Patents by Inventor Hidehiko Kato

Hidehiko Kato 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: 20130186192
    Abstract: A wind tunnel test model (1) includes a half model portion (3) that simulates a fuselage portion of an airframe with a single wing and a supporting apparatus (5) that supports the half model portion rotatably about a central axis. The supporting apparatus has a horizontal cross-sectional shape that is approximately the same as or similar to that of the fuselage portion (7) and extends rearward of the fuselage portion, includes, toward its rear end, a fixing portion (11) that fixes the half model portion to a wind tunnel test apparatus side, and includes, within a housing, a torsional rigidity imparting unit.
    Type: Application
    Filed: September 30, 2011
    Publication date: July 25, 2013
    Inventors: Motohide Uehara, Satoshi Yonemoto, Hidehiko Kato, Takayuki Nomura, Masashi Nagahata
  • Patent number: 8042386
    Abstract: A test section for a wind-tunnel testing apparatus has a mounting section that mounts an automobile along the internal floor surface of a wind tunnel. Tests are conducted by applying an airflow blown in the wind tunnel to the automobile mounted on the mounting section. The test section includes a slit that is disposed on the floor surface located on the upstream side of the mounting section with respect to the airflow direction so as to extend in the intersecting direction intersecting the airflow direction and that sucks in a portion of the airflow near the floor surface, and lateral suction portions, disposed at both sides of the mounting section, that suck in the incoming airflows R flowing in from the sides of the mounting section.
    Type: Grant
    Filed: July 24, 2008
    Date of Patent: October 25, 2011
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Hidehiko Kato, Tomohiro Sone
  • Publication number: 20100175465
    Abstract: Provided is a test section for a wind-tunnel testing apparatus that is capable of suppressing the influences of a boundary layer on the floor surface and incoming airflows from the sides, and that is capable of measuring aerodynamic forces closer to the those actually occurring. A test section for a wind-tunnel testing apparatus having a mounting section that mounts an automobile along the internal floor surface of a wind tunnel, tests being conducted by applying an airflow blown in the wind tunnel to the automobile mounted on the mounting section, includes a slit that is disposed on the floor surface located on the upstream side of the mounting section with respect to the airflow direction so as to extend in the intersecting direction intersecting the airflow direction and that sucks in a portion of the airflow near the floor surface; and lateral suction portions, disposed at both sides of the mounting section, that suck in the incoming airflows R flowing in from the sides of the mounting section.
    Type: Application
    Filed: July 24, 2008
    Publication date: July 15, 2010
    Inventors: Hidehiko Kato, Tomohiro Sone