Patents by Inventor Masaaki Monte

Masaaki Monte 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: 8866427
    Abstract: When it is determined that the number of times that motor rotation-indicative quantity has been detected has exceeded a measurement interval, a feedback speed value is calculated from a motor rotation-indicative quantity detected immediately before, a motor rotation-indicative quantity detected immediately before the last time a measurement interval determination means determined that the number of times had exceeded the measurement interval, and time that has elapsed since the last time the measurement interval determination means determined that the number of times had exceeded the measurement interval, and the measurement interval having a length calculated from a greater one between the calculated feedback speed value and a speed command value is set for the measurement interval determination means to refer to.
    Type: Grant
    Filed: March 30, 2012
    Date of Patent: October 21, 2014
    Assignees: IHI Aerospace Co., Ltd., Sinfonia Technology Co., Ltd.
    Inventors: Hitoshi Oyori, Masaaki Monte
  • Patent number: 8701400
    Abstract: The present invention is to provide an electro hydrostatic actuator excellent in a snubbing characteristic including a cylinder type actuator main body 1, a piston 2 having a piston rod, the piston slidingly moving in a cylinder of the actuator main body, a motor 18, a pump 19 for supplying fluid according to the rotation of the motor, a mechanism for adjusting a running amount of the fluid into and from the cylinder according to the motion of the piston, and a reservoir 8 for adjusting the supply of the fluid corresponding to a volume difference generated according to the motion of the piston, and a controller 17 which controls the number of revolutions of the motor according to the calculated load torque, and a snubbing control method used for this. An electro hydrostatic actuator of realizing a snubbing mechanism capable of increasing energy efficiency, when used for a landing gear retraction/extension device of an airplane, can be provided.
    Type: Grant
    Filed: November 10, 2010
    Date of Patent: April 22, 2014
    Assignees: Sumitomo Precision Products Co., Ltd., Sinfonia Technology Co., Ltd.
    Inventors: Taku Kondo, Toshiyuki Kumada, Masayuki Takada, Kazuhiro Masutani, Masaaki Monte, Hiroshi Saito, Satoshi Ihara
  • Publication number: 20120256577
    Abstract: When it is determined that the number of times that motor rotation-indicative quantity has been detected has exceeded a measurement interval, a feedback speed value is calculated from a motor rotation-indicative quantity detected immediately before, a motor rotation-indicative quantity detected immediately before the last time a measurement interval determination means determined that the number of times had exceeded the measurement interval, and time that has elapsed since the last time the measurement interval determination means determined that the number of times had exceeded the measurement interval, and the measurement interval having a length calculated from a greater one between the calculated feedback speed value and a speed command value is set for the measurement interval determination means to refer to.
    Type: Application
    Filed: March 30, 2012
    Publication date: October 11, 2012
    Applicants: Sinfonia Technology Co., Ltd., IHI Aerospace Co., Ltd.
    Inventors: Hitoshi Oyori, Masaaki Monte
  • Publication number: 20110107756
    Abstract: The present invention is to provide an electro hydrostatic actuator excellent in a snubbing characteristic including a cylinder type actuator main body 1, a piston 2 having a piston rod, the piston slidingly moving in a cylinder of the actuator main body, a motor 18, a pump 19 for supplying fluid according to the rotation of the motor, a mechanism for adjusting a running amount of the fluid into and from the cylinder according to the motion of the piston, and a reservoir 8 for adjusting the supply of the fluid corresponding to a volume difference generated according to the motion of the piston, and a controller 17 which controls the number of revolutions of the motor according to the calculated load torque, and a snubbing control method used for this. An electro hydrostatic actuator of realizing a snubbing mechanism capable of increasing energy efficiency, when used for a landing gear retraction/extension device of an airplane, can be provided.
    Type: Application
    Filed: November 10, 2010
    Publication date: May 12, 2011
    Applicants: SUMITOMO PRECISION PRODUCTS CO., LTD., SINFONIA TECHNOLOGY CO., LTD.
    Inventors: Taku KONDO, Toshiyuki Kumada, Masayuki Takada, Kazuhiro Masutani, Masaaki Monte, Hiroshi Saito, Satoshi Ihara