Patents by Inventor Seok Beom Kim
Seok Beom Kim 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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Patent number: 11967440Abstract: A paste for a reference electrode according to an embodiment of the present disclosure includes silver chloride powder and a carbon-based conductive material. The carbon-based conductive material may include at least one compound selected from the group consisting of carbon nanotubes, graphite, graphene, and carbon black. The reference electrode formed of the paste for a reference electrode according to an exemplary embodiment may provide improved mechanical properties and electrochemical properties.Type: GrantFiled: May 3, 2022Date of Patent: April 23, 2024Assignee: I-SENS, INC.Inventors: Young Jea Kang, In Seok Jeong, Chul Hyun Park, Suk Joon Kim, Yoon Beom Park
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Publication number: 20240088952Abstract: The present disclosure discloses beamforming methods and apparatuses. According to an exemplary embodiment of the present disclosure, an antenna message generation deep neural network (DNN) and a beam characteristic generation DNN of a bipartite graph neural network (BGNN) having terminals as vertices on one side and APs as vertices on another side may be constructed.Type: ApplicationFiled: August 30, 2023Publication date: March 14, 2024Applicant: ELECTRONICS AND TELECOMMUNICATIONS RESEARCH INSTITUTEInventors: Seung Eun HONG, Jun Beom KIM, Seok Hwan PARK, Hoon LEE
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Patent number: 11920496Abstract: Disclosed herein are an airfoil, and a turbine blade and gas turbine including the same. The airfoil includes a first cooling passage allowing a first cooling fluid introduced from the bottom of a leading edge to flow into a first serpentine channel formed on a pressure side, and to be then discharged to the rear of a trailing edge, and a second cooling passage allowing a second cooling fluid introduced from the bottom of a suction side to be divided and flow into at least two second serpentine channels formed on the suction side, and allowing the divided cooling fluids introduced into the at least two second serpentine channels to be joined at the bottom thereof and to be then discharged to the rear of the trailing edge.Type: GrantFiled: September 12, 2023Date of Patent: March 5, 2024Assignee: DOOSAN ENERBILITY CO., LTD.Inventors: Ki Baek Kim, Seok Beom Kim
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Patent number: 11668195Abstract: The present technique presents a gas turbine blade for re-using cooling air, a turbomachine assembly having the blade, and a gas turbine having the turbomachine assembly. The blade includes a platform and an airfoil extending from the platform. The airfoil includes a pressure surface, a suction surface, a leading edge and a trailing edge. The platform includes a pressure side, a suction side, a leading-edge side and a trailing-edge side, disposed towards the pressure surface, the suction surface, the leading edge and the trailing edge of the airfoil, respectively. The suction side of the platform includes a part of the upper surface and a suction-side lateral surface of the platform. At least a part of an edge between the suction-side lateral surface and the upper surface of the platform comprises a chamfer part.Type: GrantFiled: January 15, 2021Date of Patent: June 6, 2023Assignee: DOOSAN ENERBILITY CO., LTD.Inventors: Herbert Brandl, Willy H. Hofmann, Joerg Krueckels, Ulrich Rathmann, Seok Beom Kim
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Publication number: 20210277781Abstract: The present technique presents a gas turbine blade for re-using cooling air, a turbomachine assembly having the blade, and a gas turbine having the turbomachine assembly. The blade includes a platform and an airfoil extending from the platform. The airfoil includes a pressure surface, a suction surface, a leading edge and a trailing edge. The platform includes a pressure side, a suction side, a leading-edge side and a trailing-edge side, disposed towards the pressure surface, the suction surface, the leading edge and the trailing edge of the airfoil, respectively. The suction side of the platform includes a part of the upper surface and a suction-side lateral surface of the platform. At least a part of an edge between the suction-side lateral surface and the upper surface of the platform comprises a chamfer part.Type: ApplicationFiled: January 15, 2021Publication date: September 9, 2021Inventors: Herbert BRANDL, Willy H. Hofmann, Joerg Krueckels, Ulrich Rathmann, Seok Beom Kim
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Patent number: 11008874Abstract: A turbine blade includes a root to be mounted to a rotor; a platform having an inner side and an outer side, the inner side being coupled to the root; an airfoil extending from the outer side of the platform in a radial direction of the rotor and including an outer end on which a blade tip is formed; a protrusion formed in the blade tip; and a blade cooling passage that is formed inside the airfoil and communicates with an exit hole formed in the blade tip, the blade cooling passage to pass cooling fluid through the airfoil such that the cooling fluid exits the airfoil through the exit hole. The protrusion includes an outer side surface that is flush with an outer end surface of the airfoil and protrudes in a direction perpendicular to the radial direction to prevent hot combustion gas from invading the blade cooling passage.Type: GrantFiled: April 25, 2019Date of Patent: May 18, 2021Inventor: Seok Beom Kim
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Publication number: 20190338653Abstract: A turbine blade includes a root to be mounted to a rotor; a platform having an inner side and an outer side, the inner side being coupled to the root; an airfoil extending from the outer side of the platform in a radial direction of the rotor and including an outer end on which a blade tip is formed; a protrusion formed in the blade tip; and a blade cooling passage that is formed inside the airfoil and communicates with an exit hole formed in the blade tip, the blade cooling passage to pass cooling fluid through the airfoil such that the cooling fluid exits the airfoil through the exit hole. The protrusion includes an outer side surface that is flush with an outer end surface of the airfoil and protrudes in a direction perpendicular to the radial direction to prevent hot combustion gas from invading the blade cooling passage.Type: ApplicationFiled: April 25, 2019Publication date: November 7, 2019Inventor: Seok Beom Kim
