-
公开(公告)号：US20120186256A1
公开(公告)日：2012-07-26
申请号：US13014388
申请日：2011-01-26
IPC分类号： F02C7/04
摘要： A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler.
摘要翻译： 提供了一种用于燃气涡轮发动机的混合器组件，包括具有位于至少一个径向旋流器和至少一个轴向旋流器之间的燃料喷射孔的主混合器，其中喷射到主混合器中的燃料被流过的空气雾化和分散 径向旋流器和轴向旋流器。
-
公开(公告)号：US08973368B2
公开(公告)日：2015-03-10
申请号：US13014388
申请日：2011-01-26
摘要： A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler.
摘要翻译： 提供了一种用于燃气涡轮发动机的混合器组件，包括具有位于至少一个径向旋流器和至少一个轴向旋流器之间的燃料喷射孔的主混合器，其中喷射到主混合器中的燃料被流过的空气雾化和分散 径向旋流器和轴向旋流器。
-
公开(公告)号：US20120186258A1
公开(公告)日：2012-07-26
申请号：US13014434
申请日：2011-01-26
IPC分类号： F02C7/22
CPC分类号： F23R3/343 , F23R3/14 , F23R3/18 , F23R3/286 , Y02T50/675
摘要： A mixer assembly for a gas turbine engine is provided, including a main mixer, and a pilot mixer having an annular housing in which a corner is formed between an aft portion of the housing and a bulkhead wall in which a corner recirculation zone is located to stabilize and anchor the flame of the pilot mixer. The pilot mixer can further include features to cool the annular housing, including in the area of the corner recirculation zone.
摘要翻译： 提供了一种用于燃气涡轮发动机的混合器组件，其包括主混合器和具有环形壳体的先导混合器，其中在壳体的后部部分和角部再循环区域所在的隔壁之间形成有角部， 稳定和锚定先导混合器的火焰。 先导式混合器还可以包括冷却环形壳体的特征，包括在角落再循环区域的区域中。
-
4.发明授权Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone 有权具有具有拐角火焰稳定化再循环区域的先导式混合器的燃气涡轮发动机的混合器组件公开(公告)号：US08312724B2
公开(公告)日：2012-11-20
申请号：US13014434
申请日：2011-01-26
IPC分类号： F02C1/00
CPC分类号： F23R3/343 , F23R3/14 , F23R3/18 , F23R3/286 , Y02T50/675
摘要： A mixer assembly for a gas turbine engine is provided, including a main mixer, and a pilot mixer having an annular housing in which a corner is formed between an aft portion of the housing and a bulkhead wall in which a corner recirculation zone is located to stabilize and anchor the flame of the pilot mixer. The pilot mixer can further include features to cool the annular housing, including in the area of the corner recirculation zone.
摘要翻译： 提供了一种用于燃气涡轮发动机的混合器组件，其包括主混合器和具有环形壳体的先导混合器，其中在壳体的后部部分和角部再循环区域所在的隔壁之间形成有角部， 稳定和锚定先导混合器的火焰。 先导式混合器还可以包括冷却环形壳体的特征，包括在角落再循环区域的区域中。
-
公开(公告)号：US20140013763A1
公开(公告)日：2014-01-16
申请号：US13545418
申请日：2012-07-10
申请人： Jeffrey M. Cohen , Zhongtao Dai , Kevin E. Green
发明人： Jeffrey M. Cohen , Zhongtao Dai , Kevin E. Green
CPC分类号： F23R3/28 , F23D2900/11101
摘要： A fuel-air premixer for a combustor of a gas turbine engine includes a central passage disposed along an axis and operable to communicate a first airflow and an outer annular passage about the axis operable to communicate a second airflow. The fuel-air premixer further includes an inner annular passage about the axis and between the central passage and the outer annular passage for communicating fuel flow. The inner annular passage including an inner exit angled for directing fuel flow toward the axis into a mixer passage downstream of the outer and inner exits for mixing the fuel flow with the first and second airflows.
摘要翻译： 用于燃气涡轮发动机的燃烧器的燃料空气预混合器包括沿着轴线设置的中心通道，其可操作以使第一气流和围绕可操作以连通第二气流的轴线的外部环形通道连通。 燃料空气预混合器还包括围绕轴线的中心通道和外部环形通道之间的内部环形通道，用于连通燃料流。 内部环形通道包括一个内部出口，该内部出口成角度，用于将燃料流向轴线引导到外部和外部出口下游的混合器通道中，用于将燃料流与第一和第二气流混合。
-
公开(公告)号：US09441836B2
公开(公告)日：2016-09-13
申请号：US13545418
申请日：2012-07-10
申请人： Jeffrey M. Cohen , Zhongtao Dai , Kevin E. Green
发明人： Jeffrey M. Cohen , Zhongtao Dai , Kevin E. Green
IPC分类号： F23R3/28
CPC分类号： F23R3/28 , F23D2900/11101
摘要： A fuel-air premixer for a combustor of a gas turbine engine includes a central passage disposed along an axis and operable to communicate a first airflow and an outer annular passage about the axis operable to communicate a second airflow. The fuel-air premixer further includes an inner annular passage about the axis and between the central passage and the outer annular passage for communicating fuel flow. The inner annular passage including an inner exit angled for directing fuel flow toward the axis into a mixer passage downstream of the outer and inner exits for mixing the fuel flow with the first and second airflows.
