序号 | 专利名 | 申请号 | 申请日 | 公开(公告)号 | 公开(公告)日 | 发明人 |
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101 | Anticorrosion brick and production method of the same | JP2013111103 | 2013-05-27 | JP2014028742A | 2014-02-13 | YAMAGUCHI KENICHI; KIMURA YUSUKE |
PROBLEM TO BE SOLVED: To provide an anticorrosion brick that has excellent anticorrosion to corrosion of a solution and has a long life; and a production method of the same.SOLUTION: An anticorrosion brick is characterized by having a coating layer that is a ternary oxide of each component of a brick and Fe, and that comprises a spinel solid solution having a melting point of at least 1,600°C in an Al-Cr based brick, an Al-Mg based brick or a Cr-Mg based brick, and a production method of the anticorrosion brick is characterized in that in the Al-Cr based brick, the Al-Mg based brick or the Cr-Mg based brick, a magnetite powder layer is disposed on a brick surface, and the magnetite powder is heated to be melted, each component of the brick is reacted with Fe, thereby a coating layer that is a ternary oxide of a brick component and Fe and that comprises a spinel solid solution having a melting point of at least 1,600°C is formed. | ||||||
102 | High performance and clean pressurized gasifier and method for dry powder of a carbonaceous substance | JP2012545044 | 2009-12-25 | JP2013515789A | 2013-05-09 | チョンタオ ル,; ミンクン ワン,; ソンビン ジアン,; ウェイ シン,; ルイホン ガオ,; ホンハイ リ, |
ガス化チャンバ(II)および合成ガス冷却チャンバ(III)を備える固体燃料ガス化装置、特には石炭粉の加圧ガス化によって合成ガスを生成するための装置。 ガス化チャンバの内壁が、水冷壁(4)である。 水冷壁の内側が、耐火材料の層(16)で一様に覆われている。 ガス化チャンバの水冷壁と炉本体との間に環状の空洞が存在している。 合成ガス冷却装置、垂直パイプ(22)、ガス分配装置(24)、脱泡装置、および脱水/脱灰装置(21)が、合成ガス冷却チャンバに設けられている。 前記合成ガス冷却装置は、ガス化チャンバの底部の円すい形のディスクに接続されている。 垂直パイプ(22)が、合成ガス冷却装置に接続されている。 垂直パイプ(22)の下部が、滑らかな移行を介してトランペット状のガス分配装置(24)に接続されている。 バッフル装置が、ガス分配装置(24)の上方に配置され、その上方に脱泡装置が配置されている。 装置は、単純な構造を有しており、運転が容易である。 炭素質物質の乾燥粉末の高温ガス化方法が、可燃性の物質および酸素を炉へと噴霧し、その後に点火させるステップを含む。
【選択図】図1 |
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103 | Countercurrent combustor | JP2012523220 | 2010-07-21 | JP2013506104A | 2013-02-21 | イェルク・ミューラー; ウィンフレート・カイペルス |
燃焼室(5)を有しており、可燃ガス(B)及び酸化剤(O)が対向側から前記燃焼室に供給される向流燃焼器は、相互に連結され、他の上に一つが位置している3つの平面基板(1、2、3)を備えており、前記中基板(2)は燃焼室(5)を備えており、前記基板の平面内に位置する通路(4)が対向方向で前記燃焼室から端部へ通じており、前記上基板(3)及び前記下基板(1)は基本的に閉じられており、少なくとも前記中基板(2)はマイクロシステム技術を用いて製造されている。 | ||||||
104 | Process reduction reactor | JP2008538972 | 2006-10-30 | JP5102217B2 | 2012-12-19 | ダニエル, オー. クラーク,; セバスチャン ラオクス,; ロバート, エム. ヴァーミュレン,; シャウン, ダブリュー. クラウフォード, |
105 | Combustion apparatus having a compliant wall | JP2007524793 | 2005-05-20 | JP4886687B2 | 2012-02-29 | エイム・ジョン; オー・シージン; スタンフォード・スコット・イー.; プララッド・ハーシャ; ペルライン・ロナルド・イー. |
106 | Corrosion protective coating for the coating process and turbine components | JP2011517076 | 2009-06-23 | JP2011527382A | 2011-10-27 | ヴェルナー・シュタム; クラウス・クルシュ |
Method for coating a surface (23) of a fuel-guiding component (20) of a turbine component comprises coating the surface initially with a titanium nitride layer (21) using chemical gas phase deposition and then with an alpha-aluminum oxide layer (22). An independent claim is also included for a turbine component with the above coating. | ||||||
107 | Lining of the wall of the industrial furnace | JP2010538385 | 2008-11-21 | JP2011508173A | 2011-03-10 | イムレ・ヨハネス; ホルン・マルクス |
本発明は、コンクリート、鋼鉄、金属の薄板又はその類似物からなる耐火被覆された壁を腐食から保護するための工業炉の壁の内張りに関する。 この壁1の内張りは、少なくとも2つの層3及び4からなり、バリア層としての層3は加圧されている。 | ||||||
108 | Multilayered impingement complex for cooling wall | JP2009283250 | 2009-12-14 | JP2010144722A | 2010-07-01 | HESELHAUS ANDREAS |