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Patent number: 10378361Abstract: A gas turbine blade according to an embodiment of the present invention includes a turbine blade provided in a gas turbine; and a plurality of film coolers formed in a section from a leading edge to a trailing edge of the turbine blade, in which the film cooler includes a cooling channel through which cooling air is introduced and formed in an oval shape; and an outlet through which the cooling air passing through the cooling channel is discharged and extending from an extended end of the cooling channel toward an outer side thereof and formed in an oval shape.Type: GrantFiled: August 16, 2017Date of Patent: August 13, 2019Assignee: Doosan Heavy Industries Construction Co., LtdInventors: Ki Don Lee, Seok Beom Kim
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Patent number: 10132832Abstract: A method for manufacturing a microcantilever having a cantilever and a functional probe provided on the cantilever may include steps of: providing a probe mold which accommodates a liquid probe solution in which quantum dots for the functional probe are mixed, and has a groove corresponding to the shape of the functional probe; bringing a cantilever into contact with the probe mold on which the groove is formed to correspond to the location of the functional probe; forming the functional probe on the cantilever by curing the probe solution accommodated in the groove in a state where the cantilever contacts the probe mold; and separating the cantilever from the probe mold.Type: GrantFiled: April 1, 2016Date of Patent: November 20, 2018Assignee: INDUSTRY-UNIVERSITY COOPERATION FOUNDATION SOGANG UNIVERSITYInventors: Jung Chul Lee, Seok Beom Kim, Jae Seol Lee
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Publication number: 20180143222Abstract: A method for manufacturing a microcantilever having a cantilever and a functional probe provided on the cantilever may include steps of: providing a probe mold which accommodates a liquid probe solution in which quantum dots for the functional probe are mixed, and has a groove corresponding to the shape of the functional probe; bringing a cantilever into contact with the probe mold on which the groove is formed to correspond to the location of the functional probe; forming the functional probe on the cantilever by curing the probe solution accommodated in the groove in a state where the cantilever contacts the probe mold; and separating the cantilever from the probe mold.Type: ApplicationFiled: April 1, 2016Publication date: May 24, 2018Inventors: Jung Chul LEE, Seok Beom KIM, Jae Seol LEE
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Publication number: 20180051570Abstract: A gas turbine blade according to an embodiment of the present invention includes a turbine blade provided in a gas turbine; and a plurality of film coolers formed in a section from a leading edge to a trailing edge of the turbine blade, in which the film cooler includes a cooling channel through which cooling air is introduced and formed in an oval shape; and an outlet through which the cooling air passing through the cooling channel is discharged and extending from an extended end of the cooling channel toward an outer side thereof and formed in an oval shape.Type: ApplicationFiled: August 16, 2017Publication date: February 22, 2018Inventors: Ki Don Lee, Seok Beom Kim
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Patent number: 7160820Abstract: There is provided a process for preparing a composite material of an oxide crystal film and a substrate by forming a Y123 type oxide crystal film from a solution phase on a substrate using a liquid phase method, wherein problems such as cracking of the oxide crystal film, separation of the oxide crystal film from the substrate, and development of a reaction layer between the substrate and the solution can be minimized. The solvent for forming the solution phase uses either a BaO—CuO—BaF2 system or a BaO—CuO—Ag—BaF2 system, and when the substrate with a seed crystal film bonded to the surface is brought in contact with the solution to form (grow) the oxide crystal film on the substrate, the temperature of the solution is controlled to a temperature of no more than 850° C.Type: GrantFiled: May 15, 2002Date of Patent: January 9, 2007Assignees: International Superconductivity Technology Center, the Juridical Foundation, Fujikura Ltd.Inventors: Toshihiro Suga, Yasuji Yamada, Toshihiko Maeda, Seok Beom Kim, Haruhiko Kurosaki, Yutaka Yamada, Izumi Hirabayashi, Yasuhiro Iijima, Tomonori Watanabe, Hisashi Yoshino, Koji Muranaka
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Publication number: 20040214450Abstract: There is provided a process for preparing a composite material of an oxide crystal film and a substrate by forming a Y123 type oxide crystal film from a solution phase on a substrate using a liquid phase method, wherein problems such as cracking of the oxide crystal film, separation of the oxide crystal film from the substrate, and development of a reaction layer between the substrate and the solution can be minimized. The solvent for forming the solution phase uses either a BaO—CuO—BaF2 system or a BaO—CuO—Ag—BaF2 system, and when the substrate with a seed crystal film bonded to the surface is brought in contact with the solution to form (grow) the oxide crystal film on the substrate, the temperature of the solution is controlled to a temperature of no more than 850° C.Type: ApplicationFiled: June 7, 2004Publication date: October 28, 2004Inventors: Toshihiro Suga, Yasuji Yamada, Toshihiko Maeda, Seok Beom Kim, Haruhiko Kurosaki, Yutaka Yamada, Izumi Hirabayashi, Yasuhiro Iijima, Tomonori Watanabe, Hisashi Yoshino, Koji Muranaka