Patents by Inventor Yasutoshi HYAKUSOKU

Yasutoshi HYAKUSOKU 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).

  • Adjusting method and adjusting system for resonance frequency of vibration isolator, vibration isolator, and designing method, designing system, and manufacturing method for vibration isolator
    Patent number: 10962082
    Abstract: Provided is an adjusting method for a resonance frequency of a vibration isolator, the vibration isolator including first to n-th elastic member groups and/or an n+1-th elastic member group, the first to n-th elastic member groups and/or the n+1-th elastic member group being located on an xy plane of an xyz coordinate system, and an xy coordinate system of the xyz coordinate system being a coordinate system obtained by, when a tensor of inertia I with respect to an XYZ coordinate system having an origin in a center of gravity of a vibration sensing side structure or a vibration source side structure is represented as I, rotating an XY coordinate system by ?=tan?1(2IXY/(IXX?IYY)) around a Z axis, the adjusting method including, when rigidity Ki of the first to n-th elastic member groups is represented as [ K i ] = [ k i ? _ ? xx 0 0 0 k i ? _ ? yy 0 0 0 k i ? _ ? zz ] , rigidity Kn+1 of the n+1-th elastic member group is represented as [ K n + 1
    Type: Grant
    Filed: July 25, 2017
    Date of Patent: March 30, 2021
    Assignee: Japan Aerospace Exploration Agency
    Inventors: Yasutoshi Hyakusoku, Takafumi Kajikawa, Qinzhong Shi, Daichi Todaka
  • ADJUSTING METHOD AND ADJUSTING SYSTEM FOR RESONANCE FREQUENCY OF VIBRATION ISOLATOR, VIBRATION ISOLATOR, AND DESIGNING METHOD, DESIGNING SYSTEM, AND MANUFACTURING METHOD FOR VIBRATION ISOLATOR
    Publication number: 20190170209
    Abstract: Provided is an adjusting method for a resonance frequency of a vibration isolator, the vibration isolator including first to n-th elastic member groups and/or an n+1-th elastic member group, the first to n-th elastic member groups and/or the n+1-th elastic member group being located on an xy plane of an xyz coordinate system, and an xy coordinate system of the xyz coordinate system being a coordinate system obtained by, when a tensor of inertia I with respect to an XYZ coordinate system having an origin in a center of gravity of a vibration sensing side structure or a vibration source side structure is represented as I, rotating an XY coordinate system by ?=tan?1(2IXY/(IXX?IYY)) around a Z axis, the adjusting method including, when rigidity Ki of the first to n-th elastic member groups is represented as [ K i ] = [ k i ? _ ? xx 0 0 0 k i ? _ ? yy 0 0 0 k i ? _ ? zz ] , rigidity Kn+1 of the n+1-th elastic member group is represented as [ K n + 1 ]
    Type: Application
    Filed: July 25, 2017
    Publication date: June 6, 2019
    Applicant: Japan Aerospace Exploration Agency
    Inventors: Yasutoshi HYAKUSOKU, Takafumi KAJIKAWA, Qinzhong SHI, Daichi TODAKA