Compressor and Method for Compressing Gaseous Fuel
    1.
    发明申请
    Compressor and Method for Compressing Gaseous Fuel 审中-公开
    压缩机和压缩气体燃料的方法

    公开(公告)号:US20110045416A1

    公开(公告)日:2011-02-24

    申请号:US12920664

    申请日:2009-01-29

    IPC分类号: F23C99/00 F23L17/00

    摘要: A method for compressing gaseous fuel is disclosed. The method includes, ingesting gaseous fuel into a chamber, ingesting air into the chamber and mixing the gaseous fuel with the air, igniting and partially combusting the resulting mixture of gaseous fuel and air in a confined space such that a predominant fraction of the gaseous fuel is not combusted, causing an increased temperature and therefore an increased pressure of the fraction of the gaseous fuel which is not combusted, and discharging the resulting compressed gaseous fuel. Moreover, a compressor is provided including a casing, a rotor with at least three vanes, an inlet for gaseous fuel, an outlet for gaseous fuel, an air inlet and an igniter. The rotor is placed in the casing such that at least three variable-volume chambers part-bounded by the vanes are formed during a rotor revolution.

    摘要翻译: 公开了一种压缩气体燃料的方法。 该方法包括:将气体燃料摄入室中,将空气吸入室内并将气体燃料与空气混合,点燃和部分燃烧所产生的气体燃料和空气混合物在密闭空间中,使得气体燃料的主要部分 不燃烧,导致温度升高,因此增加未燃烧的气体燃料的分数的压力,并排出所得到的压缩气体燃料。 此外,提供一种压缩机,其包括壳体,具有至少三个叶片的转子,用于气体燃料的入口,用于气体燃料的出口,空气入口和点火器。 转子被放置在壳体中,使得在转子旋转期间形成由叶片限定的至少三个可变容积的室。

    Arrangement for Preparation of a Fuel for Combustion
    2.
    发明申请
    Arrangement for Preparation of a Fuel for Combustion 有权
    燃料燃料的制备安排

    公开(公告)号:US20120144833A1

    公开(公告)日:2012-06-14

    申请号:US13400246

    申请日:2012-02-20

    IPC分类号: F23R3/28

    摘要: An arrangement for preparation of a fuel for combustion including a burner is provided. The arrangement includes a combustion chamber associated with the burner and in which combustion of a fuel is to take place, as well as means for supplying liquid fuel to the arrangement through an internal passage in the burner for the combustion, solid portions of the burner body being heated by the combustion, wherein the internal passage is located inside the solid portions of the burner body for receiving heat energy evaporating the fuel from these body portions, and that it includes means for conveying vaporized fuel to the combustion chamber to take part in the combustion.

    摘要翻译: 提供了一种用于制备包括燃烧器的用于燃烧的燃料的装置。 该装置包括与燃烧器相关联的燃烧室,其中将发生燃料的燃烧,以及用于通过用于燃烧的燃烧器中的内部通道将液体燃料供应到该装置的装置,燃烧器本体的固体部分 通过燃烧被加热,其中内部通道位于燃烧器主体的固体部分的内部,用于接收从这些主体部分蒸发燃料的热能,并且其包括用于将蒸发的燃料输送到燃烧室以参与燃烧室 燃烧。

    Arrangement for preparation of a fuel for combustion
    3.
    发明授权
    Arrangement for preparation of a fuel for combustion 有权
    用于燃烧燃料的配制

    公开(公告)号:US08142186B2

    公开(公告)日:2012-03-27

    申请号:US11992336

    申请日:2006-08-16

    IPC分类号: F23D11/44 F23L15/00

    摘要: The invention relates to an arrangement for preparation of a fuel for combustion including a burner, a combustion chamber associated with the burner and in which combustion of a fuel is to take place in use of the arrangement as well as means for supplying liquid fuel to the arrangement through an internal passage in the burner for said combustion, solid portions of the burner body being heated by said combustion in use of the arrangement, wherein said internal passage is located inside said solid portions of the burner body for receiving heat energy evaporating said fuel from these body portions, and that it comprises means for conveying vaporized fuel to the combustion chamber to take part in the combustion.

