| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 181 | Ceramic radiator | JP19985783 | 1983-10-25 | JPS6091131A | 1985-05-22 | KOBAYASHI KOUICHI |
| PURPOSE:To contrive an improvement in thermal shock properties, by specifying a porosity of a ceramic radiator. CONSTITUTION:A porosity is made into 50-90%, in a ceramic radiator wherein a large number of pieces of linear extruded stock made of ceramic is wound and laminated spirally respectively and spiral wound laminates are molded in a state either joined or twined round with each other at adjoining faces respectively. As for a material of the ceramic radiator, eucryptite (Li2O, Al2O2, 2SiO2) and spodumene (Li2O, Al2O3, 4SiO2) which are lithium low thermal expansion material can be used beside augitite. In addition to the above, as for distinctive features of a radiating plate, as structure of the same having predetermined frame size is strong against thermal shock, when the same is used for a part wherein a temperature exceeds a heat-resisting level of the low thermal expansion material, materials such as mullite (3Al2O3, 2SiO2), alumina (Al2O3) and magnesia (MgO), whose heat resisting properties are high while a thermal expansion ratio is large are selected appropriately. | ||||||
| 182 | Kaihokoshitsukukakunoarushinamonono seiho | JP9265275 | 1975-07-31 | JPS5144109A | 1976-04-15 | REIMONDO RUISU SUTOROO; RARII RUSERU UIRUSON |
| 183 | Composite insulation panel | JP2013504844 | 2011-06-16 | JP2013524059A | 2013-06-17 | イム、ホン−ビン |
| 本発明は、発泡性合成樹脂材質によって形成された断熱材（１１０）と、合成樹脂材質によって形成され、幅方向に複数の中空部（１２１）が形成されるとともに、断熱材（１１０）の表面に接着された中空板（１２０）と、ポリマーセメントモルタル材質によって中空板（１２０）の表面に形成されたモルタル層（１３０）とを含む複合断熱パネル（１００）を提示することにより、断熱作業にかかる手間と費用を低減し、断熱構造の厚さを減らして建築物の内部空間を拡大することができ、冬期における結露現象の発生を防止できるようにする。
【選択図】図２ |
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| 184 | Honeycomb structural body | JP2007520597 | 2006-08-24 | JP5127450B2 | 2013-01-23 | 洋之 坂口; 一茂 大野 |
| 185 | Multiple of lead acid battery electrode and a method of manufacturing the same provided with a mesh-like body of the pores that penetrate the electrode | JP2012503949 | 2010-03-23 | JP2012523097A | 2012-09-27 | アンジェル、ジフコフ、キルチェフ; ニナ、キルチェバ |
| 本発明は、構造体（１）に関するものであり、前記構造体（１）は、網状体と外枠（２）とを備え、前記網状体は、前記構造体を貫通する、平行で一様な複数の気孔（１ａ）を有し、前記外枠（２）は、前記構造体（１）の側面を囲む。 前記構造体（１）と前記枠（２）とは、炭素から形成される。 電極は、鉛ベースの層により覆われている。 これらの気孔（１ａ）は、鉛ベースの活性材料により充填されている。 | ||||||
| 186 | Method for manufacturing a ceramic structure | JP2006315567 | 2006-11-22 | JP5036284B2 | 2012-09-26 | 七瀧 努; 夏己 下河; 誠 大森 |
| Striped sheets each having a structure in which two types of first layers and second layers are stacked in the X direction are prepared. More specifically, first raw material sheets having the same composition as the first layers and second raw material sheets having the same composition as the second layers are regularly alternately stacked in the X direction to prepare a uniaxial stack. The uniaxial stack is then cut along the X direction to prepare the striped sheets. A large number of striped sheets and a large number of homogeneous sheets are then collected to form a sheet group. The striped sheets and the homogeneous sheets are alternately stacked in the Y direction different from the X direction to prepare a biaxial stack having two stacking axes in the X direction and the Y direction. The biaxial stack is fired to produce a ceramic structure. | ||||||
| 187 | Ceramic honeycomb structure | JP2006540993 | 2005-10-11 | JP5001009B2 | 2012-08-15 | 雅文 国枝 |
| 188 | C / c composite material for the precursor, and c / c composite material, as well as a method for manufacturing the same | JP2005015399 | 2005-01-24 | JP4773728B2 | 2011-09-14 | 真人 宮本 |
