Patents by Inventor Yosuke Higuchi

Yosuke Higuchi 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: 20210125126
    Abstract: There is provided an information processing apparatus for efficiently processing various products. The information processing apparatus includes a determiner that receives signals from sensors respectively provided in a plurality of machine tools, determines operation statuses of the plurality of machine tools, and derives a plurality of usable machine tools, a receiver that receives product specifying data for specifying a product to be manufactured, a decider that decides, based on the product specifying data, a necessary machine tool required to process the product, and a presenter that searches for the necessary machine tool from the plurality of usable machine tools, and presents information concerning a use machine tool as a search result.
    Type: Application
    Filed: March 25, 2019
    Publication date: April 29, 2021
    Applicant: DMG MORI CO., LTD
    Inventors: Naruhiro IRINO, Yasuhiro IMABEPPU, Yosuke HIGUCHI
  • Publication number: 20200293188
    Abstract: A character input device includes an operation unit that receives a character input performed with a flick input, a slide detector that detects a starting position of the flick input, and a determination unit that adjusts an input determination area for the character input in response to the starting position in accordance with an input error count for the flick input.
    Type: Application
    Filed: February 19, 2020
    Publication date: September 17, 2020
    Applicant: OMRON Corporation
    Inventor: Yosuke HIGUCHI
  • Publication number: 20200088259
    Abstract: There is provided a vibration suppression device, a machine tool including the device and a vibration suppression method using the device. The vibration suppression device includes a flexible member having a first position F fixed to the structure to be a fixed end of a cantilever and a second position on a free end side; and a weight attached to the flexible member in the second position. The vibration suppression device has an adjustment mechanism for changing a distance between the first position and the second position. Accordingly, it can effectively suppress vibration of a structure, and that can effectively suppress the vibration by easy adjustment when the characteristic of a generated vibration is different.
    Type: Application
    Filed: December 21, 2017
    Publication date: March 19, 2020
    Inventors: Yosuke Higuchi, Yasuhiro Imabeppu, Tomohiro Tsuzuki, Naruhiro Irino, Yutaka Ido
  • Patent number: 9108722
    Abstract: An aircraft is provided with a mechanical linkage that mechanically transmits an amount of manipulation of a control stick to a rudder controlling mechanism, an amount-of-manipulation sensor that detects the amount of manipulation, and an FBW control-law computing unit that calculates an FBW control-law command indicating an amount of control for a craft in accordance with the detected amount of manipulation. Also, with the aircraft, a high-pass filter outputs, among the control-stick manipulation amounts detected by the amount-of-manipulation sensor, an amount of change in the control-stick manipulation amounts; by subtracting the amount of change that has passed through the high-pass filter by means of the subtracting portion, the FBW control-law command serves as an SAS command; and the rudder controlling mechanism is driven by adding an amount of movement of an SAS actuator in accordance with the SAS command to the control-stick manipulation amount transmitted by the mechanical linkage.
    Type: Grant
    Filed: October 12, 2012
    Date of Patent: August 18, 2015
    Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
    Inventors: Yosuke Higuchi, Takeshi Matsuda
  • Patent number: 9031718
    Abstract: An aircraft is provided with: an attitude control command calculating section which calculates an attitude control command for target attitude on the basis of a control stick operation amount; a gain value generating section which generates a gain value equal to or less than 1 which decreases as the control stick operation amount is larger; a multiplication section which multiplies the attitude control command for target attitude by the gain value; and a addition section which adds a rate damping control command to the attitude control command for target attitude multiplied by the gain value and outputs a result to a subtraction section for calculating an SAS command.
    Type: Grant
    Filed: October 12, 2012
    Date of Patent: May 12, 2015
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Yosuke Higuchi, Takeshi Matsuda
  • Publication number: 20140231591
    Abstract: An aircraft is provided with: an attitude control command calculating section which calculates an attitude control command for target attitude on the basis of a control stick operation amount; a gain value generating section which generates a gain value equal to or less than 1 which decreases as the control stick operation amount is larger; a multiplication section which multiplies the attitude control command for target attitude by the gain value; and a addition section which adds a rate damping control command to the attitude control command for target attitude multiplied by the gain value and outputs a result to a subtraction section for calculating an SAS command.
    Type: Application
    Filed: October 12, 2012
    Publication date: August 21, 2014
    Applicant: Mitsubishi Heavy Industries, Ltd.
    Inventors: Yosuke Higuchi, Takeshi Matsuda
  • Publication number: 20140191087
    Abstract: An aircraft is provided with a mechanical linkage that mechanically transmits an amount of manipulation of a control stick to a rudder controlling mechanism, an amount-of-manipulation sensor that detects the amount of manipulation, and an FBW control-law computing unit that calculates an FBW control-law command indicating an amount of control for a craft in accordance with the detected amount of manipulation. Also, with the aircraft, a high-pass filter outputs, among the control-stick manipulation amounts detected by the amount-of-manipulation sensor, an amount of change in the control-stick manipulation amounts; by subtracting the amount of change that has passed through the high-pass filter by means of the subtracting portion, the FBW control-law command serves as an SAS command; and the rudder controlling mechanism is driven by adding an amount of movement of an SAS actuator in accordance with the SAS command to the control-stick manipulation amount transmitted by the mechanical linkage.
    Type: Application
    Filed: October 12, 2012
    Publication date: July 10, 2014
    Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
    Inventors: Yosuke Higuchi, Takeshi Matsuda