    摘要翻译: 本发明涉及一种用于燃烧燃料的配置方法,包括燃烧器,与燃烧器相关的燃烧室,燃料燃烧在燃料的使用中将被发生,以及用于向液体燃料供应燃料的装置 通过用于所述燃烧的燃烧器中的内部通道布置,燃烧器主体的实心部分在使用该装置时被所述燃烧加热,其中所述内部通道位于燃烧器主体的所述实心部分的内部,用于接收蒸发所述燃料的热能 并且其包括用于将蒸发的燃料输送到燃烧室以参与燃烧的装置。

    Gas Turbine Combustor
    4.
    发明申请
    Gas Turbine Combustor 有权
    燃气轮机燃烧器

    公开(公告)号:US20090320490A1

    公开(公告)日:2009-12-31

    申请号:US12226069

    申请日:2007-04-04

    IPC分类号: F23C7/00 F23R3/12 F23R3/28

    摘要: A gas turbine combustor is provided, which comprises: a combustion chamber having an axial direction and a radial direction; air passages for feeding an air stream into the combustion chamber which are oriented such that the flowing direction for each air stream flowing into the combustion chamber includes an angle with the combustion chamber's radial direction so as to introduce a swirl in the in-flowing air and an angle of at least 60° with the combustion chamber's axial direction; and fuel injection openings which are located in the air passages. Each air passage defines a turning flow path with a turning between 70° and 150° in a radial direction of the combustion chamber and a turning between 0° and 235° in an axial direction of the combustion chamber.

    摘要翻译: 提供一种燃气轮机燃烧器,其包括:具有轴向和径向方向的燃烧室; 用于将空气流供给到燃烧室中的空气通道,其被定向成使得流入燃烧室的每个气流的流动方向与燃烧室的径向方向成一角度,以便在流入的空气中引入涡流,并且 与燃烧室的轴向方向至少为60°的角度; 和位于空气通道中的燃料喷射开口。 每个空气通道限定在燃烧室的径向方向上在70°和150°之间的转动和在燃烧室的轴向方向上在0°和235°之间的转动的转向流动路径。

    Arrangement for preparation of a fuel for combustion
    5.
    发明授权
    Arrangement for preparation of a fuel for combustion 有权
    用于燃烧燃料的配制

    公开(公告)号:US08959923B2

    公开(公告)日:2015-02-24

    申请号:US13400246

    申请日:2012-02-20

    摘要: An arrangement for preparation of a fuel for combustion including a burner is provided. The arrangement includes a combustion chamber associated with the burner and in which combustion of a fuel is to take place, as well as means for supplying liquid fuel to the arrangement through an internal passage in the burner for the combustion, solid portions of the burner body being heated by the combustion, wherein the internal passage is located inside the solid portions of the burner body for receiving heat energy evaporating the fuel from these body portions, and that it includes means for conveying vaporized fuel to the combustion chamber to take part in the combustion.

    摘要翻译: 提供了一种用于制备包括燃烧器的用于燃烧的燃料的装置。 该装置包括与燃烧器相关联的燃烧室,其中将发生燃料的燃烧,以及用于通过用于燃烧的燃烧器中的内部通道将液体燃料供应到该装置的装置,燃烧器本体的固体部分 通过燃烧被加热,其中内部通道位于燃烧器主体的固体部分的内部,用于接收从这些主体部分蒸发燃料的热能,并且其包括用于将蒸发的燃料输送到燃烧室以参与燃烧室 燃烧。