PROBLEM TO BE SOLVED: To provide a multilayered impingement complex for cooling a wall, which generates multiple collisional cooling flows, and also to provide a method of manufacturing the multilayered impingement complex. SOLUTION: The multilayered impingement complex has: a plurality of pinhole layers (2) each provided with a plurality of through-holes (3) dispersedly arranged over a surface thereof, the through-holes being configured as pinholes; and a plurality of web layers (6). The web layers are layered alternately with the pinhole layers (2), and each includes a plurality of webs (7). The webs are dispersedly arranged over the surface of the pinhole layer (2), and each bridges the pinhole layers. Each web (7) of one web layer (6) is aligned in a line with each web (7) of the other web layer (7), and each through-hole (3) of one pinhole layer (2) is offset with respect to a through-hole (3) of an adjacent pinhole layer (3). COPYRIGHT: (C)2010,JPO&INPIT | ||||||
109 | Process reduction reactor | JP2008538972 | 2006-10-30 | JP2009513347A | 2009-04-02 | ロバート, エム. ヴァーミュレン,; ダニエル, オー. クラーク,; シャウン, ダブリュー. クラウフォード,; セバスチャン ラオクス, |
特定の実施形態では、ガスストリームから汚染物質を除去する際に使用するための装置が提供される。 該装置は、複数の積層多孔性セラミックリングから形成された熱反応ユニットを含む。 該多孔性セラミックリングの第1は第1の熱膨張係数(CTE)を有しており、該多孔性セラミックリングの第2は第2のCTEを有している。 他の態様も提供される。
【選択図】 図1 |
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110 | Training method using the training facilities and the equipment of the combustion furnace | JP2003191885 | 2003-07-04 | JP4149865B2 | 2008-09-17 | 晃 名雪; 光博 山本; 浩二 岩田; 三喜男 鈴木 |
111 | Combustion apparatus having a compliant wall | JP2007524793 | 2005-05-20 | JP2008504491A | 2008-02-14 | エイム・ジョン; オー・シージン; スタンフォード・スコット・イー.; プララッド・ハーシャ; ペルライン・ロナルド・イー. |
【課題】
【解決手段】本明細書に記載された燃焼装置は、コンプライアントな燃焼室の壁または部分を備える。 コンプライアント部分は、燃焼室内での燃焼中に変形する。 一部の装置は、燃焼室内での燃料の燃焼によって生成された圧力に応じて伸長するよう構成されたコンプライアント壁を備えてよい。 結合部分は、コンプライアント部分または壁の変形を機械的出力に変換する。 1以上のポートは、酸素源および燃料を燃焼室内に取り込んで、排気ガスを燃焼室から排出するよう構成されている。 【選択図】図2B |
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112 | Combustion device | JP2006061630 | 2006-03-07 | JP2007240050A | 2007-09-20 | ABE TOSHIHIRO |
PROBLEM TO BE SOLVED: To reduce manufacturing costs by surely cooling an outer cylinder portion by allowing the water to flow between the outer cylinder portion and an inner cylinder portion, so that inexpensive materials can be used for the outer cylinder portion. SOLUTION: This combustion device comprises a combustion chamber body 1 burning a burning material and exhausting a gas after combustion, a fluid supply portion 30 supplying the fluid to the combustion chamber body, and an outer chamber body 50 rotatably and drivably supporting the combustion chamber body 1. The combustion chamber body 1 is composed of the outer cylinder portion 10 and the inner cylinder portion 20, and the inner cylinder portion 20 is composed of heat-proof fluid composed of particles 21 meltable by heat in burning the burning material, and pressed to an outer cylinder portion 10 side by centrifugal force of the combustion chamber body 1 to form an inner wall of the combustion chamber body 1. The combustion device comprises a water supply portion 100 for supplying the water in such manner that it is pressed to the outer cylinder portion 10 side by centrifugal force in rotating the combustion chamber body 1 and flows down on an inner side face of the outer cylinder portion 10, and steam taking-out portions 110, 120 for taking out the steam generated when the water from the water supply portion 100 is evaporated in a process of flowing down on the inner face of the outer cylinder portion 10. COPYRIGHT: (C)2007,JPO&INPIT | ||||||
113 | Combustor member, combustor panel, and manufacturing method of combustor member | JP2005111479 | 2005-04-08 | JP2005300141A | 2005-10-27 | SCHLICHTING KEVIN W; ALAN D SETEL; MURRAY STEPHEN D; MARCIN JOHN J JR |
