Patents by Inventor Tsuyoshi Yagishita

Tsuyoshi Yagishita 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: 10408707
    Abstract: An abnormality diagnosing method includes a model generation step of generating a simulation model of a monitoring target, an operation start step of starting an operation of the monitoring target, a measurement step of measuring an internal state quantity in the operating state of the monitoring target and extracting a measured value, a prediction step of inputting into the simulation model same control input value used in the operating state of the monitoring target and calculating a predicted value of the internal state quantity of the monitoring target, a Mahalanobis distance calculation step of calculating a Mahalanobis distance from a difference between the measured value and the predicted value, and an abnormality diagnosis step of diagnosing whether the operating state of the monitoring target is abnormal based on the Mahalanobis distance.
    Type: Grant
    Filed: July 31, 2017
    Date of Patent: September 10, 2019
    Assignee: IHI Corporation
    Inventors: Hatsuo Mori, Noriyoshi Mizukoshi, Takashi Ogai, Yusuke Maru, Takayuki Yamamoto, Shinsuke Takeuchi, Satoshi Nonaka, Tsuyoshi Yagishita
  • Publication number: 20170328811
    Abstract: An abnormality diagnosing method includes a model generation step of generating a simulation model of a monitoring target, an operation start step of starting an operation of the monitoring target, a measurement step of measuring an internal state quantity in the operating state of the monitoring target and extracting a measured value, a prediction step of inputting into the simulation model same control input value used in the operating state of the monitoring target and calculating a predicted value of the internal state quantity of the monitoring target, a Mahalanobis distance calculation step of calculating a Mahalanobis distance from a difference between the measured value and the predicted value, and an abnormality diagnosis step of diagnosing whether the operating state of the monitoring target is abnormal based on the Mahalanobis distance.
    Type: Application
    Filed: July 31, 2017
    Publication date: November 16, 2017
    Applicant: IHI Corporation
    Inventors: Hatsuo MORI, Noriyoshi Mizukoshi, Takashi Ogai, Yusuke Maru, Takayuki Yamamoto, Shinsuke Takeuchi, Satoshi Nonaka, Tsuyoshi Yagishita
  • Patent number: 8943795
    Abstract: Disclosed is a turbo pump in which a pump impeller is connected to one end of a rotary shaft and a turbine is connected to the other end of the rotary shaft. The turbo pump is designed such that an equivalent region, between a turbine efficiency curve obtained on the basis of a conditional expression where the number of rotations of the rotary shaft is maintained constant regardless of a pump flow rate and a turbine efficiency curve of an actual machine, becomes an operation region.
    Type: Grant
    Filed: September 3, 2010
    Date of Patent: February 3, 2015
    Assignees: IHI Corporation, Japan Aerospace Exploration Agency
    Inventors: Hatsuo Mori, Yoshihiro Naruo, Shinichiro Tokudome, Tsuyoshi Yagishita, Takayuki Yamamoto, Yoshifumi Inatani
  • Publication number: 20120167552
    Abstract: Disclosed is a turbo pump in which a pump impeller is connected to one end of a rotary shaft and a turbine is connected to the other end of the rotary shaft. The turbo pump is designed such that an equivalent region, between a turbine efficiency curve obtained on the basis of a conditional expression where the number of rotations of the rotary shaft is maintained constant regardless of a pump flow rate and a turbine efficiency curve of an actual machine, becomes an operation region.
    Type: Application
    Filed: September 3, 2010
    Publication date: July 5, 2012
    Inventors: Hatsuo Mori, Yoshihiro Naruo, Shinichiro Tokudome, Tsuyoshi Yagishita, Takayuki Yamamoto, Yoshifumi Inatani
  • Publication number: 20090007541
    Abstract: A thruster is provided that makes it possible to reduce and eventually eliminate the toxicity of storable liquid propellant and improve the low-temperature environment adaptability of propulsion system using the storable liquid propellant. The thruster produces thrust by using catalytic decomposition gas obtained by catalytically decomposing nitrous oxide with a nitrous oxide decomposition catalyst.
    Type: Application
    Filed: December 5, 2007
    Publication date: January 8, 2009
    Applicants: Japan Aerospace Exploration Agency, Showa Denko K.K.
    Inventors: Junichiro Kawaguchi, Shinichiro Tokudome, Hiroto Habu, Tsuyoshi Yagishita, Masatoshi Hotta