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31. 发明申请

US20100264562A1 High Density Carbon Foam Composite Tooling 有权
标题翻译：高密度碳泡沫复合模具
公开(公告)号：US20100264562A1
公开(公告)日：2010-10-21
申请号：US11751670
申请日：2007-05-22
申请人： Thomas M. Matviya
发明人： Thomas M. Matviya
IPC分类号： B28B7/30 , B28B7/34 , B28B7/38
CPC分类号： C04B35/52 , C04B38/064 , C04B2111/00413 , C04B2235/422 , C04B2235/77 , C04B2235/96 , Y10T428/24496 , C04B38/0067 , C04B38/0093
摘要： Tools for the forming of composite parts from composite forming materials, having tool bodies that comprise, at least in part, high density carbon foam where a surface of the high density carbon foam may comprise a tool face or support tool face materials. The tools of the present invention may be lighter, more durable, and less costly to produce and/or use than conventional tools used for the production of composite parts, particularly those tools used for the production of carbon composites. Additionally, such tools may be reusable, repairable, and more readily modifiable.
摘要翻译：用于从复合成形材料形成复合部件的工具，其具有至少部分包括高密度碳泡沫的工具主体，其中高密度碳泡沫的表面可以包括工具面或支撑工具面材料。本发明的工具可以比用于生产复合部件的传统工具，特别是用于生产碳复合材料的那些工具更便于生产和/或使用成本更低，成本更低。此外，这样的工具可以是可重复使用的，可修复的并且更易于修改。

32. 发明授权

US07129193B2 Catalyst body 失效
公开(公告)号：US07129193B2
公开(公告)日：2006-10-31
申请号：US10364532
申请日：2003-02-12
申请人： Miho Ito , Jun Hasegawa , Tosiharu Kondo , Tomohiko Nakanishi
发明人： Miho Ito , Jun Hasegawa , Tosiharu Kondo , Tomohiko Nakanishi
IPC分类号： B01J23/00 , B01J35/00
CPC分类号： C04B35/46 , B01J23/58 , B01J23/652 , B01J23/6527 , B01J23/6562 , B01J35/002 , B01J37/0207 , C04B35/117 , C04B35/195 , C04B38/0067 , C04B38/0093 , C04B2111/0081 , C04B2235/3217 , C04B2235/3218 , C04B2235/3232 , C04B2235/3244 , C04B2235/3258 , C04B2235/3275 , C04B2235/3445 , C04B2235/349 , C04B38/0006 , C04B35/185 , C04B35/565 , C04B35/04
摘要： This invention aims at providing a catalyst body exhibiting a lower degradation of a catalyst due to thermal durability and capable of keeping higher catalyst performance for a long time. A catalyst component such as Pt is directly supported by Zr, W, etc, replacing elements inside a support such as Al of cordierite to provide a catalyst body without forming a coating layer. A combination of the catalyst component and the element inside the support is selected so that support strength is greater than 5 eV by simulation using a density functional method. Coarsening of catalyst particles can be suppressed and a high-performance catalyst body excellent in thermal durability can be obtained.

33. 发明公开

EP3135999A1 CMC COMBUSTOR SHELL WITH INTEGRAL CHUTES 无效
标题翻译： CMC-BRENNKAMMERSCHALE MIT INTEGRIERTEN RINNEN
公开(公告)号：EP3135999A1
公开(公告)日：2017-03-01
申请号：EP16185097.9
申请日：2016-08-22
申请人： Rolls-Royce Corporation
发明人： Varney, Bruce
IPC分类号： F23R3/00 , F23R3/06
CPC分类号： F23R3/007 , B28B21/72 , B28B21/98 , C04B35/71 , C04B38/0093 , C04B41/4523 , C04B41/4529 , C04B41/4539 , C04B41/81 , F23R3/045 , F23R3/06 , F23R2900/00018
摘要： A combustion assembly for a gas turbine engine may be provided. The combustion assembly may include a ceramic matrix composite combustor shell, which may include a chamber defined by a wall of the ceramic matrix composite combustor shell, and the ceramic matrix composite combustor shell may include a ceramic matrix composite chute integral with the ceramic matrix composite combustor shell. The ceramic matrix composite chute may extend towards a midline of the chamber. A method for fabricating a ceramic matrix composite chute may be provided. At least one chute may be woven in three dimensions into a ceramic preform. A layup tool may be inserted into the chute. The chute may be enlarged with the layup tool. The ceramic preform may be formed into a ceramic matrix composite body, which includes a combustor shell and the chute.
摘要翻译：可以提供用于燃气涡轮发动机的燃烧组件。燃烧组件可以包括陶瓷基体复合燃烧器壳体，其可以包括由陶瓷基体复合燃烧器壳体的壁限定的腔室，并且陶瓷基体复合燃烧器壳体可以包括与陶瓷基体复合燃烧器一体的陶瓷基体复合滑槽贝壳。陶瓷基质复合滑槽可以朝着腔室的中线延伸。可以提供一种制造陶瓷基质复合滑槽的方法。至少一个滑槽可以三维地编织成陶瓷预制件。上料工具可以插入滑槽。滑槽可以用铺设工具放大。陶瓷预制件可以形成为包括燃烧器壳体和滑槽的陶瓷基体复合体。

