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1. 发明申请

US20080084010A1 METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE AND MATERIAL COMPOSITION FOR HONEYCOMB FIRED BODY 有权
标题翻译：蜂窝结构燃烧体系制备蜂窝结构和材料组成的方法
公开(公告)号：US20080084010A1
公开(公告)日：2008-04-10
申请号：US11849861
申请日：2007-09-04
申请人： Kazuya Naruse , Daniel Merle , Koji Shimato , Kazutomo Matsui
发明人： Kazuya Naruse , Daniel Merle , Koji Shimato , Kazutomo Matsui
IPC分类号： C04B35/565 , B29C35/02
CPC分类号： C04B35/64 , C04B35/565 , C04B38/0006 , C04B2111/00793 , C04B2111/0081 , C04B38/0074 , C04B38/0645
摘要： The method for manufacturing a honeycomb structure includes preparing a material composition containing at least a silicon carbide powder, a binder and an additive; molding the material composition to form a pillar-shaped honeycomb molded body in which a number of cells are placed in parallel with one another in a longitudinal direction with a cell wall therebetween; carrying out a degreasing treatment on the honeycomb molded body; and carrying out a firing treatment on the honeycomb degreased body to manufacture a honeycomb fired body. The additive contains at least one kind selected from the group consisting of alumina, silica, titania, zirconia, magnesia, and a chemical composite containing any of alumina, silica, titania, zirconia and magnesia.
摘要翻译：蜂窝结构体的制造方法包括：制备至少包含碳化硅粉末，粘合剂和添加剂的材料组合物; 模塑所述材料组合物以形成柱状蜂窝模制体，其中多个孔体沿纵向彼此平行地放置，其间具有孔壁; 对蜂窝成型体进行脱脂处理; 并在蜂窝状脱脂体上进行烧成处理，制造蜂窝烧制体。添加剂含有选自氧化铝，二氧化硅，二氧化钛，氧化锆，氧化镁和含有氧化铝，二氧化硅，二氧化钛，氧化锆和氧化镁中的任何一种的化学复合物中的至少一种。

2. 发明授权

US07951324B2 Method for manufacturing honeycomb structure 有权
标题翻译：蜂窝结构体的制造方法
公开(公告)号：US07951324B2
公开(公告)日：2011-05-31
申请号：US11849861
申请日：2007-09-04
申请人： Kazuya Naruse , Daniel Merle , Koji Shimato , Kazutomo Matsui
发明人： Kazuya Naruse , Daniel Merle , Koji Shimato , Kazutomo Matsui
IPC分类号： C04B35/64
CPC分类号： C04B35/64 , C04B35/565 , C04B38/0006 , C04B2111/00793 , C04B2111/0081 , C04B38/0074 , C04B38/0645
摘要： The method for manufacturing a honeycomb structure includes preparing a material composition containing at least a silicon carbide powder, a binder and an additive; molding the material composition to form a pillar-shaped honeycomb molded body in which a number of cells are placed in parallel with one another in a longitudinal direction with a cell wall therebetween; carrying out a degreasing treatment on the honeycomb molded body; and carrying out a firing treatment on the honeycomb degreased body to manufacture a honeycomb fired body. The additive contains at least one kind selected from the group consisting of alumina, silica, titania, zirconia, magnesia, and a chemical composite containing any of alumina, silica, titania, zirconia and magnesia.
摘要翻译：蜂窝结构体的制造方法包括：制备至少包含碳化硅粉末，粘合剂和添加剂的材料组合物; 模塑所述材料组合物以形成柱状蜂窝模制体，其中多个孔体沿纵向彼此平行地放置，其间具有孔壁; 对蜂窝成型体进行脱脂处理; 并在蜂窝状脱脂体上进行烧成处理，制造蜂窝烧制体。添加剂含有选自氧化铝，二氧化硅，二氧化钛，氧化锆，氧化镁和含有氧化铝，二氧化硅，二氧化钛，氧化锆和氧化镁中的任何一种的化学复合物中的至少一种。

3. 发明授权

US06935150B2 Superplasticity forming mould and mould insert 失效
标题翻译：超塑性成型模具和模具插件
公开(公告)号：US06935150B2
公开(公告)日：2005-08-30
申请号：US10380487
申请日：2001-09-12
申请人： Daniel Merle , Frédéric Caillaud
发明人： Daniel Merle , Frédéric Caillaud
IPC分类号： B21D26/055 , B21D37/01 , B21D37/02 , B21D37/16 , B21D37/20 , B30B5/00 , B21D26/02
CPC分类号： B21D26/055 , B21D37/20
摘要： The mould (10) includes at least one part (20), intended to be in contact with the component (12) being moulded, made from sintered vitreous silica. According to the process, said component (12) is formed by the superplastic forming in the mould (10) of a plate (18) made of a material capable of undergoing superplastic deformation, for example titanium or titanium alloy, aluminium or aluminium alloy, or any material exhibiting superplastic properties. Preferably, a barrier is formed between at least a part of the contact surfaces of the mould (10) and the component (12) being moulded, for example by coating with boron nitride, at least partially, the contact surfaces of the mould (10) and the component (12) being moulded, before placing the plate (18) in the mould (10), and/or by injecting an inert gas, notably helium or argon, between the contact surfaces of the mould (10) and the component (12) being moulded.
摘要翻译：模具（10）包括至少一个部分（20），其旨在与被模制的组件（12）接触，由烧结玻璃状二氧化硅制成。根据该方法，所述部件（12）通过在由能够经历超塑性变形的材料（例如钛或钛合金，铝或铝合金）制成的板（18）的模具（10）中形成超塑性，或任何具有超塑性的材料。优选地，在模具（10）的接触表面的至少一部分和被模制的部件（12）之间形成阻挡层，例如通过用氮化硼至少部分地涂覆模具（10）的接触表面）和组件（12）在将板（18）放置在模具（10）中之前，和/或通过在模具（10）的接触表面与模具（10）的接触表面之间注入惰性气体，特别是氦或氩组件（12）被模制。

4. 发明申请

US20130074440A1 GEOMETRIC CONNECTING ASSEMBLY AND METHOD FOR BRACED FRAME CONNECTIONS 审中-公开
标题翻译：几何连接组件和用于制动框架连接的方法
公开(公告)号：US20130074440A1
公开(公告)日：2013-03-28
申请号：US13432928
申请日：2012-03-28
申请人： Cameron John Black , Ian David Aiken , Daniel Merle Andreason , Junichi Yazawa
发明人： Cameron John Black , Ian David Aiken , Daniel Merle Andreason , Junichi Yazawa
IPC分类号： E04B1/38
CPC分类号： E04B1/38 , E04B1/54 , E04B2001/2496 , E04H9/02 , E04H9/028
摘要： The present invention is directed towards improved apparatuses and methods for connecting a structural bracing system having a first geometry to a structure or structural component having a second geometry.
摘要翻译：本发明涉及用于将具有第一几何结构的结构支撑系统连接到具有第二几何形状的结构或结构部件的改进的装置和方法。

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