Patents by Inventor Yu Shigenari
Yu Shigenari 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: 11826976Abstract: A fiber reinforced plastic (FRP) molding system in which FRP material, having stacked prepregs, is molded to manufacture an arc-shaped FRP component. The FRP molding system comprises inner and outer jig plates, a partial pressing device, and transfer devices. The jig plates are arc-shaped members having outer and inner surfaces that respectively fit with inner and outer surface shapes of the FRP component. The FRP material is sandwiched between the jig plates to form an integrated jig plate. The partial pressing device intermittently compresses a portion of the integrated jig plate in a radial direction orthogonal to an arc of the FRP component so that the FRP component is partially molded. The transfer devices intermittently move the compressed portion of the integrated jig plate by the partial pressing device. By repeating the partial pressing and the transport, the entire integrated jig plate is compressed to form the FRP component.Type: GrantFiled: March 8, 2019Date of Patent: November 28, 2023Assignee: IHI AEROSPACE CO., LTD.Inventors: Takashi Harada, Yu Shigenari, Toyoharu Akimoto
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Publication number: 20230123571Abstract: An FRP material has a circular arc part, and a member fixed to the circular arc part. The FRP forming system has a portion-pressing device, a member positioning mechanism, and a transport device configured to form the FRP material as a single body of a circular arc-shaped FRP part. The FRP material may comprise a single layer prepreg or a plurality of prepregs that have been layered. The portion-pressing device has upper and lower molds sandwiching a portion of the FRP material in a radial direction orthogonal to the circular arc part, and compresses intermittently a portion of the FRP part. The member positioning mechanism locates the position of the member relatively to the upper or lower mold. The transport device moves the portion of the FRP material that is compressed by the portion-pressing device. The portion-pressing and the transport are repeated to form the FRP part.Type: ApplicationFiled: August 31, 2020Publication date: April 20, 2023Applicant: IHI Aerospace Co., Ltd.Inventors: Takashi HARADA, Yu SHIGENARI, Toyoharu AKIMOTO, Ikuo OKUMURA, Shinichi TANAKA
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Publication number: 20220169359Abstract: A joint structure includes a connection member provided between a reinforced member and a reinforcing member and connecting both of them to each other. The connection member includes a first coupling portion and a second coupling portion that are coupled to one and another of the reinforced member and the reinforcing member, respectively. The first coupling portion is coupled to a joint portion of one of the reinforced member and the reinforcing member by an adhesive or welding. The first coupling portion and the joint portion are shaped so as to be caught by each other in a joining direction in which the reinforced member and the reinforcing member are joined to each other.Type: ApplicationFiled: April 12, 2019Publication date: June 2, 2022Applicant: IHI Aerospace Co., Ltd.Inventors: Takashi HARADA, Yu SHIGENARI, Ikuo OKUMURA, Toyoharu AKIMOTO
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Publication number: 20220134688Abstract: Produce prepreg with a matrix resin adhering to the cloth. Arranging a release sheet on each surface of the cloth; passing the cloth and a pair of the release sheets through a gap portion positioned in a clearance of a pair of heating rollers to be overlaid on each other and supplying the matrix resin to be accumulated above the gap portion of the heating rollers and between the pair of release sheets; and adjusting an interval of the pair of heating rollers to thereby control an adhesion amount of the matrix resin.Type: ApplicationFiled: March 27, 2020Publication date: May 5, 2022Applicant: IHI AEROSPACE CO., LTD.Inventors: Hiroyuki SATO, Yu SHIGENARI, Tatsuya KADO, Kazuyuki ORIHARA
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Publication number: 20220009178Abstract: A fiber reinforced plastic (FRP) molding system in which FRP material, having stacked prepregs, is molded to manufacture an arc-shaped FRP component. The FRP molding system comprises inner and outer jig plates, a partial pressing device, and transfer devices. The jig plates are arc-shaped members having outer and inner surfaces that respectively fit with inner and outer surface shapes of the FRP component. The FRP material is sandwiched between the jig plates to form an integrated jig plate. The partial pressing device intermittently compresses a portion of the integrated jig plate in a radial direction orthogonal to an arc of the FRP component so that the FRP component is partially molded. The transfer devices intermittently move the compressed portion of the integrated jig plate by the partial pressing device. By repeating the partial pressing and the transport, the entire integrated jig plate is compressed to form the FRP component.Type: ApplicationFiled: March 8, 2019Publication date: January 13, 2022Applicant: IHI AEROSPACE CO., LTD.Inventors: Takashi HARADA, Yu SHIGENARI, Toyoharu AKIMOTO
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Publication number: 20220001630Abstract: An FRP continuous molding apparatus continuously molds an FRP from a layered sheet that includes prepreg sheets layered over each other. The prepreg sheets each include thermoplastic resin and reinforcement fibers, and differ from each other in fiber orientation. The FRP continuous molding apparatus includes: sheet feeding devices continuously feeding the layered sheets in a feeding direction; a layering device layering, over each other, the layered sheets fed from the sheet feeding devices, and thereby forming a sheet layered body; and a shaping mechanism molding the sheet layered body into an FRP while the sheet layered body is being transferred in the feeding direction. The FRP has a cross section that is a target shape. The sheet layered body includes the reinforcement fibers whose fiber orientation is the feeding direction.Type: ApplicationFiled: March 8, 2019Publication date: January 6, 2022Applicant: IHI AEROSPACE CO., LTD.Inventors: Yu SHIGENARI, Takashi HARADA, Toyoharu AKIMOTO
