Patents by Inventor Takaaki YUMITORI

Takaaki YUMITORI 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).

  • Patent number: 11364989
    Abstract: A wing used for an aircraft includes a configuration member formed of a composite material. The configuration member is divided into a plurality of regions along a surface thereof. The plurality of regions include a first region formed of the composite material of a high strength type, and a second region formed of the composite material of a high elasticity type having higher rigidity than the high strength type. The first region includes any region closest to a wing end side out of the plurality of regions, and the second region includes a region closest to the wing end side and a trailing edge side out of the plurality of regions.
    Type: Grant
    Filed: September 10, 2018
    Date of Patent: June 21, 2022
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Takayuki Nomura, Satoshi Kodama, Takaaki Yumitori, Kiyoka Takagi, Tooru Shitani, Toshio Abe
  • Publication number: 20210039800
    Abstract: An aircraft includes a main wing, a mounted object mounted to the main wing, and a connecting structure for connecting the main wing and the mounted object. The connecting structure includes a pylon that is provided to extend in a yaw axis direction of the aircraft from the main wing and connects the main wing and a directly upper portion of the mounted object to support the mounted object, and a support rod that is provided to extend from a position closer to a tip side of the main wing than the pylon toward a mounted object side located on a base end side of the main wing and connects the main wing and the mounted object, and a truss structure is formed by the main wing, the pylon, and the support rod.
    Type: Application
    Filed: September 7, 2018
    Publication date: February 11, 2021
    Inventors: Takaaki YUMITORI, Takayuki NOMURA, Satoshi KODAMA
  • Publication number: 20200298955
    Abstract: A wing used for an aircraft includes a configuration member formed of a composite material. The configuration member is divided into a plurality of regions along a surface thereof. The plurality of regions include a first region formed of the composite material of a high strength type, and a second region formed of the composite material of a high elasticity type having higher rigidity than the high strength type. The first region includes any region closest to a wing end side out of the plurality of regions, and the second region includes a region closest to the wing end side and a trailing edge side out of the plurality of regions.
    Type: Application
    Filed: September 10, 2018
    Publication date: September 24, 2020
    Inventors: Takayuki NOMURA, Satoshi KODAMA, Takaaki YUMITORI, Kiyoka TAKAGI, Tooru SHITANI, Toshio ABE