公开(公告)号：US07232853B2

公开(公告)日：2007-06-19

申请号：US10033897

申请日：2002-01-03

申请人： Michiei Nakamura ,  Shigeru Takarada ,  Hiroyuki Shimanaka ,  Kotaro Ohshima ,  Shinya Tuchida

发明人： Michiei Nakamura ,  Shigeru Takarada ,  Hiroyuki Shimanaka ,  Kotaro Ohshima ,  Shinya Tuchida

IPC分类号： B22F1/00

CPC分类号： B01J2/02 ,  C08J3/12 ,  C08J2367/02

摘要： Colored fine particulate resins can each be produced by bringing a colored resin, which comprises a thermally fusible resin and a colorant evenly distributed in the thermally fusible resin, into a molten state; forming the colored resin, which is in the molten state, into droplet-shaped fine particles in a non-dissolving medium which does not dissolve the colored resin; and then cooling and solidifying the droplet-shaped fine particles. The colored fine particulate resins are useful in image recording materials, printing materials and paints. Articles can be colored with the image recording materials, printing materials or paints.

摘要翻译： 可以通过将包含热熔性树脂和均匀分布在热熔树脂中的着色剂的着色树脂引入熔融状态来分别制造着色的细颗粒树脂。 将处于熔融状态的着色树脂形成不溶于着色树脂的不溶解介质中的液滴状微粒; 然后冷却并固化液滴状微粒。 着色的细颗粒树脂可用于图像记录材料，印刷材料和油漆中。 物品可以用图像记录材料，印刷材料或油漆着色。

公开(公告)号：US06811373B2

公开(公告)日：2004-11-02

申请号：US10067947

申请日：2002-02-08

申请人： Yasuoki Tomita ,  Shigehiro Shiozaki ,  Kengo Yamaguchi ,  Hideaki Kaneko ,  Kotaro Ohshima

发明人： Yasuoki Tomita ,  Shigehiro Shiozaki ,  Kengo Yamaguchi ,  Hideaki Kaneko ,  Kotaro Ohshima

IPC分类号： F01D518

CPC分类号： F01D5/288 ,  C23C28/00 ,  F01D9/02 ,  F05D2230/90 ,  F05D2240/80 ,  F05D2300/611

摘要： The present invention provides a turbine moving blade, a turbine stationary blade, and a turbine split ring which are capable of restraining the deterioration and peeling-off of a thermal barrier coating easily and surely, and a gas turbine capable of enhancing the energy efficiency by increasing the temperature of combustion gas. The turbine moving blade provided in a turbine constituting the gas turbine includes a platform having a gas path surface extending in the combustion gas flow direction, and a blade portion erecting on the platform. The thermal barrier coating covering the gas path surface is formed so as to go around from the gas path surface to an upstream-side end face and a downstream-side end face of the outer peripheral faces of the platform.

摘要翻译： 本发明提供了能够容易且可靠地抑制热障涂层的劣化和剥离的涡轮机动叶片，涡轮静叶片和涡轮分裂环，以及能够通过以下方式提高能量效率的燃气轮机 增加燃烧气体的温度。 设置在构成燃气轮机的涡轮机中的涡轮机动叶片具有在燃烧气体流动方向上具有气体流路面的平台和在平台上竖起的叶片部。 覆盖气体路径表面的隔热涂层形成为从气体路径表面到平台的外周面的上游侧端面和下游侧端面。

公开(公告)号：US06893215B2

公开(公告)日：2005-05-17

申请号：US10025593

申请日：2001-12-26

申请人： Masamitsu Kuwabara ,  Yoshiyuki Morii ,  Yasuoki Tomita ,  Shunsuke Torii ,  Shigehiro Shiozaki ,  Kotaro Ohshima ,  Tatsuaki Fujikawa ,  Ryotaro Magoshi ,  Shinichi Inoue

发明人： Masamitsu Kuwabara ,  Yoshiyuki Morii ,  Yasuoki Tomita ,  Shunsuke Torii ,  Shigehiro Shiozaki ,  Kotaro Ohshima ,  Tatsuaki Fujikawa ,  Ryotaro Magoshi ,  Shinichi Inoue

IPC分类号： F01D5/34 ,  F01D9/02 ,  F01D9/04 ,  F01D11/00 ,  F01D25/24 ,  F01D25/26

CPC分类号： F01D11/005 ,  F01D11/006 ,  F01D11/008

摘要： The division wall is made up of a plurality of division wall sections forming a passage wall of high temperature gas which are connected in the direction of arrangement of blades to form a wall surface having a roughly circular cross section as a whole, a gas flow restricting structure for preventing high temperature gas from passing through a gap formed at a connecting portion between the division wall sections in the flow direction of the high temperature gas from the opening on the upstream side of the high temperature gas in the gap, or a gas flow restricting structure for preventing the high temperature gas from being embraced in the gap, for example, a sealing member formed into a prism having a T-shape cross section as a whole composed of a plane portion as a sealing portion and a projected portion for filling the gap is provided.

摘要翻译： 分隔壁由多个分隔壁部分构成，形成高温气体的通道壁，其沿着叶片的排列方向连接以形成整个具有大致圆形横截面的壁表面， 结构，用于防止高温气体从形成在高温气体的流动方向上的分隔壁部分之间的连接部分处的间隙从间隙中的高温气体的上游侧的开口或气流 限制结构用于防止高温气体包围在间隙中，例如，形成为具有作为整体的T形横截面的棱镜的密封构件由作为密封部分的平面部分和用于填充的突出部分组成 提供了差距。