公开(公告)号：US20140099876A1

公开(公告)日：2014-04-10

申请号：US13646944

申请日：2012-10-08

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Rajesh Prabhakaran Saraswathi ,  Venkateswara Rao Akana ,  Len Alan Wolf

IPC: F24F11/04 ,  F24F13/16

CPC classification number: F02C7/18 ,  F05D2240/12 ,  F05D2260/60 ,  F05D2260/608 ,  Y10T137/87812

Abstract: A flow balancing ventilation system includes a ventilation inlet for receiving an airflow, the ventilation inlet having a cavity defined by an outer wall. Also included is a plurality of ventilation ducts each having a first end and a second end, the first end of each of the plurality of ventilation ducts disposed in operable communication with the ventilation inlet for receiving the airflow, the second end of each of the plurality of ventilation ducts disposed at least partially within an enclosure. Further included is at least one vane disposed within the cavity of the ventilation inlet for manipulating the airflow proximate the first end of each of the plurality of ventilation ducts.

Abstract translation: 流量平衡通风系统包括用于接收气流的通风入口，通风入口具有由外壁限定的空腔。 还包括多个通风管道，每个通风管道具有第一端和第二端，多个通气管道中的每一个的第一端设置成与通风入口可操作地连通以接收气流，多个通风管道的第二端 至少部分地设置在外壳内的通风管道。 进一步包括设置在通风入口的空腔内的至少一个叶片，用于操纵靠近多个通风管道中的每一个的第一端的气流。

公开(公告)号：US08677766B2

公开(公告)日：2014-03-25

申请号：US12859948

申请日：2010-08-20

Applicant: Vincent P. Laurello ,  Keith D. Kimmel ,  Todd Ebert

Inventor： Vincent P. Laurello ,  Keith D. Kimmel ,  Todd Ebert

IPC: F02C7/18 ,  F01D5/08

CPC classification number: F01D5/081 ,  F01D5/082 ,  F02C7/28 ,  F05D2250/322 ,  F05D2260/20 ,  F05D2260/2212 ,  F05D2260/60

Abstract: A gas turbine engine comprises a pre-swirl structure coupled to a shaft cover structure and located radially between a supply of cooling fluid and a flow path. The pre-swirl structure defines a flow passage and includes a plurality of swirl members in the flow passage. A flow direction of cooling fluid passing through the flow passage is altered by the swirl members such that the cooling fluid has a velocity component in a direction tangential to the circumferential direction. The bypass passages provide cooling fluid into a turbine rim cavity associated with a first row vane assembly to prevent hot gas ingestion into the turbine rim cavity from a hot gas flow path associated with a turbine section of the engine.

Abstract translation: 燃气涡轮发动机包括联接到轴罩结构并且径向位于冷却流体供应源和流动路径之间的预旋转结构。 预旋涡结构限定了流动通道并且在流动通道中包括多个涡流构件。 通过流道的冷却流体的流动方向被涡旋部件改变，使得冷却流体在与圆周方向相切的方向上具有速度分量。 旁路通道将冷却流体提供到与第一行叶片组件相关联的涡轮机边缘空腔中，以防止热气体从与发动机的涡轮机部分相关联的热气流路径进入涡轮机边缘空腔。

公开(公告)号：US08449941B2

公开(公告)日：2013-05-28

申请号：US12616128

申请日：2009-11-10

Applicant: Min Tae Kim ,  Doo Soo Kim ,  Won Young Oh

Inventor： Min Tae Kim ,  Doo Soo Kim ,  Won Young Oh

IPC: C23C16/00

CPC classification number: C23C4/04 ,  C23C4/02 ,  C23C4/11 ,  C23C4/12 ,  C23C4/123 ,  C23C18/122 ,  C23C18/1225 ,  C23C18/1241 ,  F01D5/288 ,  F02C3/30 ,  F05D2230/90 ,  F05D2260/60 ,  Y02T50/67 ,  Y02T50/671

Abstract: Disclosed is a method for formation of a thermal bather coating on a gas turbine during operation thereof, which includes addition of an organic compound containing silicon to a fuel under a first condition in order to form a base layer on the surface of a part coming into contact with a combustion gas of the fuel in the gas turbine during operation thereof, as well as addition of the organic compound containing silicon to the fuel under a second condition in order to form a porous layer having more pores than the base layer above the base layer.

