专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08370084B2 Method for estimating physical property of ceramic, method for estimating physical property of thermal barrier coating, method for estimating remaining lifetime of thermal barrier coating, method for estimating remaining lifetime of high-temperature member, and physical property acquiring apparatus 有权
标题翻译：用于估计陶瓷的物理性能的方法，用于估计热障涂层的物理性质的方法，用于估计热障涂层的剩余寿命的方法，用于估计高温部件的剩余寿命的方法和物理性能获取装置
公开(公告)号：US08370084B2
公开(公告)日：2013-02-05
申请号：US12681704
申请日：2009-03-13
申请人： Katsumi Namba , Taiji Torigoe , Ikuo Okada , Kazutaka Mori , Yasuhiko Tsuru , Masato Shida , Ichiro Nagano , Eisaku Ito , Koji Takahashi
发明人： Katsumi Namba , Taiji Torigoe , Ikuo Okada , Kazutaka Mori , Yasuhiko Tsuru , Masato Shida , Ichiro Nagano , Eisaku Ito , Koji Takahashi
IPC分类号： G01B3/44 , C22C32/00 , B05D3/02
CPC分类号： G01N33/388 , C04B38/0074 , C04B2111/28 , G01N15/088 , G01N25/18 , C04B35/00
摘要： A method by which physical properties, including the Young's modulus and thermal conductivity of a ceramic layer of a thermal barrier coating formed on a high-temperature member, are quickly and accurately estimated. A method for estimating a physical property of a ceramic includes a step of calculating the Larson-Miller parameter from the time for which and the temperature at which the ceramic is heated; a step of acquiring the porosity of the ceramic corresponding to the calculated Larson-Miller parameter, based on the calculated Larson-Miller parameter and a diagram correlating the Larson-Miller parameter and the porosity obtained from samples having the same composition as the ceramic; and a step of acquiring the physical property of the ceramic corresponding to the acquired porosity, based on the acquired porosity and a diagram correlating the porosity and the physical property obtained from samples having the same composition as the ceramic.
摘要翻译：通过该方法可以快速，准确地估计包括形成在高温部件上的热障涂层的陶瓷层的杨氏模量和热导率的物理性质。用于估计陶瓷的物理性质的方法包括从陶瓷被加热的时间和温度计算出Larson-Miller参数的步骤; 基于所计算的Larson-Miller参数获得对应于计算的Larson-Miller参数的陶瓷的孔隙率的步骤，以及将与Larson-Miller参数和从具有与陶瓷相同组成的样品获得的孔隙率相关联的图; 以及基于获得的孔隙率获得与所获得的孔隙率相对应的陶瓷的物理性质的步骤，以及与具有与陶瓷相同组成的样品获得的孔隙率和物理性质相关联的图。

