Patents by Inventor Masanobu Fujimura

Masanobu Fujimura 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: 10829249
    Abstract: 1. A satellite constellation forming method comprises a satellite deployment step S2, a spacecraft acceleration step S4, a spacecraft orbiting step S5 and spacecraft deceleration step, and the aforementioned steps are repeated in order. In the satellite deployment step S2, deploying one of the satellites into the circular orbit 2 from the spacecraft 10 on the circular orbit 2. In the spacecraft acceleration step S4, accelerating the spacecraft 10 and switching the orbit from the circular orbit 2 to a spacecraft transfer orbit 3 in the same orbit plane. In the spacecraft orbiting step S5, making the spacecraft 10 orbit along the spacecraft transfer orbit 3 a plurality of times. In the spacecraft deceleration step, decelerating the spacecraft 10 and switching the orbit from the spacecraft transfer orbit 3 to the circular orbit 2 in the same orbit plane.
    Type: Grant
    Filed: April 18, 2016
    Date of Patent: November 10, 2020
    Assignee: IHI AEROSPACE CO., LTD.
    Inventors: Junichi Amimoto, Masanobu Fujimura
  • Publication number: 20180370658
    Abstract: 1. A satellite constellation forming method comprises a satellite deployment step S2, a spacecraft acceleration step S4, a spacecraft orbiting step S5 and spacecraft deceleration step, and the aforementioned steps are repeated in order. In the satellite deployment step S2, deploying one of the satellites into the circular orbit 2 from the spacecraft 10 on the circular orbit 2. In the spacecraft acceleration step S4, accelerating the spacecraft 10 and switching the orbit from the circular orbit 2 to a spacecraft transfer orbit 3 in the same orbit plane. In the spacecraft orbiting step S5, making the spacecraft 10 orbit along the spacecraft transfer orbit 3 a plurality of times. In the spacecraft deceleration step, decelerating the spacecraft 10 and switching the orbit from the spacecraft transfer orbit 3 to the circular orbit 2 in the same orbit plane.
    Type: Application
    Filed: April 18, 2016
    Publication date: December 27, 2018
    Inventors: Junichi Amimoto, Masanobu Fujimura
  • Patent number: 10029807
    Abstract: A spacecraft 10 includes wings 11 or an airframe 12 which generates lift in an atmosphere 2, a thruster 14 which accelerates or decelerates rotating speed in an orbit, an attitude controller 16 which controls an attitude of the airframe 12, and an orbital plane controller 18 which controls the orbital plane change. The orbital plane controller causes the spacecraft 10 to enter the earth's atmosphere 2 within a pre-change orbital plane Fb (A?B?C), changes the orbital plane by using the lift of the wings 11 or airframe 12 in the earth's atmosphere 2 (C?D?E), and then lifts the spacecraft 10 up to the post-change orbital altitude (E?F).
    Type: Grant
    Filed: May 19, 2016
    Date of Patent: July 24, 2018
    Assignee: IHI AEROSPACE CO., LTD.
    Inventors: Masanobu Fujimura, Fumitaka Sugimura, Junichi Amimoto, Tetsuya Takada, Hirotake Morisaki
  • Publication number: 20160376034
    Abstract: A spacecraft 10 includes wings 11 or an airframe 12 which generates lift in an atmosphere 2, a thruster 14 which accelerates or decelerates rotating speed in an orbit, an attitude controller 16 which controls an attitude of the airframe 12, and an orbital plane controller 18 which controls the orbital plane change. The orbital plane controller causes the spacecraft 10 to enter the earth's atmosphere 2 within a pre-change orbital plane Fb (A?B?C), changes the orbital plane by using the lift of the wings 11 or airframe 12 in the earth's atmosphere 2 (C?D?E), and then lifts the spacecraft 10 up to the post-change orbital altitude (E?F).
    Type: Application
    Filed: May 19, 2016
    Publication date: December 29, 2016
    Inventors: Masanobu Fujimura, Fumitaka Sugimura, Junichi Amimoto, Tetsuya Takada, Hirotake Morisaki