34. 发明授权

EP2380650B1 Honeycomb catalyst body 有权
公开(公告)号：EP2380650B1
公开(公告)日：2013-07-31
申请号：EP11250155.6
申请日：2011-02-11
申请人： NGK Insulators, Ltd.
发明人： Goto, Chika , Yamashita, Masataka , Miyairi, Yukio
IPC分类号： B01J23/63 , B01J35/00 , B01J35/02 , B01J35/04 , B01J37/02 , B01D46/24
CPC分类号： B01D46/247 , B01D46/2429 , B01D46/2466 , B01D46/2474 , B01D53/9454 , B01D2046/2433 , B01D2046/2437 , B01D2255/102 , B01D2255/9155 , B01J23/63 , B01J35/0006 , B01J35/023 , B01J35/04 , B01J37/0248 , C04B35/195 , C04B38/0009 , C04B2111/0081 , C04B2235/6567 , Y02T10/22 , C04B35/00 , C04B38/0054 , C04B38/0074 , C04B38/0093

35. 发明公开

US20240034677A1 PRODUCTION OF FOAMED SAND USING NEAR INFRARED 审中-公开
公开(公告)号：US20240034677A1
公开(公告)日：2024-02-01
申请号：US18481378
申请日：2023-10-05
申请人： ThermPro TEC GmbH
发明人： Rainer Gaus
IPC分类号： C04B20/06 , B01D45/16 , B01J19/12 , C04B14/06 , C04B20/00 , C04B38/00
CPC分类号： C04B20/066 , B01D45/16 , B01J19/128 , C04B14/06 , C04B20/002 , C04B38/0093 , B01J2219/0801 , B01J2219/0869 , B01J2219/0879
摘要： An arrangement for producing a bulk material consisting substantially of foamed or blown mineral or oxide particles by thermal treatment of a bulk material of basic particles. The arrangement includes NIR halogen radiators for generating a NIR radiation field of radiation with an active component in a near infrared, NIR, range having a wavelength in a range between 0.8 μm and 1.5 μm and which has a power density of at least 50 kW/m2 for thermally treating the basic particles, a conveying device for transporting a layer or stream of the bed of basic particles through the radiation field, and a controller that controls heating of the bed of basic particles such that a maximum temperature in the layer or stream is in a temperature range between 600 and 1500° C.

36. 发明授权

US11796174B2 CMC combustor shell with integral chutes 有权
公开(公告)号：US11796174B2
公开(公告)日：2023-10-24
申请号：US16518575
申请日：2019-07-22
申请人： Rolls-Royce Corporation
发明人： Bruce Edward Varney
IPC分类号： C04B35/66 , C04B41/81 , F23R3/06 , F23R3/00 , C04B41/45 , B28B21/72 , B28B21/98 , C04B35/71 , C04B38/00 , F23R3/04
CPC分类号： F23R3/007 , B28B21/72 , B28B21/98 , C04B35/71 , C04B38/0093 , C04B41/45 , C04B41/4523 , C04B41/4529 , C04B41/4539 , C04B41/81 , F23R3/045 , F23R3/06 , F23R2900/00018
摘要： A combustion assembly for a gas turbine engine may be provided. The combustion assembly may include a ceramic matrix composite combustor shell, which may include a chamber defined by a wall of the ceramic matrix composite combustor shell, and the ceramic matrix composite combustor shell may include a ceramic matrix composite chute integral with the ceramic matrix composite combustor shell. The ceramic matrix composite chute may extend towards a midline of the chamber. A method for fabricating a ceramic matrix composite chute may be provided. At least one chute may be woven in three dimensions into a ceramic preform. A layup tool may be inserted into the chute. The chute may be enlarged with the layup tool. The ceramic preform may be formed into a ceramic matrix composite body, which includes a combustor shell and the chute.

