    Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
    Type: Grant
    Filed: September 3, 2013
    Date of Patent: December 15, 2015
    Assignee: AEROVIRONMENT, INC.
    Inventor: Carlos Miralles
  • Publication number: 20140172200
    Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
    Type: Application
    Filed: September 3, 2013
    Publication date: June 19, 2014
    Applicant: AEROVIRONMENT, INC.
    Inventor: Carlos Miralles