Patents by Inventor Hidemi Kurita

Hidemi Kurita 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: 10704526
    Abstract: Through dividing all blades into four or more blade groups including a certain number, which is three or more, of the blades, the blade located in the rearmost portion of each blade group in a direction of rotation is selected as a main blade, and remaining blades are selected as auxiliary blades, the length of each of the auxiliary blades is set to be shorter than the length of the main blade, and corresponding inner edge portions are positioned to the front, in the direction of rotation, of a normal line that passes through an outer edge portion of the blade, and an extension line of a chord line that connects the outer edge portion and the inner edge portion of the blade to one another are made to intersect with the main blade that is adjacent to the front in the direction of rotation.
    Type: Grant
    Filed: June 22, 2016
    Date of Patent: July 7, 2020
    Inventor: Hidemi Kurita
  • Patent number: 10072608
    Abstract: The displacer 2d . . . has a gas retention space Hg . . . formed therein. The gas retention space Hg . . . enables a working gas G to be alternately moved between a heating unit 3h side and a cooling unit 3c side of a displacer cylinder 2c . . . by the movement of the displacer 2d . . . . The displacer 2d . . . and the displacer cylinder 2c . . . have an outer circumferential surface 2df and an inner circumferential surface 2ci, respectively, formed into such shapes as to be able to permit the movement of the displacer 2d . . . and inhibit passage of the working gas G. The displacer 2d . . . has a gas passageway 7 which is formed on its outer circumferential surface 2df and includes a gas passage groove that allows the gas retention space Hg to communicate with a working gas inlet/outlet 6 . . . provided in the displacer cylinder 2c . . . and connected to a power cylinder 5c.
    Type: Grant
    Filed: April 13, 2015
    Date of Patent: September 11, 2018
    Inventors: Hidemi Kurita, Masanori Shimizu
  • Publication number: 20180180018
    Abstract: Through dividing all blades into four or more blade groups including a certain number, which is three or more, of the blades, the blade located in the rearmost portion of each blade group in a direction of rotation is selected as a main blade, and remaining blades are selected as auxiliary blades, the length of each of the auxiliary blades is set to be shorter than the length of the main blade, and corresponding inner edge portions are positioned to the front, in the direction of rotation, of a normal line that passes through an outer edge portion of the blade, and an extension line of a chord line that connects the outer edge portion and the inner edge portion of the blade to one another are made to intersect with the main blade that is adjacent to the front in the direction of rotation.
    Type: Application
    Filed: June 22, 2016
    Publication date: June 28, 2018
    Inventor: Hidemi KURITA
  • Publication number: 20170045018
    Abstract: The displacer 2d . . . has a gas retention space Hg . . . formed therein. The gas retention space Hg . . . enables a working gas G to be alternately moved between a heating unit 3h side and a cooling unit 3c side of a displacer cylinder 2c . . . by the movement of the displacer 2d . . . . The displacer 2d . . . and the displacer cylinder 2c . . . have an outer circumferential surface 2df and an inner circumferential surface 2ci, respectively, formed into such shapes as to be able to permit the movement of the displacer 2d . . . and inhibit passage of the working gas G. The displacer 2d . . . has a gas passageway 7 which is formed on its outer circumferential surface 2df and includes a gas passage groove that allows the gas retention space Hg to communicate with a working gas inlet/outlet 6 . . . provided in the displacer cylinder 2c . . . and connected to a power cylinder 5c.
    Type: Application
    Filed: April 13, 2015
    Publication date: February 16, 2017
    Inventors: Hidemi KURITA, Masanori SHIMIZU
  • Publication number: 20150148508
    Abstract: A (meth)acrylic resin composition comprising not less than 99.5% by mass of (meth)acrylic resin composed of 80 to 100% by mass of a structural unit derived from methyl methacrylate and 0 to 20% by mass of a structural unit derived from acrylic acid ester, wherein a difference between YI4 and YI1 is not more than 3, in which the YI4 is a yellowness index at optical path length 200 mm of an article obtained by injection molding of the (meth)acrylic resin composition at a cylinder temperature of 280° C. and a molding cycle of 4 minutes, and the YI1 is a yellowness index at optical path length 200 mm of an article obtained by injection molding of the (meth)acrylic resin composition at a cylinder temperature of 280° C. and a molding cycle of 1 minute; and the (meth)acrylic resin composition has a melt flow rate under conditions of 230° C. and 3.8 kg load of not less than 25 g/10 min.
    Type: Application
    Filed: April 22, 2013
    Publication date: May 28, 2015
    Applicant: KURARAY CO., LTD.
    Inventors: Takuro Niimura, Hiroyuki Konishi, Hiroshi Ozawa, Hidemi Kurita, Hideyuki Tamura
  • Publication number: 20150126697
    Abstract: A (meth)acrylic resin composition comprising 99.5% by mass or more of a (meth)acrylic resin composed of 80 to 100% by mass of a structural unit derived from methyl methacrylate and 0 to 20% by mass of a structural unit derived from an acrylic acid ester, wherein the (meth)acrylic resin composition has the rate of loss on heat of 0.5%/minute or less in a nitrogen atmosphere at 300° C., and the melt flow rate of 10 g/10 minutes or more under conditions of 230° C. and 3.8 kg load.
    Type: Application
    Filed: April 22, 2013
    Publication date: May 7, 2015
    Applicant: KURARAY CO., LTD.
    Inventors: Takuro Niimura, Hiroyuki Konishi, Hiroshi Ozawa, Hidemi Kurita, Hideyuki Tamura
  • Patent number: 7094017
    Abstract: A vertical shaft driving device wherein a plurality of rotary blades (8a, 8b, 8c and 8d) each including a blade (10) supported on a planetary shaft are equally arranged circumferentially of a central shaft (12) and capable of orbital motion integrally with the central shaft (12), and wherein the rotary blades are arranged in a multipoint intersection form, in which blade faces of the blades (10) are obliquely disposed with respect to radial directions with a center at the central shaft (12). By arranging the blades (10) in the multipoint intersection form, it is possible to provide the vertical shaft driving device, in which air flows or water flows can be efficiently utilized to obtain a great output power.
    Type: Grant
    Filed: May 14, 2003
    Date of Patent: August 22, 2006
    Inventor: Hidemi Kurita
  • Publication number: 20050079054
    Abstract: A vertical shaft driving device wherein a plurality of rotary blades (8a, 8b, 8c and 8d) each including a blade (10) supported on a planetary shaft are equally arranged circumferentially of a central shaft (12) and capable of orbital motion integrally with the central shaft (12), and wherein the rotary blades are arranged in a multipoint intersection form, in which blade faces of the blades (10) are obliquely disposed with respect to radial directions with a center at the central shaft (12). By arranging the blades (10) in the multipoint intersection form, it is possible to provide the vertical shaft driving device, in which air flows or water flows can be efficiently utilized to obtain a great output power.
    Type: Application
    Filed: May 14, 2003
    Publication date: April 14, 2005
    Inventor: Hidemi Kurita