Yoshiguchi
Hitoshi Yoshiguchi, Okazaki-Shi JP
Patent application number | Description | Published |
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20110113688 | REFORMING APPARATUS - A reforming apparatus includes: an evaporation part that heats reforming water to generate steam; a reforming part having a reforming catalyst that is supplied with a mixture of the steam generated by the evaporation part and reforming fuel and generates reforming gas; a mixing part that is disposed on the lower side of the reforming part in the gravity direction and mixes the reforming fuel with the steam; a reforming fuel supply pipe having a desulfurizer for removing a sulfur content of the reforming fuel; and a reforming fuel connecting pipe connected at one end to the reforming fuel supply pipe and opened at the other end to the mixing part. A connecting part between the reforming fuel supply pipe and the reforming fuel connecting pipe is disposed above the mixing part in the gravity direction. | 05-19-2011 |
Manabu Yoshiguchi, Kamakura-Shi JP
Patent application number | Description | Published |
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20090293243 | Buckle - A buckle includes a male member, a female member for engaging with the male member and having a first portion and a second portion, a first engaging portion provided on the first portion, and a second engaging portion provided on the male member for engaging with the first engaging portion. The second portion can bend so as to receive a part of the male member between the first and second portions. The second portion presses the male member toward the first portion to engage the first engaging portion with the second engaging portion when the male member is inserted between the first and second portions. | 12-03-2009 |
Takuya Yoshiguchi, Aichi JP
Patent application number | Description | Published |
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20150036364 | LIGHTING SYSTEM OF TRANSPORT AND AIRCRAFT - To provide a lighting system which can solve the inconvenience experienced by a pilot entering and leaving a control cabin of a transport such as an aircraft. A lighting system LS of an aircraft | 02-05-2015 |
20150045978 | METHOD OF LOAD SHEDDING IN AIRCRAFT AND CONTROLLER - To properly execute load shedding in an aircraft to maintain power supply to more devices. A method of load shedding includes a failure detection step of detecting a failure in a generator, and a load-shedding step. The load-shedding step includes determination step, and execution step, respectively, the determination step in which the load shedding is determined to be needed if the state where a power consumption exceeds a power-generation capacity continues for a monitoring time, and the execution step in which the load shedding is executed step-by-step while advancing a priority given to a target device until the power consumption falls below the power-generation capacity. | 02-12-2015 |