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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1 | 粉状燃料、其弥散体及其相关燃烧装置 | CN200780049429.8 | 2007-11-16 | CN101730797B | 2015-11-25 | J·K·麦奈特; J·T·麦奈特; E·巴科恩; K·W·怀特 |
本申请描述了粉状燃料、产生粉状燃料源的方法和粉状燃料的弥散,以及用于生产并改装燃烧装置从而燃烧粉状燃料(作为单一燃料源或与现有燃料源相结合)的系统、套件和方法。示例性实施例包括改造成燃烧粉状燃料的发动机和熔炉。 | ||||||
2 | 粉状燃料、其弥散体及其相关燃烧装置 | CN200780049429.8 | 2007-11-16 | CN101730797A | 2010-06-09 | J·K·麦奈特; J·T·麦奈特; E·巴科恩; K·W·怀特 |
本申请描述了粉状燃料、产生粉状燃料源的方法和粉状燃料的弥散,以及用于生产并改装燃烧装置从而燃烧粉状燃料(作为单一燃料源或与现有燃料源相结合)的系统、套件和方法。示例性实施例包括改造成燃烧粉状燃料的发动机和熔炉。 | ||||||
3 | 用于煤燃烧的气化器和旋风分离器 | CN200910204966.6 | 2009-09-30 | CN101717661A | 2010-06-02 | S·K·维德纳; L·B·小达维斯 |
本发明涉及用于煤燃烧的气化器和旋风分离器。具体而言,一种直燃煤燃烧系统(100)包括涡流室(114),其具有构造成用以接收水煤浆的输入件,以及致使水煤浆与来自压缩机(106)的排出空气混合,以使水煤浆气化并产生合成气。该系统还包括直接联接在涡流室的第二端上的旋风分离器(116)和联接在旋风分离器的输出端上的第二级燃烧输入件(112)。 | ||||||
4 | Powder fuel, the powder fuel dispersion, and the powder fuel-related combustion equipment | JP2009537216 | 2007-11-16 | JP2010510469A | 2010-04-02 | ベイコーン エドワード; ダブリュー ホワイト ケン; ケイ マクナイト ジェームズ; ティー マクナイト ジェームズ |
本願は、粉末燃料、粉末燃料源の生成方法、および粉末燃料のディスパージョン、ならびに粉末燃料を唯一の燃料源として燃焼させ、あるいは既存の燃料源との組み合わせにおいて燃焼させるために、燃焼装置を製造および適合させるためのシステム、キット、および方法を説明する。 典型的な態様は、粉末燃料を燃焼させるように構成されたエンジンおよび炉を含んでいる。
【選択図】図2 |
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5 | JPS625241B2 - | JP1417079 | 1979-02-09 | JPS625241B2 | 1987-02-04 | PEERU BORUIESUGARUDO; ANDERUSU KURENDORUFU; YAN UITSUKUNERU |
6 | JPS56501460A - | JP50237780 | 1980-10-21 | JPS56501460A | 1981-10-08 | |
7 | アルミニウムを再生可能燃料として利用する方法 | JP2012183301 | 2012-08-22 | JP6080034B2 | 2017-02-15 | 後藤 徹也; 荒川 義博; 高橋 周平; 中野 正勝; 松井 信 |
8 | Power plant comprises a combustor for performing combustion in a fluidized bed | JP51006690 | 1990-06-20 | JP2788117B2 | 1998-08-20 | BURANSUTOROOMU ROINE; MARUMUKUBISUTO REOHORUDO |
9 | Gas generator for high temperature propelling gas for gas turbines and others | JP12844580 | 1980-09-16 | JPS5653318A | 1981-05-12 | GUNNAA HARUKEGARUDO; ANDERUSU KURENDORUFU; YAN UIKUNAA; TEIGE BINDO |
10 | Staustrahltriebwerk mit verschmeltzbarer Gasleitrohrbeschichtung | EP09006869.3 | 2009-05-22 | EP2148073A3 | 2013-08-07 | Ramsel, Jürgen; Klose, Göran |
Ein Flugkörper (1) mit einem Staustrahltriebwerk (2) mit einer Brennkammer (3) weist einen Generator (11) mit einem Festtreibstoff (14) zur Erzeugung eines Brenngases (7) in einer Brenngasgeneratorkammer (9) auf, welche mit der Brennkammer (3) über ein Gasleitrohr (8) verbunden ist. Die Innenwand (15) des Gasleitrohres (8) ist mit einer Beschichtung (17) versehen, die bei einer Temperatur unterhalb der Brenngastemperatur schmilzt oder sich zersetzt. |
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11 | Method and device for feeding powdered fuel into the combustor of an open cycle gas turbine | EP10170050.8 | 2010-07-19 | EP2317228A2 | 2011-05-04 | Kuo, Mr, Tsung-Hsien |
The present invention provides a device for feeding powdered fuel into the combustor of an open cycle gas turbine for combustion and then working in the gas turbine so as to generate power, and more particularly to an innovative method and device with use of closed helical feeder that can prevent leakage of high-pressure combusting gas along the rotating shaft of helical fin within the containment vessel. |
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12 | Staustrahltriebwerk mit verschmeltzbarer Gasleitrohrbeschichtung | EP09006869.3 | 2009-05-22 | EP2148073A2 | 2010-01-27 | Ramsel, Jürgen; Klose, Göran |
Ein Flugkörper (1) mit einem Staustrahltriebwerk (2) mit einer Brennkammer (3) weist einen Generator (11) mit einem Festtreibstoff (14) zur Erzeugung eines Brenngases (7) in einer Brenngasgeneratorkammer (9) auf, welche mit der Brennkammer (3) über ein Gasleitrohr (8) verbunden ist. Die Innenwand (15) des Gasleitrohres (8) ist mit einer Beschichtung (17) versehen, die bei einer Temperatur unterhalb der Brenngastemperatur schmilzt oder sich zersetzt. |
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13 | Verfahren zum Abschalten einer Wirbelschichtfeuerung für pulverisierte, feste Brennstoffe | EP80107738.9 | 1980-12-09 | EP0052163B1 | 1984-10-10 | Brunner, Alfred, Dr. |
14 | Powdered fuels, dispersions thereof, and combustion devices related thereto | US12466899 | 2009-05-15 | US09057522B2 | 2015-06-16 | James K. McKnight; James T. McKnight |