<P>PROBLEM TO BE SOLVED: To provide a combustor member and a combustor panel for a gas turbine engine, and a manufacturing method of the combustor member. <P>SOLUTION: Articles 37C, 38C, 31 have characteristic heat-mechanical stress principal directions 516, 524, 532. The articles 37C, 38C, 31 are provided with a single crystal base body having the lowest modulus direction (for example, [001]) within target alignment to the principal directions. The member may be selected from a group comprising a combustor shell component 30 and a heat shielding component 31. The member may have the whole shape of a truncated cone-shaped shell segment. The gas turbine engine may include the plurality of such members used as heat shielding components 37, 38. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
114 | Improved high temperature combustor wall for reducing temperature by optical reflection and its manufacturing method | JP2003431900 | 2003-12-26 | JP2004211701A | 2004-07-29 | ACKERMAN JOHN FREDERICK; ARSZMAN PAUL VINCENT; NAGARAJ BANGALORE ASWATHA; YOUNG CRAIG DOUGLAS; JUSTIS NICOLE BARBARA |
<P>PROBLEM TO BE SOLVED: To provide a high temperature gas turbine constituting part being a mirror surface optical reflector, and used in a gas passage 120. <P>SOLUTION: A heat insulating coating film 114 is polished so as to form a surface 115 for properly reflecting radiation heat in the gas passage. Next, a thin layer of a high temperature reflector 116 is stuck on the polished heat insulating coating film 114 by a method of properly fixing the reflector to the polished surface without increasing roughness of the surface. The high temperature reflector 116 is stuck to a rear optional surface of a compressor 16, for example, a combustor wall surface. The surface reflects the radiation heat, and returns the heat in the high temperature gas passage 120. The reflected radiation heat is not focused on the other any hardware constituting part. The constituting part is designed so that the radiation heat is returned to the gas passage 120, not by absorption into a wall of the constituting part having the only action for only raising a temperature of the wall. <P>COPYRIGHT: (C)2004,JPO&NCIPI | ||||||
115 | Combustor liner equipped with inverted turbulator | JP2003362644 | 2003-10-23 | JP2004144469A | 2004-05-20 | BUNKER RONALD SCOTT |
PROBLEM TO BE SOLVED: To provide a combustor liner for a gas turbine for enhancing a cooling level with the minimum pressure loss. SOLUTION: This combustor liner has a substantially cylindrical shape, and has a plurality of circumferential-directional grooves 48 arranged with spacing along an axial direction formed on an outer surface of the combustor liner. The groove 48 has a substantially semi-circular cross-section, and arrayed laterally with respect to a cooling air flowing direction. The groove 48 has the substantially semi-circular cross-section, has a diameter D, and a depth of the groove is equal to about 0.05-0.50D. COPYRIGHT: (C)2004,JPO | ||||||
116 | Lining for thermal insulation bricks of the combustor wall, combustor and gas turbine | JP2002536468 | 2001-10-04 | JP2004511751A | 2004-04-15 | クリスチーネ タウト |
高温媒体(M)に曝される高温側面(3)と、この高温側面(3)と反対側の壁側面(5)と、高温側面(3)に隣接する高温側面部(7)と、壁側面(5)に隣接する壁側面部(9)とを備えた特に燃焼器壁(43)を内張りするための断熱煉瓦(1、1A、1B)に関する。 本発明に基づいて、壁側面部(9)における平均粒度(D)を、高温側面部(7)におけるそれより小さくし、壁側面部では大きな強度、高温側面では熱応力、温度および交番温度負荷に対する大きな耐力を得て、煉瓦の寿命を延ばす。 | ||||||
117 | Protective layer for component to be subjected to thermal load, particularly for turbine blade | JP2001386385 | 2001-12-19 | JP2002241961A | 2002-08-28 | BOSSMANN HANS-PETER; KRANZMANN AXEL; REISS HARALD; SCHMUTZLER HANS JOACHIM; SOMMER MARIANNE; WEILER LUDWIG |