2. 发明申请

US20100242797A1 THERMAL BARRIER COATING MATERIAL 审中-公开
标题翻译：热障涂层材料
公开(公告)号：US20100242797A1
公开(公告)日：2010-09-30
申请号：US12675307
申请日：2009-02-03
申请人： Ichiro Nagano , Taiji Torigoe , Katsunori Akiyama , Masato Shida , Kazutaka Mori , Yasuhiko Tsuru , Ikuo Okada
发明人： Ichiro Nagano , Taiji Torigoe , Katsunori Akiyama , Masato Shida , Kazutaka Mori , Yasuhiko Tsuru , Ikuo Okada
IPC分类号： C09D5/00
CPC分类号： C23C30/00 , C04B35/495 , C04B2235/3224 , C04B2235/3225 , C04B2235/3251 , C04B2235/76 , C04B2235/9607 , C23C4/11 , C23C28/322 , C23C28/3455 , F05B2230/90 , Y02T50/67 , Y02T50/6765
摘要： A thermal barrier coating material having a lower thermal conductivity than rare earth stabilized zirconia materials. A thermal barrier coating material comprising mainly a compound represented by composition formula (1): Ln1-xTaxO1.5+x wherein 0.13≦x≦0.24, and Ln represents one or more elements selected from the group consisting of Sc, Y and the lanthanoid elements. Also, a thermal barrier coating material comprising mainly a compound represented by composition formula (2): Ln1-xNbxO1.5+x wherein 0.13≦x≦0.24, and Ln represents one or more elements selected from the group consisting of Sc, Y and the lanthanoid elements. Also, a thermal barrier coating material comprising mainly a cubic compound having a fluorite structure represented by composition formula (3): Ln3NbO7 wherein Ln represents one or more elements selected from the group consisting of Sc, Y and the lanthanoid elements.
摘要翻译：一种具有比稀土稳定的氧化锆材料更低热导率的热障涂层材料。主要由组成式（1）表示的化合物：Ln1-xTaxO1.5 + x的热障涂层材料，其中0.13＆nlE; x＆lt; lE; 0.24和Ln表示选自Sc，Y和镧系元素。此外，主要由组成式（2）表示的化合物：Ln1-xNbxO1.5 + x，其中0.13和n1E; x和nlE; 0.24和Ln表示选自Sc，Y的一种或多种元素的热障涂层材料和镧系元素。另外，主要包含由组成式（3）表示的萤石结构的立方体化合物：Ln3NbO7的热障涂层材料，其中Ln表示选自Sc，Y和镧系元素中的一种或多种元素。

3. 发明申请

US20100221441A1 HEAT TREATMENT METHOD 有权
标题翻译：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
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
CPC分类号： C23C26/00 , C21D1/70 , C23C4/01 , C23C8/04 , C23C8/10
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。

4. 发明授权

US07655326B2 Thermal barrier coating material and method for production thereof, gas turbine member using the thermal barrier coating material, and gas turbine 有权
标题翻译：隔热涂料及其制造方法，使用该热障涂层材料的燃气轮机部件和燃气轮机
公开(公告)号：US07655326B2
公开(公告)日：2010-02-02
申请号：US10478690
申请日：2002-06-14
申请人： Taiji Torigoe , Kazutaka Mori , Ikuo Okada , Sunao Aoki , Kouji Takahashi , Minoru Ohara , Takehiko Hirata
发明人： Taiji Torigoe , Kazutaka Mori , Ikuo Okada , Sunao Aoki , Kouji Takahashi , Minoru Ohara , Takehiko Hirata
IPC分类号： B32B15/04 , B32B18/00
CPC分类号： C23C4/18 , C23C4/073 , C23C4/11 , C23C28/3215 , C23C28/3455 , F01D5/288 , F05D2230/31 , F05D2230/311 , F05D2230/312 , F05D2230/40 , F05D2230/90 , F05D2300/2118
摘要： A thermal barrier coating material, containing a metal binding layer laminated on a base material and a ceramic layer laminated on the metal binding layer, the ceramic layer comprising partially stabilized ZrO2 which is partially stabilized by additives of Dy2O3 and Yb2O3.
摘要翻译：一种隔热涂料，其包含层叠在基材上的金属粘合层和层压在金属粘合层上的陶瓷层，所述陶瓷层包含部分稳定化的ZrO 2，其通过Dy2O3和Yb2O3的添加剂部分稳定。

