Patents by Inventor Kazuyuki Oguri

Kazuyuki Oguri 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).

  • Publication number: 20190018029
    Abstract: An automatic analyzer provided with a probe provided with an opening end for discharging a dispensing liquid, a pump connected to a side opposite to the opening end of the probe, and a dispensing mechanism provided with a drive control unit which controls drive of the pump, in which the drive control unit controls the drive of the pump to realize a discharging speed at which a droplet of the dispensing liquid is formed at the opening end of the probe at an initial stage of discharge drive and a discharging speed at which a liquid column of the dispensing liquid is formed at the opening end of the probe at a later stage of the discharge drive at the time of the discharge drive of the pump to discharge a predetermined amount of dispensing liquid into a dispensing container from the opening end of the probe.
    Type: Application
    Filed: December 8, 2016
    Publication date: January 17, 2019
    Inventors: Takeshi Muranaka, Mizuki Nakamura, Kazuyuki Oguri, Narihito Ishihara
  • Patent number: 9835639
    Abstract: The gripping mechanism is a gripping mechanism for gripping a cuvette T, the gripping mechanism comprising: a sandwiching section 50 for holding the cuvette T in a laterally sandwiching manner; a pressing section 60 for pressing downward an upper end surface of the cuvette T held in a sandwiching manner by the sandwiching section 50, wherein the pressing section 60 is arranged such that, with the cuvette T being held in a sandwiching manner by the sandwiching section 50, a central axis of the cuvette T along a vertical direction coincides mutually with a central axis of the pressing section 60 in the vertical direction.
    Type: Grant
    Filed: November 25, 2015
    Date of Patent: December 5, 2017
    Assignees: FUJIREBIO INC., JEOL LTD.
    Inventors: Kazuyuki Oguri, Tomohiro Endo, Toshiaki Ohtake, Hidenobu Kawada, Takahiro Matsumoto
  • Patent number: 9709502
    Abstract: A measurement device that includes a plurality of lines for conveying a reaction container containing a sample and measures a predetermined material included in the sample while conveying the reaction container by the plurality of lines, wherein the plurality of lines include: a first reaction line for conveying a reaction container at a first convey speed; a second reaction line for conveying a reaction container at a second convey speed; and a measurement line for measuring a predetermined material included in a sample reacted with a reagent within the reaction container in the first reaction line and a sample reacted with a reagent within the reaction container in the second reaction line, the measurement line conveying the reaction containers at a third convey speed that is higher than the first convey speed and the second convey speed.
    Type: Grant
    Filed: February 14, 2012
    Date of Patent: July 18, 2017
    Assignee: Fujirebio Inc.
    Inventors: Kazuyuki Oguri, Tomohiro Endo, Hidenobu Kawada, Yasushi Kondo, Takeshi Muranaka
  • Publication number: 20160154017
    Abstract: [PROBLEMS] It is an object to provide a gripping mechanism that enables inhibition of possible static electricity and contamination in a gripping object such as a reaction container, while enabling the orientation of the gripping object to be stabilized. [MEANS TO SOLVE PROBLEMS] The gripping mechanism is a gripping mechanism for gripping a cuvette T, the gripping mechanism comprising: a sandwiching section 50 for holding the cuvette T in a laterally sandwiching manner; a pressing section 60 for pressing downward an upper end surface of the cuvette T held in a sandwiching manner by the sandwiching section 50, wherein the pressing section 60 is arranged such that, with the cuvette T being held in a sandwiching manner by the sandwiching section 50, a central axis of the cuvette T along a vertical direction coincides mutually with a central axis of the pressing section 60 in the vertical direction.
    Type: Application
    Filed: November 25, 2015
    Publication date: June 2, 2016
    Applicants: FUJIREBIO INC., JEOL LTD.
    Inventors: Kazuyuki OGURI, Tomohiro ENDO, Toshiaki OHTAKE, Hidenobu KAWADA, Takahiro MATSUMOTO
  • Patent number: 9156539
    Abstract: An aircraft window member includes film made of acrylic resin, a conductive mesh, which is formed on the film and in which a conductive material, is formed in a mesh shape so as to have optical transparency for ensuring visibility and to have electromagnetic-wave shielding properties, and a window main body, which is made of acrylic resin, and to which the film on which the conductive mesh is formed is attached.