37. 发明申请

US20170259472A1 CLOSED-CELL POLYURETHANE STRUCTURE METHOD AND SYSTEM 审中-公开
公开(公告)号：US20170259472A1
公开(公告)日：2017-09-14
申请号：US15470456
申请日：2017-03-27
申请人： Douglas E. Reeves
发明人： Douglas E. Reeves
IPC分类号： B29C44/12 , B01F11/00 , C04B38/00 , B01F13/00 , B29B7/00 , B29C44/34 , B01F3/08 , B01F15/00
CPC分类号： B29C44/1242 , B01F3/0803 , B01F3/0853 , B01F11/0005 , B01F13/0022 , B01F15/00857 , B01F2215/0047 , B29B7/005 , B29C44/3442 , B29K2075/00 , B29K2105/046 , B29K2995/002 , B29L2031/766 , C04B38/0093 , C04B2103/42 , C04B2111/40 , Y10T428/1376
摘要： A container, that includes a transparent portion, which reveals an interior portion of the container, an access aperture communicating with the interior portion of the container, and a lid adjacent the access aperture. A first liquid component is placed into the interior portion. A second liquid component is poured into the interior portion. The lid of the container is closed to fully enclose the first and second liquid components. The components are agitated until the first and second liquid components are a mixture of uniform color, without an appearance of marbling and swirling, when viewed through the transparent portion of the container. The lid is opened to expose the mixture of uniform color. The mixture of uniform color is poured from the container into a receiving structure. The mixture of uniform color is transformed into a closed-cell polyurethane structure within the receiving structure.

38. 发明申请

US20170059159A1 CMC COMBUSTOR SHELL WITH INTEGRAL CHUTES 审中-公开
标题翻译： CMC COMBUSTOR SHELL带有一体化套管
公开(公告)号：US20170059159A1
公开(公告)日：2017-03-02
申请号：US14834605
申请日：2015-08-25
申请人： Rolls-Royce Corporation
发明人： BRUCE EDWARD VARNEY
IPC分类号： F23R3/00 , C04B38/00 , B28B21/72 , C04B41/81 , C04B41/45 , B28B21/98 , F23R3/04 , C04B35/71
CPC分类号： F23R3/007 , B28B21/72 , B28B21/98 , C04B35/71 , C04B38/0093 , C04B41/4523 , C04B41/4529 , C04B41/4539 , C04B41/81 , F23R3/045 , F23R3/06 , F23R2900/00018
摘要： A combustion assembly for a gas turbine engine may be provided. The combustion assembly may include a ceramic matrix composite combustor shell, which may include a chamber defined by a wall of the ceramic matrix composite combustor shell, and the ceramic matrix composite combustor shell may include a ceramic matrix composite chute integral with the ceramic matrix composite combustor shell. The ceramic matrix composite chute may extend towards a midline of the chamber. A method for fabricating a ceramic matrix composite chute may be provided. At least one chute may be woven in three dimensions into a ceramic preform. A layup tool may be inserted into the chute. The chute may be enlarged with the layup tool. The ceramic preform may be formed into a ceramic matrix composite body, which includes a combustor shell and the chute.
摘要翻译：可以提供用于燃气涡轮发动机的燃烧组件。燃烧组件可以包括陶瓷基体复合燃烧器壳体，其可以包括由陶瓷基体复合燃烧器壳体的壁限定的腔室，并且陶瓷基体复合燃烧器壳体可以包括与陶瓷基体复合燃烧器一体的陶瓷基体复合滑槽贝壳。陶瓷基质复合滑槽可以朝着腔室的中线延伸。可以提供一种制造陶瓷基质复合滑槽的方法。至少一个滑槽可以三维地编织成陶瓷预制件。上料工具可以插入滑槽。滑槽可以用铺设工具放大。陶瓷预制件可以形成为陶瓷基体复合体，其包括燃烧器壳体和滑槽。