Abstract translation: 公开了一种在其运行期间在燃气轮机上形成热浴用涂层的方法，其包括在第一条件下向燃料中添加含硅的有机化合物，以在形成基底层的部分的表面上形成基层 在操作期间与燃气轮机中的燃料的燃烧气体接触，以及在第二条件下向燃料中加入含硅的有机化合物，以形成具有比基体上方的基底层更多的孔的多孔层 层。

公开(公告)号：US20120232768A1

公开(公告)日：2012-09-13

申请号：US13042322

申请日：2011-03-07

Applicant: Vijay Raghavendran Nenmeni ,  Michael John Rozdolski ,  Rahul Jaikaran Chillar

Inventor： Vijay Raghavendran Nenmeni ,  Michael John Rozdolski ,  Rahul Jaikaran Chillar

IPC: G06F19/00 ,  F02C7/22

CPC classification number: F02C9/40 ,  F02C7/232 ,  F05D2260/60 ,  F05D2260/602

Abstract: A system includes a turbine fuel controller. The turbine fuel controller includes a purge control logic configured to control a purge sequence of mixing a purge gas with a first fuel during a first fuel shutdown, wherein the purge sequence is configured to open a purge valve for the purge gas before fully closing a fuel valve for the first fuel.

Abstract translation: 一种系统包括涡轮燃料控制器。 涡轮燃料控制器包括净化控制逻辑，其被配置为在第一燃料关闭期间控制将净化气体与第一燃料混合的吹扫顺序，其中所述吹扫顺序被配置为在完全关闭燃料之前打开净化气体的净化阀 用于第一燃料的阀。

公开(公告)号：US20120063916A1

公开(公告)日：2012-03-15

申请号：US12878075

申请日：2010-09-09

Applicant: Bradley Taylor Boyer

Inventor： Bradley Taylor Boyer

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F05D2240/305 ,  F05D2240/306 ,  F05D2240/81 ,  F05D2260/2212 ,  F05D2260/60

Abstract: The present application provides a turbine blade cooling system. The turbine blade cooling system may include a first turbine blade with a first turbine blade platform having a cooling cavity in communication with a pressure side passage and a second turbine blade with a second turbine blade platform having a platform cooling cavity with a suction side passage. The pressure side passage of the first turbine blade platform is in communication with the suction side passage of the second turbine blade platform.

Abstract translation: 本申请提供了一种涡轮叶片冷却系统。 涡轮叶片冷却系统可以包括具有第一涡轮机叶片平台的第一涡轮机叶片，其具有与压力侧通道连通的冷却腔和具有带有吸入侧通道的平台冷却腔的第二涡轮叶片平台的第二涡轮叶片。 第一涡轮叶片平台的压力侧通道与第二涡轮叶片平台的吸入侧通道连通。

公开(公告)号：US20110265490A1

公开(公告)日：2011-11-03

申请号：US13072206

申请日：2011-03-25

Applicant: Kevin Samuel Klasing ,  Robert Proctor ,  Bradley Willis Fintel

Inventor： Kevin Samuel Klasing ,  Robert Proctor ,  Bradley Willis Fintel

IPC: F02C6/04

CPC classification number: F02C9/18 ,  F02K3/06 ,  F05D2240/127 ,  F05D2260/20 ,  F05D2260/60 ,  Y02T50/672 ,  Y02T50/675

Abstract: A vent system is disclosed having a first flow stream flowing over a first surface in a flow path, a conduit that channels a second flow stream and an aero-chimney that is in flow communication with the conduit and located near the first surface wherein the aero-chimney has a body having an aerodynamic shape having a leading edge portion and a trailing edge portion such that the first flow stream flows around the aero-chimney near the first surface.

Abstract translation: 公开了一种排气系统，其具有在流动路径中流过第一表面的第一流动流，引导第二流动的管道和与导管流动连通并位于第一表面附近的空气烟囱，其中航空 烟囱具有具有前缘部分和后缘部分的空气动力学形状的主体，使得第一流动流在靠近第一表面的空气烟囱周围流动。

公开(公告)号：US08015821B2

公开(公告)日：2011-09-13

申请号：US12013085

申请日：2008-01-11

Applicant: Christopher J. Spytek

Inventor： Christopher J. Spytek

IPC: F02C3/00 ,  F02C3/14

CPC classification number: F02C3/14 ,  F02C6/003 ,  F05D2250/25 ,  F05D2260/2212 ,  F05D2260/60 ,  F23M9/08 ,  F23R3/58 ,  Y02T50/676

Abstract: This invention relates to an apparatus for an entrainment system of a vortex burning combustion chamber or a vortex burning inter-turbine burner in a gas turbine. The entrainment system rapidly and thoroughly mixes hot combustion gases with non-combustion gases to reduce the gas temperature before entering a turbine. The entrainment system includes a plurality of helical vanes forming trenches and resulting in a highly helical flow path. The highly helical flow path provides an increased residence time for mixing of the combustion gases and non-combustion gases. Radial cavities in the helical vanes, canted vane angles and varying geometries further facilitate mixing while reducing losses. This invention also includes a method of mixing combustion and non-combustion gases in an entrainment system.