    Gas turbine combustor
    6.
    发明授权
    Gas turbine combustor 有权
    燃气轮机燃烧器

    公开(公告)号:US08596074B2

    公开(公告)日:2013-12-03

    申请号:US12226069

    申请日:2007-04-04

    IPC分类号: F23R3/14 F23R3/28 F23R3/36

    摘要: A gas turbine combustor is provided, which comprises: a combustion chamber having an axial direction and a radial direction; air passages for feeding an air stream into the combustion chamber which are oriented such that the flowing direction for each air stream flowing into the combustion chamber includes an angle with the combustion chamber's radial direction so as to introduce a swirl in the in-flowing air and an angle of at least 60° with the combustion chamber's axial direction; and fuel injection openings which are located in the air passages. Each air passage defines a turning flow path with a turning between 70° and 150° in a radial direction of the combustion chamber and a turning between 0° and 235° in an axial direction of the combustion chamber.

    摘要翻译: 提供一种燃气轮机燃烧器,其包括:具有轴向和径向方向的燃烧室; 用于将空气流供给到燃烧室中的空气通道,其被定向成使得流入燃烧室的每个气流的流动方向与燃烧室的径向方向成一角度,以便在流入的空气中引入涡流,并且 与燃烧室的轴向方向至少为60°的角度; 和位于空气通道中的燃料喷射开口。 每个空气通道限定在燃烧室的径向方向上在70°和150°之间的转动和在燃烧室的轴向方向上在0°和235°之间的转动的转向流动路径。

    Arrangement for Preparation of a Fuel for Combustion
    7.
    发明申请
    Arrangement for Preparation of a Fuel for Combustion 有权
    燃料燃料的制备安排

    公开(公告)号:US20090170043A1

    公开(公告)日:2009-07-02

    申请号:US11992336

    申请日:2006-08-16

    摘要: The invention relates to an arrangement for preparation of a fuel for combustion including a burner, a combustion chamber associated with the burner and in which combustion of a fuel is to take place in use of the arrangement as well as means for supplying liquid fuel to the arrangement through an internal passage in the burner for said combustion, solid portions of the burner body being heated by said combustion in use of the arrangement, wherein said internal passage is located inside said solid portions of the burner body for receiving heat energy evaporating said fuel from these body portions, and that it comprises means for conveying vaporized fuel to the combustion chamber to take part in the combustion.

    摘要翻译: 本发明涉及一种用于燃烧燃料的配置方法,包括燃烧器,与燃烧器相关的燃烧室,燃料燃烧在燃料的使用中将被发生,以及用于向液体燃料供应燃料的装置 通过用于所述燃烧的燃烧器中的内部通道布置,燃烧器主体的实心部分在使用该装置时被所述燃烧加热,其中所述内部通道位于燃烧器主体的所述实心部分的内部,用于接收蒸发所述燃料的热能 并且其包括用于将蒸发的燃料输送到燃烧室以参与燃烧的装置。

    Apparatus for Modifying the Content of a Gaseous Fuel
    8.
    发明申请
    Apparatus for Modifying the Content of a Gaseous Fuel 审中-公开
    用于改变气态燃料含量的装置

    公开(公告)号:US20090249793A1

    公开(公告)日:2009-10-08

    申请号:US11990467

    申请日:2006-07-31

    IPC分类号: F02C6/18 F23R3/26 F02C7/22

    摘要: There is described an apparatus for modifying the content of a gaseous fuel comprising: a supply of the gaseous fuel; a supply of an oxidant; and a combustion device for utilising the oxidant to partially combust a first proportion of the fuel thereby to produce products of the partial combustion including intermediate combustion products, the products of the partial combustion mixing with the remaining proportion of fuel not partially combusted thereby to provide the modified fuel, wherein the partial combustion is controlled so as to provide the intermediate combustion products required to produce a predetermined modified fuel.

