公开(公告)号：US09518741B2

公开(公告)日：2016-12-13

申请号：US13972449

申请日：2013-08-21

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Darren Matthew Stratton ,  Behnood Miri

IPC: F23R3/28 ,  F23K5/00 ,  F23N1/00 ,  F02C7/22

CPC classification number: F23R3/28 ,  F02C7/222 ,  F23K5/007 ,  F23K2401/201 ,  F23N1/002 ,  F23N2041/20

Abstract: A fuel control module including a gas vent manifold is disclosed. The gas vent manifold includes a first gas vent portion including a first gas vent connection and a second gas vent portion including a second gas vent connection. The gas vent manifold also includes a condensation portion extending between the first gas vent portion and the second gas vent portion. The gas vent manifold further includes a condensation drain port fluidly connected to the condensation portion. The gas vent manifold also includes a plurality of connection ports. Each connection port is configured to fluidly couple the gas vent manifold to a vent line of one or more pneumatic valves.

Abstract translation: 公开了一种包括排气歧管的燃料控制模块。 排气歧管包括包括第一气体排放连接的第一气体排出部分和包括第二排气连接的第二气体排放部分。 排气歧管还包括在第一排气部分和第二排气部分之间延伸的冷凝部分。 排气歧管还包括流体连接到冷凝部分的冷凝排放口。 排气歧管还包括多个连接口。 每个连接端口被配置成将排气歧管流体耦合到一个或多个气动阀的排气管线。

公开(公告)号：US20160290554A1

公开(公告)日：2016-10-06

申请号：US15181958

申请日：2016-06-14

Applicant: Solar Turbines Incorporated

Inventor： Nicholas O. Saintarbor ,  David C. Taylor ,  Christopher M Moffatt ,  Darren M. Stratton

IPC: F16M13/02

CPC classification number: F16M13/02 ,  B60R11/00

Abstract: A module mounting system for a structure is provided. The module mounting system includes a supporting member having at least one slot. The module mounting system also includes at least one mounting assembly coupled to the at least one slot. The at least one mounting assembly is adapted to couple the supporting member with the structure. The at least one mounting assembly is movable within the at least one slot. The at least one mounting assembly includes a first mounting member. The at least one mounting assembly also includes a second mounting member having a first portion and a second portion. The first portion is received within the at least one slot. The first mounting member is coupled with the second mounting member through a first fastening member. The first mounting member and the second mounting member are coupled with the structure through a second fastening member.

Abstract translation: 提供了一种用于结构的模块安装系统。 模块安装系统包括具有至少一个槽的支撑构件。 模块安装系统还包括耦合到至少一个槽的至少一个安装组件。 所述至少一个安装组件适于将所述支撑构件与所述结构物联接。 所述至少一个安装组件可在所述至少一个槽内移动。 所述至少一个安装组件包括第一安装构件。 所述至少一个安装组件还包括具有第一部分和第二部分的第二安装构件。 第一部分被接收在至少一个时隙内。 第一安装构件通过第一紧固构件与第二安装构件联接。 第一安装构件和第二安装构件通过第二紧固构件与结构联接。

公开(公告)号：US20160281517A1

公开(公告)日：2016-09-29

申请号：US14669902

申请日：2015-03-26

Applicant: Solar Turbines Incorporated

Inventor： Yong Weon Kim ,  Garrett P. Prins

IPC: F01D9/04 ,  F01D25/12

CPC classification number: F01D9/065 ,  F01D5/189 ,  F05D2230/21 ,  F05D2240/121

Abstract: A nozzle segment for a turbine nozzle of a gas turbine engine is disclosed. The nozzle segment includes an upper endwall, a lower endwall spaced apart from the upper endwall, a pressure portion, and a suction portion. The pressure portion extends between the upper endwall and the lower endwall adjacent a first side of the nozzle segment. The suction portion is spaced apart from the pressure portion and extends between the upper endwall and the lower endwall adjacent a second side of the nozzle segment. The second side is opposite the first side.

Abstract translation: 公开了一种用于燃气涡轮发动机的涡轮喷嘴的喷嘴段。 喷嘴段包括上端壁，与上端壁间隔开的下端壁，压力部分和抽吸部分。 压力部分在上端壁和下端壁之间相邻于喷嘴段的第一侧延伸。 抽吸部分与压力部分间隔开并且在上端壁和下端壁之间延伸，邻近喷嘴段的第二侧。 第二面与第一面相对。

公开(公告)号：US09447976B2

公开(公告)日：2016-09-20

申请号：US14152821

申请日：2014-01-10

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Christopher Zdzislaw Twardochleb ,  Rasoul Z. Paydar

IPC: F23R3/28 ,  F23R3/14

CPC classification number: F23R3/286 ,  F23C2900/07001 ,  F23R3/14

Abstract: A fuel injector for a combustor of a gas turbine engine is disclosed. The fuel injector includes a gas gallery and a gas passage. The gas gallery is an annular passage configured to circumferentially distribute gas fuel. The gas passage includes an inlet and an outlet. The inlet is distal to the gas gallery and includes an inlet area with a circular shape. The outlet adjoins the gas gallery and includes an outlet area including an annular sector shape. The gas passage is configured to diffuse the gas fuel and discharge the gas fuel from the outlet and into the gas gallery.

