DUAL FUEL COMBUSTOR FOR A GAS TURBINE ENGINE
    1.
    发明申请
    DUAL FUEL COMBUSTOR FOR A GAS TURBINE ENGINE 有权
    用于燃气涡轮发动机的双燃料燃烧器

    公开(公告)号:US20150059352A1

    公开(公告)日:2015-03-05

    申请号:US14017509

    申请日:2013-09-04

    CPC classification number: F23R3/36 F02C7/22 F02C7/222 F02C9/40

    Abstract: The present application and the resultant patent provide a dual fuel combustor for a gas turbine engine. The combustor may include a primary premixer positioned within a head end plenum of the combustor, and a dual fuel, injection system positioned within the head end plenum and upstream of the premixer. The injection system may be configured to inject a gas fuel about an inlet end of the premixer when the combustor operates on the gas fuel. The injection system also may be configured to vaporize and inject a liquid fuel about the inlet end of the premixer when the combustor operates on the liquid fuel. The present application and the resultant patent also provide a related method of operating a dual fuel combustor.

    Abstract translation: 本申请和所得专利提供了一种用于燃气涡轮发动机的双燃料燃烧器。 燃烧器可以包括位于燃烧器的头端集气室内的初级预混合器,以及位于前端集气室内和预混合器上游的双燃料喷射系统。 注射系统可以被配置为当燃烧器对气体燃料进行操作时,在预混合器的入口端附近注入气体燃料。 喷射系统还可以被配置为当燃烧器对液体燃料进行操作时,在预混合器的入口端附近蒸发和喷射液体燃料。 本申请和所得专利还提供了操作双燃料燃烧器的相关方法。

    Dual fuel combustor for a gas turbine engine including a toroidal injection manifold with inner and outer sleeves
    2.
    发明授权
    Dual fuel combustor for a gas turbine engine including a toroidal injection manifold with inner and outer sleeves 有权
    用于燃气涡轮发动机的双燃料燃烧器,其包括具有内套筒和外套筒的环形注射歧管

    公开(公告)号:US09416975B2

    公开(公告)日:2016-08-16

    申请号:US14017509

    申请日:2013-09-04

    CPC classification number: F23R3/36 F02C7/22 F02C7/222 F02C9/40

    Abstract: The present application and the resultant patent provide a dual fuel combustor for a gas turbine engine. The combustor may include a primary premixer positioned within a head end plenum of the combustor, and a dual fuel injection system positioned within the head end plenum and upstream of the premixer. The injection system may be configured to inject a gas fuel about an inlet end of the premixer when the combustor operates on the gas fuel. The injection system also may be configured to vaporize and inject a liquid fuel about the inlet end of the premixer when the combustor operates on the liquid fuel. The present application and the resultant patent also provide a related method of operating a dual fuel combustor.

    Abstract translation: 本申请和所得专利提供了一种用于燃气涡轮发动机的双燃料燃烧器。 燃烧器可以包括位于燃烧器的头端集气室内的初级预混合器,以及位于前端集气室内和预混合器上游的双燃料喷射系统。 注射系统可以被配置为当燃烧器对气体燃料进行操作时,在预混合器的入口端附近注入气体燃料。 喷射系统还可以被配置为当燃烧器对液体燃料进行操作时,在预混合器的入口端附近蒸发和喷射液体燃料。 本申请和所得专利还提供了操作双燃料燃烧器的相关方法。

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