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公开(公告)号：US07232495B2
公开(公告)日：2007-06-19
申请号：US10485210
申请日：2002-07-29
申请人： Eiji Sakaguchi , Hitoshi Morimoto
发明人： Eiji Sakaguchi , Hitoshi Morimoto
CPC分类号： H01F13/003 , H02K15/03 , Y10T29/4902
摘要： The method of the present invention includes a step of preparing a rare earth magnet 22 disposed for forming a cylinder 22a, a first magnetizing step of applying a first external magnetic field H1 to the rare earth magnet 22, thereby forming a first region R1 magnetized from an inner side to an outer side of the cylinder 22a and a second region R2 magnetized from the outer side to the inner side, and a second magnetizing step of applying a second external magnetic field H2 so that an external magnetic field component forming an angle of more than 0° and less than 50° with a direction of the external magnetic field component applied in the first magnetizing step to a boundary between the first region R1 and the second region R2.
摘要翻译： 本发明的方法包括制备用于形成气缸22a的稀土磁体22的制备步骤，向稀土磁体22施加第一外部磁场H 1的第一磁化步骤，从而形成第一区域R 1从气缸22a的内侧到外侧被磁化，从外侧到内侧被磁化的第二区R 2和施加第二外部磁场H 2的第二磁化步骤，使得外部磁 场分量通过在第一磁化步骤中施加的外部磁场分量的方向形成大于0°且小于50°的角度至第一区域R 1和第二区域R 2之间的边界。
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公开(公告)号：US08313283B2
公开(公告)日：2012-11-20
申请号：US12066731
申请日：2006-09-11
申请人： Hitoshi Morimoto
发明人： Hitoshi Morimoto
IPC分类号： F01D25/00
CPC分类号： F01D25/00 , F01D21/003 , F05D2260/80
摘要： Provided is a vane tip clearance management structure for a gas turbine which allows a vane tip clearance to be confirmed easily at the time of completing assembly. For this purpose, there are provided: a casing (3) rotatably supporting a rotor (2); stator vane retainer rings (11, 12, and 13) and a turbine vane ring (16) provided to have predetermined clearances from tips of rotor vanes (10 and 15) fitted in multiple steps to the rotor (2) inside in the radial direction of the casing (3); guide frames (26) penetrating the casing (3), the stator vane retainer rings (11, 12, and 13) and the turbine vane ring (16) in the radial direction and being supported by stepped portions (21a, 22a, 23a, and 24a); and rods (25) movably supported by the guide frames (26) and abutting on the tips of the rotor vanes (10 and 15). Clearances (C1 and C2) are measured based on the amounts of movement of the rods (25) relative to the guide frames (26).
摘要翻译： 提供一种用于燃气轮机的叶片顶端间隙管理结构，其允许在组装完成时容易地确认叶片顶端间隙。 为此，提供：可旋转地支撑转子（2）的壳体（3）; 定子叶片保持环（11,12,13）和涡轮叶片环（16），其被设置成具有从转子叶片（10和15）的顶端到径向方向上安装到转子（2）的多个台阶的预定间隙 的壳体（3）; 定子叶片保持环（11,12,13）和涡轮叶片环（16）沿径向穿过壳体（3）的引导框架（26），并由台阶部分（21a，22a，23a， 和24a）; 以及由引导框架（26）可移动地支撑并抵靠转子叶片（10和15）的顶端的杆（25）。 基于杆（25）相对于引导框架（26）的移动量来测量间隙（C1和C2）。
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3.发明申请Plate-like-object manufacturing method, plate-like objects, gas-turbine combustor, and gas turbine 有权板状物体制造方法，板状物体，燃气轮机燃烧器和燃气轮机公开(公告)号：US20110146284A1
公开(公告)日：2011-06-23
申请号：US12646115
申请日：2009-12-23
申请人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
发明人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
CPC分类号： B23K26/30 , B23K1/0018 , B23K2101/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： A plate-like-object manufacturing method, plate-like objects, a gas-turbine combustor, and a gas turbine, in which degradation in the cooling performance can be suppressed, the time required for manufacturing a gas-turbine combustor can be shortened, and deterioration of the working environment can be prevented are provided. A plate-like-object manufacturing method includes a step of forming a plate-like object by stacking a plurality of plates and arranging a plurality of channels, through which a cooling medium flows, side-by-side between the plurality of plates; and a step of arranging a plurality of the plate-like objects side-by-side in a direction in which the channels are arranged, butting the plurality of plate-like objects against each other, and performing welding at an abutment section. The channels adjacent to the abutment section extend along the abutment section and have a greater dimension in the direction in which the channels are arranged, as compared with that of other channels.