Abstract translation: 本发明涉及一种用于燃气轮机中的涡流燃烧燃烧室或涡流燃烧式涡轮机间燃烧器的夹带系统的装置。 夹带系统快速且彻底地将热燃烧气体与非燃烧气体混合，以在进入涡轮机之前降低气体温度。 夹带系统包括形成沟槽并产生高度螺旋形流动路径的多个螺旋叶片。 高度螺旋流动路径提供了用于混合燃烧气体和非燃烧气体的增加的停留时间。 螺旋叶片中的径向空腔，倾斜叶片角度和变化的几何形状进一步有助于混合，同时减少损失。 本发明还包括在夹带系统中混合燃烧和非燃烧气体的方法。

公开(公告)号：US20100162708A1

公开(公告)日：2010-07-01

申请号：US12345721

申请日：2008-12-30

Applicant: Dean M. Erickson ,  David W. Smith ,  Douglas S. Byrd ,  Hua Zhang ,  Daniel B. Holcombe

Inventor： Dean M. Erickson ,  David W. Smith ,  Douglas S. Byrd ,  Hua Zhang ,  Daniel B. Holcombe

IPC: F02C1/00

CPC classification number: F16K17/046 ,  F02C7/232 ,  F02C9/40 ,  F05D2260/60 ,  F16K15/08 ,  F16K15/18 ,  Y10T137/2564 ,  Y10T137/87652 ,  Y10T137/87676

Abstract: An assembly for delivering a supply of liquid fuel and a supply of purge air to a gas turbine engine, the assembly comprising: an annular dual-flow check valve for controlling the flow through concentric channels that have a common outlet, the annular dual-flow check valve comprising: an outer body and an inner body that define the concentric channels, which include an outer channel and an inner channel formed therein; a spring activated annular poppet that resides in the outer channel and has a range of motion in the axial direction; and an opening through the inner body that connects the outer channel to the inner channel; wherein the axial movement of the annular poppet is regulated by the pressure of the flow upstream of the annular poppet in the outer channel; and the axial range of motion of the annular poppet includes at least two axial positions.

Abstract translation: 一种用于输送液体燃料供应和向燃气涡轮发动机供应吹扫空气的组件，该组件包括：环形双流止回阀，用于控制具有共同出口的同心通道的流动，环形双流 止回阀包括：外体和内体，其限定同心通道，其包括形成在其中的外通道和内通道; 弹簧活动的环形提升阀，其位于外部通道中并具有在轴向方向上的运动范围; 以及通过将所述外部通道连接到所述内部通道的所述内部主体的开口; 其中所述环形提升阀的轴向运动由外部通道中的环形提升阀上游的压力调节; 并且所述环形提升阀的轴向运动范围包括至少两个轴向位置。

公开(公告)号：US20100068066A1

公开(公告)日：2010-03-18

申请号：US12209239

申请日：2008-09-12

Applicant: Ronald Scott Bunker

Inventor： Ronald Scott Bunker

IPC: F01D5/08 ,  F01D5/18 ,  F15C1/06 ,  F15C1/22

CPC classification number: F15D1/00 ,  F01D5/081 ,  F01D5/187 ,  F01D5/20 ,  F05D2260/16 ,  F05D2260/2212 ,  F05D2260/22141 ,  F05D2260/60 ,  F05D2260/963 ,  F05D2270/58 ,  Y02T50/676 ,  Y10T137/2185

Abstract: A device includes a fluid flow channel having a channel inlet for receiving a pressurized fluid for flow through the fluid flow channel and a channel outlet for discharging the pressurized fluid therefrom. A passive flow element is situated within the fluid flow channel or proximate to the channel inlet. The passive flow element includes an element inlet for receiving the pressurized fluid, and an element outlet. The passive flow element also includes a cavity for receiving the pressurized fluid from the element inlet and generating a periodic flow variation of the pressurized fluid so as to modulate the pressurized fluid flow rate through the element outlet.

Abstract translation: 一种装置包括具有通道入口的流体流动通道，该通道入口用于接收用于流过流体流动通道的加压流体和用于从其中排出加压流体的通道出口。 被动流动元件位于流体流动通道内或靠近通道入口。 被动流动元件包括用于接收加压流体的元件入口和元件出口。 被动流动元件还包括用于从元件入口接收加压流体并产生加压流体的周期性流量变化的空腔，以便调节通过元件出口的加压流体流速。

公开(公告)号：US07625126B2

公开(公告)日：2009-12-01

申请号：US12102997

申请日：2008-04-15

Applicant: Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hslanmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

Inventor： Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hslanmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

IPC: F16C33/66

CPC classification number: F01D25/18 ,  F05D2260/60 ,  F05D2260/602 ,  F16C33/6685 ,  F16C2360/23

Abstract: An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

Abstract translation: 油清除系统包括切向扫气勺和与其相邻的沉降区域，其与将油输送到油流路并返回到油底壳的管道分开连通。 屏蔽件安装在沉降区域上以至少部分地屏蔽收集液体油不受界面剪切。 通过屏蔽件定位了多个孔，以允许油流过屏蔽并流入管道。 扫气勺形成将管道分成第一部分和第二部分的隔板。 第一部分处理由切向勺捕获的上游空气/油混合物，而第二部分接收在沉降区域中收集的油。