Abstract translation: 公开了一种用于燃气涡轮发动机的燃烧器的燃料喷射器。 燃料喷射器包括气体通道和气体通道。 气体通道是构造成周向分布气体燃料的环形通道。 气体通道包括入口和出口。 入口远离气体通道并且包括具有圆形形状的入口区域。 出口邻接气体通道并且包括包括环形扇形形状的出口区域。 气体通道构造成扩散气体燃料并将气体燃料从出口排放到气体库中。

公开(公告)号：US09404367B2

公开(公告)日：2016-08-02

申请号：US13684056

申请日：2012-11-21

Applicant: Solar Turbines Incorporated

Inventor： Cory Patrick Muscat ,  Laura Elizabeth McDonald ,  James Eric Miller ,  Gary Paul Vavrek

IPC: F01D5/02 ,  F01D5/06 ,  F01D5/30

CPC classification number: F01D5/027 ,  F01D5/06 ,  F01D5/3015 ,  F01D5/3038

Abstract: A method for balancing a compressor rotor assembly including a forward weldment (211) and an aft weldment (212) includes pre-balancing the aft weldment (212) of the compressor rotor assembly (210) with compressor disks (220) prior to populating the compressor disks (220) with circumferentially installed compressor rotor blades (230). Pre-balancing the aft weldment (212) includes measuring a rotational balance of the aft weldment (212). Pre-balancing the aft weldment (212) also includes determining a number of underplatform weights (260) needed and a location for each underplatform weight (260) within a circumferential slot (236) of one the compressor disks (220). Pre-balancing the aft weldment (212) further includes mounting each underplatform weight (260) in the determined location.

Abstract translation: 一种用于平衡包括前向焊接件（211）和后部焊件（212）的压缩机转子组件的方法包括：在压缩机转子组件（210）的后部焊件（212）与压缩机盘（220）预先平衡之前， 具有周向安装的压缩机转子叶片（230）的压缩机盘（220）。 预平衡后焊件（212）包括测量后焊件（212）的旋转平衡。 预平衡船尾焊件（212）还包括确定在压缩机盘（220）之一的圆周槽（236）内的所需的底板数量（260）和每个底板下重量（260）的位置。 预平衡船尾焊件（212）还包括将每个底板重量（260）安装在所确定的位置。

公开(公告)号：US20160201489A1

公开(公告)日：2016-07-14

申请号：US14593998

申请日：2015-01-09

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Yong Weon Kim ,  Tsuhon Lin ,  Jeffrey Stephen Carullo

IPC: F01D9/04

CPC classification number: F01D9/047 ,  F01D5/189 ,  F01D9/02

Abstract: An insert tube of a turbine vane is disclosed. The insert tube includes a pressure side wall, a suction side wall opposite and spaced apart from the pressure side wall, a leading edge, and a trailing edge opposite the leading edge. The insert tube includes a plurality of cooling channels spaced along the pressure side wall. The insert tube includes an indented portion located between the trailing edge and the pressure side wall.

Abstract translation: 公开了一种涡轮叶片的插入管。 插入管包括压力侧壁，与压力侧壁相对且间隔开的吸力侧壁，前缘和与前缘相对的后缘。 插入管包括沿着压力侧壁间隔开的多个冷却通道。 插入管包括位于后缘和压力侧壁之间的凹入部分。

公开(公告)号：US09388742B2

公开(公告)日：2016-07-12

申请号：US13889954

申请日：2013-05-08

Applicant: Solar Turbines Incorporated

Inventor： Georgina J. McGee ,  Thomas John Chipman Rogers ,  Anthony Fahme ,  Daniel Paul Panayil

IPC: F23R3/26 ,  F23R3/10 ,  F23R3/28 ,  F02C7/232 ,  F23R3/14 ,  F23C7/00

CPC classification number: F02C7/232 ,  F23C7/008 ,  F23R3/10 ,  F23R3/14 ,  F23R3/26 ,  F23R3/283 ,  F23R3/286

Abstract: A swirler inlet valve plate for a fuel injector of a gas turbine engine includes a blocker ring and a pivot sleeve mechanically connected to the blocker ring. The blocker ring is formed from at least a portion of a toroid shape. The blocker ring includes a blocking surface perpendicular to an axis of the blocker ring formed from at least a portion of an annulus. The blocker ring also includes a flow surface, an inner circumferential surface of the toroidal shape. The pivot sleeve includes a sleeve portion extending adjacent the blocker ring. The sleeve portion includes a rotation transmission mechanism.

