Patents by Inventor Kazuyuki Akimoto

Kazuyuki Akimoto 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: 20240140124
    Abstract: Provided is a heat-sensitive recording material that can provide clear and high print image quality with less printing omission, and that has high sensitivity and is excellent in recording density in halftone printing.
    Type: Application
    Filed: October 16, 2020
    Publication date: May 2, 2024
    Applicant: OJI HOLDING CORPORATION
    Inventors: Kentaro MOROFUJI, Kazuyuki SAKAMOTO, Shinya AKIMOTO, Takashi TAKEMURA
  • Patent number: 6637168
    Abstract: An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building, the exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building, and one or a plurality of current deflecting members are disposed near a lower end of the air inlet structure to deflect air currents flowing through the air inlet structure into the building toward an aircraft housed in the building. A current-straightening structure is incorporated into the air inlet structure. A current-straightening space is defined under the air inlet structure.
    Type: Grant
    Filed: April 3, 2002
    Date of Patent: October 28, 2003
    Assignee: Kawasaki Jukogyo Kabushiki Kaisha
    Inventors: Takayuki Satomi, Kazushi Ogawa, Takashi Kawashima, Hidenori Yoshida, Yasuo Saito, Hajime Hirakawa, Kazuyuki Akimoto
  • Patent number: 6560936
    Abstract: An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building. The exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building. A ceiling included in the building has an inclined section sloping down backward to straighten air currents, and a groove is formed in a middle part, with respect to width, of the inclined section to permit a vertical tail fin of an aircraft to pass when the aircraft is carried into or out of the test chamber.
    Type: Grant
    Filed: April 3, 2002
    Date of Patent: May 13, 2003
    Assignee: Kawasaki Jukogyo Kabushiki Kaisha
    Inventors: Takayuki Satomi, Kazushi Ogawa, Takashi Kawashima, Hidenori Yoshida, Yasuo Saito, Hajime Hirakawa, Kazuyuki Akimoto
  • Publication number: 20020144473
    Abstract: An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building, the exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building, and one or a plurality of current deflecting members are disposed near a lower end of the air inlet structure to deflect air currents flowing through the air inlet structure into the building toward an aircraft housed in the building. A current-straightening structure is incorporated into the air inlet structure. A current-straightening space is defined under the air inlet structure.
    Type: Application
    Filed: April 3, 2002
    Publication date: October 10, 2002
    Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA
    Inventors: Takayuki Satomi, Kazushi Ogawa, Takashi Kawashima, Hidenori Yoshida, Yasuo Saito, Hajime Hirakawa, Kazuyuki Akimoto
  • Publication number: 20020144474
    Abstract: An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building. The exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building. A ceiling included in the building has an inclined section sloping down backward to straighten air currents, and a groove is formed in a middle part, with respect to width, of the inclined section to permit a vertical tail fin of an aircraft to pass when the aircraft is carried into or out of the test chamber.
    Type: Application
    Filed: April 3, 2002
    Publication date: October 10, 2002
    Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA
    Inventors: Takayuki Satomi, Kazushi Ogawa, Takashi Kawashima, Hidenori Yoshida, Yasuo Saito, Hajime Hirakawa, Kazuyuki Akimoto
  • Patent number: 5927022
    Abstract: Provided are a method for moving a multipurpose field and an apparatus for the same wherein the multipurpose field can be caused to float above a basic floor plate under a fluid pressure and can be moved and placed in a desired position by delivery means. The moving apparatus comprises a nozzle provided over a basic floor plate common to a field region of a roofed stadium and an outdoor region for detecting existence of the multipurpose field and for jetting a fluid upward in response to a detection signal, and delivery means for alternately moving the multipurpose field between both the regions.
    Type: Grant
    Filed: July 21, 1997
    Date of Patent: July 27, 1999
    Assignee: Kawasaki Jukogyo Kabushiki
    Inventors: Hajime Hirakawa, Kazuyuki Akimoto, Shigemi Okada, Sadaaki Murakawa, Shinichi Sugiyama, Taizo Tsutusi