    Type: Grant
    Filed: February 18, 2008
    Date of Patent: October 13, 2015
    Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
    Inventors: Kazuyuki Oguri, Katsuto Okada
  • Patent number: 8678320
    Abstract: An aircraft fuel tank that is capable of suppressing the occurrence of sparks on a pipe caused by a lightning current through the pipe during a lightning strike, and also suppressing static electricity charging of a pipe caused by flow electrification generated by the fuel. An aircraft fuel tank (1) in which a storage section is formed using a conductive upper skin (5), a conductive lower skin (7) and conductive spars (9), the tank comprising: pipes inside the tank, such as a refuel pipe (17), an engine feed pipe (19) and an inert gas pipe (21), which are disposed inside the storage section and are earthed (27) at a plurality of locations, and pipe outer surface layers (31) having semiconductor properties that are formed in an integrated manner on the outer surfaces of the pipes inside the tank such as the replenishing pipe (17), the supply pipe (19) and the gas pipe (21).
    Type: Grant
    Filed: June 24, 2009
    Date of Patent: March 25, 2014
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Hiroaki Yamaguchi, Yuichiro Kamino, Tooru Hashigami, Kazuyuki Oguri
  • Patent number: 8651413
    Abstract: A lightning-protection fastener is provided that is capable of reliably preventing peeling off of an insulation layer during the operation of an aircraft and improving the anti-lightning-strike capability and reliability. There is a lightning-protection fastener that fastens a skin of an aircraft and a structural member positioned inside the skin, in which an insulation layer is melt adhered so as to cover one end surface of a head portion and also to mechanically engage with a fastener-side engagement portion (engagement portion) formed on the end surface.
    Type: Grant
    Filed: September 25, 2008
    Date of Patent: February 18, 2014
    Assignee: Mitsubishi Heavy Industries
    Inventors: Masahiro Kashiwagi, Yuichiro Kamino, Kazuyuki Oguri, Takeyasu Tarumi, Masahiro Bessho, Hideo Yamakoshi, Naomoto Ishikawa
  • Publication number: 20130323758
    Abstract: A measurement device that includes a plurality of lines for conveying a reaction container containing a sample and measures a predetermined material included in the sample while conveying the reaction container by the plurality of lines, wherein the plurality of lines include: a first reaction line for conveying a reaction container at a first convey speed; a second reaction line for conveying a reaction container at a second convey speed; and a measurement line for measuring a predetermined material included in a sample reacted with a reagent within the reaction container in the first reaction line and a sample reacted with a reagent within the reaction container in the second reaction line, the measurement line conveying the reaction containers at a third convey speed that is higher than the first convey speed and the second convey speed.
    Type: Application
    Filed: February 14, 2012
    Publication date: December 5, 2013
    Applicant: Fujirebio Inc.
    Inventors: Kazuyuki Oguri, Tomohiro Endo, Hidenobu Kawada, Yasushi Kondo, Takeshi Muranaka
  • Patent number: 8550403
    Abstract: An aircraft fuel tank capable of suppressing electrostatic charging caused, for example, by flow electrification with the fuel. The aircraft fuel tank comprises an upper skin (5) and a lower skin (7) that exhibit conductivity and form a portion of a container for storing fuel, an internal structure (19) formed from a metal, and an inner surface layer (15) which has semiconductor properties or insulating properties and is formed in an integral manner on the inner surfaces of the upper skin (5) and the lower skin (7) in a location where the internal structure (19) contacts the upper skin (5) and the lower skin (7), and in the surrounding portion thereof, wherein the inner surface layer (15) is formed, at least in the surrounding portion, from a material having semiconductor properties.