| 189 | Honeycomb structure, manufacturing method and the exhaust gas purifying apparatus of the honeycomb structure | JP2006519312 | 2004-12-24 | JP4666390B2 | 2011-04-06 | 豊 吉田 |
| 190 | Device for manufacturing ceramic structure and method for manufacturing ceramic structure | JP2010225796 | 2010-10-05 | JP2011046607A | 2011-03-10 | ONO MASAHARU; TAKAHASHI KOJI; HOSHINO TAKAFUMI; KAWADA HIDEYA |
| <P>PROBLEM TO BE SOLVED: To provide a method for easily manufacturing a ceramic structure in which a plurality of column-like porous ceramic members are bonded with an adhesive layer in between. <P>SOLUTION: The method for manufacturing a ceramic structure includes: a step of assembling a plurality of column-like porous ceramic members in such a way that a gap is formed between the members; a step of filling a paste adhesive into the gap; and a step of forming an adhesive layer by curing the adhesive. <P>COPYRIGHT: (C)2011,JPO&INPIT | ||||||
| 191 | Honeycomb structural body | JP2004541299 | 2003-10-07 | JP4437085B2 | 2010-03-24 | 豊 吉田 |
| 192 | Honeycomb filter and exhaust gas purification system | JP2003039426 | 2003-02-18 | JP4369141B2 | 2009-11-18 | 敏雄 山田; 結輝人 市川 |
| 193 | Porous strength ceramics or metal implant | JP2008541425 | 2006-11-20 | JP2009516544A | 2009-04-23 | アカシュ・アカシュ |
| 本発明は、金属製またはセラミックス製インプラントの弾性率、曲げ弾性率および孔構造を調節する方法および装置に関し、１実施態様として、固体インプラント構造（４４）に組み込まれる金属、セラミックス又はそれらの混合物粒子から成るグリーンテープを開示する。 開口部（３２）は、固体インプラント構造（４４）の所望の孔構造を形成するためにグリーンテープ（３４）の特定の領域に刻まれる。 この孔構造は、固体インプラント構造（４４）のに所望の弾性率、曲げ強度および多孔性を付与するだけでなく、骨成長を促進する。 グリーンテープ（３４）は１方向に積層され、所望の孔構造を付与され、金属またはセラミックス粒子の層は溶融結合され、固体インプラント構造（４４）が形成される。 | ||||||
| 194 | ハニカム構造体 | JP2006517886 | 2005-09-22 | JPWO2006112061A1 | 2008-11-27 | 吉田 豊; 豊 吉田 |
| 排気ガス温度の高温化を防いで、排気ガス浄化特性をよくすることのできるハニカム構造体を提供する。このハニカム構造体は、長手方向に沿って並列して配置されたセルとそのセルどうしを隔てるセル壁とからなる複数のハニカムユニットどうしを、シール材層を介して接合し一体化させてなる集合型ハニカムブロックまたは一体型ハニカムモノリスにおいて、前記シール材層もしくはハニカムモノリスの外周に設けるシール材層を、酸化物粒子、無機結合剤、着色剤を含むものにて形成したことを特徴とする。 | ||||||
| 195 | ハニカム構造体 | JP2007508081 | 2006-03-07 | JPWO2006098191A1 | 2008-08-21 | 市川 周一; 周一 市川; 岩田 浩一; 浩一 岩田; 桝川 直; 直 桝川; 渡辺 篤; 篤 渡辺 |
| 複数のハニカムセグメント2が接合材層9を介して互いの接合面で一体的に接合されたハニカムセグメント接合体10を備え、流体の流路となる複数のセル5が中心軸方向に互いに並行するように配設された構造を有するハニカム構造体10であり、接合材層9の外側部分(ハニカムセグメントの接合面との界面からそれぞれ全体の層厚の20%に相当する長さだけ離れた箇所までの部分)における気孔率が、外側部分より内方に位置する中心部分の気孔率よりも小であるように構成されている。 | ||||||
| 196 | Ceramic honeycomb structure and method of manufacturing the same | JP2005300227 | 2005-10-14 | JP2006225250A | 2006-08-31 | KONDO TAKASHI; TANAKA MASAICHI; ISHIHARA MIKIO |
| <P>PROBLEM TO BE SOLVED: To provide a ceramic honeycomb structure having excellent thermal shock resistance and outer diameter dimensional accuracy and a method of manufacturing the same. <P>SOLUTION: The ceramic honeycomb structure 1 comprises a cordierite ceramic having an outer peripheral skin part 2 provided on the outer periphery in the diameter direction and a cell wall 3 forming a honeycomb like cell 11 inside the outer peripheral skin part 2. The ratio A/B of the degree A of crystal orientation of the cordierite ceramic in the cell wall 3 to the degree B of crystal orientation of the cordierite ceramic in the outer peripheral skin part 2 is 0.80-1.25. In the manufacture of the ceramic honeycomb structure 1, the relation between the temperature T1 at the center part of a base material and the temperature T2 at the outer peripheral edge part of the base material in drying a honeycomb formed body 10 formed by extrusion satisfies T1>T2 in ≥50% of a time required from the starting of temperature rising till the temperature T1 reaches 95°C. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
