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1. 发明专利

JP2012117985A Current measurement method 有权
标题翻译：电流测量方法
公开(公告)号：JP2012117985A
公开(公告)日：2012-06-21
申请号：JP2010269792
申请日：2010-12-02
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： TSUMURA YOICHIRO , YAMAKOSHI HIDEO , AOI TATSUFUMI
IPC分类号： G01R15/24
摘要： PROBLEM TO BE SOLVED: To provide a method for measuring a current flowing through a fastener in a structure similar to an actual structure.SOLUTION: A current measurement method includes: a step (a) in which an optical fiber is wound around the periphery of the fastener; a step (b) in which a first linearly polarized light is made incident from the other end of the optical fiber; a step (c) in which the incident first linearly polarized light is reflected at one end and a second linearly polarized light emitted from the other end of the optical fiber is detected; and a step (d) in which a current I is specified based on a rotational angle of a polarization plane of the second linearly polarized light with respect to the first linearly polarized light.
摘要翻译：要解决的问题：提供一种用于测量流过紧固件的电流的方法，其结构类似于实际结构。解决方案：电流测量方法包括：步骤（a），其中光纤缠绕在紧固件的周边; 从光纤的另一端入射第一直线偏振光的步骤（b）; 其中检测入射的第一直线偏振光在一端反射并从光纤的另一端发射的第二线偏振光的步骤（c）; 以及基于第二线偏振光的偏振面的旋转角相对于第一线偏振光来指定电流I的步骤（d）。版权所有（C）2012，JPO＆INPIT

2. 发明专利

JP2014144697A Tool and method for molding sealant layer of lightning-resistant fastener, lightning-resistant fastener, and aircraft wing 有权
标题翻译：用于模制耐高温紧固件，防雷紧固件和飞机机的密封层的工具和方法
公开(公告)号：JP2014144697A
公开(公告)日：2014-08-14
申请号：JP2013014092
申请日：2013-01-29
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： YAMAKOSHI HIDEO , ASAHARA YUJI , NISHIMURA WATARU , TARUMI TAKEYASU , TAKADA KENCHI , KAWAGUCHI JUN , RIKUKAWA KOJI , OKUMURA TOMONORI , NOMIYA KENGO
IPC分类号： B64D45/02 , B64C1/00 , B64F5/00
CPC分类号： B64D45/02 , B23P11/00 , F16B33/004 , F16B37/14
摘要： PROBLEM TO BE SOLVED: To provide a tool for forming a sealant layer of a lightning-resistant fastener, which can rapidly and accurately obtain the sealant layer with necessary thickness.SOLUTION: A guide tool 30 is used to form a sealant layer 29 around a fastener member 24 for fastening a plurality of members, which configure an airframe of an aircraft, in such a manner as to pass through them. The guide tool includes a cup 31 that has a cavity 33 filled with an uncured sealant agent 28, and a guide that is provided within the cavity 33 and that is locked to the fastener member 24 to make the cavity 33 agree with a central axis of the fastener member 24.
摘要翻译：要解决的问题：提供一种用于形成防雷紧固件的密封剂层的工具，其可以快速且准确地获得具有所需厚度的密封剂层。解决方案：引导工具30用于形成围绕紧固构件24，用于紧固构成飞行器机身的多个构件，以便穿过它们。引导工具包括具有填充有未固化的密封剂28的空腔33的杯31和设置在空腔33内并且被锁定到紧固构件24以使空腔33与中心轴线一致的导向件紧固件24。