5. 发明申请

US20090176059A1 Thermal Barrier Coating Member, Method for Producing the Same, Thermal Barrier Coating Material, Gas Turbine, and Sintered Body 有权
标题翻译：热障涂层部件，其制造方法，热障涂层材料，燃气轮机和烧结体
公开(公告)号：US20090176059A1
公开(公告)日：2009-07-09
申请号：US12225490
申请日：2006-10-06
申请人： Katsumi Namba , Taiji Torigoe , Ikuo Okada , Kazutaka Mori , Ichiro Nagano , Yutaka Kawata , Koji Takahashi
发明人： Katsumi Namba , Taiji Torigoe , Ikuo Okada , Kazutaka Mori , Ichiro Nagano , Yutaka Kawata , Koji Takahashi
IPC分类号： B32B15/00 , C09D1/00 , B05D1/36 , B05D5/00 , C23C14/34
CPC分类号： F02K9/974 , C04B35/486 , C04B2235/3206 , C04B2235/3208 , C04B2235/3224 , C04B2235/3225 , C04B2235/3227 , C04B2235/3229 , C04B2235/441 , C04B2235/656 , C04B2235/76 , C04B2235/77 , C04B2235/787 , C04B2235/9607 , C23C4/02 , C23C4/11 , C23C30/00 , F01D5/288 , F05D2230/90 , Y10T428/24471 , Y10T428/24999 , Y10T428/31678
摘要： There are provided a thermal barrier coating material and a thermal barrier coating member that can suppress spalling when used at a high temperature and have a high thermal barrier effect, a method for producing the same, a turbine member coated with a thermal barrier coating, and a gas turbine. The thermal barrier coating member comprises a heat resistant substrate, a bond coat layer formed thereon, and a ceramic layer formed further thereon, wherein the ceramic layer comprises an oxide which consists of an oxide represented by the general formula A2Zr2O7 doped with a predetermined amount of CaO or MgO and has 10 volume % or more of a pyrochlore type crystal structure, where A represents any of La, Nd, Sm, Gd, and Dy.
摘要翻译：提供了在高温下使用时具有高的隔热效果，能够抑制剥落的热障涂层材料及其制造方法，具有隔热涂层的涡轮部件，以及一个燃气轮机。隔热涂层构件包括耐热基材，形成在其上的粘合涂层和其上形成的陶瓷层，其中陶瓷层包括氧化物，该氧化物由掺杂有预定量的金属的通式A2Zr2O7表示， CaO或MgO，并且具有10体积％以上的烧绿石型晶体结构，其中A表示La，Nd，Sm，Gd和Dy中的任一种。

6. 发明申请

US20070155052A1 Method of fabricating a semiconductor integrated circuit that includes patterning a semiconductor substrate with a first photomask that uses metal for blocking light and patterning the same substrate with a second photomask that uses organic resin for blocking light 有权
公开(公告)号：US20070155052A1
公开(公告)日：2007-07-05
申请号：US11714837
申请日：2007-03-07
申请人： Tsuneo Terasawa , Toshihiko Tanaka , Ko Miyazaki , Norio Hasegawa , Kazutaka Mori
发明人： Tsuneo Terasawa , Toshihiko Tanaka , Ko Miyazaki , Norio Hasegawa , Kazutaka Mori
IPC分类号： H01L21/58
CPC分类号： G03F7/70425 , G03F1/00 , G03F1/56 , H01L2224/05001 , H01L2224/05008 , H01L2224/05022 , H01L2224/05024 , H01L2224/05569 , H01L2224/05572 , H01L2224/16225 , H01L2224/32225 , H01L2224/73204 , H01L2224/92125 , H01L2924/15311 , Y10S438/944 , Y10S438/946 , H01L2924/00
摘要： Productivity of a semiconductor integrated circuit device is improved. According to how many times the photomask is used, a photomask having an opaque pattern made of metal and a photomask having an opaque pattern made of a resist film are properly used, and thereby an exposure treatment is performed.

