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1. 发明专利

JP2014189070A Fuel tank, main wing, aircraft fuselage, aircraft, and movable body 有权
标题翻译：燃油箱，主机，飞机熔接，飞机和可移动机身
公开(公告)号：JP2014189070A
公开(公告)日：2014-10-06
申请号：JP2013064444
申请日：2013-03-26
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KAMIHARA NOBUYUKI , KISHIMOTO KAZUAKI , ABE TOSHIO , KAMINO YUICHIRO
IPC分类号： B64C3/34 , B32B5/00 , B32B7/02 , B60K15/03 , B64C1/00 , B64D45/02 , H01M8/00 , H01M8/04
CPC分类号： B64D37/32 , B32B1/02 , B32B7/08 , B32B15/08 , B32B27/12 , B32B27/20 , B32B2262/106 , B32B2307/20 , B32B2605/00 , B32B2605/18 , B64C3/34 , B64D37/005 , B64D37/04 , B64D37/06 , B64D45/02 , Y02T50/44
摘要： PROBLEM TO BE SOLVED: To provide a fuel tank capable of preventing an increase in weight by reducing operation time and cost for quality control, a main wing, an aircraft fuselage, an aircraft, and a movable body.SOLUTION: A fuel tank comprises a structural member that uses carbon fiber-reinforced plastics (CFRP) 15 having a reinforcement material including a carbon fiber, and a matrix including plastics. The structural member is molded in such a manner that a conductive sheet 17 is superposed between prepregs of the carbon fiber-reinforced plastics (CFRP) 15, and a fastening hole 22, to which a bolt 20 is to be fastened, is formed.
摘要翻译：要解决的问题：提供一种能够通过减少质量控制的操作时间和成本来防止重量增加的燃料箱，主翼，飞机机身，飞行器和移动体。解决方案：燃料箱包括使用具有碳纤维的增强材料的碳纤维增强塑料（CFRP）15和包括塑料的基体的结构构件。结构构件以如下方式成型：导电片17叠置在碳纤维增强塑料（CFRP）15的预浸料和紧固孔22之间，紧固孔22形成有螺栓20。

2. 发明专利

JP2012146256A Traffic flow simulation device, traffic flow simulation program and traffic flow simulation method 有权
标题翻译：交通流量模拟装置，交通流量模拟程序和交通流量模拟方法
公开(公告)号：JP2012146256A
公开(公告)日：2012-08-02
申请号：JP2011006029
申请日：2011-01-14
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SONODA TAKASHI , ITO YOKO , NISHIMAE ETSUSHI , KAMINO YUICHIRO , OGAWA HIROSHI , KAWAGUCHI KENTARO , MORISHITA KEIICHI
IPC分类号： G08G1/00
CPC分类号： G08G1/0104 , B61L27/0055 , B61L29/24 , G08G1/123 , G09B29/007
摘要： PROBLEM TO BE SOLVED: To predict an impact of public transportation system on traffic.SOLUTION: An automobile traveling simulation section 84 simulates traffic of an automobile model simulating an automobile in a road network model simulating a road network including a plurality of roads and an intersection which connects the roads. A public transportation system traveling simulation section 88 simulates the traffic of a rail transportation system model simulating a rail transportation system in a railway network model simulating a rail route of rail transportation system. A crossing gate simulation section 90 operates a crossing gate model which is positioned at an intersection point where the road and the rail route of the rail transportation system intersect and simulates a crossing gate which temporarily blocks the traffic of the automobiles at the intersection position when the rail transportation system passes through the intersection position.
摘要翻译：要解决的问题：预测公共交通系统对交通的影响。汽车旅行模拟部84模拟模拟道路网络的道路网络模型中的模拟汽车模型的交通，该道路网模型包括多条道路和连接道路的交叉路口。公共交通系统旅行模拟部分88模拟模拟轨道交通系统铁路线路的铁路网模型中轨道交通系统模拟轨道交通系统模型的流量。交叉门模拟部90操作交叉门模型，其位于轨道交通系统的道路和轨道交叉点的交点处，并且模拟交叉门，临时阻止汽车在交叉位置处的交通，轨道交通系统通过交叉口。版权所有（C）2012，JPO＆INPIT