    摘要翻译: 描述了一种用于改变气体燃料的含量的装置,包括:气体燃料的供应; 供应氧化剂; 以及燃烧装置,用于利用氧化剂部分地燃烧第一比例的燃料,从而产生包括中间燃烧产物的部分燃烧产物,部分燃烧混合的产物与未部分燃烧的剩余部分燃料混合,从而提供 改进的燃料,其中控制部分燃烧以提供产生预定改性燃料所需的中间燃烧产物。

    Fuel injector arrangement; method of operating a fuel injector
arrangement
    9.
    发明授权
    Fuel injector arrangement; method of operating a fuel injector arrangement 失效
    燃油喷射器装置 操作燃料喷射器装置的方法

    公开(公告)号:US6095791A

    公开(公告)日:2000-08-01

    申请号:US755978

    申请日:1996-11-25

    申请人: Peter Senior

    发明人: Peter Senior

    CPC分类号: F23D17/00 F23C7/00 F23D14/24

    摘要: A fuel injector arrangement for fluid fuel combustion apparatus comprises a conduit 31 for the flow of an airstream, a conduit 56 for the flow of fluid fuel to a housing 15 incorporating a fuel plenum chamber 25, the fuel plenum chamber 25 having at least one inlet orifice 22 and at least one outlet orifice 34 in substantially direct alignment, the inlet orifice(s) 22 being connected to the conduit 31 whereby, in use, air in the airstream flows into the plenum chamber to thereby force fuel out of the plenum chamber via the outlet orifice(s). The airstream may constitute a secondary airstream, there being, in use, a primary airstream which flows around and beyond the housing in a conduit 10 to receive the fuel forced out of the fuel plenum chamber.

    摘要翻译: 用于流体燃料燃烧装置的燃料喷射器装置包括用于气流流动的导管31,用于将流体燃料流动到包含燃料增压室25的壳体15的导管56,燃料增压室25具有至少一个入口 孔22和至少一个出口孔34基本上直接对准,入口孔22连接到管道31,由此在使用中气流中的空气流入增压室,从而迫使燃料流出增压室 通过出口孔。 气流可能构成二次气流,在使用中存在在导管10中流动并超出壳体的主气流,以接收被迫从燃料增压室排出的燃料。

    Method of establishing part-load operation in a gas turbine group
    10.
    发明授权
    Method of establishing part-load operation in a gas turbine group 失效
    在燃气轮机组中建立部分负荷运行的方法

    公开(公告)号:US5465569A

    公开(公告)日:1995-11-14

    申请号:US290287

    申请日:1994-08-15

    摘要: A method of establishing part-load operation is proposed for a turbine group. This gas turbine group consists essentially of a compressor unit (1), of an HP combustion chamber (4) downstream of the compressor unit (1), of an HP turbine (5) downstream of this HP combustion chamber (4), of an LP combustion chamber (8) operating by self-ignition and arranged downstream of the HP turbine (5), the hot gases (10) of which LP combustion chamber (8) being admitted to an LP turbine (11). The temperature at outlet from the HP turbine (5) remains essentially the same due to the reduction of the fuel quantity in the LP combustion chamber (8) to zero. Furthermore, the fuel quantity of the HP combustion chamber (4) remains approximately constant during the reduction of the fuel quantity in the LP combustion chamber (8) so that the temperature at inlet to the HP turbine (5) likewise remains constant.

    摘要翻译: 对涡轮机组提出了建立部分负荷运行的方法。 该燃气轮机组基本上由在该HP燃烧室(4)下游的HP涡轮机(5)的压缩机单元(1)下游的HP燃烧室(4),HP涡轮机(5)的压缩机单元(1) LP燃烧室(8)通过自点火操作并且布置在HP涡轮机(5)的下游,LP燃烧室(8)的热气体(10)被允许进入LP涡轮机(11)。 由于LP燃烧室(8)中的燃料量减少到零,来自HP涡轮(5)的出口处的温度保持基本相同。 此外,在LP燃烧室(8)中的燃料量的减少期间,HP燃烧室(4)的燃料量保持大致恒定,使得HP涡轮机(5)入口处的温度同样保持恒定。