摘要翻译： 能够抑制冷却性能的劣化的板状物体，燃气轮机燃烧器和燃气轮机，能够缩短制造燃气轮机燃烧器所需的时间， 并且可以防止工作环境的劣化。 板状物体的制造方法包括通过堆叠多个板并且在多个板之间并排布置冷却介质流过的多个通道来形成板状物体的步骤; 以及在排列通道的方向并列配置多个板状物体的步骤，使多个板状物体彼此抵接，并在邻接部分进行焊接。 与邻接部分相邻的通道相对于其它通道而言沿着邻接部分延伸并且在通道布置方向上具有更大的尺寸。
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公开(公告)号：US20100221441A1
公开(公告)日：2010-09-02
申请号：US12377408
申请日：2007-09-14
申请人： Hitoshi Morimoto , Hidenobu Tamai , Yuya Fujii , Kazutaka Mori , Taiji Torigoe , Yasuhiko Tsuru
发明人： Hitoshi Morimoto , Hidenobu Tamai , Yuya Fujii , Kazutaka Mori , Taiji Torigoe , Yasuhiko Tsuru
IPC分类号： B05D3/02
摘要： A silicon resin (7) is applied to the outer wall (1b) of the transition piece (1) subjected to the thermal barrier coating by caulking the cooling holes (2a) provided in the inner wall (1a) by a resin (4). Then, the transition piece (1) is heated in an atmosphere furnace in order to burn or decompose the resin (4). A part of the silicon resin (7) applied to the outer wall (1b) of the transition piece (1) is decomposed or evaporated by the heating to be discharged to the atmosphere in the furnace, but a part of the silicon resin (7) remains and protects the outer wall (1b). Then, since the remaining silicon resin (7) protects the outer wall (1b), it is possible to reduce oxidization of the outer wall (1b) or an unevenness in color caused by the oxidization. Accordingly, it is possible to remarkably reduce the time required to improve an external appearance of the transition piece (1) after the ashing process for the transition piece (1). Moreover, the heat treatment method according to the present invention is not limited to the application to the ashing process for the transition piece (1), but can be applied to the whole product required to be subjected to the heat treatment.
摘要翻译： 通过用树脂（4）铆接设置在内壁（1a）中的冷却孔（2a），将硅树脂（7）施加到经过隔热涂层的过渡件（1）的外壁（1b） 。 然后，将过渡件（1）在气氛炉中加热，以使树脂（4）燃烧或分解。 施加到过渡件（1）的外壁（1b）上的硅树脂（7）的一部分通过加热分解或蒸发，以排放到炉中的大气中，但是部分硅树脂（7） ）保留并保护外壁（1b）。 然后，由于剩余的硅树脂（7）保护外壁（1b），所以可以减少外壁（1b）的氧化或氧化引起的不均匀性。 因此，可以显着地减少在过渡件（1）的灰化处理之后改善过渡件（1）的外观所需的时间。 此外，本发明的热处理方法不限于对过渡件（1）的灰化处理的应用，而是可以应用于要进行热处理的整个产品。
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公开(公告)号：US07581922B1
公开(公告)日：2009-09-01
申请号：US11344340
申请日：2006-02-01
申请人： Hitoshi Morimoto , Taichi Ozaki
发明人： Hitoshi Morimoto , Taichi Ozaki
IPC分类号： F01D25/24
CPC分类号： F01D25/26 , F01D25/285
摘要： A turbine casing structure having an outer casing, and an inner casing disposed in the outer casing, comprising: a bush disposed in a concave portion formed in the inner casing; an eccentric shaft inserted into a communication hole formed in the outer casing, and having a front end disposed in contact with the bush; and a fixing member disposed in engagement with the eccentric shaft, and fixed to the outer casing.