3. 发明专利

JP2014144696A Tool and method for molding sealant layer of lightning-resistant fastener, and aircraft wing 有权
标题翻译：用于模制耐冲击紧固件的密封层的工具和方法，以及飞机机
公开(公告)号：JP2014144696A
公开(公告)日：2014-08-14
申请号：JP2013014091
申请日：2013-01-29
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： NISHIMURA WATARU , YAMAKOSHI HIDEO , ASAHARA YUJI , IYOMASA ATSUHIRO , TARUMI TAKEYASU , TAKADA KENCHI , KAWAGUCHI JUN , RIKUKAWA KOJI , OKUMURA TOMONORI , NOMIYA KENGO , HASHIGAMI TORU
IPC分类号： B64D45/02 , B64C1/00 , B64F5/00
CPC分类号： B64D45/02 , F16B37/14
摘要： PROBLEM TO BE SOLVED: To provide a tool for molding a sealant layer, which can rapidly and accurately obtain the sealant layer with necessary film thickness.SOLUTION: A tool for molding a sealant layer includes a sealant cup 13 for covering a periphery of a collar 26 with a sealant agent 28, a cup holder 12 for positioning the sealant cup 13 with respect to a fastener member 24, and a dummy cup 11 for positioning the cup holder 12 with respect to the fastener member 24. The cup holder 12 is positioned with respect to the fastener member 24 by being guided to the dummy cup 11 positioned with respect to the fastener member 24. Additionally, after the dummy cup 11 is removed from the cup holder 12 positioned with respect to the fastener member 24, the sealant cup 13 is guided to the cup holder 12 to cover the periphery of the collar 26 with the sealant agent 28.
摘要翻译：要解决的问题：提供一种用于模制密封剂层的工具，其可以以必要的膜厚度快速且准确地获得密封剂层。解决方案：用于模制密封剂层的工具包括密封剂杯13，其用于覆盖环的周边 26具有密封剂28，用于将密封剂杯13相对于紧固件24定位的杯保持器12和用于相对于紧固件24定位杯保持器12的虚拟杯11.杯保持器12定位相对于紧固件构件24被引导到相对于紧固构件24定位的假杯11.另外，在从相对于紧固构件24定位的杯保持器12移除虚拟杯11之后，密封杯 13被引导到杯架12以用密封剂28覆盖套环26的周边。

4. 发明专利

JP2013095423A Lightning-resistant fastener and cap for the same 有权
标题翻译：防雷紧固件和盖帽
公开(公告)号：JP2013095423A
公开(公告)日：2013-05-20
申请号：JP2012274549
申请日：2012-12-17
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： ASAHARA YUJI , YAMAKOSHI HIDEO , IYOMASA ATSUHIRO , TARUMI TAKEYASU , NISHIMURA WATARU , WATANABE YASUNORI , HASHIGAMI TORU , RIKUKAWA HIROSHI , IMAMURA HIDEO , TANIGUCHI NAOKI
IPC分类号： B64C1/00 , B64D45/02 , F16B37/14 , F16B41/00
摘要： PROBLEM TO BE SOLVED: To provide a lightning-resistant fastener capable of reliably encapsulating an arc between a cap and a member such as a wing panel, even when the cap is lifted, and a cap for the lightning-resistant fastener.SOLUTION: The cap 30C has its inside provided with a step part (butt part) 50 which butts against a collar 26 fastened to a fastener member 24. A clearance 51 is formed between one end 30a of the cap 30C and a member 22 while making the step part 50 butt against the collar 26. When a sealant material 34 infilled into the cap 30C overflows from an opening at the one end 30a of the cap 30C, it extends to an outer peripheral side from the clearance 51. This can prevent the cap 30C from being pushed back in the direction of isolation from the member 22, by suppressing an increase in the pressure of the sealant material 34 in the cap 30C.
摘要翻译：要解决的问题：提供一种能够在帽和诸如翼板之类的构件之间可靠地封装电弧的防雷紧固件，即使当盖被提起时，还有用于防雷紧固件的帽。解决方案：盖30C的内部设置有台阶部分（对接部分）50，该台阶部分（对接部分）50抵靠紧固到紧固件24的轴环26上。在盖30C的一个端部30a和一个部件同时使台阶部分50对准套环26.当填充到盖30C中的密封剂材料34从帽30C的一端30a处的开口溢出时，其从间隙51延伸到外周侧。这通过抑制盖30C中的密封剂材料34的压力的增加，能够防止盖30C从构件22隔离的方向被推回。版权所有（C）2013，JPO＆INPIT

