GAS TURBINE FUEL BLENDING USING INFERRED FUEL COMPOSITIONS
    1.
    发明申请
    GAS TURBINE FUEL BLENDING USING INFERRED FUEL COMPOSITIONS 审中-公开
    使用推荐燃料组合物的燃气涡轮机燃油混合

    公开(公告)号:US20160068777A1

    公开(公告)日:2016-03-10

    申请号:US14478973

    申请日:2014-09-05

    Abstract: A system, method, and computer-readable medium for blending a fuel for use in a gas turbine are disclosed. A measurement of a heating value of a process gas and a measurement of a molecular weight of the process gas is obtained. An estimate of a composition of the process gas is obtained using the obtained measurement of the heating value and the obtained measurement of the molecular weight. A blending ratio of the process gas and a natural gas is selected based on the estimate of the composition of the process gas. The process gas and the natural gas are then blended according to the selected blending ratio to obtain a fuel mixture for use in the gas turbine.

    Abstract translation: 公开了一种用于混合用于燃气轮机中的燃料的系统,方法和计算机可读介质。 获得处理气体的加热值的测定和处理气体的分子量的测定。 使用所得到的热值的测定和所得到的分子量的测定,求出处理气体的组成的估计。 基于处理气体的组成的估计来选择处理气体和天然气的共混比。 然后根据所选择的混合比率混合处理气体和天然气,以获得用于燃气轮机的燃料混合物。

    FLAME DETECTOR AND METHOD
    2.
    发明申请

    公开(公告)号:US20220307385A1

    公开(公告)日:2022-09-29

    申请号:US17210754

    申请日:2021-03-24

    Abstract: A method of detecting flame state of a combustor of a turbine engine. The method includes determining at least one of a first derivative and a second derivative of a compressor discharge pressure of a compressor of the turbine engine; determining at least one of a first derivative and a second derivative of a gas turbine exhaust gas temperature of the exhaust gases output by the turbine engine; determining at least one of a first derivative and a second derivative of a gas turbine shaft/rotor speed of the turbine engine; determining at least one of a first derivative and a second derivative of combustor dynamic pressure monitoring; and determining a flame state of a combustor of the turbine engine based on the combustor dynamic pressure monitoring, the determined derivatives of the combustion dynamics, compressor discharge pressure, gas turbine shaft/rotor speed, and gas turbine exhaust gas temperature of the exhaust gases.

    SYSTEM AND METHOD FOR CONTROLLED FUEL BLENDING IN GAS TURBINES
    3.
    发明申请
    SYSTEM AND METHOD FOR CONTROLLED FUEL BLENDING IN GAS TURBINES 有权
    用于气体涡轮机中控制燃料混合的系统和方法

    公开(公告)号:US20140283523A1

    公开(公告)日:2014-09-25

    申请号:US13848500

    申请日:2013-03-21

    CPC classification number: F02C9/40 F02C7/22 F02C7/232 F23N2037/08

    Abstract: A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured operating parameter of the combustor.

    Abstract translation: 一种系统包括具有燃烧器的燃气涡轮发动机和燃料混合系统。 燃料混合系统还包括构造成供应第一燃料的第一燃料供应,构造成供应第二燃料的第二燃料供应,第一燃料电路,第二燃料电路和控制器。 第一燃料回路可以被配置为混合第一燃料和第二燃料以形成第一燃料以形成第一燃料混合物。 第二燃料回路可以被配置成混合第一燃料和第二燃料以形成第二燃料混合物。 控制器可以被配置为基于所测量的燃烧器的操作参数来调节第一燃料混合物和第二燃料混合物的混合。

    SYSTEM AND METHOD FOR FUEL BLENDING AND CONTROL IN GAS TURBINES
    4.
    发明申请
    SYSTEM AND METHOD FOR FUEL BLENDING AND CONTROL IN GAS TURBINES 有权
    燃气混合和控制在气体涡轮机中的系统和方法

    公开(公告)号:US20140260309A1

    公开(公告)日:2014-09-18

    申请号:US13842075

    申请日:2013-03-15

    Abstract: A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured composition of the first fuel.

