序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
121 Method of making fire resistant sustainable aircraft interior panels US14591875 2015-01-07 US09925728B2 2018-03-27 Pedro P. Martin; Ana Gonzalez-Garcia; Nieves Lapena
The present invention relates to method of manufacturing an aircraft interior panel comprising a core sandwiched between first and second skins, wherein both of the first and second skins are formed from natural fibers containing non-halogenated fire-retardant and set within an inorganic thermoset resin, thereby forming a fire-resistant sustainable aircraft interior panel. The method comprises impregnating the natural fibers with non-halogenated fire retardant and an inorganic thermoset resin, and laying up the resin-impregnated natural fibers to sandwich the core. This stack is then cured by raising the temperature of the stack sufficient to initiate curing but without reaching the boiling point of water in the stack, holding the stack at that first temperature before raising the temperature again to reach the boiling point of water in the stack, before cooling the stack.
122 Metal Oxide Activated Cement US15625349 2017-06-16 US20170283322A1 2017-10-05 Trevor Cyril Waters
A cement including: an alkali silicate; an organic silicate; a compound selected from a group consisting of Pozzolanic compounds and synthetic Pozzolanic substitutes; a metal oxide; an activator.
123 Light weight structural materials US15394505 2016-12-29 US09771468B2 2017-09-26 William Brenden Carlson; Gregory David Phelan; Vincenzo Casasanta, III; Feng Wan
Functionalized microspheres for being dispersed in matrix materials to reduce the density and weight of the materials may be configured to include a covalently bound surface component which is configured to covalently bond with the matrix material so that when combined with the matrix material a strong, light-weight matrix material may be produced.
124 LIGHT WEIGHT STRUCTURAL MATERIALS US15394505 2016-12-29 US20170107353A1 2017-04-20 William Brenden CARLSON; Gregory David PHELAN; Vincenzo CASASANTA, III; Feng WAN
Functionalized microspheres for being dispersed in matrix materials to reduce the density and weight of the materials may be configured to include a covalently bound surface component which is configured to covalently bond with the matrix material so that when combined with the matrix material a strong, light-weight matrix material may be produced.
125 Light weight structural materials US14764302 2013-01-31 US09567255B2 2017-02-14 William Brenden Carlson; Gregory D. Phelan; Vincenzo Casasanta, III; Feng Wan
Functionalized microspheres for being dispersed in matrix materials to reduce the density and weight of the materials may be configured to include a covalently bound surface component which is configured to covalently bond with the matrix material so that when combined with the matrix material a strong, light-weight matrix material may be produced.
126 Method of Making Nanoporous Structures US14912278 2014-08-13 US20160200632A1 2016-07-14 John Aikens; John C. Parker
A method of making a nanoporous structure comprising a matrix and at least one nanosized pore within the matrix, wherein the method comprises contacting at least a portion of a templated matrix with an acid t solution, wherein the templated matrix comprises a matrix that selected from the group consisting of an organic polymer, a sol-based ceramic, an inorganic salt, an organoaluminate, and combinations thereof, and one or more nanosized templates within the matrix, wherein each nanosized template comprises a core that comprises an inorganic oxide, to dissolve at least a portion of the inorganic oxide of at least one of the cores and form the at least one nanosized pore within the matrix thereby forming the nanoporous structure.
127 INSULATING COMPOSITE MATERIALS COMPRISING AN INORGANIC AEROGEL AND A MELAMINE FOAM US14897982 2014-06-13 US20160115685A1 2016-04-28 Pierre-Antoine BONNARDEL; Sophie CHAUSSON; Emilie GERARDIN
The invention relates to insulating composite materials comprising an inorganic aerogel and a melamine foam. The invention also relates to the production method of said materials, and to the use of same.
128 LIGHT WEIGHT STRUCTURAL MATERIALS US14764302 2013-01-31 US20150360995A1 2015-12-17 William Brenden CARLSON; Gregory D. PHELAN; Vincent CASASANTA, III; Feng WAN
Functionalized microspheres for being dispersed in matrix materials to reduce the density and weight of the materials may be configured to include a covalently bound surface component which is configured to covalently bond with the matrix material so that when combined with the matrix material a strong, light-weight matrix material may be produced.