39. 发明申请

US20140087128A1 HONEYCOMB STRUCTURE 有权
标题翻译：蜂窝结构
公开(公告)号：US20140087128A1
公开(公告)日：2014-03-27
申请号：US14029846
申请日：2013-09-18
申请人： HONDA MOTOR CO. LTD. , NGK INSULATORS, LTD.
发明人： Hidetoshi YANASE , Tomokatsu AOYAMA , Yoshiaki HATAKEYAMA
IPC分类号： C04B38/00
CPC分类号： C04B38/0009 , B01D46/2462 , B01D46/2466 , B28B11/12 , B28B19/0038 , C04B38/0093 , Y10T428/24149 , C04B35/10 , C04B35/185 , C04B35/195 , C04B35/478 , C04B35/565
摘要： There are disclosed a honeycomb structure hardly generates ring cracks; and a honeycomb structure 100 includes a honeycomb basal body 4 having porous partition walls 1 defining a plurality of cells 2 to become through channels of a fluid; and a ring-shaped convex portion 10 being a ring of convex portion surrounding an outer periphery of the honeycomb basal body 4 over the whole periphery; and the ring-shaped convex portion 10 is disposed to project outwardly from the outer periphery of the honeycomb basal body 4 and to cover a part of the outer periphery of the honeycomb basal body 4, the shapes of both end portions of the ring-shaped convex portion are tapered shape, and a thickness of the ring-shaped convex portion 10 in a cross section perpendicular to an extending direction of the cells 2 is from 3 to 20 mm.
摘要翻译：公开了一种几乎不产生环形裂纹的蜂窝结构; 蜂窝结构体100具有蜂窝基体4，蜂窝基体4具有多孔分隔壁1，该多孔分隔壁限定多个细胞2，通过流体通道; 以及围绕蜂窝基体4的外周的整周的环状的环状的凸部10。并且环状凸部10从蜂窝基体4的外周向外突出并覆盖蜂窝基体4的外周的一部分，环状的两端部的形状凸部为锥形，环状凸部10的与电池2的延伸方向垂直的截面的厚度为3〜20mm。

40. 发明申请

US20130260089A1 BODY FORMED OF REFRACTORY MATERIAL HAVING STRESS RELIEF SLITS AND METHOD OF FORMING THE SAME 审中-公开
标题翻译：具有应力缓冲片的耐火材料的制造方法及其形成方法
公开(公告)号：US20130260089A1
公开(公告)日：2013-10-03
申请号：US13852839
申请日：2013-03-28
申请人： REFRACTORY SPECIALTIES, INC.
发明人： Gregory J. GORBY , Dale R. SAARI
IPC分类号： C04B38/00 , C04B40/00
CPC分类号： C04B38/0093 , B28B7/0082 , B28B7/46 , C04B35/18 , C04B35/622 , C04B35/6316 , C04B35/803 , C04B38/0006 , C04B40/0089 , C04B2235/5228 , C04B2235/6027 , C04B2235/775 , C04B2235/945 , Y10T428/24149 , Y10T428/2457
摘要： The present invention is directed to a body formed of a refractory material and a method of forming a refractory body. The body formed of a refractory material comprises a plurality of slits formed into one of its surfaces. The slits relieve thermal stress in the body and prevent cracking that would otherwise occur. In one embodiment, the invention can be a body formed of a refractory material comprising: a first surface and an opposing second surface; and a pattern of stress relief slits formed into at least one of the first and second surfaces of the body.
摘要翻译：本发明涉及由耐火材料形成的本体和形成耐火体的方法。由耐火材料形成的主体包括形成其一个表面中的多个狭缝。狭缝减轻了身体的热应力，并防止了另外会发生的裂纹。在一个实施例中，本发明可以是由耐火材料形成的主体，包括：第一表面和相对的第二表面; 以及形成在身体的第一和第二表面中的至少一个中的应力释放狭缝的图案。

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