5. 发明专利

JP2012192752A Coupling structure for airframe component 有权
标题翻译： AIRFRAME组件联轴器结构
公开(公告)号：JP2012192752A
公开(公告)日：2012-10-11
申请号：JP2011055999
申请日：2011-03-14
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： KAWAHARA KOJI , YAMAKOSHI HIDEO , KAMINO YUICHIRO , IYOMASA ATSUHIRO , HASHIGAMI TORU
IPC分类号： B64D45/02 , B64C3/26
CPC分类号： H01R4/06 , B64C3/34 , B64D45/02 , F16B5/02 , F16B15/02 , F16B37/14 , F16B2001/0064 , H05H3/02
摘要： PROBLEM TO BE SOLVED: To provide a coupling structure for airframe components that is capable of ensuring sufficient lightning protection capability.SOLUTION: A conductive pattern part 40 made of a conductive material is formed around each fastener member 24 between wing surface panels 21A and 21B. The conductive pattern part 40 is formed, for example, around each of holes 21c and 21d on the plane on which the wing surface panel 21A and the wing surface panel 21B abut against each other. Then, the conductive pattern part 40 is pushed against both the wing surface panel 21A and the wing surface panel 21B by the fastening power of the fastener members 24, whereby electrical conduction between the wing surface panel 21A and the wing surface panel 21B can be achieved.
摘要翻译：要解决的问题：提供能够确保足够的防雷能力的机身部件的联接结构。解决方案：在机翼表面面板21A和21B之间的每个紧固件24周围形成由导电材料制成的导电图案部分40。导电图案部40例如形成在机翼面板21A和翼面板21B彼此抵接的平面上的各孔21c，21d的周围。然后，通过紧固件24的紧固力将导电图案部40推压到翼面21A和翼面板21B上，由此能够实现翼面21A和翼面面板21B之间的导电。版权所有（C）2013，JPO＆INPIT

6. 发明专利

JP2013195321A Lightning stroke evaluation system 有权
标题翻译：闪电探测系统
公开(公告)号：JP2013195321A
公开(公告)日：2013-09-30
申请号：JP2012064890
申请日：2012-03-22
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： AOI TATSUFUMI , YAMAGUCHI KENGO , IKEDA AKIO , YAMAKOSHI HIDEO , HASHIGAMI TORU
IPC分类号： G01R19/00
摘要： PROBLEM TO BE SOLVED: To provide a lightning stroke evaluation system capable of detecting presence/absence of spark when a craft structure and a test piece are struck by lightning, and various quantities caused by the lightning, and highly efficiently and accurately evaluate lightning resistance.SOLUTION: A lightning stroke evaluation system 1 includes: an image sensor 4 for detecting spark generated on a test piece 100 by lightning stroke; a trigger device 6 that emits a trigger signal for acquiring detection data synchronized with the lightning stroke onto the test piece 100; and an evaluation device 7 for evaluating lightning resistance of the test piece 100 on the basis of the detection data. The image sensor 4 and the evaluation device 7 are connected via an optical fiber cable 10 for transmitting an optical signal obtained by photoelectrically converting the detection data. The trigger device 6 and the image sensor 4 are connected via an optical fiber cable 11 for transmitting an optical signal obtained by photoelectrically converting the trigger signal.
摘要翻译：要解决的问题：提供一种能够在飞行结构和试验片遭受雷击时检测火花的存在/不存在的雷击评价系统，以及由雷击引起的各种量，并且高效准确地评估耐雷性。解决方案：雷击评估系统1包括：图像传感器4，用于通过雷击检测在测试片100上产生的火花; 触发装置6，其发射用于获取与雷击同步的检测数据的触发信号到测试片100上; 以及评价装置7，用于根据检测数据评价试验片100的耐雷电性。图像传感器4和评价装置7通过光纤电缆10连接，用于发送通过光电转换检测数据而获得的光信号。触发装置6和图像传感器4通过光纤电缆11连接，用于发送通过光电转换触发信号而获得的光信号。

