Patents by Inventor Kiwamu ARIKAWA

Kiwamu ARIKAWA 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: 10343761
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.
    Type: Grant
    Filed: August 22, 2018
    Date of Patent: July 9, 2019
    Assignee: MITSUBISHI AIRCRAFT CORPORATION
    Inventors: Kiwamu Arikawa, Masayoshi Suhara, Hiroyuki Iseki, Shuhei Muto
  • Publication number: 20180354604
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.
    Type: Application
    Filed: August 22, 2018
    Publication date: December 13, 2018
    Inventors: Kiwamu Arikawa, Masayoshi Suhara, Hiroyuki Iseki, Shuhei Muto
  • Patent number: 10065727
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.
    Type: Grant
    Filed: March 27, 2014
    Date of Patent: September 4, 2018
    Assignee: MITSUBISHI AIRCRAFT CORPORATION
    Inventors: Kiwamu Arikawa, Masayoshi Suhara, Hiroyuki Iseki, Shuhei Muto
  • Patent number: 9751266
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes a repairing material disposing step of disposing a repairing patch 20 and an adhesive 21A to the repair target portion 14; and a heating-hardening step of heating and hardening the adhesive 21A by irradiating it with electromagnetic waves.
    Type: Grant
    Filed: March 27, 2014
    Date of Patent: September 5, 2017
    Assignee: MITSUBISHI AIRCRAFT CORPORATION
    Inventors: Kiwamu Arikawa, Masayoshi Suhara, Hiroyuki Iseki, Shuhei Muto
  • Publication number: 20160257430
    Abstract: An object of the present invention is to visualize an internal structural members, which are covered with a skin and therefore unrecognizable to the naked eye, from the outside of the skin. There is provided an internal structure visualization method applied to a main wing of an aircraft, which includes a skin with a front surface and a back surface and structural members supporting the skin from the back surface side, to display, when necessary, a trace map composed of lines extending along projection regions of the structural members, wherein functional lines, which are a developing element of the trace map, are provided along the projection regions of the front surface, and the trace map is displayed by performing a predetermined process on a predetermined region of the front surface where the functional lines are provided.
    Type: Application
    Filed: February 11, 2016
    Publication date: September 8, 2016
    Inventors: Shotaro Hayashi, Ryuichi Nagase, Masayoshi Suhara, Hiromu Okamoto, Kiwamu Arikawa, Morimasa Ishida
  • Publication number: 20140290832
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes a repairing material disposing step of disposing a repairing patch 20 and an adhesive 21A to the repair target portion 14; and a heating-hardening step of heating and hardening the adhesive 21A by irradiating it with electromagnetic waves.
    Type: Application
    Filed: March 27, 2014
    Publication date: October 2, 2014
    Applicant: MITSUBISHI AIRCRAFT CORPORATION
    Inventors: Kiwamu ARIKAWA, Masayoshi SUHARA, Hiroyuki ISEKI, Shuhei MUTO
  • Publication number: 20140295125
    Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.
    Type: Application
    Filed: March 27, 2014
    Publication date: October 2, 2014
    Applicant: MITSUBISHI AIRCRAFT CORPORATION
    Inventors: Kiwamu ARIKAWA, Masayoshi SUHARA, Hiroyuki ISEKI, Shuhei MUTO