Method and apparatus for producing compact of rare earth alloy powder and rare earth magnet
    1.
    发明授权
    Method and apparatus for producing compact of rare earth alloy powder and rare earth magnet 有权
    制造稀土合金粉末和稀土磁体的方法和装置

    公开(公告)号:US06756010B2

    公开(公告)日:2004-06-29

    申请号:US10166250

    申请日:2002-06-11

    IPC分类号: B22F300

    摘要: A method for producing a compact of rare earth alloy powder of the present invention includes: a powder-filling step of filling rare earth allow powder in a cavity formed by inserting a lower punch into a through hall of a die of a powder compacting machine; and a compression step of pressing the rare earth alloy powder while applying a magnetic field, the steps being repeated a plurality of times. When the (n+1)th (n is an integer equal to or more than 1) stage compression step is to be carried out, the top surface of a compact produced in the n-th stage compression step is placed at a position above the bottom surface of a magnetic portion of a die.

    摘要翻译: 本发明的稀土类合金粉末的成型体的制造方法包括:粉末填充工序,其向粉末压制机的模具的通孔内插入下冲头而形成的空腔中填充稀土, 以及在施加磁场的同时挤压稀土合金粉末的压缩步骤,重复该步骤多次。 当要执行第(n + 1)(n是等于或大于1)的级压缩步骤时,在第n级压缩步骤中产生的压块的顶表面被放置在 模具的磁性部分的底表面。

    Vane tip clearance management structure for gas turbine
    4.
    发明授权
    Vane tip clearance management structure for gas turbine 有权
    燃气轮机叶片间隙管理结构

    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

    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)。

    Plate-like-object manufacturing method, plate-like objects, gas-turbine combustor, and gas turbine
    5.
    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

    IPC分类号: F02C3/00 B23P19/00 B32B15/00

    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。

    HEAT TREATMENT METHOD
    6.
    发明申请
    HEAT TREATMENT METHOD 有权
    热处理方法

    公开(公告)号:US20100221441A1

    公开(公告)日:2010-09-02

    申请号:US12377408

    申请日:2007-09-14

    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。

    Turbine casing structure
    7.
    发明授权
    Turbine casing structure 有权
    涡轮机壳结构

    公开(公告)号:US07581922B1

    公开(公告)日:2009-09-01

    申请号:US11344340

    申请日:2006-02-01

    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。

    Method of magnetizing rare-earth magnet and rare-earth magnet
    8.
    发明授权
    Method of magnetizing rare-earth magnet and rare-earth magnet 有权
    稀土磁体和稀土磁体的磁化方法

    公开(公告)号:US07232495B2

    公开(公告)日:2007-06-19

    申请号:US10485210

    申请日:2002-07-29

    IPC分类号: H01F1/053 H01F7/06

    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。

    Ink-jet textile printing method
    9.
    发明申请
    Ink-jet textile printing method 有权
    喷墨纺织印花法

    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

    IPC分类号: B41J2/015 B41J2/17

    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。

    Plasma spray coating method
    10.
    发明授权
    Plasma spray coating method 有权
    等离子喷涂法

    公开(公告)号:US08617637B2

    公开(公告)日:2013-12-31

    申请号:US12991905

    申请日:2008-06-25

    IPC分类号: C23C4/00 B05D3/06

    CPC分类号: C23C4/02 C23C4/12

    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。