3. 发明专利

JP2012053008A Capacitive level gage 有权
标题翻译：电容水平仪
公开(公告)号：JP2012053008A
公开(公告)日：2012-03-15
申请号：JP2010197819
申请日：2010-09-03
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： YAMAGUCHI HIROAKI , KAMINO YUICHIRO
IPC分类号： G01F23/26
CPC分类号： G01F23/263 , G01F23/266 , G01F23/268
摘要： PROBLEM TO BE SOLVED: To provide a capacitive level gage capable of suppressing generation of electrification even if an insulator is used for a structure.SOLUTION: A fuel oil gage 15 includes: a columnar inner structure 27 formed from an insulator; a hollow cylindrical outer structure 23 disposed in the outer peripheral side of the inner structure 27 with the entire circumference spaced therefrom and formed from an insulator; an inner electrode 29 stuck to the outer peripheral face of the inner structure 27; and an outer electrode 25 stuck to the inner peripheral face of the outer structure 23: measures a capacitance between the inner electrode 29 and the outer electrode 25; and detects a level of fuel being present between the inner electrode 29 and the outer electrode 25. The outer structure 23 includes a plurality of outside through-holes 31 allowing the movement of charges from the outer peripheral surface to the outer electrode 25.
摘要翻译：要解决的问题：提供即使绝缘体用于结构也能够抑制产生电气的电容电平计。解决方案：燃料油表15包括：由绝缘体形成的柱状内部结构27; 中空圆柱形外部结构23设置在内部结构27的外周侧，其整个圆周与其隔开并由绝缘体形成; 内部电极29粘附到内部结构27的外周面上; 和外部电极25，其粘附到外部结构23的内周面上：测量内部电极29和外部电极25之间的电容; 并且检测存在于内部电极29和外部电极25之间的燃料的水平。外部结构23包括允许电荷从外周表面移动到外部电极25的多个外部通孔31。 >版权所有（C）2012，JPO＆INPIT

4. 发明专利

JP2011051517A Aircraft wing 审中-公开
标题翻译：飞机票
公开(公告)号：JP2011051517A
公开(公告)日：2011-03-17
申请号：JP2009203600
申请日：2009-09-03
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KAMINO YUICHIRO , YAMAKOSHI HIDEO , HASHIGAMI TORU
IPC分类号： B64C3/34 , B64C3/28 , B64D37/32
摘要： PROBLEM TO BE SOLVED: To provide an aircraft wing surely suppressing the generation of high voltage due to a lightning strike, and reducing the inflow of thunder current to a fuel tank even if the wing is formed of a resin material reinforced with fibers. SOLUTION: A main wing of the aircraft is provided with the fuel tank 3 whose container surface comprises: an upper side skin 15 constituting the upper side surface; a lower side skin 17 constituting the lower side surface; and a front side spar 19 and a rear side spar 21 reinforcing the upper and lower side skins and extended in the wing length direction. At least a part of the upper side skin 15, the lower side skin 17, the front side spar 19 and the rear side spar 21 is formed of a resin material reinforced with fibers. A fixed leading edge 5 and a fixed trailing edge 9 both of which are made of metal and electrically continuous from the end of the wing to the root of the wing coming in contact with a fuselage conductivity part, are formed on at least one of the upper side surface and the lower side surface. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：为了提供飞机机翼可靠地抑制由雷击引起的高电压的产生，并且即使机翼由用纤维增强的树脂材料形成，也减少雷电流到燃料箱的流入。解决方案：飞机的主翼设有燃料箱3，其容器表面包括：构成上侧表面的上侧皮肤15; 构成下侧面的下侧皮肤17; 以及前侧翼梁19和后侧梁21，其加强上侧和下侧表皮并且在机翼长度方向上延伸。上侧皮肤15，下侧皮肤17，前侧翼片19和后侧翼片21的至少一部分由用纤维增强的树脂材料形成。在机身的端部与机身导电部分接触的机翼的根部，由金属制成且电连续的固定前缘5和固定后缘9形成在至少一个上侧面和下侧面。版权所有（C）2011，JPO＆INPIT

