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公开(公告)号：US20150217523A1
公开(公告)日：2015-08-06
申请号：US14568279
申请日：2014-12-12
CPC分类号： B29C73/34 , B29C35/041 , B29C65/18 , B29C65/4835 , B29C66/81455 , B29C66/8183 , B29C66/87 , B29C66/91431 , B29C66/91631 , B29C73/02 , B29C73/10 , B29C2035/043 , B29L2031/3076 , Y10T156/10
摘要： The present invention provides a device which can uniformize heat distribution by using an existing heater mat for repairing or joining members. A heat dispersion device includes a bag with a fluid sealed inside, and is disposed on a second surface of a heater mat which has a first surface to be directed toward an object to be heated and the second surface opposite to the first surface. The fluid inside the bag is preferably heated with a heat source.
摘要翻译： 本发明提供一种能够通过使用现有的用于修理或接合构件的加热垫来均匀分配热量的装置。 散热装置包括具有密封在内部的流体的袋，并且设置在加热垫的第二表面上，所述加热垫具有要朝向待加热物体的第一表面和与第一表面相对的第二表面。 袋内的流体优选用热源加热。
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公开(公告)号：US20160185469A1
公开(公告)日：2016-06-30
申请号：US14950655
申请日：2015-11-24
发明人： Tomohiro UJITA , Masayoshi SUHARA
CPC分类号： G01N21/8806 , B64F5/60 , G01N21/8851 , G01N2021/8887
摘要： An aircraft appearance inspection method includes an initial data acquisition step of acquiring initial data at an initial time, an inspection data acquisition step of acquiring inspection data at the time of inspection, and a difference acquisition step of acquiring differences between the initial data and the inspection data. A first step through a third step are performed at the initial time and at the time of inspection. The first step is to radiate light toward an applicable area of an airframe of an aircraft through a member having a repetitive pattern, in which a predetermined shape is repeated, to display on the airframe a repetitive pattern corresponding to the repetitive pattern of the member. The second step is to image the applicable area over which the repetitive pattern is displayed. The third step is to acquire data of an image taken of the applicable area.
摘要翻译： 飞机外观检查方法包括初始数据获取步骤，初始时间获取初始数据，检查数据获取步骤，在检查时获取检查数据;以及差异获取步骤，获取初始数据和检查之间的差异 数据。 在第三步骤的第一步是在初始时间和检查时进行。 第一步是通过具有重复图案的构件向飞机的机身的适用区域辐射光，其中重复了预定的形状，以在机身上显示与构件的重复图案相对应的重复图案。 第二步是对显示重复图案的适用区域进行成像。 第三步是获取拍摄适用区域的图像的数据。
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公开(公告)号：US20140290831A1
公开(公告)日：2014-10-02
申请号：US14220624
申请日：2014-03-20
CPC分类号： B29C73/10 , B29C73/12 , B29C2035/1616 , B29C2035/1658
摘要： To reduce a time required for repairing a honeycomb core sandwich panel. A repair method according to the present invention is a repair method, in which a repair patch 20 is disposed on a repair target portion that exists on the side of a repair surface 1A of a honeycomb core sandwich panel 1, the honeycomb core sandwich panel 1 being formed by sandwiching a honeycomb structured core 10 with a plurality of cells between skins 11 and 12, the method including: a heating step of heating the repair patch 20; and a cooling step of cooling the honeycomb core sandwich panel 1 from the side of a second surface 1B opposing the repair surface 1A of the honeycomb core sandwich panel 1.
摘要翻译： 以减少修理蜂窝芯夹芯板所需的时间。 根据本发明的修复方法是修复方法，其中将修补贴片20设置在存在于蜂窝芯夹层板1的修复面1A侧的修复对象部分上，蜂窝芯夹层板1 通过将具有多个细胞的蜂窝结构核心10夹在皮肤11和12之间而形成，所述方法包括：加热修补贴片20的加热步骤; 以及从与蜂窝芯夹层板1的修复面1A相对的第二面1B的一侧冷却蜂窝芯夹层板1的冷却工序。
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4.发明申请METHOD FOR REPAIRING LIGHTNING PROTECTION MATERIAL, AND MEMBER PROVIDED WITH LIGHTNING PROTECTION MATERIAL 审中-公开用于维护防雷材料的方法，以及提供防雷材料的部件公开(公告)号：US20160137310A1
公开(公告)日：2016-05-19
申请号：US14876137
申请日：2015-10-06
CPC分类号： B64D45/02
摘要： The present invention provides a method for repairing a lightning protection material that is made of a metal material and is provided along a surface of a member formed by using a fiber reinforced resin includes: bonding a repair material made of a metal material over a lost region of the member where the lightning protection material is lost by using a liquid adhesive and a sheet-shaped holder that contains and holds the adhesive and is arranged at the lost region.