摘要翻译： 一种涡轮机壳体结构，具有外壳和设置在所述外壳中的内壳，包括：衬套，设置在形成在所述内壳中的凹部中; 插入到形成在所述外壳中的连通孔中并且具有与所述衬套接触设置的前端的偏心轴; 以及固定部件，与所述偏心轴配合配置，并固定在所述外壳体上。
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公开(公告)号：US07045093B2
公开(公告)日：2006-05-16
申请号：US10399252
申请日：2002-07-26
CPC分类号： C04B35/5805 , B22F5/003 , B22F2998/10 , B28D5/007 , B28D5/0076 , B28D5/045 , C04B35/5156 , C22C1/0441 , H01F1/0577 , H01F41/0253 , H01F41/0266 , Y02P70/179 , Y10T29/49995 , Y10T83/9292 , B22F3/02 , B22F3/10
摘要： A method for manufacturing a sintered magnet includes the steps of producing a green compact of powder for the sintered magnet, machining the green compact with a wire-saw, and sintering the green compact.
摘要翻译： 制造烧结磁体的方法包括以下步骤：制造用于烧结磁体的粉末的生坯，用线锯加工生坯，并烧结生坯。
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公开(公告)号：US20060087540A1
公开(公告)日：2006-04-27
申请号：US11255672
申请日：2005-10-20
申请人： Hitoshi Morimoto
发明人： Hitoshi Morimoto
CPC分类号： D06P5/30 , D06P1/46 , D06P1/5221 , D06P1/5257 , D06P1/653 , D06P1/67316 , D06P3/54
摘要： A method of forming an ink-jet image containing the steps of: applying a pre-treatment solution to a textile; and ejecting droplets of an ink-jet ink on the textile through an ink-jet head, wherein the ink-jet ink comprises a disperse dye, a dispersing agent, water and a water-soluble organic solvent; the pre-treatment solution comprises an organic acid; and a pH value of the pre-treatment solution is smaller than a pH value of the ink-jet ink.
摘要翻译： 一种形成喷墨图像的方法，包括以下步骤：将预处理溶液施加到织物上; 并通过喷墨头将喷墨墨滴喷射到纺织品上，其中喷墨油墨包括分散染料，分散剂，水和水溶性有机溶剂; 预处理溶液包含有机酸; 并且预处理溶液的pH值小于喷墨油墨的pH值。
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公开(公告)号：US08617637B2
公开(公告)日：2013-12-31
申请号：US12991905
申请日：2008-06-25
申请人： Hitoshi Morimoto , Yoriaki Inoue
发明人： Hitoshi Morimoto , Yoriaki Inoue
摘要： A thermal spraying method includes forming a coating layer of heat resistant resin on the whole spray area of the metal surface, securely fixing a test piece of the same material as that of the metal as a constituent of heat resistant equipment on the surface of the coating layer, spraying a heat shield coating material onto the test piece, detaching the test piece from the surface of the coating layer, inspecting the condition of spray and setting spray conditions, removing the coating layer and, under the above set spray conditions, spraying the heat shield coating material onto the metal surface to thereby form a heat shield coating layer.