This application describes powdered fuels, methods of producing powdered fuels source, and dispersions of powdered fuels, as well as systems, kits, and methods for producing and adapting combustion devices to burn powdered fuel, either as a sole fuel source or in combination with existing fuel sources. Exemplary embodiments include engines and furnaces adapted to combust powdered fuel. | ||||||
15 | GASIFIER AND CYCLONE SEPARATOR FOR COAL COMBUSTION | US12247706 | 2008-10-08 | US20100083882A1 | 2010-04-08 | Stanley Kevin Widener; Lewis Berkley Davis, JR. |
A direct-fired coal combustion system includes a swirl chamber having an input configured to receive a coal-water slurry and causing the coal-water slurry to mix with discharge air from a compressor to gasify the coal-water slurry and create a synthesis gas. The system also includes a cyclone separator directly coupled to the second end of the swirl chamber and a second stage combustion input coupled to an output of the cyclone separator. | ||||||
16 | Method and Means for Using Commom Dusts as Fuel for and Engine | US12551576 | 2009-09-01 | US20100064952A1 | 2010-03-18 | Lawrence George BROWN |
A combustion device, relying on the Newtonian principle of equal and opposite reaction to create rotational output, using dust/air mixtures for creating explosions within the burn chambers, creating distilled water and sodium carbonate as byproducts, and using washable rotating screens and liquid scrubbers to purify exhaust, and centrifuges in turn to purify and recirculate the scrubbing means | ||||||
17 | POWDERED FUELS, DISPERSIONS THEREOF, AND COMBUSTION DEVICES RELATED THERETO | US12466899 | 2009-05-15 | US20100055629A1 | 2010-03-04 | James K. McKnight; James T. McKnight |
This application describes powdered fuels, methods of producing powdered fuels source, and dispersions of powdered fuels, as well as systems, kits, and methods for producing and adapting combustion devices to burn powdered fuel, either as a sole fuel source or in combination with existing fuel sources. Exemplary embodiments include engines and furnaces adapted to combust powdered fuel. | ||||||
18 | Power plant with a combustor for combustion in a fluidized bed | US778970 | 1991-12-23 | US5163384A | 1992-11-17 | Roine Brannstrom; Leopold Malmkvist |
The invention relates to a power plant with a combustor (10) with combustion of a fuel in a fluidized bed of a particulate material and with a storage container (36) for hot bed material for adjusting the bed height upon changes of the load by the transfer of bed material from the combustor (10) to the storage container (36) and vice versa. It is primarily intended for a PFBC power plant with the combustor (10) and the container (36) in a pressure vessel (14) filled with compressed combustion air. The container (36) is provided with an internal mantle (66) which surrounds the storage space (40) for the bed material and an internal insulation (68) in the gap (70) which is formed between the container wall (36a) and the mantle (66). The lower part of the mantle (66) is joined to the container wall by means of an outwardly and upwardly directed skirt-like flange (66a-c). | ||||||
19 | Fluidized bed combustion chamber | US9571 | 1979-02-05 | US4237823A | 1980-12-09 | Pehr Borjesgard; Anders Kullendorff; Jan Wikner |
A fluidized bed combustion chamber adaptable for use with relatively large gas turbines and the like, wherein a substantially spherically-shaped outer casing encloses an annular fluidized bed combustion chamber which is mounted on a double bottom air distribution box. A cleaning assembly is positioned within the fluidized bed and the entire combustion chamber is supported on a base plate which extends through the casing and into contact with the box. Compressed air enters the spherical casing, is directed through a pair of cooling gaps, is caused to enter the air distribution box and then passes through the fluidized bed. | ||||||
20 | Use of high energy propellant in gas generators | US558194 | 1975-03-13 | US4115999A | 1978-09-26 | James P. Diebold |
Thin pieces of high energy propellant are potted in a potting material suchs isocyanates cured hydroxy terminated polybutadiene, hydroxy terminated polybutadiene, polyurethane, polyester or polysulfide so that they will primarily end burn. The result is a composite structure that can be used to produce cool gases suitable for use in gas generator applications. |