Patents Assigned to Showa Aircraft Industry Co., Ltd.
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Publication number: 20210221241Abstract: A power transmission coupler void space (20) and a power transmission hose void space (21) are allowed to communicate with each other. A viscous resin (D) is sealed in each of the power transmission coupler void space (20) and the power transmission hose void space (21). A power reception coupler void space (22) and a power reception hose void space (23) are allowed to communicate with each other. A viscous resin (D) is sealed in each of the power reception coupler void space (22) and the power reception hose void space (23).Type: ApplicationFiled: March 10, 2020Publication date: July 22, 2021Applicant: Showa Aircraft Industry Co., Ltd.Inventors: Kitao YAMAMOTO, Hiroshi WATANABE, Masashi MOCHIZUKI, Yasuyuki OKIYONEDA, Atushi WATANABE
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Patent number: 8528710Abstract: A non-contact power feeding device feeds power from a power transmission coil to a power receiving coil based on a mutual induction effect of electromagnetic induction. In such a non-contact power feeding device, power can be fed to the power receiving coil by a mobile power feeding method whereby the power receiving coil is moved corresponding to the stationary power transmission coil through an air gap in the case of power feeding. The power transmission coil and the power receiving coil are respectively formed in a loop-shaped flat structure. A crossover coil is adopted to serve as the power transmission coil. The crossover coil is formed in a long loop shape along the direction of movement of the power receiving side and is crossed along the way to provide a plurality of units. It is however to be noted that a resonant repeating coil can be used together with the power transmission coil to adopt the crossover coil as its repeating coil.Type: GrantFiled: April 6, 2011Date of Patent: September 10, 2013Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Kitao Yamamoto, Takeshi Sato, Keisuke Abe, Masashi Mochizuki, Yasuyuki Okiyoneda
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Patent number: 8299654Abstract: A high frequency electric wire is provided in such a manner that a large number of wires are bundled, twisted and insulated with an outer sheath S. Each wire has an extra-fine hollow pipe structure of a capillary shape. The wire is provided to make its hollow section with the extra-fine hollow pipe structure an air cavity or to cause its hollow section to house an insulating material. In the latter case, the wire is provided by causing a metal conductor to adhere to the outer periphery of an extra-fine insulating yarn, which serves as the insulating material, by plating or vapor-deposition. The electric wire is used as a circuit cable or a coil in a non-contact power feeding device which supplies power based on a mutual induction action of the electromagnetic induction. In this manner, the electric wire fulfills its function to suppress and reduce an increase of the alternating current resistance due to a high frequency alternating current.Type: GrantFiled: June 2, 2010Date of Patent: October 30, 2012Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Kitao Yamamoto, Takeshi Sato, Keisuke Abe, Masashi Mochizuki, Yasuyuki Okiyoneda
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Publication number: 20120169135Abstract: In this non-contact power feeding apparatus, a power feeding circuit is provided with a power transmission coil and a first parallel capacitor to provide a first parallel resonance circuit, while a power receiving circuit is provided with a power receiving coil and a second parallel capacitor to provide a second parallel resonance circuit. Both parallel resonant circuits are set to have the same resonance frequency and a power frequency of a high-frequency power source in the power feeding side circuit is set to be the same as this resonance frequency. A circuit section including the high-frequency power source and a circuit section including the first parallel capacitor and the power transmission coil are connected by the electric field coupling of electric field coupling capacitors.Type: ApplicationFiled: September 8, 2011Publication date: July 5, 2012Applicant: Showa Aircraft Industry Co., Ltd.Inventors: Kitao YAMAMOTO, Takeshi Sato, Keisuke Abe, Masashi Mochizuki, Yasuyuki Okiyoneda
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Publication number: 20110304217Abstract: In a non-contact power feeding device of the present invention, power is fed through an air gap with no contact from a power transmission coil of a power feeding side circuit to a power receiving coil of a power receiving side circuit, which are located to face each other, based on a mutual induction effect of electromagnetic induction. In such a non-contact power feeding device, a resonant coil of a repeating circuit is disposed on the power transmission coil side and/or the power receiving coil side. The resonant coil is wound in parallel on the same plane as the power transmission coil and/or the power receiving coil. The resonant coil the power transmission coil and the power receiving coil are respectively composed of a single insulated conducting wire or a number of insulated conducting wires.Type: ApplicationFiled: June 9, 2011Publication date: December 15, 2011Applicant: Showa Aircraft Industry Co., Ltd.Inventors: Kitao Yamamoto, Takeshi Sato, Keisuke Abe, Masashi Mochizuki, Yasuyuki Okiyoneda
