Patents by Inventor Norimasa Takagi

Norimasa Takagi 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: 8505848
    Abstract: A first actuator drives a control surface by being operated by supply of pressure oil from a first aircraft central hydraulic power source including a first aircraft central hydraulic pump. A second actuator drives the control surface by being operated by supply of pressure oil from a second aircraft central hydraulic power source including a second aircraft central hydraulic pump. A backup hydraulic pump is installed inside a wing of the aircraft and is provided so as to be able to supply pressure oil to the first actuator when a loss or degradation in a function of at least one of the first aircraft central hydraulic power source and the second aircraft central hydraulic power source occurs. A maximum discharge pressure of the backup hydraulic pump is set to be greater than maximum discharge pressures of the first aircraft central hydraulic pump and the second aircraft central hydraulic pump.
    Type: Grant
    Filed: October 20, 2011
    Date of Patent: August 13, 2013
    Assignee: Nabtesco Corporation
    Inventors: Atsushi Fukui, Norimasa Takagi
  • Publication number: 20120131912
    Abstract: A first actuator drives a control surface by being operated by supply of pressure oil from a first aircraft central hydraulic power source including a first aircraft central hydraulic pump. A second actuator drives the control surface by being operated by supply of pressure oil from a second aircraft central hydraulic power source including a second aircraft central hydraulic pump. A backup hydraulic pump is installed inside a wing of the aircraft and is provided so as to be able to supply pressure oil to the first actuator when a loss or degradation in a function of at least one of the first aircraft central hydraulic power source and the second aircraft central hydraulic power source occurs. A maximum discharge pressure of the backup hydraulic pump is set to be greater than maximum discharge pressures of the first aircraft central hydraulic pump and the second aircraft central hydraulic pump.
    Type: Application
    Filed: October 20, 2011
    Publication date: May 31, 2012
    Applicant: NABTESCO CORPORATION
    Inventors: Atsushi FUKUI, Norimasa TAKAGI
  • Patent number: 4941794
    Abstract: As automated loading/unloading system is shown, which uses a lift truck 10 for loading and unloading cargos and adpated to travel between a container 90 and a coneyor 50, a rotatably disposed turntable 60 for rotation about a vertical axis, the turntable being rotated when the lift truck 10 is on top thereof so as to turn the lift truck to face the container 90 or conveyor 50. A transport passage 80 installed between the turntable 60 and container 90 to permit the lift truck 10 to reach the container 90. An external power unit 100 is employed for controlling the lift truck and the turntable 60. Guide rails 70 and 81 are provided to extend along the turntable 60 and the transport passage 80 along one edge. The lift truck 10 is designed so as to urge its body to one side in its movement so that the movement of the lift truck is guided by the rails 70 and 81 and the inside wall of the container on the same side of the rails.
    Type: Grant
    Filed: November 30, 1989
    Date of Patent: July 17, 1990
    Assignees: Honda Giken Kogyo Kabushiki Kaisha, Nittsu Shoji Kabushiki Kaisha
    Inventors: Yoshimasa Hara, Seisaku Ohkura, Fumio Iijima, Isamu Tamura, Tetsuro Fukai, Sumiho Tagiri, Norimasa Takagi