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公开(公告)号：US07669422B2
公开(公告)日：2010-03-02
申请号：US11460114
申请日：2006-07-26
IPC分类号： F23R3/06
CPC分类号： F23R3/06 , F23R2900/03042 , Y02T50/675 , Y10T29/4932
摘要： A combustor liner includes a liner having an upstream end and a downstream end having a longitudinal axis extending therethrough, and a plurality of cooling holes formed in the liner, the cooling holes are arranged along the longitudinal axis into a plurality of circumferentially extending rows that are variably spaced apart along the longitudinal axis.
摘要翻译： 燃烧器衬套包括具有上游端和具有延伸穿过其中的纵向轴线的下游端的衬套和形成在衬套中的多个冷却孔，所述冷却孔沿着纵向轴线布置成多个周向延伸的行， 沿着纵轴可变地间隔开。
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公开(公告)号：US20100011773A1
公开(公告)日：2010-01-21
申请号：US11460114
申请日：2006-07-26
CPC分类号： F23R3/06 , F23R2900/03042 , Y02T50/675 , Y10T29/4932
摘要： A combustor liner includes a liner having an upstream end and a downstream end having a longitudinal axis extending therethrough, and a plurality of cooling holes formed in the liner, the cooling holes are arranged along the longitudinal axis into a plurality of circumferentially extending rows that are variably spaced apart along the longitudinal axis.
摘要翻译： 燃烧器衬套包括具有上游端和具有延伸穿过其中的纵向轴线的下游端的衬套和形成在衬套中的多个冷却孔，冷却孔沿着纵向轴线布置成多个周向延伸的行， 沿着纵轴可变地间隔开。
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公开(公告)号：US06513331B1
公开(公告)日：2003-02-04
申请号：US09934182
申请日：2001-08-21
IPC分类号： F02C304
CPC分类号： F23R3/06 , Y02T50/675
摘要： A multi-hole cooled combustor liner is provided which reduces hot streaks and associated material distress in the liner. Areas of increased cooling hole density are disposed upstream of the primary dilution holes and in circumferential alignment with fuel cup centers. Additional cooling holes are provided in between primary dilution holes are arranged in alternating pairs of circumferentially angled holes so as to provide a converging cooling air flow in the downstream direction.
摘要翻译： 提供了多孔冷却的燃烧器衬套，其减少衬里中的热条纹和相关材料的窘迫。 增加冷却孔密度的区域设置在初级稀释孔的上游并且与燃料杯中心周向对准。 主要稀释孔之间设置有另外的冷却孔，交替成对的周向成角度的孔，以便在下游方向提供会聚的冷却空气流。
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公开(公告)号：US20130081270A1
公开(公告)日：2013-04-04
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译： 一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。 该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。
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公开(公告)号：US06758045B2
公开(公告)日：2004-07-06
申请号：US10233356
申请日：2002-08-30
IPC分类号： F02C314
CPC分类号： F23R3/002 , F23R3/346 , F23R3/50 , F23R2900/00005
摘要： A method enables a gas turbine engine multi-domed combustor including an outer liner and an inner liner that define a combustion chamber therebetween to be assembled. The method comprises coupling a first dome including a heat shield that includes an annular endbody that extends a first distance axially from the heat shield to the combustor outer liner, and coupling a second dome including a heat shield that includes an annular endbody that extends a second distance axially from the heat shield to the first dome, such that the second dome is radially aligned with respect to the first dome, and wherein the second dome second distance is less than the first dome first distance.
摘要翻译： 一种方法能够使燃气涡轮发动机多圆顶燃烧器包括在其间限定燃烧室以组装的外衬套和内衬套。 该方法包括联接包括隔热罩的第一穹顶，所述隔热罩包括环形端体，所述环形端体从所述隔热罩轴向延伸到所述燃烧器外衬套，并且连接包括隔热罩的第二穹顶，所述隔热罩包括环形端体， 从隔热板轴向延伸到第一圆顶，使得第二圆顶相对于第一圆顶径向对准，并且其中第二圆顶第二距离小于第一圆顶第一距离。
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公开(公告)号：US08893382B2
公开(公告)日：2014-11-25
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译： 一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。 该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。
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公开(公告)号：US07578134B2
公开(公告)日：2009-08-25
申请号：US11329783
申请日：2006-01-11
IPC分类号： F02C7/20
摘要： A method for assembling a gas turbine engine is provided. The method includes providing a combustor liner support including a first portion formed with a plurality of circumferentially-spaced recessed areas, and a second portion extending from the first portion. The method also includes coupling the combustor liner support within a combustor such that during engine operations cooling air is channeled through the plurality of recessed areas to facilitate cooling the combustor liner support.