5. 发明专利

JP2009227166A Aircraft assembly 有权
标题翻译：飞机装配
公开(公告)号：JP2009227166A
公开(公告)日：2009-10-08
申请号：JP2008076547
申请日：2008-03-24
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KAMINO YUICHIRO , OGURI KAZUYUKI , NAKAMURA KOICHI
IPC分类号： B64C1/00 , B64D45/02 , F16B5/02 , F16B33/06 , F16B35/00
CPC分类号： B64C3/26 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/43441 , B29C66/474 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72321 , B29C66/742 , B29C70/088 , B29C70/885 , B29D99/001 , B29K2105/06 , B29K2305/02 , B29K2305/10 , B29K2307/00 , B29K2309/08 , B29K2705/10 , B29K2995/0005 , B29L2009/003 , B29L2031/3082 , B29L2031/3085 , B64D45/02 , F16B33/004 , F16B35/06 , F16B37/14 , B29K2307/04 , B29K2079/08 , B29K2071/00
摘要： PROBLEM TO BE SOLVED: To provide an aircraft assembly having a thunder resistance structure which can not be easily broken by a lightning current and is highly reliable.
SOLUTION: The aircraft assembly, which includes an outer board 10 having a CFRP layer 12 as a main structure, a sea-tie 11 for supporting the outer board 10 from within and fasteners 1 for joining the outer board 10 and the sea-tie 11, is characterized in that copper foil 13 and an outer GFRP layer 14 are provided outward in this order on the outer surface of the outer board 10, and a copper paint layer 19 including copper powder is provided on the outer GFRP layer 14.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供一种具有雷电阻结构的飞行器组件，其不易被雷电流破坏并且是高度可靠的。解决方案：飞行器组件包括具有CFRP层12作为主要结构的外板10，用于从内部支撑外板10的海带11和用于连接外板10和海的紧固件1 其特征在于，在外板10的外表面上依次向外设置有铜箔13和外侧GFRP层14，在外侧GFRP层14上设置有包含铜粉末的铜涂层19 。版权所有（C）2010，JPO＆INPIT

6. 发明专利

JP2012141799A Road traffic flow simulation device, road traffic flow simulation program and road traffic flow simulation method 有权
标题翻译：道路交通流量模拟装置，道路交通流量模拟程序和道路交通流量模拟方法
公开(公告)号：JP2012141799A
公开(公告)日：2012-07-26
申请号：JP2010294240
申请日：2010-12-28
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NISHIMAE ETSUSHI , SONODA TAKASHI , ITO YOKO , ONO HIDEKAZU , KAMINO YUICHIRO , OGAWA HIROSHI , HIBINO HIROSHI , MORISHITA KEIICHI
IPC分类号： G08G1/00
CPC分类号： B60L11/1861 , B60L1/003 , B60L1/14 , B60L11/1824 , B60L11/1846 , B60L11/185 , B60L2200/12 , B60L2230/40 , B60L2240/12 , B60L2240/14 , B60L2240/34 , B60L2240/642 , B60L2240/645 , B60L2240/662 , B60L2240/68 , B60L2240/72 , B60L2250/16 , B60L2260/52 , B60L2260/54 , G08G1/0104 , Y02T10/7005 , Y02T10/7044 , Y02T10/705 , Y02T10/7088 , Y02T10/7291 , Y02T90/121 , Y02T90/128 , Y02T90/14 , Y02T90/16 , Y02T90/163 , Y02T90/169 , Y04S30/14
摘要： PROBLEM TO BE SOLVED: To simulate charging behavior of an electric vehicle.SOLUTION: A road traffic flow simulation has: a step 100 to set a ratio of a number of electric vehicle models simulating electric vehicles with residual charged power of batteries as attribute values to a total number of vehicle models and to set a number as well as installation positions of charging station models that charge the batteries on the electric vehicle models; a step 108 to calculate residual power of the batteries on the electric vehicle models traveling in a road network model simulating a road network including a plurality of roads and intersections connecting the roads; and a step 112 to select the charging station models to charge the batteries on the electric vehicle models which require charging with values based on the calculated residual power of the batteries lower than a preliminary determined threshold.
摘要翻译：要解决的问题：模拟电动车辆的充电行为。道路交通流模拟具有：步骤100，将模拟电动车辆的电动汽车模型的数量与电池的剩余充电功率的比率作为属性值设置为车辆模型的总数，并设定数量以及在电动车型上对电池充电的充电站型号的安装位置; 步骤108，用于计算在模拟包括连接道路的多个道路和交叉点的道路网络的道路网络模型中行驶的电动汽车模型上的电池的剩余电力; 以及步骤112，以选择充电站模型，以在需要充电的电动车辆模型上对基于所计算的电池剩余电量低于初步确定的阈值的值进行充电。版权所有（C）2012，JPO＆INPIT