    Type: Grant
    Filed: March 26, 2010
    Date of Patent: October 8, 2013
    Assignees: Mitsubishi Heavy Industries, Ltd., The Society of Japanese Aerospace Companies
    Inventors: Hiroaki Yamaguchi, Yuichiro Kamino, Tooru Hashigami, Kazuyuki Oguri, Koichi Nakamura
  • Patent number: 8482897
    Abstract: An aircraft assembly having improved durability and capable of providing good lightning protection is provided. Provided is an aircraft assembly (1) equipped with an outer panel (5) that is constructed using an outer-panel resin material reinforced with fiber as a main element; a structural member (7) that supports the outer panel (5) from the inside; and a fastener (3) that joins the outer panel (5) and the structural member (7), the aircraft assembly including an insulator layer (23) having insulating properties and disposed so as to cover at least the head (17) of the fastener (3); and a conductor layer (25) disposed so as to cover at least the insulator layer (23) and formed of a conductor-layer resin material containing copper powder having electrical conductivity.
    Type: Grant
    Filed: May 14, 2008
    Date of Patent: July 9, 2013
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Kazuyuki Oguri, Takahiro Sekigawa
  • Publication number: 20130152821
    Abstract: Provided is a coating material that can prevent galvanic corrosion and is resistant to electrostatic charging. An antistatic coating comprising a primer containing either an inorganic fiber comprising Si, Ti or Zr, C, and O, or an Ag filler. Further, a structure made of a composite material which is resistant to galvanic corrosion and electrostatic charging is obtained by applying the antistatic coating containing either an inorganic fiber comprising Si, Ti or Zr, C, and O, or an Ag filler to the surface of the structure made of a composite material to form a layers.
    Type: Application
    Filed: June 30, 2011
    Publication date: June 20, 2013
    Inventors: Yuichiro Kamino, Kazuyuki Oguri, Hiroaki Yamaguchi
  • Patent number: 8413929
    Abstract: An aircraft assembly is equipped with a lightning protection structure that is not easily destroyed by lightning current and that is highly reliable. The aircraft assembly includes a skin in which a CFRP layer serves as a main structure, a shear-tie that supports the skin from the inside, and a fastener that couples the skin and the shear-tie. A copper foil and an outside GRFP layer are provided on an outer surface side of the skin, in this order towards the outside, and a copper paint layer, which contains copper powder, is provided on the outside GFRP layer.
    Type: Grant
    Filed: March 23, 2009
    Date of Patent: April 9, 2013
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Yuichiro Kamino, Kazuyuki Oguri, Koichi Nakamura
  • Patent number: 8363375
    Abstract: An aircraft assembly having improved durability and capable of providing good lightning protection is provided. Provided is an aircraft assembly (1) equipped with an outer panel (5) that is constructed using an outer-panel resin material reinforced with fiber as a main element; a structural member (7) that supports the outer panel (5) from the inside; and a fastener (3) that joins the outer panel (5) and the structural member (7), the aircraft assembly including an insulator layer (23) having insulating properties and disposed so as to cover at least the head (17) of the fastener (3); and a conductor layer (25) disposed so as to cover at least the insulator layer (23) and formed of a conductor-layer resin material containing copper powder having electrical conductivity.
    Type: Grant
    Filed: May 14, 2008
    Date of Patent: January 29, 2013
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Kazuyuki Oguri, Takahiro Sekigawa
  • Patent number: 8323729
    Abstract: A process for producing a metal member that enables both the fatigue properties and the corrosion resistance of the member to be improved, a structural member that includes a thus produced metal member, and a method of repairing a metal member. The process for producing a metal member comprises a projecting particles having an average particle size of not more than 200 ?m onto the surface of a metal material comprising an aluminum alloy using compressed air or a compressed gas, and a chemical conversion treatment including forming a film on the surface of the metal material by performing a chemical conversion treatment following projecting the particles.
    Type: Grant
    Filed: October 2, 2008
    Date of Patent: December 4, 2012
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Akiko Inoue, Takahiro Sekigawa, Kazuyuki Oguri
  • Patent number: 8252130
    Abstract: Surface processing of titanium alloy members for aerospace equipment imparts high wear resistance, lubricity and high fatigue strength. The method includes an oxygen diffusion step for causing oxygen to diffuse and penetrate in solid solution form into a surface of a titanium alloy member under an oxygen-containing gas atmosphere and a particle bombardment step for bombarding the surface of the titanium alloy member with an airflow containing particles. The aerospace equipment can include a flap rail member and slat rail member for aircraft.
