Patents by Inventor Ryota TAKAYA

Ryota TAKAYA 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).

  • SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT
    Publication number: 20240102850
    Abstract: A shock wave detection system includes a light beam emitter, a light beam receiver and an analysis unit. The light beam emitter emits a light beam oblique to a direction of an air flow through which a shock wave may propagate. The light beam receiver receives the light beam that has passed through the air flow. The analysis unit is configured to detect a presence and a position of the shock wave based on a change in a receiving position of the light beam by the light beam receiver.
    Type: Application
    Filed: September 15, 2023
    Publication date: March 28, 2024
    Inventors: Ryosuke SATO, Ryota TAKAYA
  • Wall surface pressure measurement structure and wind-tunnel test apparatus
    Patent number: 11022518
    Abstract: A wall surface pressure measurement structure measures a wall surface pressure in a duct. Measurement holes are formed in different positions in a circumferential direction on an inspection surface of a wall surface of the duct. The inspection surface is orthogonal to an extending direction of the duct. A pressure chamber communicating with the measurement holes is provided on an outer peripheral side of the duct. The pressure chamber is coupled to a pressure gauge via a pressure pipe.
    Type: Grant
    Filed: October 26, 2018
    Date of Patent: June 1, 2021
    Assignees: SUBARU CORPORATION, Japan Aerospace Exploration Agency
    Inventors: Toshiteru Mitomo, Ryota Takaya, Yoshikazu Makino
  • WALL SURFACE PRESSURE MEASUREMENT STRUCTURE AND WIND-TUNNEL TEST APPARATUS
    Publication number: 20190128773
    Abstract: A wall surface pressure measurement structure measures a wall surface pressure in a duct. Measurement holes are formed in different positions in a circumferential direction on an inspection surface of a wall surface of the duct. The inspection surface is orthogonal to an extending direction of the duct. A pressure chamber communicating with the measurement holes is provided on an outer peripheral side of the duct. The pressure chamber is coupled to a pressure gauge via a pressure pipe.
    Type: Application
    Filed: October 26, 2018
    Publication date: May 2, 2019
    Applicants: SUBARU CORPORATION, Japan Aerospace Exploration Agency
    Inventors: Toshiteru MITOMO, Ryota TAKAYA, Yoshikazu MAKINO