Patents by Inventor Minoru TABATA
Minoru TABATA 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).
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Publication number: 20210369453Abstract: To provide an artificial heart valve capable of aiding the functions of the mitral valve of a patient in a minimally invasive manner. An artificial heart valve 1 which includes a valve leaflet securing part 2 and valve leaflets (a first valve leaflet 5 and a second valve leaflet 7), and in which the valve leaflets are connected to the valve leaflet securing part 2 at the top portion of the artificial heart valve 1, the valve leaflets each have a region which narrows in width toward the bottom of the leaflet, and the artificial heart valve is an artificial mitral valve or an artificial tricuspid valve.Type: ApplicationFiled: August 17, 2021Publication date: December 2, 2021Inventor: Minoru TABATA
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Publication number: 20190358034Abstract: To provide an artificial heart valve capable of aiding the functions of the mitral valve of a patient in a minimally invasive manner. An artificial heart valve 1 which includes a valve leaflet securing part 2 and valve leaflets (a first valve leaflet 5 and a second valve leaflet 7), and in which the valve leaflets are connected to the valve leaflet securing part 2 at the top portion of the artificial heart valve 1, the valve leaflets each have a region which narrows in width toward the bottom of the leaflet, and the artificial heart valve is an artificial mitral valve or an artificial tricuspid valve.Type: ApplicationFiled: February 16, 2018Publication date: November 28, 2019Inventor: Minoru TABATA
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Patent number: 9774092Abstract: A deployable antenna reflector includes a surface cable network formed of a plurality of cables coupled to each other in a mesh pattern. The surface cable network includes at least one rigid rod member that reduces a maximum tensile force caused in the surface cable network.Type: GrantFiled: February 8, 2013Date of Patent: September 26, 2017Assignee: NEC Space Technologies, Ltd.Inventors: Kiyoshi Fujii, Minoru Tabata, Kyoji Shintate
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Patent number: 9051983Abstract: In the interior of a brake drum, the arrangement space in the rotational axis direction of the brake drum is spacious in comparison with that in the direction orthogonal to the rotational axis direction in which an anchor portion, hub components on the vehicle body side and the like are arranged. An electric parking brake device is provided with the anchor portion that supports respective one ends of brake shoes. A parking lever is pivotally moved by a drive unit operated by an electric motor for pushing the brake shoes toward the brake drum. The anchor portion and the drive unit are arranged to be piled up in the rotational axis direction of the brake drum which is spacious in comparison with the direction orthogonal to the rotational axis direction.Type: GrantFiled: March 28, 2012Date of Patent: June 9, 2015Assignees: ADVICS CO., LTD., HOSEI BRAKE INDUSTRY CO., LTD.Inventors: Keiichi Tsurumi, Hideyuki Kai, Mitsuyasu Mizuno, Eiji Inaya, Jin Yamada, Hisashi Kobayashi, Minoru Tabata, Kazuhiro Suzuki
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Patent number: 8922456Abstract: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.Type: GrantFiled: January 30, 2012Date of Patent: December 30, 2014Assignees: NEC TOSHIBA Space Systems, Ltd., Japan Aerospace Exploration AgencyInventors: Minoru Tabata, Kiyoshi Fujii, Kyoji Shintate, Satoru Ozawa
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Publication number: 20130207881Abstract: A deployable antenna reflector includes a surface cable network formed of a plurality of cables coupled to each other in a mesh pattern. The surface cable network includes at least one rigid rod member that reduces a maximum tensile force caused in the surface cable network.Type: ApplicationFiled: February 8, 2013Publication date: August 15, 2013Inventors: Kiyoshi FUJII, Minoru TABATA, Kyoji SHINTATE
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Publication number: 20120247895Abstract: In the interior of a brake drum, the arrangement space in the rotational axis direction of the brake drum is spacious in comparison with that in the direction orthogonal to the rotational axis direction in which an anchor portion, hub components on the vehicle body side and the like are arranged. An electric parking brake device is provided with the anchor portion that supports respective one ends of brake shoes. A parking lever is pivotally moved by a drive unit operated by an electric motor for pushing the brake shoes toward the brake drum. The anchor portion and the drive unit are arranged to be piled up in the rotational axis direction of the brake drum which is spacious in comparison with the direction orthogonal to the rotational axis direction.Type: ApplicationFiled: March 28, 2012Publication date: October 4, 2012Applicants: HOSEI BRAKE INDUSTRY CO., LTD., ADVICS CO., LTD.Inventors: Keiichi Tsurumi, Hideyuki Kai, Mitsuyasu Mizuno, Eiji Inaya, Jin Yamada, Hisashi Kobayashi, Minoru Tabata, Kazuhiro Suzuki
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Publication number: 20120193498Abstract: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.Type: ApplicationFiled: January 30, 2012Publication date: August 2, 2012Applicants: JAPAN AEROSPACE EXPLORATION AGENCY, NEC TOSHIBA Space Systems, Ltd.Inventors: Minoru TABATA, Kiyoshi FUJII, Kyoji SHINTATE, Satoru OZAWA