摘要翻译： 用于燃气涡轮发动机的燃烧器的燃料空气预混合器包括沿着轴线设置的中心通道，其可操作以使第一气流和围绕可操作以连通第二气流的轴线的外部环形通道连通。 燃料空气预混合器还包括围绕轴线的中心通道和外部环形通道之间的内部环形通道，用于连通燃料流。 内部环形通道包括一个内部出口，该内部出口成角度，用于将燃料流向轴线引导到外部和外部出口下游的混合器通道中，用于将燃料流与第一和第二气流混合。
-
公开(公告)号：US20130232978A1
公开(公告)日：2013-09-12
申请号：US13417380
申请日：2012-03-12
申请人： Zhongtao Dai , Jeffrey M. Cohen , Kevin E. Green
发明人： Zhongtao Dai , Jeffrey M. Cohen , Kevin E. Green
CPC分类号： F23R3/14 , F23R3/28 , Y02T50/675
摘要： A fuel-air premixer for a combustor of a turbine engine includes a central passage along an axis. The central passage is operable to communicate an unswirled airflow. An outer annular passage is located around the axis and includes a multiple of first swirl vanes that are operable to communicate a first swirled airflow in a first direction. An inner annular passage is located around the axis between the central passage and the outer annular passage. The inner annular passage includes a multiple of second swirl vanes that are operable to communicate a second swirled airflow in a second direction different than the first direction.
摘要翻译： 用于涡轮发动机的燃烧器的燃料 - 空气预混合器包括沿轴线的中心通道。 中央通道可操作以传达不流动的气流。 外部环形通道围绕轴线定位并且包括多个第一旋转叶片，其可操作以在第一方向上连通第一旋转气流。 内环形通道围绕中心通道和外环形通道之间的轴线定位。 内环形通道包括多个第二旋流叶片，其可操作以在不同于第一方向的第二方向上连通第二旋流气流。
-
公开(公告)号：US08943833B2
公开(公告)日：2015-02-03
申请号：US13542985
申请日：2012-07-06
IPC分类号： F02C1/00
摘要： A disclosed fuel injector provides mixing of fuel with airflow by surrounding a swirled fuel flow with first and second swirled airflows that ensures mixing prior to or upon entering the combustion chamber. Fuel tubes produce a central fuel flow along with a central airflow through a plurality of openings to generate the high velocity fuel/air mixture along the axis of the fuel injector in addition to the swirled fuel/air mixture.
摘要翻译： 所公开的燃料喷射器通过围绕具有第一和第二旋转气流的涡流燃料流来提供燃料与气流的混合，其确保在进入燃烧室之前或之后的混合。 燃料管产生中心燃料流以及中心气流通过多个开口，除了旋转的燃料/空气混合物之外，还沿着燃料喷射器的轴线产生高速燃料/空气混合物。
-
公开(公告)号：US20140007581A1
公开(公告)日：2014-01-09
申请号：US13542985
申请日：2012-07-06
IPC分类号： F23R3/28
摘要： A disclosed fuel injector provides mixing of fuel with airflow by surrounding a swirled fuel flow with first and second swirled airflows that ensures mixing prior to or upon entering the combustion chamber. Fuel tubes produce a central fuel flow along with a central airflow through a plurality of openings to generate the high velocity fuel/air mixture along the axis of the fuel injector in addition to the swirled fuel/air mixture.
摘要翻译： 所公开的燃料喷射器通过围绕具有第一和第二旋转气流的涡流燃料流来提供燃料与气流的混合，其确保在进入燃烧室之前或之后的混合。 燃料管产生中心燃料流以及中心气流通过多个开口，除了旋转的燃料/空气混合物之外，还沿着燃料喷射器的轴线产生高速燃料/空气混合物。
-
公开(公告)号：US08596071B2
公开(公告)日：2013-12-03
申请号：US11418613
申请日：2006-05-05
申请人： Mark Anthony Mueller , Zhongtao Dai , Michael Louis Vermeersch , Venkatraman Ananthakrishnanlyer , Timothy James Held , Jun Xu , Keith Robert McManus
发明人： Mark Anthony Mueller , Zhongtao Dai , Michael Louis Vermeersch , Venkatraman Ananthakrishnanlyer , Timothy James Held , Jun Xu , Keith Robert McManus
IPC分类号： F02C3/14
CPC分类号： F23R3/00 , F23R2900/00017
摘要： A method for assembling a gas turbine engine combustor is provided. The method includes providing a heat shield defined by a perimeter. The perimeter includes a radially inner edge, a radially outer edge, an axially inner edge, an axially outer edge, and an opening that extends from an upstream side of the heat shield to a downstream side of the heat shield. The method further includes coupling the heat shield to a domeplate such that the perimeter of the heat shield is positioned a distance downstream from an edge of the heat shield defining the opening. The method additionally includes coupling at least one fuel injector to the domeplate such that a portion of the fuel injector extends through the heat shield opening.
摘要翻译： 提供了一种用于组装燃气涡轮发动机燃烧器的方法。 该方法包括提供由周边限定的热屏蔽。 周边包括径向内边缘，径向外边缘，轴向内边缘，轴向外边缘和从隔热板的上游侧延伸到隔热罩的下游侧的开口。 该方法还包括将隔热罩联接到三脚架，使得隔热罩的周边定位在限定开口的隔热板的边缘的下游的距离处。 该方法另外包括将至少一个燃料喷射器联接到多孔板，使得燃料喷射器的一部分延伸穿过隔热开口。
-
-
-
-
-
-
-
-
-
搜索结果
11 条记录 (耗时 0.02 秒)