7. 发明授权

US07129549B2 Semiconductor integrated circuit device 失效
标题翻译：半导体集成电路器件
公开(公告)号：US07129549B2
公开(公告)日：2006-10-31
申请号：US10866991
申请日：2004-06-15
申请人： Masatoshi Hasegawa , Kazutaka Mori , Tomofami Hokari
发明人： Masatoshi Hasegawa , Kazutaka Mori , Tomofami Hokari
IPC分类号： H01L27/92
CPC分类号： G11C11/4085 , G11C5/063 , G11C7/18 , G11C11/4097 , H01L27/0207 , H01L27/10897
摘要： A semiconductor integrated circuit device realizing high integration and a simplified manufacturing process. The circuit includes a gate insulator with a first film thickness, a first N-channel MOSFET and a first P-channel MOSFET, in which a polysilicon layer consists of a gate electrode including an N-type impurity dose, and a gate insulator with a second film thickness thinner than the first film thickness. The circuit also includes a second N-channel MOSFET and a second P-channel MOSFET in which the polysilicon layers are doped with N-type impurity and P-type impurity, respectively. Gate electrodes of said first N-channel MOSFET and first P-channel MOSFET are formed as one body and connected to each other.
摘要翻译：实现高集成度和简化制造工艺的半导体集成电路器件。该电路包括具有第一膜厚度的栅极绝缘体，第一N沟道MOSFET和第一P沟道MOSFET，其中多晶硅层由包括N型杂质剂量的栅电极组成，栅绝缘体具有第二膜厚比第一膜厚薄。该电路还包括第二N沟道MOSFET和第二P沟道MOSFET，其中多晶硅层分别掺杂有N型杂质和P型杂质。所述第一N沟道MOSFET和第一P沟道MOSFET的栅极形成为一体并彼此连接。

8. 发明授权

US07109076B2 Method of manufacturing semiconductor integrated circuit device, and semiconductor integrated circuit device made by its method 失效
标题翻译：半导体集成电路器件的制造方法以及由其制造的半导体集成电路器件
公开(公告)号：US07109076B2
公开(公告)日：2006-09-19
申请号：US10855402
申请日：2004-05-28
申请人： Satoshi Sakai , Daichi Matsumoto , Katsuyuki Asaka , Masatoshi Hasegawa , Kazutaka Mori
发明人： Satoshi Sakai , Daichi Matsumoto , Katsuyuki Asaka , Masatoshi Hasegawa , Kazutaka Mori
IPC分类号： H01L21/336 , H01L21/8234 , H01L21/8238
CPC分类号： H01L27/10894 , H01L27/105 , H01L27/10814 , H01L27/10897 , H01L27/11 , H01L27/1104 , H01L27/1116
摘要： Mutual diffusion of impurities in a gate electrode is suppressed near a boundary between an n-channel type MISFET and a p-channel type MISFET, which adopt a polycide's dual-gate structure. Since a gate electrode of an n-channel type MISFET and a gate electrode of a p-channel type MISFET are of mutually different conductivity types, they are separated to prevent the mutual diffusion of the impurities and are electrically connected to each other via a metallic wiring formed in the following steps. In a step before a gate electrode material is patterned to separate the gate electrodes, the mutual diffusion of the impurities before forming the gate electrodes is prevented by performing no heat treatment at a temperature of 700° C. or higher.
摘要翻译：在n沟道型MISFET和p型沟道型MISFET之间的边界附近，抑制了栅电极中的杂质的相互扩散，其采用多选择性双栅结构。由于n沟道型MISFET的栅电极和p沟道型MISFET的栅电极具有相互不同的导电类型，它们被分离以防止杂质的相互扩散，并且通过金属布线按以下步骤形成。在将栅电极材料图案化以分离栅电极之前的步骤中，通过在700℃以上的温度下不进行热处理来防止在形成栅电极之前杂质的相互扩散。