7. 发明专利

JP2010234900A Fuel tank for aircraft 有权
标题翻译：燃油舱
公开(公告)号：JP2010234900A
公开(公告)日：2010-10-21
申请号：JP2009083361
申请日：2009-03-30
申请人： Mitsubishi Heavy Ind Ltd , Society Of Japanese Aerospace Co Inc , 三菱重工業株式会社 , 社団法人日本航空宇宙工業会
发明人： YAMAGUCHI HIROAKI , KAMINO YUICHIRO , HASHIGAMI TOORU , OGURI KAZUYUKI , NAKAMURA KOICHI
IPC分类号： B64C3/34
CPC分类号： B64C3/34 , B64D37/32 , B64D45/02
摘要： PROBLEM TO BE SOLVED: To provide a fuel tank for an aircraft, capable of suppressing electrostatic charge, for example, caused by flow electrification with fuel. SOLUTION: The fuel tank for an aircraft includes an upper outer plate 5 and a lower outer plate 7 which have electric conductivity and form part of a container for housing fuel, an inner structure 19 which is formed of metal, and an inner surface layer 15 which has a semiconductor property or an insulation property and is formed integrally on the inner surfaces of the upper outer plate 5 and the lower outer plate 7 in a location where the inner structure 19, and the upper outer plate 5 and the lower outer plate 7 are in contact with each other and in a surrounding portion thereof, wherein the inner surface layer 15 at least in the surrounding portion is formed of a material having the semiconductor property. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种用于飞机的燃料箱，其能够抑制例如由与燃料的流动通电引起的静电荷。解决方案：用于飞机的燃料箱包括具有导电性并形成用于容纳燃料的容器的一部分的上外板5和下外板7，由金属形成的内部结构19和内部表面层15具有半导体特性或绝缘性，并且在内部结构19和上部外板5和下部外板5的位置一体地形成在上外板5和下外板7的内表面上外板7彼此接触并且在其周围部分中，其中至少在周围部分中的内表面层15由具有半导体特性的材料形成。版权所有（C）2011，JPO＆INPIT

8. 发明专利

JP2010126133A Fuel tank of aircraft 有权
标题翻译：飞机燃油箱
公开(公告)号：JP2010126133A
公开(公告)日：2010-06-10
申请号：JP2008306573
申请日：2008-12-01
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： YAMAGUCHI HIROAKI , KAMINO YUICHIRO , HASHIGAMI TOORU , OGURI KAZUYUKI
IPC分类号： B64D37/32
CPC分类号： B64D37/32 , B64C3/34 , B64D45/02
摘要： PROBLEM TO BE SOLVED: To provide the fuel tank of an aircraft suppressing the occurrence of spark in pipes due to flow of a thunder current upon lightning strike, and suppressing electrostatic charge in the pipes due to flow charge with a fuel.
SOLUTION: This fuel tank 1 of the aircraft includes a storage part formed by using a conductive upper outer plate 5, lower outer plate 7, and spars 9. The fuel tank includes the pipes in the fuel tank such as a fuel resupply pipe 17, fuel supply pipe 19, and inert gas pipe 21, that are arranged in the storage part and grounded 27 at a plurality of places, and a pipe outer surface layer 31 with semiconducting characteristics formed integrally on the outer surface of the pipe in the fuel tank such as the fuel resupply pipe 17, fuel supply pipe 19, and inert gas pipe 21.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供一种飞机的燃料箱，其在雷击时由于雷电流的流动而抑制管道中的火花的发生，并且由于燃料的流动负荷而抑制管道中的静电电荷。解决方案：飞机的该燃料箱1包括通过使用导电上外板5，下外板7和翼梁9形成的储存部。燃料箱包括燃料箱中的管道，例如燃料补给管17，燃料供给管19和惰性气体配管21，配置在储存部上并在多个地方接地27，并且具有半导体特性的管外表面层31整体地形成在管的外表面上燃料补给管17，燃料供给管19和惰性气体管21等。燃料箱（C）2010，JPO＆INPIT