| 197 | Method of impregnation impregnation material to the concrete base material | JP6406896 | 1996-03-21 | JP3804095B2 | 2006-08-02 | 哲司 佐藤 |
| 198 | Emission gas purification filter and its production method | JP2005152028 | 2005-05-25 | JP2006110538A | 2006-04-27 | ISHIHARA MIKIO |
| <P>PROBLEM TO BE SOLVED: To provide an emission gas purification filter having superior plug strength with only one baking process required. <P>SOLUTION: A production method of an emission gas purification filter 1 purifying an emission gas 5 by catching with a particulate in the emission gas 5 emitted from an international combustion engine is comprised of an extrusion molding process for producing a honeycomb molded body 10 by extrusion molding a substrate which is a material for forming the honeycomb molded body 10 having a partition 11 arranged in honeycomb shaped and a plurality of cells 12 which are partitioned by the partition 11 and are passed through both end surfaces 18, 19, a masking process for arranging a masking material at an opening 3 of the cells 12, a plug material arranging process for arranging a plug material which is a material for a plug part 2, and a baking process for simultaneously baking the substrate and the plug material and the plug material fulfills a formula of 0≤A<B if a shrinkage rate is A when baking the plug material and a shrinkage rate is B when baking the substrate. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
| 199 | C/c composite material precursor, c/c composite material and method for producing c/c composite material | JP2005015399 | 2005-01-24 | JP2006062943A | 2006-03-09 | MIYAMOTO MASATO |
| <P>PROBLEM TO BE SOLVED: To provide a C/C composite material precursor which enables easy manufacture of a C/C composite material, and to provide the C/C composite material and a method of producing the same. <P>SOLUTION: The C/C composite material precursor which gives the C/C composite material includes carbon fiber, a matrix and a void 5 which has openings on the surface of the C/C composite material after firing and further includes a plurality of prepregs and a mesh-like void-forming core which is sandwiched between the prepregs and is burnt out or reduces the volume thereof at a lower temperature than a temperature of the firing to form the void 5. The method for producing a C/C composite material by firing of the precursor is provided. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
| 200 | Integrated ceramic/metallic component and method of making same | JP2005131265 | 2005-04-28 | JP2005350341A | 2005-12-22 | FRELING MELVIN; SCHLICHTING KEVIN W; DIERBERGER JAMES A |
| <P>PROBLEM TO BE SOLVED: To provide an integrated ceramic/metallic component and a method of making same. <P>SOLUTION: The integrated ceramic/metallic component (50) comprises a metallic non-foam region (52) and ceramic foam regions (60, 70, 80) comprising a gradient porosity therein, wherein the ceramic foam regions and the metallic non-foam region are integrally formed together to create the integrated ceramic/metallic component. The integrated ceramic/metallic component (50) comprises a metallic region (52) and a single piece ceramic foam construction (58) comprising a plurality of ceramic foam regions (60, 70, 80) therein, each ceramic foam region comprising a predetermined pore size and a predetermined volume percent porosity, wherein the single piece ceramic foam construction (58) is integrally joined to the metallic region (52) to form the integrated ceramic/metallic component. These components may be utilized in gas turbine engines. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
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