PROBLEM TO BE SOLVED: To provide a protective layer having prolonged life used for a component to be subjected to thermal load. SOLUTION: The protective layer is used for the component (1) to be subjected to thermal load, particularly for a turbine blade, for protecting it from corrosion and/or oxidation and/or erosion. This protective layer (3) has a sealing layer (4) having a form of single layer or multilayer and composed of amorphous material. | ||||||
118 | Method of manufacturing a hydrogen bromide gas and its implementation device | JP18931497 | 1997-06-30 | JP3105834B2 | 2000-11-06 | ドリヴォン ジル; デル シルヴィー; ノダリ ティエリ; レイデッケル ミシェル |
119 | Inflator treatment apparatus and inflator charge judgment method | JP26457497 | 1997-09-29 | JPH11101422A | 1999-04-13 | FUKAHORI MITSUHIKO; NAKABAYASHI YASUO; SAKAI TSURAYUKI; SUZUKI YASUMASA; YOSHITAKE TOMOO; FUJIOKA MASATO |
PROBLEM TO BE SOLVED: To prevent a furnace wall refractory from being damaged and a metal case of an inflator from melting at the time of action of a chemical, by providing a metallic bulkhead between a furnace wall inner face of a furnace for effecting inflator treatment and an inflator in such a manner as to cover the furnace wall inner face. SOLUTION: An inflator treatment apparatus is constructed by connecting a treatment furnace 2 of an inflator 1 and a combustion furnace 3, and furnace shells of the treatment furnace 2 and the combustion furnace 3 are formed of furnace walls 4a, 4b. A charge device 7 comprising a seal valve 5 and a charge pusher 6 is provided on a side part of the furnace wall 4a of the treatment furnace 2, and the inflator 1 is charged intermittently into the treatment furnace 2 by the charge device 7. Metallic bulkheads 8a-8c are installed between an inner face of the furnace wall 4a of the treatment furnace 2 and the inflator 1 charged into the treatment furnace 2. By such a construction, at the time of action of a chemical, furnace wall refractory is prevented from being damaged due to the inflator or scattering pieces thereof, the metallic case of the inflator 1 is prevented from melting and the metallic bulkheads 8a-8c of the treatment furnace 2 is prevented from undergoing high temperature oxidation. COPYRIGHT: (C)1999,JPO | ||||||
120 | Furnace for melting ash obtained from waste material combustion facility | JP12228495 | 1995-05-22 | JPH07324724A | 1995-12-12 | MARUKUSU PUFUISHIYUTAA; KURISUCHIYAN BUITSUKAATO |
PURPOSE: To improve life expectancy by a method wherein an inner wall of a lower structure acting as a melting region is made of refractory material containing mainly a specified rate of Cr 2O 3 in addition to other metallic oxides, and an inner wall of an upper structure acting as a gas region is made of a refractory material scarcely containing or containing no Cr 2O 3 but containing MgO of a specified rate or more. CONSTITUTION: This is a furnace for use in melting ash obtained from a waste material combustion facility including a furnace 1 which is comprised of a lower structure 2 and an upper structure covered by inner walls 4, 5 of which inner parts are made of a refractory material. The inner wall of the lower structure 2 acting as a melting region is made of a refractory material mainly containing Cr 2O 3 of 10 to 50% in addition to other metallic oxides The inner 23. wall of the upper structure 3 acting as the gas region is made of a refractory material containing MgO of 80% or more and scarcely containing Cr 2O 3 or substantially no Cr 2O 3. The melting furnace having this type of different configuration at the melting region of the lower part of the furnace or at the inner wall of the upper part of the furnace may provide a long life expectancy. COPYRIGHT: (C)1995,JPO |