129 HONEYCOMB STRUCTURE US14560159 2014-12-04 US20150087499A1 2015-03-26 Masafumi KUNIEDA; Yosuke MATSUKAWA
A honeycomb structure includes a honeycomb unit. The honeycomb unit has a plurality of through holes defined by partition walls along a longitudinal direction of the honeycomb unit. The partition walls have a thickness of approximately 0.1 mm to approximately 0.4 mm. The honeycomb unit is manufactured by molding raw material paste by extrusion molding and thereafter by firing the molded raw material paste. The raw material paste contains zeolite and an inorganic binder. A specific surface area of the zeolite is more than or equal to approximately 500 m2/g and less than or equal to approximately 800 m2/g. An external surface area of the zeolite is more than or equal to approximately 40 m2/g and less than or equal to approximately 80 m2/g.
130 CEMENT AND SKINNING MATERIAL FOR CERAMIC HONEYCOMB STRUCTURES US14236141 2012-09-20 US20140199482A1 2014-07-17 Jun Cai; Chan Han; Michael T. Malanga; Ashish Kotnis
Skins and/or adhesive layers are formed on a porous ceramic honeycomb by applying a layer of a cement composition to a surface of the honeycomb and firing the cement composition. The cement composition contains inorganic filler particles, a carrier fluid and a clay material rather than the colloidal alumina and/or silica materials that are conventionally used in such cements. The cement compositions resist permeation into the porous walls of the ceramic honeycomb. As a result, lower temperature gradients are seen in the honeycomb structure during rapid temperature changes, which results in an increased thermal shock resistance.
131 GLASS FIBERBOARD AND PRODUCTION METHOD THEREFOR US14112166 2012-05-11 US20140034868A1 2014-02-06 Myung Lee; Seong-Moon Jung; Suk Jang; Eun-Joo Kim
The present invention relates to a glass fiberboard and to a production method therefor, and more specifically, to technology for providing a glass fiberboard for vacuum heat insulation and a production method therefor, which have outstanding initial heat insulation performance and economic advantages through application of an optimized inorganic binder.
132 Filter element, in particular for filtering exhaust gases of an internal combustion engine US12303724 2007-07-27 US08632619B2 2014-01-21 Teruo Komori; Rainer Mueller; Lars Thuener
A filter element, in particular for filtering exhaust gases of an internal combustion engine, includes mutually parallel flow channels, at least two filter segments being provided which each have a subset of flow channels, the filter segments having a spacing from one another and being interconnected via connecting device(s) arranged integrally with the filter segments.
133 Honeycomb structure, exhaust gas conversion apparatus, and manufacturing method of the honeycomb structure US12472268 2009-05-26 US08609031B2 2013-12-17 Kazushige Ohno; Masafumi Kunieda; Takahiko Ido
A honeycomb structure includes at least one honeycomb unit including zeolite, an inorganic binder, and cell walls. The cell walls extend from a first end face to a second end face to define cells along a longitudinal direction of the at least one honeycomb unit. Each of the cell walls includes a center part in the longitudinal direction and a first end part adjacent to the first end face. The first end part has a thickness larger than a thickness of the center part, and/or the first end part has a porosity smaller than a porosity of the center part.
134 INORGANIC FIBROUS MOLDED REFRACTORY ARTICLE, METHOD FOR PRODUCING INORGANIC FIBROUS MOLDED REFRACTORY ARTICLE, AND INORGANIC FIBROUS UNSHAPED REFRACTORY COMPOSITION US13520891 2010-12-24 US20130090224A1 2013-04-11 Koji Iwata; Ken Yonaiyama
An inorganic fibrous shaped refractory article having a high bio-solubility which is capable of exhibiting a desired heat resistance without containing expensive ceramic fibers, alumina powder and silica powder can be provided at a low production cost and with a low product price.An inorganic fibrous shaped refractory article includes 2 to 95 mass % of rock wool, 2 to 95 mass % of inorganic powder having a needle-like crystal structure and 3 to 32 mass % of a binder. Preferably, in the an inorganic fibrous shaped refractory article, the inorganic powder having a needle-like crystal structure has an average length of 1 to 3000 μm and an aspect ratio of 1 to 1000, and more preferably the inorganic powder having a needle-like crystal structure is wollostonite powder or sepiolite powder.