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Publication number: 20110248574Abstract: A non-contact power feeding device feeds power from a power transmission coil to a power receiving coil based on a mutual induction effect of electromagnetic induction. In such a non-contact power feeding device, power can be fed to the power receiving coil by a mobile power feeding method whereby the power receiving coil is moved corresponding to the stationary power transmission coil through an air gap in the case of power feeding. The power transmission coil and the power receiving coil are respectively formed in a loop-shaped flat structure. A crossover coil is adopted to serve as the power transmission coil. The crossover coil is formed in a long loop shape along the direction of movement of the power receiving side and is crossed along the way to provide a plurality of units. It is however to be noted that a resonant repeating coil can be used together with the power transmission coil to adopt the crossover coil as its repeating coil.Type: ApplicationFiled: April 6, 2011Publication date: October 13, 2011Applicant: Showa Aircraft Industry Co., Ltd.Inventors: Kitao YAMAMOTO, Takeshi SATO, Keisuke ABE, Masashi MOCHIZUKI, Yasuyuki OKIYONEDA
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Publication number: 20110140539Abstract: A high frequency electric wire is provided in such a manner that a large number of wires are bundled, twisted and insulated with an outer sheath S. Each wire has an extra-fine hollow pipe structure of a capillary shape. The wire is provided to make its hollow section with the extra-fine hollow pipe structure an air cavity or to cause its hollow section to house an insulating material. In the latter case, the wire is provided by causing a metal conductor to adhere to the outer periphery of an extra-fine insulating yarn, which serves as the insulating material, by plating or vapor-deposition. The electric wire is used as a circuit cable or a coil in a non-contact power feeding device which supplies power based on a mutual induction action of the electromagnetic induction. In this manner, the electric wire fulfills its function to suppress and reduce an increase of the alternating current resistance due to a high frequency alternating current.Type: ApplicationFiled: June 2, 2010Publication date: June 16, 2011Applicant: Showa Aircraft Industry Co., Ltd.Inventors: Kitao YAMAMOTO, Takeshi Sato, Keisuke Abe, Masashi Mochizuki, Yasuyuki Okiyoneda
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Patent number: 6841135Abstract: According to the invention, there are provided catalyst carrier 14 for an exhaust gas purification system, and the method therefor. The catalyst carrier 14 has a honeycomb structure formed of a roll of bands of stainless steel-made one corrugated sheet 1 and one plain sheet 2, which hold stainless steel-made bonding assistants 15 therebetween. Said bonding assistants 15 have width narrower than those of said sheets 1,2, wherein they are positioned at locations radially inside the projections 6 formed at side ends of the corrugated sheet 1 and have thickness T greater than height H of projections 6. Thus, corrugated sheet 1 and plain sheet 2 are diffusion bonded to each other with locally centered high contact pressure, without the influence of projections 6.Type: GrantFiled: March 21, 2001Date of Patent: January 11, 2005Assignee: Showa Aircraft Industry Co., Ltd.Inventor: Katsunori Matsuoka
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Patent number: 6544622Abstract: A novel aramid honeycombs 11 and a method therefor are provided, wherein aramid sheets 1 are used as the base material for forming cell walls 18 of the honeycombs 11. The aramid sheets 1 comprise para-aramid pulps 2, an amount of 40% by weight or less of para-aramid fibers 3 and a binder 4. Each of the aramid sheets 1 is calendered to produce pores 9, which extend from the outer surface to inside, with a porosity of 20% to 60%. Further, a reinforcing resin 10 is adhered to the cell walls 18 of the aramid sheets 1 and the pores are filled with the resin in an amount of 50% by volume based on the pore volume.Type: GrantFiled: October 11, 2000Date of Patent: April 8, 2003Assignee: Showa Aircraft Industry Co., Ltd.Inventor: Kazuhiko Nomoto
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Patent number: 6331340Abstract: A honeycomb structure comprising a supporting base of glass fibers impregnated with a polyamide imide resin prepolymer. The honeycomb structure is free of radio obstruction problem and is excellent in mechanical strength and heat formability to curved surface.Type: GrantFiled: December 9, 1999Date of Patent: December 18, 2001Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Hajime Noguchi, Takaya Komine
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Publication number: 20010043892Abstract: According to the invention, there are provided catalyst carrier 14 for an exhaust gas purification system, and the method therefor. The catalyst carrier 14 has a honeycomb structure formed of a roll of bands of stainless steel-made one corrugated sheet 1 and one plain sheet 2, which hold stainless steel-made bonding assistants 15 therebetween. Said bonding assistants 15 have width narrower than those of said sheets 1,2, wherein they are positioned at locations radially inside the projections 6 formed at side ends of the corrugated sheet 1 and have thickness T greater than height H of projections 6. Thus, corrugated sheet 1 and plain sheet 2 are diffusion bonded to each other with locally centered high contact pressure, without the influence of projections 6.Type: ApplicationFiled: March 21, 2001Publication date: November 22, 2001Applicant: Showa Aircraft Industry Co., Ltd.Inventor: Katsunori Matsuoka
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Patent number: 6240640Abstract: A titanium honeycomb 1 is manufactured by using titanium or titanium alloy as the base material 2, performing diffusion bonding in a striped pattern with heating and pressing, and elongating the stacked base materials 2 . Further, a powder of rare earth oxide, such as yttrium oxide with a particle size of, for example, 30 &mgr;m or less, is employed as the parting agent 5. The oxide is mixed in an amount of 1% by weight or more with the organic binder vaporizing at 350° C. A parting agent is applied at a thickness of 0.3-30 &mgr;m.Type: GrantFiled: July 6, 1999Date of Patent: June 5, 2001Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Katsunori Matsuoka, Jun Nakajima