9. 发明专利

JP2013213687A Sealant inspection method, sealant inspection apparatus and aircraft member 审中-公开
标题翻译：密封检测方法，密封检测装置和飞机会员
公开(公告)号：JP2013213687A
公开(公告)日：2013-10-17
申请号：JP2012083058
申请日：2012-03-30
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： TAKIZAWA TOMOO , YAMAGUCHI HIROAKI , YAMAKOSHI HIDEO , KAMINO YUICHIRO , NISHIZAWA SEIJI
IPC分类号： G01B15/00 , G01B15/02 , G01N21/35
摘要： PROBLEM TO BE SOLVED: To provide a sealant inspection method and a sealant inspection apparatus, which can inspect the state of a seal portion of an aircraft member non-destructively, and the aircraft member.SOLUTION: The sealant inspection method for inspecting a seal portion which is a portion of the aircraft member sealed by sealant includes: a laser irradiation step S2 of radiating laser; an electromagnetic wave irradiation step S3 of generating a terahertz electromagnetic wave by the radiated laser and irradiating the seal portion with the generated terahertz electromagnetic wave as an irradiation wave; a laser delay step S4 of separating the laser radiated by the laser irradiation step S2 to delay the laser; a laser detection step S5 of detecting the delayed laser; a reflection wave detection step S6 of detecting a reflection wave from the seal portion; a waveform data derivation step S7 of deriving time characteristics waveform data representing a temporal change in electromagnetic wave intensity of the reflection wave on the basis of the detected reflection wave and laser; and a seal portion state estimation step S8 of estimating the state of the seal portion on the basis of the derived time characteristics waveform data.
摘要翻译：要解决的问题：提供一种密封件检查方法和密封件检查装置，其可以非飞行地检查飞机构件的密封部分的状态和飞行器构件。解决方案：用于检查密封部分的密封剂检查方法由密封件密封的飞行器部件的一部分包括：激光照射步骤S2，其辐射激光; 电磁波照射步骤S3，通过所述辐射激光产生太赫兹电磁波，并用产生的太赫兹电磁波照射所述密封部分作为照射波; 激光延迟步骤S4，分离由激光照射步骤S2辐射的激光以延迟激光; 检测延迟激光的激光检测步骤S5; 检测来自密封部的反射波的反射波检测工序S6; 波形数据导出步骤S7，其基于检测到的反射波和激光器导出表示反射波的电磁波强度的时间变化的时间特性波形数据; 以及基于导出的时间特性波形数据来估计密封部的状态的密封部状态估计步骤S8。

10. 发明专利

JP2013198364A Vehicle, power utilization system, on-board device, and external system 审中-公开
标题翻译：车辆，动力利用系统，车载装置和外部系统
公开(公告)号：JP2013198364A
公开(公告)日：2013-09-30
申请号：JP2012065476
申请日：2012-03-22
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KAMINO YUICHIRO , ISHII SHINYA , ONO HIDEKAZU
IPC分类号： H02J7/00 , B60L11/18 , B60M7/00 , H01M10/44 , H02J17/00
CPC分类号： Y02T10/7005 , Y02T10/7241
摘要： PROBLEM TO BE SOLVED: To provide a vehicle in which the power, charging a secondary battery in the vehicle, can be utilized effectively, and to provide a power utilization system.SOLUTION: A vehicle includes a power discharge mechanism for outputting the electric power, charging a secondary battery, by wireless energy in non-contact. A shop device has a charge mechanism for receiving wireless energy in non-contact from the power discharge mechanism and charging the secondary battery by converting the wireless energy into electric power. In response to input of a power discharge control start request, the vehicle controls the power discharge mechanism so as to output the electric power, charging the secondary battery, to the charge mechanism by wireless energy.
摘要翻译：要解决的问题：提供一种能够有效利用车辆中的二次电池的充电电力并提供电力利用系统的车辆。解决方案：车辆包括用于输出电力的功率放电机构，充电二次电池，通过无线电能进行非接触。商店装置具有用于从功率放电机构接收非接触的无线能量并通过将无线能量转换为电力来对二次电池进行充电的充电机构。响应于放电控制开始请求的输入，车辆控制功率放电机构，以便通过无线能量将二次电池的电力输出到充电机构。

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