专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 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。

2. 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

3. 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

4. 发明专利

JP2003316403A Dynamic air data generation method and equipment thereof 有权
标题翻译：动态空气数据生成方法及其设备
公开(公告)号：JP2003316403A
公开(公告)日：2003-11-07
申请号：JP2002122797
申请日：2002-04-24
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： YAMAGUCHI HIROAKI
IPC分类号： B64F5/00 , G05B11/36 , G05B13/04 , G05B17/02
摘要： PROBLEM TO BE SOLVED: To provide a dynamic air data generation equipment which can generate air data (dynamic air data) which varies dynamically.
SOLUTION: This method is a dynamic air data generation method which controls an air pressure control circuit 25 by inverse transfer function compensation method, and generates dynamic air data which varies continuously concerning air pressure output from the air pressure control circuit. The method is provided with a step which controls the air pressure control circuit by a simple adaptive controller 21, a step which generates an inverse model 22 of the air pressure control circuit formed into the low dimension by adapting the simple adaptive controller, and a step which executes inverse transfer function compensation method using the inverse model.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供可以产生动态变化的空气数据（动态空气数据）的动态空气数据生成设备。解决方案：该方法是通过逆传递函数补偿方法控制气压控制电路25的动态空气数据生成方法，并且生成与气压控制电路输出的空气压力连续变化的动态空气数据。该方法具有通过简单的自适应控制器21控制气压控制电路的步骤，通过适应简单的自适应控制器生成形成为低维的气压控制电路的逆模型22的步骤，以及步骤其使用逆模型执行逆传递函数补偿方法。版权所有（C）2004，JPO

5. 发明专利

JP2010235133A Composite tank, wing, and manufacturing method of composite tank 有权
标题翻译：复合油罐，复合油罐及其制造方法
公开(公告)号：JP2010235133A
公开(公告)日：2010-10-21
申请号：JP2009083366
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 , NAKAMURA KOICHI , HASHIGAMI TOORU
IPC分类号： B65D90/46 , B64C3/34 , B64D37/06 , B65D90/02
CPC分类号： B64D37/06 , B64C3/34 , B64D37/32 , Y02T50/44
摘要： PROBLEM TO BE SOLVED: To provide a composite tank that can curb static buildup, corrosion, and strength degradation, a wing provided with the composite tank, and a method for manufacturing the composite tank. SOLUTION: The composite tank is characterized by being provided with: a tank body, inside which combustible material is stored, having a first resin part 11, 12 formed from fiber-reinforced resin as well as a metal part formed from metal; a second resin part 22 comprising fiber-reinforced resin and covering at least the area of the first resin part 11, 12, on the inner surface of the tank body, that adjoins the metal part; and multiple conductive parts 23 that enable transfer of charge to the first resin part 11, 12 from the surface of the second resin part 22 that is in contact with the combustible material. The fibers included in the second resin part 22 have higher electrical resistance than the fibers included in the first resin part 11, 12. The second resin part 22 forms a layer that isolates the first resin part 11, 12 and the metal part from each other. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种可以抑制静电积聚，腐蚀和强度劣化的复合罐，设置有复合罐的翼，以及制造复合罐的方法。解决方案：复合罐的特征在于：容纳有可燃材料的罐体，其具有由纤维增强树脂形成的第一树脂部分11,12以及由金属形成的金属部分; 第二树脂部分22，其包括纤维增强树脂，并且至少覆盖在罐主体的内表面上的第一树脂部分11,12的与金属部分相邻的区域; 以及能够从与可燃材料接触的第二树脂部22的表面向第一树脂部11,12转移电荷的多个导电部23。包含在第二树脂部分22中的纤维具有比包含在第一树脂部分11,12中的纤维更高的电阻。第二树脂部分22形成使第一树脂部分11,12和金属部分彼此隔离的层。版权所有（C）2011，JPO＆INPIT

6. 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

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式