摘要翻译： 热喷涂方法包括在金属表面的整个喷涂区域上形成耐热树脂涂层，将与金属相同的材料作为耐热设备的组分的试样牢固地固定在涂层的表面上 将隔热涂料喷涂到试片上，将试片从涂层表面上分离出来，检查喷雾状况和设定喷雾条件，除去涂层，并在上述设定的喷雾条件下喷涂 将金属表面上的隔热涂层材料隔热，从而形成隔热涂层。
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公开(公告)号：US20120269622A1
公开(公告)日：2012-10-25
申请号：US13357179
申请日：2012-01-24
IPC分类号： F01D9/02
CPC分类号： F16J15/0887 , F01D9/04 , F01D11/005 , F05D2240/55 , F16J15/4476
摘要： A turbine vane of the invention includes: a plurality of outer shrouds (8a) that are provided along the turbine circumferential direction so as to be adjacent to each other and form an outer wall of a main passageway; inner shrouds (8b) that form an inner wall; a airfoil body (8c) that protrudes from a front surface of the inner shroud (8b) and defines a flow of combustion gas directed from the upstream side of the main passageway toward the downstream side thereof; and a retainer (8d) which protrudes from a rear surface of the inner shroud (8b) and extends along the turbine circumferential direction, wherein the retainer (8d) is disposed on the downstream side in relation to an intersection point (Q) between a dividing gap (K1) of the adjacent inner shrouds (8b) and a throat line (P) which connects the contact points of a minimal inscribed circle according to the blade shapes of the adjacent airfoil bodies (8c).
摘要翻译： 本发明的涡轮叶片包括：沿着涡轮机圆周方向设置成彼此相邻并形成主通道的外壁的多个外护罩（8a）; 形成内壁的内护罩（8b） 从所述内护罩（8b）的前表面突出并限定从所述主通道的上游侧向其下游侧引导的燃烧气体流的翼型体（8c）; 以及从所述内罩（8b）的后表面突出并沿着所述涡轮机周向延伸的保持器（8d），其中，所述保持器（8d）相对于所述内护罩 根据相邻翼型体（8c）的叶片形状，相邻的内护罩（8b）的分隔间隙（K1）和连接最小内切圆的接触点的喉管（P）。
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公开(公告)号：US20110104382A1
公开(公告)日：2011-05-05
申请号：US12991905
申请日：2008-06-25
申请人： Hitoshi Morimoto , Yoriaki Inoue
发明人： Hitoshi Morimoto , Yoriaki Inoue
摘要： A thermal spraying method in which masking operation on the surface of a spray object can be facilitated and in which a test piece can be fixed securely so as to enable setting of spray conditions. There is disclosed a thermal spraying method of performing a thermal spraying of heat shield coating material on the surface of a metal as a constituent of heat resistant equipment to thereby form a heat shield coating layer. The thermal spraying method is characterized by including the step of forming a coating layer of heat resistant resin on the whole spray area of the metal surface, securely fixing a test piece of the same material as that of the metal as a constituent of heat resistant equipment on the surface of the coating layer, spraying a heat shield coating material onto the test piece, detaching the test piece from the surface of the coating layer, inspecting the condition of spray and setting spray conditions; and the step of removing the coating layer and under the above set spray conditions, spraying the heat shield coating material onto the metal surface to thereby form a heat shield coating layer.
摘要翻译： 一种热喷涂方法，其中可以方便地对喷涂物体的表面进行掩蔽操作，并且可以牢固地固定试件，以便能够设定喷射条件。 公开了一种在作为耐热设备的组成部件的金属表面上进行热屏蔽涂层材料的热喷涂以形成隔热涂层的热喷涂方法。 热喷涂方法的特征在于包括在金属表面的整个喷涂区域上形成耐热树脂涂层的步骤，将与金属相同的材料作为耐热设备的组分牢固地固定 在涂层的表面上，将热屏蔽涂层材料喷涂在试件上，将试件从涂层表面上分离出来，检查喷涂条件和设定喷涂条件; 以及在上述设定的喷雾条件下除去涂层的步骤，将隔热涂料喷涂到金属表面上，从而形成隔热涂层。
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