7. 发明专利

JP2013095371A Lightning-resistant fastener and cap for the same 有权
标题翻译：防雷紧固件和盖帽
公开(公告)号：JP2013095371A
公开(公告)日：2013-05-20
申请号：JP2011242552
申请日：2011-11-04
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： ASAHARA YUJI , YAMAKOSHI HIDEO , IYOMASA ATSUHIRO , TARUMI TAKEYASU , NISHIMURA WATARU , WATANABE YASUNORI , HASHIGAMI TORU , RIKUKAWA HIROSHI , IMAMURA HIDEO , TANIGUCHI NAOKI
IPC分类号： B64C1/00 , B64D45/02 , F16B37/14
CPC分类号： F16B43/001 , B64D45/02 , F16B33/004 , F16B37/14
摘要： PROBLEM TO BE SOLVED: To provide a lightning-resistant fastener capable of reliably encapsulating an arc on an interface between a cap and a member such as a wing panel, even when the cap is lifted, and a cap for the lightning-resistant fastener.SOLUTION: A tapered surface 30c having its outside diameter gradually reduced toward one end 30a from the side of the other end 30b is formed at the outer periphery of the one end 30a of the cap 30A. A sealant 34B overflowing from the cap 30A in the attachment of the cap 30A is interposed between the tapered surface 30c and a surface 22f of a member 22. Even when the cap 30A is pushed back in the direction of isolation from the member 22 by the pressure and elasticity of the sealant 34 sandwiched between the cap 30A and the member 22, the sealant 34B is reliably interposed between the tapered surface 30c and the surface 22f of the member 22.
摘要翻译：要解决的问题：为了提供一种能够可靠地将电弧封装在帽和诸如翼片之类的部件之间的界面上的防雷紧固件，即使当盖被提起时，抵抗紧固件。解决方案：在帽30A的一端30a的外周形成有从其另一端30b侧朝向一端30a逐渐减小的锥形面30c。在锥形表面30c和构件22的表面22f之间插入从盖30A溢出的密封剂34B，即使在帽30A被隔离的方向从构件22向后推动密封剂34夹在盖30A和构件22之间的压力和弹性，密封剂34B可靠地插入在锥形表面30c和构件22的表面22f之间。（C）2013，JPO＆INPIT

8. 发明专利

JP2012206662A Lightning-resistant and explosion-proof fastener 有权
标题翻译：防雷和防爆型紧固件
公开(公告)号：JP2012206662A
公开(公告)日：2012-10-25
申请号：JP2011075143
申请日：2011-03-30
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： UMEMOTO SOICHIRO , YAMAKOSHI HIDEO , IYOMASA ATSUHIRO , HASHIGAMI TORU
IPC分类号： B64C1/00 , B64C3/34 , F16B37/00 , F16B43/00
CPC分类号： B64D45/02
摘要： PROBLEM TO BE SOLVED: To provide a lightning-resistant and explosion-proof fastener that exhibits sufficient arc control effect, reliable fastening force of a fastener member and a fastening member and excellent work stability.SOLUTION: An insulation cover 50A is configured so that the dimensions in an axial direction of a fastener body 25 of outer and inner periphery side cylindrical parts 50c, 50b to be fitted into step parts 40, 41, respectively, are larger than a tip covering part 50a for covering a tip surface 26a of a fastening member 26. On the outer and inner periphery sides of the fastening member 26, a distance to a member 22 is sufficiently secured by the outer and inner periphery side cylindrical parts 50c, 50b. The tip covering part 50a is thinner than the outer and inner periphery side cylindrical parts 50c, 50b. When the fastener body 25 is fastened to the fastening member 26, the deformation of the tip covering part 50a in the thickness direction can be reduced.
摘要翻译：要解决的问题：提供具有足够的电弧控制效果的防雷和防爆紧固件，紧固构件和紧固构件的可靠的紧固力以及优异的工作稳定性。解决方案：绝缘盖50A被构造成使得分别嵌合在台阶部分40,41中的外周侧圆筒部50c和内周侧圆筒部50b的紧固件主体25的轴向尺寸大于用于覆盖紧固构件26的末端表面26a的末端覆盖部分50a。在紧固构件26的外周侧和内周侧，通过外周侧圆筒部50c和内周侧圆筒部50c充分确保与构件22的距离， 50B。尖端覆盖部50a比外周侧圆筒部50c和内周侧圆筒部50b薄。当紧固件主体25紧固到紧固件26时，可以减小顶部覆盖部分50a在厚度方向上的变形。版权所有（C）2013，JPO＆INPIT