摘要翻译： 本发明提供一种修复由金属材料制成的防雷材料的方法，沿着通过使用纤维增强树脂形成的构件的表面设置，包括：将由金属材料制成的修补材料粘结在失去的区域上 通过使用液体粘合剂而损坏防雷材料的构件和包含并保持粘合剂并且布置在丢失区域的片状保持器。
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5.发明申请REPAIR METHOD OF REPAIR TARGET PORTION, AND REPAIRED PRODUCT OBTAINED FROM REPAIRING 有权维修对象部分修理方法及修理后的维修产品公开(公告)号：US20140295124A1
公开(公告)日：2014-10-02
申请号：US14226983
申请日：2014-03-27
IPC分类号： B29C73/10
CPC分类号： B29C73/10 , B29C73/12 , Y10T428/20
摘要： The present invention relates to a repair method using a pre-cured repairing patch, and a repaired product obtained from repairing using the repairing patch, and the present invention securely bonds a repairing patch, where an out-of-plane stiffness is required, to a repair target. In order to cover a repair target portion 23 formed in an outer panel 2 with a repairing patch 30, and bond the repairing patch 30 to a repair target, repairing plates 31, 32 that are formed of fibers and thermosetting resin, and pre-cured before repairing are used as the repairing patch 30, and a laminating step S4 of laminating the repairing plates 31, 32, and a bonding step S7 of bonding the repairing plates 31, 32 to each other are performed.
摘要翻译： 本发明涉及一种使用预固化修复补片的修复方法以及使用修补补片进行修复的修补产品，并且本发明将需要的平面外刚度的修复补片牢固地结合到 修复目标。 为了覆盖用修补补片30形成在外板2中的修补目标部分23，并将修补补片30粘合到修复对象上，由纤维和热固性树脂形成的修复板31,32和预固化 在修复之前用作修补贴片30，并且执行层压修复板31,32的层压步骤S4和将修复板31,32彼此粘合的粘合步骤S7。
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公开(公告)号：US20150228064A1
公开(公告)日：2015-08-13
申请号：US14614587
申请日：2015-02-05
IPC分类号： G06T7/00
CPC分类号： G06T7/75 , G06T2207/10028 , G06T2207/30108 , G06T2207/30248
摘要： To provide a structure maintenance supporting system that can accurately and quickly associate any position on a structure with a position in the drawing of the structure that is referred to at the time of maintenance. A maintenance supporting system includes an image displaying device that displays an image of a structure to be referred to when any damaged position on the structure is maintained, and a processing unit that performs calculation to associate the damaged position with a position in the image. The processing unit includes a damaged position calculating section that calculates a target coordinate which is the coordinate of the damaged position using known coordinates given to a plurality of reference points, and a position specifying section that specifies a position in the image corresponding to the target coordinate with an indication on the image displaying device.
摘要翻译： 提供一种结构维护支持系统，其可以将结构上的任何位置准确和快速地关联到在维护时所参考的结构的图中的位置。 维护支持系统包括图像显示装置，其在保持结构上的任何损坏位置时显示要参考的结构的图像;以及处理单元，其执行将损坏位置与图像中的位置相关联的计算。 处理单元包括：损坏位置计算部，使用已知的多个基准点的坐标来计算作为损伤位置的坐标的目标坐标;以及位置确定部，其指定与目标坐标对应的图像中的位置 在图像显示装置上具有指示。
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7.发明申请REPAIR METHOD OF REPAIR TARGET PORTION, REPAIRED PRODUCT, AND REPAIR APPARATUS 审中-公开维修目标部件，维修产品和维修设备的维修方法公开(公告)号：US20140295125A1
公开(公告)日：2014-10-02
申请号：US14227171
申请日：2014-03-27
发明人： Kiwamu ARIKAWA , Masayoshi SUHARA , Hiroyuki ISEKI , Shuhei MUTO
CPC分类号： B64C3/26 , B29C35/0272 , B29C65/342 , B29C65/348 , B29C65/4835 , B29C66/1122 , B29C66/71 , B29C66/7212 , B29C73/10 , B29C73/12 , B29C2035/0211 , B29L2031/608 , B32B27/04 , B32B27/12 , B64C1/12 , B64F5/40 , Y10T428/20
摘要： The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.
