Patents by Inventor Maroosol YUN

Maroosol YUN 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).

  • Airfoil wing-shaped aircraft
    Patent number: 12043379
    Abstract: Proposed is an airfoil wing-shaped aircraft including a body having a wing-shaped longitudinal cross-section and having an upper surface on which a shape of a concave curvature-surface portion is formed along a center axis in a streamwise direction, a fluid inlet being formed in each of the opposite lateral sides of a leading portion of the body, and a fluid output being formed in each of the opposite lateral sides of a tail portion of the body, wherein a duct connects the fluid inlet and the fluid outlet to each other.
    Type: Grant
    Filed: October 4, 2021
    Date of Patent: July 23, 2024
    Assignee: UIF (UNIVERSITY INDUSTRY FOUNDATION), YONSEI UNIVERSITY
    Inventors: Hyung Hee Cho, Seungyeong Choi, Jihyuk Kim, Juyeong Nam, Maroosol Yun, Taedoo Yoon, Minho Bang, Joon-soo Lim
  • FLEXIBLE INFRARED SELECTIVE EMITTER AND MANUFACTURING METHOD THEREOF
    Publication number: 20230221618
    Abstract: The present invention provides an infrared selective emitter in which since infrared energy can be emitted in a desired wavelength band by adjusting a metamaterial having a repeating structure on a plane, infrared camouflage is possible by attaching to the surface of the shape of an object to be camouflaged, and at the same time, the infrared selective emitter has flexible characteristics that can be applied to curved surfaces without limitations on the shape of an object.
    Type: Application
    Filed: December 22, 2022
    Publication date: July 13, 2023
    Applicant: UIF (University Industry Foundation), Yonsei University
    Inventors: Hyung Hee CHO, Namkyu LEE, Joon-Soo LIM, Injoong CHANG, Juyeong NAM, Hyung Mo BAE, Maroosol YUN
  • AIRFOIL WING-SHAPED AIRCRAFT
    Publication number: 20220106035
    Abstract: Proposed is an airfoil wing-shaped aircraft including a body having a wing-shaped longitudinal cross-section and having an upper surface on which a shape of a concave curvature-surface portion is formed along a center axis in a streamwise direction, a fluid inlet being formed in each of the opposite lateral sides of a leading portion of the body, and a fluid output being formed in each of the opposite lateral sides of a tail portion of the body, wherein a duct connects the fluid inlet and the fluid outlet to each other.
    Type: Application
    Filed: October 4, 2021
    Publication date: April 7, 2022
    Inventors: Hyung Hee CHO, Seungyeong CHOI, Jihyuk KIM, Juyeong NAM, Maroosol YUN, Taedoo YOON, Minho BANG, Joon-soo LIM