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Patent number: 5789059Abstract: A honeycomb core or honeycomb structure 1 is made up of an arrangement of hollow cylindrical cells individually separated by cell walls made of base sheets 4. Each base sheet is a complex mixture of para-aramid fibers 2 and meta-aramid pulp material. The para-aramid fibers 2 occupy a weight percentage of from not less than 20% to less than 50% The honeycomb core is made by either the expanding method of the steps of stacking a plurality of base sheets 4, applying stripes of adhesive and then extending the stack or by the corrugating method of the steps of corrugating respective base sheets, stacking and bonding the corrugated sheets. If desired, after-treatment for reinforcement may be executed to apply or impregnating phenolic resin or other impregnating agent.Type: GrantFiled: April 28, 1995Date of Patent: August 4, 1998Assignee: Showa Aircraft Industry Co., Ltd.Inventor: Kazuhiko Nomoto
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Patent number: 5685936Abstract: Disclosed is a method for preparing a carbon honeycomb structure that includes the steps of: alternately stacking a plurality of corrugated sheets each of which is produced by corrugating a supporting base of carbon fibers impregnated with an epoxy resin prepolymer and then curing the prepolymer, and a plurality of flat sheets, each of which is prepared by curing a supporting base of carbon fibers impregnated with an epoxy resin prepolymer, through a node bond adhesive; curing the adhesive to form a honeycomb structure; dipping the resulting honeycomb structure in a phenolic resin prepolymer solution; evaporating the solvent; then curing the phenolic resin prepolymer; repeating these dip, evaporation and curing processes to coat the honeycomb structure with a predetermined amount of the phenolic resin; and cutting the coated honeycomb structure to a predetermined thickness.Type: GrantFiled: October 10, 1995Date of Patent: November 11, 1997Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Takaya Komine, Kimitoshi Katoh
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Patent number: 5591413Abstract: A first honeycomb structure not bonded with brazing filler metal and having a catalyst-carrying layer, and two second honeycomb structures bonded together with brazing filler metal and without applying a catalyst-carrying layer arranged before and after the first honeycomb structure are aligned coaxially inside a cylindrical casing. The first honeycomb structure preferably has a greater concentration of air passages than the second honeycomb structures and moreover, is spaced a fixed distance from each of the second honeycomb structures.Type: GrantFiled: June 5, 1995Date of Patent: January 7, 1997Assignee: Showa Aircraft Industry Co., Ltd.Inventor: Tetsuro Toyoda
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Patent number: 5336472Abstract: This device provides a honeycomb structure in which stress concentration on a flat plate in the area of weld with a corrugated plate is avoided in the outer side area of the honeycomb structure, for example, the first and second layers from the outside thereof, whereby cracks and exfoliation of the flat plate are avoided in the area of the weld and the core is also protected from slipping out.In honeycomb structure 5, corrugated plate 3 and flat plate 1 are disposed alternately and welded to form a wound block. In the range of at least not less than two layers from the outside in the honeycomb structure 5, two sheets of flat plate 1 are used in a pair so that they overlap without welding therebetween.Type: GrantFiled: June 22, 1993Date of Patent: August 9, 1994Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Tetsuro Toyoda, Katsunori Matsuoka
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Patent number: 5316997Abstract: An improved heat resisting structure for treating the exhaust gas of a gas engine is disclosed. The heat resisting structure has a honeycomb-form structure formed of corrugated and flat sheets which are alternately overlapped, rolled up, and joined via a brazing filler metal to make a roll-form structure. The brazing filler metal is made of iron(Fe)-base brazing filler metal, and the stainless steel corrugated sheet and flat sheet constituting the base metal are similar in composition. Accordingly, almost no difference exists in the coefficient of thermal expansion between the brazing filler metal and the base metal. As a result, cracks caused by thermal stress between them due to a difference in coefficient of thermal expansion is avoided even when used repeatedly.Type: GrantFiled: March 26, 1991Date of Patent: May 31, 1994Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Tetsuro Toyoda, Katsunori Matsuoka
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Patent number: 5084361Abstract: A heat resistant structure of a honeycomb type which is used for a catalytic reactor for purification of exhaust gases in the internal combustion engine of a motor vehicle. A catalytic carrier matrix is prepared by joining a corrugated sheet and flat sheet which are alternately placed in layers in a wound from. A pair of pieces of brazing materials made of amorphous alloy are interposed along the longitudinal direction of the matrix at predetermined intervals in the width direction of the matrix. A pair of pieces of said brazing material interposed at both end portions of the matrix face each other across the flat sheet and are deviatedly placed from each other in the width direction of the matrix.Type: GrantFiled: April 8, 1991Date of Patent: January 28, 1992Assignee: Showa Aircraft Industry Co., Ltd.Inventors: Tetsuro Toyoda, Katsunori Matsuoka