135 Inorganic fiber paper and method of producing the same US13064639 2011-04-05 US20120247695A1 2012-10-04 Tetsuya Mihara; Ken Yonaiyama; Tetsuya Ishihara; Tomohiko Kishiki
Inorganic fiber paper includes first biosoluble inorganic fibers having an average fiber diameter of 3 to 7 μm, second biosoluble inorganic fibers having an average fiber diameter of 2 to 3 μm, and a binder, the average fiber diameter of the second biosoluble inorganic fibers being smaller than that of the first biosoluble inorganic fibers.
136 HONEYCOMB STRUCTURE US12711206 2010-02-23 US20100247398A1 2010-09-30 Takahiko IDO; Chizuru Kasai
A disclosed honeycomb structure includes at least one honeycomb unit having parallel through holes separated by partition walls and extending in the longitudinal direction, the honeycomb unit including a first SOx-occluding agent, first inorganic particles, and an inorganic binder; and coating layers formed on the partition walls and including a second SOx-occluding agent and second inorganic particles. In the honeycomb structure, the basicity of the honeycomb unit is higher than that of the coating layers.
137 BONDING MATERIAL FOR HONEYCOMB STRUCTURE AND HONEYCOMB STRUCTURE UTILIZING THE MATERIAL US12688055 2010-01-15 US20100119769A1 2010-05-13 Atsushi Watanabe; Suguru Kodama; Shuichi Ichikawa; Fumiharu Sato
A bonding material for a honeycomb structure comprises inorganic particles in which D90/D10 is from 10 to 500, D10 is 100 μm or less and D90 is 4 μm or more, and the D10 and D90 are the values of 10% diameter and 90% diameter from a smaller particle diameter side, respectively, in volume-based integrated fractions of a particle diameter distribution measurement by a laser diffraction/scattering method.
138 HONEYCOMB STRUCTURE, EXHAUST GAS CONVERSION APPARATUS, AND MANUFACTURING METHOD OF THE HONEYCOMB STRUCTURE US12472268 2009-05-26 US20090291034A1 2009-11-26 Kazushige OHNO; Masafumi Kunieda; Takahiko Ido
A honeycomb structure includes at least one honeycomb unit including zeolite, an inorganic binder, and cell walls. The cell walls extend from a first end face to a second end face to define cells along a longitudinal direction of the at least one honeycomb unit. Each of the cell walls includes a center part in the longitudinal direction and a first end part adjacent to the first end face. The first end part has a thickness larger than a thickness of the center part, and/or the first end part has a porosity smaller than a porosity of the center part.
139 HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE US12407645 2009-03-19 US20090239744A1 2009-09-24 Kazushige Ohno; Yuki Fujita
A honeycomb structure includes a plurality of honeycomb fired bodies combined with one another. The honeycomb fired bodies include a center-portion honeycomb fired body located in a center portion in a cross section perpendicular to a longitudinal direction and a peripheral-portion honeycomb fired body located in a peripheral portion in the cross section. The center-portion honeycomb fired body has a substantially rectangular cross-sectional shape and has an area from about 2500 mm2 to about 5000 mm2 in the cross-section. A cross-sectional shape of the peripheral-portion honeycomb fired body is different from the cross-sectional shape of the center-portion honeycomb fired body. A cross-sectional area of the peripheral-portion honeycomb fired body perpendicular to the longitudinal direction is from about 0.9 times to about 1.3 times as large as the cross-sectional area of the center-portion honeycomb fired body.
140 Compositions For Applying To Ceramic Honeycomb Bodies US12179863 2008-07-25 US20090033005A1 2009-02-05 Dana Craig Bookbinder; James Arthur Griffin, JR.; David Lambie Tennent; Lung-Ming Wu
Disclosed are compositions for applying to honeycomb bodies. The compositions can be used as plugging mixtures for forming a ceramic wall flow filter. Alternatively, the compositions can be used to form skin coatings on exterior portions of a honeycomb body. The disclosed compositions include an inorganic powder batch composition, an organic binder, a liquid vehicle, and a rheology modifier. The compositions exhibit improved rheological properties, including an increased yield strength and reduced viscosity under shear, which, among various embodiments, can enable the manufacture of sintered phase end plugs having reduced levels of dimple and pinhole formations in the final dried and fired end plugs as well as end plugs having relatively uniform and desired depths. Also disclosed are methods for forming end plugged ceramic wall flow filters from the plugging mixtures disclosed herein.
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