    Abstract translation: 一种系统包括具有燃烧器的燃气涡轮发动机和燃料混合系统。 燃料混合系统还包括构造成供应第一燃料的第一燃料供应,构造成供应第二燃料的第二燃料供应,第一燃料电路,第二燃料电路和控制器。 第一燃料回路可以被配置成混合第一燃料和第二燃料以形成第一燃料混合物。 第二燃料回路可以被配置成混合第一燃料和第二燃料以形成第二燃料混合物。 控制器可以被配置为基于测量的第一燃料的组成来调节第一燃料混合物和第二燃料混合物的混合。

    Non-optical flame detector and method for a combustor of a turbine engine

    公开(公告)号:US11519292B2

    公开(公告)日:2022-12-06

    申请号:US17210754

    申请日:2021-03-24

    Abstract: A method of detecting flame state of a combustor of a turbine engine. The method includes determining at least one of a first derivative and a second derivative of a compressor discharge pressure of a compressor of the turbine engine; determining at least one of a first derivative and a second derivative of a gas turbine exhaust gas temperature of the exhaust gases output by the turbine engine; determining at least one of a first derivative and a second derivative of a gas turbine shaft/rotor speed of the turbine engine; determining at least one of a first derivative and a second derivative of combustor dynamic pressure monitoring; and determining a flame state of a combustor of the turbine engine based on the combustor dynamic pressure monitoring, the determined derivatives of the combustion dynamics, compressor discharge pressure, gas turbine shaft/rotor speed, and gas turbine exhaust gas temperature of the exhaust gases.

    Model-less combustion dynamics autotune

    公开(公告)号:US10830443B2

    公开(公告)日:2020-11-10

    申请号:US15391450

    申请日:2016-12-27

    Abstract: This disclosure relates to systems and methods for tuning combustion dynamics in a combustor. In one embodiment of the disclosure, a method includes providing, via at least one sensor, combustion dynamics amplitude data associated with a combustor. Method may allow monitoring, by an equipment controller communicatively coupled to the at least one sensor, the combustion dynamics amplitude data. The method may allow detecting at least one change in acoustic pressure amplitude associated with combustion in the combustor. In response to detecting the change in the acoustic pressure amplitude, the method proceeds with determining a fuel split change to at least two fuel circuits configured to supply fuel to the combustor, and applying the fuel split change to the combustor.

    System and method for fuel blending and control in gas turbines
    7.
    发明授权
    System and method for fuel blending and control in gas turbines 有权
    燃气轮机燃油混合和控制系统和方法

    公开(公告)号:US09377202B2

    公开(公告)日:2016-06-28

    申请号:US13842075

    申请日:2013-03-15

    Abstract: A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured composition of the first fuel.

    Abstract translation: 一种系统包括具有燃烧器的燃气涡轮发动机和燃料混合系统。 燃料混合系统还包括构造成供应第一燃料的第一燃料供应,构造成供应第二燃料的第二燃料供应,第一燃料电路,第二燃料电路和控制器。 第一燃料回路可以被配置成混合第一燃料和第二燃料以形成第一燃料混合物。 第二燃料回路可以被配置成混合第一燃料和第二燃料以形成第二燃料混合物。 控制器可以被配置为基于测量的第一燃料的组成来调节第一燃料混合物和第二燃料混合物的混合。

    MODEL-LESS COMBUSTION DYNAMICS AUTOTUNE
    8.
    发明申请

    公开(公告)号:US20180149363A1

    公开(公告)日:2018-05-31

    申请号:US15391450

    申请日:2016-12-27

    Abstract: This disclosure relates to systems and methods for tuning combustion dynamics in a combustor. In one embodiment of the disclosure, a method includes providing, via at least one sensor, combustion dynamics amplitude data associated with a combustor. Method may allow monitoring, by an equipment controller communicatively coupled to the at least one sensor, the combustion dynamics amplitude data. The method may allow detecting at least one change in acoustic pressure amplitude associated with combustion in the combustor. In response to detecting the change in the acoustic pressure amplitude, the method proceeds with determining a fuel split change to at least two fuel circuits configured to supply fuel to the combustor, and applying the fuel split change to the combustor.

    System and method for controlled fuel blending in gas turbines
    9.
    发明授权
    System and method for controlled fuel blending in gas turbines 有权
    燃气轮机控制燃料混合的系统和方法

    公开(公告)号:US09382850B2

    公开(公告)日:2016-07-05

    申请号:US13848500

    申请日:2013-03-21

    CPC classification number: F02C9/40 F02C7/22 F02C7/232 F23N2037/08

    Abstract: A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured operating parameter of the combustor.

    Abstract translation: 一种系统包括具有燃烧器的燃气涡轮发动机和燃料混合系统。 燃料混合系统还包括构造成供应第一燃料的第一燃料供应,构造成供应第二燃料的第二燃料供应,第一燃料电路,第二燃料电路和控制器。 第一燃料回路可以被配置为混合第一燃料和第二燃料以形成第一燃料以形成第一燃料混合物。 第二燃料回路可以被配置成混合第一燃料和第二燃料以形成第二燃料混合物。 控制器可以被配置为基于所测量的燃烧器的操作参数来调节第一燃料混合物和第二燃料混合物的混合。

Patent Agency Ranking