9. 发明专利

JP2014080055A Lightening-resistant fastener and aircraft 有权
标题翻译：防辐射紧固件和飞机
公开(公告)号：JP2014080055A
公开(公告)日：2014-05-08
申请号：JP2012227650
申请日：2012-10-15
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： WATANABE YASUNORI , HIMENO HIROMITSU , YAMAKOSHI HIDEO
IPC分类号： B64C1/00 , B64D45/02 , F16B25/00 , F16B37/14
CPC分类号： B64D45/02 , F16B33/004 , F16B37/14
摘要： PROBLEM TO BE SOLVED: To secure smoothness of the airframe of an aircraft provided with an outer skin formed with a fiber-reinforced resin and a fastener provided with an insulation member used to fasten the outer skin to a supporting material.SOLUTION: An aircraft includes an outer skin 4 formed with a fiber-reinforced resin material, a supporting material and a lightening-resistant fastener 1. The lightening-resistant fastener 1 comprises a metal-made fastener body 2 having a shank part and a head part 20 and an insulation member 30 made of an insulating resin material and mounted on the head part 20. In the head part 20, a truncated cone like fastener seating surface 211 is formed. In the outer skin 4, a receiving surface 41 corresponding to the fastener seating surface 211 is formed. In the insulation member 30, there is formed an insulation seating surface 321 retracted from the fastener seating surface 211 and brought in contact with the receiving surface 41 by caving an area 41A of the receiving surface 41 opposite to the fastener seating surface 211.
摘要翻译：要解决的问题：为了确保设置有由纤维增强树脂形成的外皮的飞行器的机身的平滑度以及设置有用于将外皮固定到支撑材料的绝缘构件的紧固件。解决方案：飞机包括形成有纤维增强树脂材料的外皮4，支撑材料和防闪除紧固件1.防雷紧固件1包括金属制紧固件主体2，其具有柄部分和头部20以及绝缘体构件30由绝缘树脂材料制成并且安装在头部20上。在头部20中形成有截锥形的紧固件座表面211。在外皮4中形成有与紧固件安装面211对应的接收面41。在绝缘构件30中，形成有从紧固件座表面211缩回的绝缘座表面321，并且通过使接收表面41的与紧固件座面211相对的区域41A开口而与接收面41接触。

10. 发明专利

JP2013147079A Lightning protection fastener and method of mounting lightning protection fastener 有权
标题翻译：闪电保护紧固件和安装防雷保护装置的方法
公开(公告)号：JP2013147079A
公开(公告)日：2013-08-01
申请号：JP2012007469
申请日：2012-01-17
申请人： Mitsubishi Aircraft Corp , 三菱航空機株式会社
发明人： ASAHARA YUJI , YAMAKOSHI HIDEO , IYOMASA ATSUHIRO , NISHIMURA WATARU , TARUMI TAKEYASU , WATANABE YASUNORI , HASHIGAMI TORU , RIKUKAWA HIROSHI , IMAMURA HIDEO , TANIGUCHI NAOKI
IPC分类号： B64C1/00 , B64D45/02 , F16B37/14
CPC分类号： F16B39/225 , B64D45/02 , F16B5/02 , F16B33/004 , F16B37/14
摘要： PROBLEM TO BE SOLVED: To surely seal an arc by preventing a rise of a cap.SOLUTION: A sealant 34 filled in a cap 30A is made to overflow through both an opening at an end 30a of the cap 30A and a through-hole 40 of the cap 30A when the cap is pressed against a fastener member 25. With regard to the cap 30A, a ratio between the inside diameter D1 of the opening on the side of the one end 30a and the inside diameter D2 of the through-hole 40 at the other end 30b is set as follows: 0.10≤D2/D1≤0.27.
摘要翻译：要解决的问题：通过防止帽的上升来确实地密封电弧。解决方案：填充在帽30A中的密封剂34通过帽30A的端部30a处的开口和通孔40 当帽被压靠在紧固构件25上时，盖30A的关系。关于帽30A，一端30a侧的开口的内径D1和通孔的内径D2之间的比率 40的另一端30b设定如下：0.10≤D2/D1≤0.27。

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