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Patent number: 9739175Abstract: An additional pad 27 is additionally and integrally arranged from an outer surface of a flange 17 opposite to a contacting side of the flange 17 to a small-diameter curved surface of a bend 19 and from there to an end of an outer surface of a part body 13. On an outer surface side of the additional pad 27, a fastening seat 27f is formed by machining. An area end PAe of a processed area PA formed by machining is positioned on the part body 13 beyond the bend 19.Type: GrantFiled: October 18, 2013Date of Patent: August 22, 2017Assignees: IHI Corporation, IHI AEROSPACE CO., LTD.Inventors: Takashi Harada, Yu Shigenari, Koichi Inagaki, Agamu Tanaka, Tadahiro Ishigure
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Patent number: 9695712Abstract: A boss for attachment of an auxiliary device to a fan case of an engine includes a pedestal including a plurality of accumulated layers of reinforcement fibers and a matrix combining the reinforcement fibers together, the pedestal including a bottom face in a shape capable of being in close contact with an outer periphery of the fan case; and an embedded body embedded in the pedestal and including a combining structure combinable with the auxiliary device.Type: GrantFiled: June 4, 2014Date of Patent: July 4, 2017Assignees: IHI Corporation, IHI AEROSPACE CO., LTD.Inventors: Osamu Otsu, Yu Shigenari, Takashi Harada, Tsutomu Murakami
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Patent number: 9427934Abstract: Each sheet material is formed by arraying carbon fiber lines, each having a predetermined width, in parallel with one another. Meanwhile, an array direction of the carbon fiber lines of each sheet material is set to form an angle in a range from ±30° to ±60° to a weaving advancing direction of a stitching yarn. Moreover, a stretch ratio of the stitched base material in its lengthwise direction in a case where a load per inch width of the stitched base material is applied in the weaving advancing direction of the stitching yarn is equal to or below 4% when the load is 5 N, and is equal to or above 10% when the load is 25 N.Type: GrantFiled: January 15, 2015Date of Patent: August 30, 2016Assignees: IHI Corporation, IHI AEROSPACE CO., LTD.Inventors: Yoshinobu Tsuchiya, Hidetoshi Kasakawa, Masahiko Murata, Yu Shigenari, Hiroyuki Satoh
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Publication number: 20150125651Abstract: Each sheet material is formed by arraying carbon fiber lines, each having a predetermined width, in parallel with one another. Meanwhile, an array direction of the carbon fiber lines of each sheet material is set to form an angle in a range from ±30° to ±60° to a weaving advancing direction of a stitching yarn. Moreover, a stretch ratio of the stitched base material in its lengthwise direction in a case where a load per inch width of the stitched base material is applied in the weaving advancing direction of the stitching yarn is equal to or below 4% when the load is 5 N, and is equal to or above 10% when the load is 25 N.Type: ApplicationFiled: January 15, 2015Publication date: May 7, 2015Applicants: IHI AEROSPACE CO., LTD., IHI CORPORATIONInventors: Yoshinobu TSUCHIYA, Hidetoshi KASAKAWA, Masahiko MURATA, Yu SHIGENARI, Hiroyuki SATOH
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Publication number: 20140286769Abstract: A boss for attachment of an auxiliary device to a fan case of an engine is comprised of a pedestal including a plurality of accumulated layers of reinforcement fibers and a matrix combining the reinforcement fibers together, the pedestal comprising a bottom face in a shape capable of being in close contact with an outer periphery of the fan case; and an embedded body embedded in the pedestal and including a combining structure combinable with the auxiliary device.Type: ApplicationFiled: June 4, 2014Publication date: September 25, 2014Applicants: IHI Corporation, IHI AEROSPACE CO., LTD.Inventors: Osamu OTSU, Yu SHIGENARI, Takashi HARADA, Tsutomu MURAKAMI
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Publication number: 20140044539Abstract: An additional pad 27 is additionally and integrally arranged from an outer surface of a flange 17 opposite to a contacting side of the flange 17 to a small-diameter curved surface of a bend 19 and from there to an end of an outer surface of a part body 13. On an outer surface side of the additional pad 27, a fastening seat 27f is formed by machining. An area end PAe of a processed area PA formed by machining is positioned on the part body 13 beyond the bend 19.Type: ApplicationFiled: October 18, 2013Publication date: February 13, 2014Applicants: IHI AEROSPACE CO., LTD., IHI CorporationInventors: Takashi HARADA, Yu Shigenari, Koichi Inagaki, Agamu Tanaka, Tadahiro Ishigure
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Publication number: 20120219741Abstract: A method for manufacturing a cylindrical structure having an axial direction includes: winding a first layer around a mandrel; winding a second layer around the mandrel; winding a third layer around the mandrel; and joining the layers together by using a resin. Each layer includes a plurality of fabrics each made of fibers. The fabrics of each layer form a join line extending in a circumferential direction with edges of the fabrics in contact with each other. The join lines of the first, second and third layers are displaced in the axial direction from one another.Type: ApplicationFiled: November 5, 2010Publication date: August 30, 2012Applicants: IHI Aerospace Co., Ltd., IHI CorporationInventors: Takashi Harada, Yu Shigenari, Masayori Miyashita, Tsutomu Murakami, Agamu Tanaka
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Publication number: 20120219408Abstract: A method for manufacturing a cylindrical structure having an axial direction includes: winding a fabric around a mandrel in a circumferential direction that is perpendicular to the axial direction, the fabric containing first fibers oriented in a first direction intersecting the circumferential direction; winding a roving into a helical shape around the mandrel, the roving containing second fibers oriented in a longitudinal direction of the roving; and joining the fabric and the roving together by using a resin.Type: ApplicationFiled: November 5, 2010Publication date: August 30, 2012Applicants: IHI AEROSPACE CO., LTD., IHI CORPORATIONInventors: Takashi Harada, Yu Shigenari, Masayori Miyashita, Tsutomu Murakami