9. 发明申请

US20060151856A1 Thermal barrier coating material, thermal barrier member, and member coated with thermal barrier and method for manufacturing the same 有权
标题翻译：热障涂层材料，热障部件和涂有热障的部件及其制造方法
公开(公告)号：US20060151856A1
公开(公告)日：2006-07-13
申请号：US11301339
申请日：2005-12-13
申请人： Taiji Torigoe , Ikuo Okada , Katsumi Namba , Kazutaka Mori , Wei Pan , Qiang Xu
发明人： Taiji Torigoe , Ikuo Okada , Katsumi Namba , Kazutaka Mori , Wei Pan , Qiang Xu
IPC分类号： H01L23/58
CPC分类号： F01D5/288 , C23C4/11 , C23C28/3215 , C23C28/3455 , C23C30/00 , F05D2230/90 , F05D2300/611 , Y02T50/67 , Y02T50/672
摘要： Provided are a thermal barrier coating material and a member coated with thermal barrier that can suppress the separation when used at a high temperature, and have a high thermal barrier effect; a method for manufacturing the member coated with thermal barrier; a turbine member coated with the thermal barrier coating material; and a gas turbine. More specifically provided are a shield coating member comprising a heat-resistant substrate, a bond coat layer formed on the heat-resistant substrate, and a ceramic layer formed on the bond coat layer, wherein the ceramic layer comprises a ceramic represented by a general formula A2Zr2O7, wherein A denotes a rare earth element, and the ceramic layer has (a) a porosity of 1 to 30%, (b) cracks in a thickness direction in pitches of 5 to 100% the total thickness of layers other than the bond coat layer on the heat-resistant substrate, or (c) columnar crystals.
摘要翻译：提供了一种隔热涂层材料和涂有热障的构件，其可以在高温下使用时抑制分离，并且具有高的隔热效果; 制造涂有热障的部件的方法; 涂覆有所述热障涂层材料的涡轮机构件; 和燃气轮机。更具体地提供了一种屏蔽涂层构件，其包括耐热衬底，形成在耐热衬底上的接合涂层和形成在接合涂层上的陶瓷层，其中陶瓷层包括由通式 A 2表示稀土元素，陶瓷层的（a）的孔隙率为1〜30 ％，（b）在耐热基板上的接合涂层以外的层的总厚度为5〜100％的间距的厚度方向的裂纹，（c）柱状晶体。

10. 发明申请

US20050221109A1 Thermal barrier coating, manufacturing method thereof, turbine part and gas turbine 有权
标题翻译：热障涂层，其制造方法，涡轮机部件和燃气轮机
公开(公告)号：US20050221109A1
公开(公告)日：2005-10-06
申请号：US10815734
申请日：2004-04-02
申请人： Taiji Torigoe , Kazutaka Mori , Sunao Aoki , Kouji Takahashi , Minoru Ohara
发明人： Taiji Torigoe , Kazutaka Mori , Sunao Aoki , Kouji Takahashi , Minoru Ohara
IPC分类号： B32B15/04 , C23C4/10 , C23C28/00
CPC分类号： C23C4/11 , B32B15/04 , C23C28/3215 , C23C28/3455 , F05B2230/90 , F05C2253/12 , Y02T50/67 , Y10T428/12618
摘要： A thermal barrier coating enabling to prevent peeling of layer in a high temperature use and still having a high thermal barrier effect, a turbine part coated by this thermal barrier coating and a gas turbine comprising this turbine part are provided. The thermal barrier coating comprises a base material 21 of high temperature heat resistant alloy and a ceramics layer 23 formed on the base material 21. The ceramics layer 23 comprises ZrO2 added with Yb2O3 as stabilizer and is laminated on the base material via a bond coat layer 22 laminated as a metallic bond layer. A plurality of cracks 23A are preferably introduced in the ceramics layer 23. The turbine part is constructed having its surface coated with the above thermal barrier coating.
摘要翻译：提供能够防止在高温使用中并且仍然具有高热障效应的层的剥离的热障涂层，由该热障涂层涂覆的涡轮部分和包括该涡轮部的燃气轮机。隔热涂层包括高温耐热合金的基材21和形成在基材21上的陶瓷层23。陶瓷层23包含添加有Yb 2 O 3 O 3的稳定剂的ZrO 2，并且通过层压的粘合涂层22层压在基材上作为金属结合层。在陶瓷层23中优选引入多个裂纹23A。涡轮机部件被构造成具有涂覆有上述热障涂层的表面。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式