摘要翻译： 提供一种用于组装燃气涡轮发动机的方法。 该方法包括提供包括形成有多个周向间隔开的凹陷区域的第一部分和从第一部分延伸的第二部分的燃烧器衬套支撑件。 该方法还包括将燃烧器衬套支撑件联接在燃烧器内，使得在发动机操作期间，冷却空气被引导通过多个凹陷区域以便于冷却燃烧器衬套支撑件。
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公开(公告)号：US20080110022A1
公开(公告)日：2008-05-15
申请号：US11558652
申请日：2006-11-10
IPC分类号： B23P15/04
CPC分类号： F23R3/60 , F23R3/10 , F23R3/14 , F23R3/286 , F23R3/50 , F23R2900/00017 , Y10T29/4932
摘要： A method of assembling a combustor for use in a turbine engine is disclosed. The method includes providing a dome assembly ring including a plurality of assembly ring openings, positioning a plurality of elongated rings on the dome assembly ring, providing a cowl assembly including an inner cowl portion and an outer cowl portion that are fabricated from sheet metal, and coupling the inner and outer cowl portions to the dome assembly ring such that each of the plurality of elongated rings is coupled to the dome assembly ring.
摘要翻译： 公开了一种组装用于涡轮发动机的燃烧器的方法。 该方法包括提供包括多个组装环开口的圆顶组件环，将多个细长环定位在圆顶组件环上，提供包括由金属板制成的内整流罩部分和外整流罩部分的整流罩组件，以及 将内外罩部分连接到圆顶组件环，使得多个细长环中的每一个联接到圆顶组件环。
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公开(公告)号：US08726669B2
公开(公告)日：2014-05-20
申请号：US13174027
申请日：2011-06-30
IPC分类号： F23R3/14
CPC分类号： F23R3/283 , F23R3/14 , F23R2900/00017 , Y02T50/675 , Y10T29/49348
摘要： A combustor dome assembly includes a dome plate with upstream and downstream faces and an aperture therein; a deflector with body and a tube section, the deflector fixedly attached to the dome plate adjacent the downstream face with the tube section in the aperture; a retainer having an annular body with a central opening therein, an annular flange, and at least one hook defining a slot, the retainer being fixedly attached to the dome plate adjacent the upstream face of the dome plate with the flange received in the aperture; and an annular mixer with a radial array of swirl vanes and an annular mounting flange, with a retention tab extending radially outward from the mounting flange. The mixer is disposed adjacent the upstream face with the mounting flange against the retainer. The retention tab is engaged in the slot to prevent axial withdrawal of the mixer from the retainer.
摘要翻译： 燃烧器穹顶组件包括具有上游和下游面的圆顶板和其中的孔; 具有主体和管部分的偏转器，偏转器固定地附接到邻近下游面的圆顶板，孔中的管部分; 保持器，其具有在其中具有中心开口的环形体，环形凸缘和限定狭槽的至少一个钩，所述保持器固定地附接到邻近圆顶板的上游面的圆顶板，凸缘容纳在孔中; 以及具有旋转叶片的径向阵列和环形安装凸缘的环形混合器，其具有从安装凸缘径向向外延伸的保持翼片。 混合器邻近上游面设置有安装凸缘抵靠保持器。 保持片接合在槽中以防止混合器从保持器轴向退出。
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公开(公告)号：US07765809B2
公开(公告)日：2010-08-03
申请号：US11558636
申请日：2006-11-10
CPC分类号： F23R3/10 , F23R3/50 , F23R3/60 , F23R2900/00017
摘要： A method of assembling a dome assembly for use in a turbine engine combustor is disclosed. The method includes providing a dome assembly ring, an inner liner portion, and an outer liner portion. The method also includes coupling the inner liner portion and the outer liner portion to the dome assembly ring, positioning a plurality of rings on the dome assembly ring, and coupling at least one of an inner cowl and an outer cowl to the dome assembly ring such that each of the plurality of rings and at least one of the inner and outer cowls are removable without uncoupling the dome assembly ring from either the inner or outer liner portions.
摘要翻译： 公开了一种组装用于涡轮发动机燃烧器的圆顶组件的方法。 该方法包括提供一个圆顶组件环，一个内衬部分和一个外衬套部分。 该方法还包括将内衬部分和外衬套部分联接到圆顶组件环，将多个环定位在圆顶组件环上，并将内罩和外罩中的至少一个联接到圆顶组件环， 所述多个环中的每个以及所述内罩和所述外罩中的至少一个是可移除的，而不使所述圆顶组件环与所述内衬部分或所述外衬套部分脱离联接。
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