摘要翻译： 本发明充分地加热修复材料，同时防止设置有修补材料的基材的质量变化，从而将修复材料牢固地粘合到修复目标部分。 为了修复存在于外板1中的修理对象部分14，本发明的修理方法包括：修复材料配置步骤，配置包括电阻加热元件23和碳纤维增强树脂的修补贴片21， 以及在硬化之前包括热固性树脂的粘合剂22A，用于将修复补片21粘合在修复对象部分14上; 以及通过使电阻加热元件23通过向其供电而产生热量来加热和硬化粘合剂22A的热固性树脂的加热 - 硬化步骤。
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公开(公告)号：US20160236769A1
公开(公告)日：2016-08-18
申请号：US14977928
申请日：2015-12-22
IPC分类号： B64C7/00
CPC分类号： B64C5/02 , B64C1/1453
摘要： There is provided a drainage system of an aircraft which discharges moisture having entered inside horizontal tails, which are structures of an airframe of an aircraft, toward the rear end of a fuselage, the drainage system including: a drainage channel which includes an introduction end and a discharge end, and by a capillary action delivers moisture introduced from the introduction end toward the discharge end; and a heater which heats and dries the moisture delivered through the drainage channel. The drainage channel of the present invention is preferably composed of a paper drainage material. It is also preferable that the introduction end of the drainage channel is provided in a lowermost region in the vertical direction within an area in which moisture can accumulate inside the horizontal tails while the aircraft is parked.
摘要翻译： 提供了一种飞机的排水系统，其排出作为机身的机身的结构的飞机内侧的水平尾部朝向机身的后端排出的水分，该排水系统包括：排水通道，其包括引入端和 排出端，并且通过毛细管作用将从引入端引入的湿气输送到排出端; 以及对通过排水通道输送的水分进行加热和干燥的加热器。 本发明的排水通道优选由排纸材料构成。 还优选的是，在飞行器停放的同时，在水平尾部内的水分积聚的区域内，排水通道的引导端部设置在垂直方向的最下部的区域。
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公开(公告)号：US20140290851A1
公开(公告)日：2014-10-02
申请号：US14227211
申请日：2014-03-27
发明人： Katsumi TAKAGI , Masayoshi SUHARA , Shuhei MUTO
IPC分类号： B29C73/02
CPC分类号： B29C73/12 , B29C73/10 , B29K2301/10 , B29L2031/3076
摘要： A repair method according to the present invention is a method for repairing a honeycomb core sandwich panel 1, the method including: a repair patch disposing step S1 of disposing a repair patch 20 and an adhesive 21A on at least one of a first surface 1A and a second surface 1B of the panel 1, the first outer skin 11 being located on the first surface 1A, and the second outer skin 12 being located on the second surface 1B; a panel restraining step S3 of sandwiching the panel 1 and the repair patch 20 from both surface sides of the first surface 1A and the second surface 1B and thereby restraining the panel 1; and a heating step (thermal curing step) S4 of heating the adhesive 21A while the panel 1 is restrained.
摘要翻译： 根据本发明的修复方法是一种修复蜂窝芯夹层板1的方法，该方法包括：修复贴片设置步骤S1，将修补贴片20和粘合剂21A设置在第一表面1A和 面板1的第二表面1B，第一外皮11位于第一表面1A上，第二外皮12位于第二表面1B上; 面板限制步骤S3，从第一表面1A和第二表面1B的两个表面侧夹住面板1和修补贴片20，从而限制面板1; 以及在限制面板1的同时加热粘合剂21A的加热步骤（热固化步骤）S4。
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公开(公告)号：US20140290832A1
公开(公告)日：2014-10-02
申请号：US14227362
申请日：2014-03-27
发明人： Kiwamu ARIKAWA , Masayoshi SUHARA , Hiroyuki ISEKI , Shuhei MUTO
CPC分类号： B29C73/10 , B29C73/12 , B29C73/30 , B29C73/34 , B29C2035/0855
摘要： The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes a repairing material disposing step of disposing a repairing patch 20 and an adhesive 21A to the repair target portion 14; and a heating-hardening step of heating and hardening the adhesive 21A by irradiating it with electromagnetic waves.
摘要翻译： 本发明充分地加热修复材料，同时防止设置有修补材料的基材的质量变化，从而将修复材料牢固地粘合到修复目标部分。 为了修复存在于外板1中的修理对象部分14，本发明的修复方法包括将修补补片20和粘合剂21A设置到修复对象部14的修复材料配置工序; 以及通过用电磁波照射粘合剂21A进行加热硬化的加热硬化工序。
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