    Type: Grant
    Filed: February 16, 2005
    Date of Patent: August 28, 2012
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Kazuyuki Oguri, Takashi Kimura, Takahiro Sekigawa, Takayuki Takahashi
  • Patent number: 8092134
    Abstract: A fastener, of which severe strength is demanded and which can also be applied to a location, in which a flush surface equipment is taken into consideration, and which can be manufactured readily and quickly and reduced in manufacturing cost, is provided. A fastener (1) joins a skin of an airplane and a structural material positioned inside the skin and one end surface of a flush head (3) is covered by an insulator layer (5).
    Type: Grant
    Filed: June 11, 2007
    Date of Patent: January 10, 2012
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Kazuyuki Oguri, Yuichiro Kamino
  • Publication number: 20110297790
    Abstract: An aircraft fuel tank capable of suppressing electrostatic charging caused, for example, by flow electrification with the fuel. The aircraft fuel tank comprises an upper skin (5) and a lower skin (7) that exhibit conductivity and form a portion of a container for storing fuel, an internal structure (19) formed from a metal, and an inner surface layer (15) which has semiconductor properties or insulating properties and is formed in an integral manner on the inner surfaces of the upper skin (5) and the lower skin (7) in a location where the internal structure (19) contacts the upper skin (5) and the lower skin (7), and in the surrounding portion thereof, wherein the inner surface layer (15) is formed, at least in the surrounding portion, from a material having semiconductor properties.
    Type: Application
    Filed: March 26, 2010
    Publication date: December 8, 2011
    Inventors: Hiroaki Yamaguchi, Yuichiro Kamino, Tooru Hashigami, Kazuyuki Oguri, Koichi Nakamura
  • Publication number: 20110297315
    Abstract: Provided is a method for producing, with good workability, a composite having a lightning-resistant layer that exhibits excellent adhesion to a resin-based composite and good fatigue properties. The method for producing a resin-based composite comprises a step of forming a laminate by successively laminating, on a first resin sheet (11) comprising mainly a fiber-reinforced resin, a conductive layer (12) formed from a resin containing a metal powder, and a second resin sheet (13) comprising mainly a fiber-reinforced resin, and a step of forming a resin-based composite (10) by baking the laminate to bond the first resin sheet (11), the conductive layer (12) and the second resin sheet (13).
    Type: Application
    Filed: February 8, 2010
    Publication date: December 8, 2011
    Inventors: Tomone Kishida, Kazuyuki Oguri
  • Publication number: 20110284694
    Abstract: An aircraft fuel tank that is capable of suppressing the occurrence of sparks on a pipe caused by a lightning current through the pipe during a lightning strike, and also suppressing static electricity charging of a pipe caused by flow electrification generated by the fuel. An aircraft fuel tank (1) in which a storage section is formed using a conductive upper skin (5), a conductive lower skin (7) and conductive spars (9), the tank comprising: pipes inside the tank, such as a refuel pipe (17), an engine feed pipe (19) and an inert gas pipe (21), which are disposed inside the storage section and are earthed (27) at a plurality of locations, and pipe outer surface layers (31) having semiconductor properties that are formed in an integrated manner on the outer surfaces of the pipes inside the tank such as the replenishing pipe (17), the supply pipe (19) and the gas pipe (21).
    Type: Application
    Filed: June 24, 2009
    Publication date: November 24, 2011
    Inventors: Hiroaki Yamaguchi, Yuichiro Kamino, Tooru Hashigami, Kazuyuki Oguri
  • Publication number: 20110103999
    Abstract: Provided are a method for forming a metal coating at high speed by using a simple cold spray apparatus, and an aerospace structural member on which a metal coating is formed by the cold spray method. In the metal coating forming method, nonspherical heteromorphous particles made of metal are projected onto a base material surface by the cold spray method to form a metal coating on the base material surface.
    Type: Application
    Filed: August 20, 2009
    Publication date: May 5, 2011
    Inventors: Kazuyuki Oguri, Makoto Senda, Takahiro Sekigawa