Abstract translation: 用于燃气涡轮发动机的燃料喷射器的旋流器入口阀板包括阻塞环和与阻塞环机械连接的枢轴套筒。 阻挡环由环形面的至少一部分形成。 阻挡环包括垂直于由环的至少一部分形成的阻挡环的轴线的阻挡表面。 阻塞环还包括流动表面，环形形状的内圆周表面。 枢轴套筒包括在阻挡环附近延伸的套筒部分。 套筒部分包括旋转传动机构。

公开(公告)号：US20160169114A1

公开(公告)日：2016-06-16

申请号：US14571829

申请日：2014-12-16

Applicant: Solar Turbines Incorporated

Inventor： Cody Charles Howarth ,  Gregory Palczewski ,  Nicholas Owen Saintarbor

IPC: F02C7/24 ,  F01D25/24 ,  F02C9/18

CPC classification number: F02C7/24 ,  F05D2220/40 ,  F05D2220/76 ,  F05D2260/231

Abstract: A shield assembly for shielding a housing of an electro-mechanical device from a hot body includes a first sidewall and a second sidewall disposed in a spaced apart relation from each other. A third sidewall extends between the first sidewall and the second sidewall to define a space therebetween. The first, second, and third sidewalls are configured to receive the housing of the electro-mechanical device in the space defined therebetween. The shield assembly further includes a backing plate extending laterally from a bottom end of at least one of the first, second, and third sidewalls. The backing plate is releasably fastened with a bottom end of the housing. The shield assembly further includes a tab member extending away from a top end of at least one of the first, second, and third sidewalls. The tab member is releasably fastened with a bracket associated with the housing of the electro-mechanical device.

Abstract translation: 用于将机电装置的壳体与热体屏蔽的屏蔽组件包括以彼此间隔开的关系设置的第一侧壁和第二侧壁。 第三侧壁在第一侧壁和第二侧壁之间延伸以在其间限定一个空间。 第一，第二和第三侧壁被配置为在其间限定的空间中容纳机电装置的壳体。 屏蔽组件还包括从第一，第二和第三侧壁中的至少一个侧壁的底端横向延伸的背板。 背板与壳体的底端可释放地紧固。 屏蔽组件还包括从第一，第二和第三侧壁中的至少一个侧壁的顶端延伸的突片构件。 突片构件可释放地用与机电装置的壳体相关联的支架紧固。

公开(公告)号：US09347325B2

公开(公告)日：2016-05-24

申请号：US13665453

申请日：2012-10-31

Applicant: Solar Turbines Incorporated

Inventor： Leslie John Faulder ,  Jeffrey Eugene Tarczy

IPC: F01D5/22 ,  F01D5/30 ,  F01D11/00 ,  F01D5/10

CPC classification number: F01D5/22 ,  F01D5/10 ,  F01D5/3015 ,  F01D5/3069 ,  F01D11/006

Abstract: A damper for a turbine rotor assembly of a gas turbine engine may include a forward plate with a forward face and an aft face, and an aft plate with a forward face and an aft face. The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure. An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket on the forward face of the forward plate.

Abstract translation: 用于燃气涡轮发动机的涡轮转子组件的阻尼器可以包括具有前表面和后表面的前板，以及具有前表面和后表面的后板。 前板的后表面可以以纵向结构连接到后板的前表面。 后板在横向于纵向结构的平面中的区域可以大于横向于纵向结构的平面中的前板的面积。 阻尼器还可以包括在前板的前表面上的凹槽。

公开(公告)号：US09341194B2

公开(公告)日：2016-05-17

申请号：US13666758

申请日：2012-11-01

Applicant: Solar Turbines Incorporated

Inventor： John Frederick Lockyer

IPC: F04D29/56 ,  F01D17/16 ,  F01D11/00

CPC classification number: F04D29/563 ,  F01D11/001 ,  F01D17/162 ,  F05D2300/501

Abstract: An inner bushing assembly (280) to provide a biasing force between a guide vane (260) and an inner ring half (261) of a gas turbine engine compressor (200) is disclosed. The inner bushing assembly (280) includes a first bushing (281), a second bushing (282), and a biasing element (283). The first bushing (281) is configured to be installed about an inner vane shaft (267) of the guide vane (260) adjacent to an airfoil (265) of the guide vane (260). The second bushing (282) is configured to be installed about the inner vane shaft (267) distal to the airfoil (265). The biasing element (283) is configured to be installed about the inner vane shaft (267) between the first bushing (281) and the second bushing (282).

Abstract translation: 公开了一种用于在燃气涡轮发动机压缩机（200）的引导叶片（260）和内环半部（261）之间提供偏置力的内衬套组件（280）。 内衬套组件（280）包括第一衬套（281），第二衬套（282）和偏压元件（283）。 第一衬套（281）构造成围绕与导叶（260）的翼型件（265）相邻的导叶（260）的内叶片轴（267）安装。 第二衬套（282）构造成围绕翼型（265）远侧的内叶片轴（267）安装。 偏置元件（283）构造成围绕第一衬套（281）和第二衬套（282）之间的内部叶片轴（267）安装。