Gas Turbine Energy Storage and Energy Supplementing Systems And Methods of Making and Using the Same
    2.
    发明申请
    Gas Turbine Energy Storage and Energy Supplementing Systems And Methods of Making and Using the Same 审中-公开
    燃气轮机储能和能源补充系统及其使用方法

    公开(公告)号:US20150184593A1

    公开(公告)日:2015-07-02

    申请号:US14357136

    申请日:2013-01-29

    IPC分类号: F02C9/18 F01D25/10

    摘要: The current invention provides several options, depending on specific plant needs, to improve the efficiency and power output of a plant at low loads, reduce the lower limit of power output capability of a gas turbine while at the same time increasing the upper limit of the power output of the gas turbine, thus increasing the capacity and regulation capability Of a new or existing gas turbine system. One aspect of the present invention relates to an energy storage and retrieval system for obtaining useful work from an existing source of a Gas Turbine (GT) power plant while preferably providing an efficient heated air inlet charger.

    摘要翻译: 根据具体的设备需求,本发明提供了若干选项,以提高工厂在低负载下的效率和功率输出,降低了燃气轮机功率输出能力的下限,同时增加了燃气轮机的上限 燃气轮机的功率输出,从而增加新的或现有的燃气轮机系统的容量和调节能力。 本发明的一个方面涉及一种用于从燃气轮机(GT)发电厂的现有源获得有用功的能量储存和取回系统,同时优选地提供有效的加热空气入口充电器。

    Secondary fuel nozzle with readily customizable pilot fuel flow rate
    4.
    发明授权
    Secondary fuel nozzle with readily customizable pilot fuel flow rate 有权
    二次燃料喷嘴具有易于定制的先导燃料流量

    公开(公告)号:US06857271B2

    公开(公告)日:2005-02-22

    申请号:US10320990

    申请日:2002-12-16

    CPC分类号: F23D14/64 F02C7/32 F23R3/286

    摘要: An improved secondary fuel distribution system having a readily adjustable premix pilot nozzle for use in a gas turbine combustor is disclosed. The secondary fuel nozzle assembly has a premix fuel nozzle comprising an annular tubular manifold and a premix pilot nozzle. Multiple embodiments of premix pilot nozzles are disclosed that have a fuel flow rate that can be controlled and adjusted as required, including a plate and feed hole combination, a pressfit premix pilot nozzle, and a premix pilot nozzle that is threaded into the secondary fuel nozzle assembly.

    摘要翻译: 公开了一种改进的二次燃料分配系统,其具有用于燃气轮机燃烧器中的易于调节的预混合引燃喷嘴。 二次燃料喷嘴组件具有包括环形管状歧管和预混合引燃喷嘴的预混合燃料喷嘴。 公开了预混合引燃喷嘴的多个实施例,其具有可根据需要进行控制和调节的燃料流量,包括板和进料孔组合,加压预混合引燃喷嘴和螺旋进入次燃料喷嘴的预混合引燃喷嘴 部件。

    Insulated cooling passageway for cooling a shroud of a turbine blade

    公开(公告)号:US06811378B2

    公开(公告)日:2004-11-02

    申请号:US10209392

    申请日:2002-07-31

    申请人: Robert J. Kraft

    发明人: Robert J. Kraft

    IPC分类号: F01D522

    摘要: A turbine blade is disclosed having a tip shroud that includes internal passages through which cooling air is flowed to minimize creep. The cooling air is provided to the shroud through dedicated cooling passageways which include tube inserts that restrict the transfer of heat from the airfoil portion of the turbine blade to the cooling air within the tube as the cooling air passes through the airfoil portion.

    Pool deck drain and safety fence support structure
    6.
    发明授权
    Pool deck drain and safety fence support structure 失效
    泳池甲板排水和安全围栏支撑结构

    公开(公告)号:US06810631B2

    公开(公告)日:2004-11-02

    申请号:US10302200

    申请日:2002-11-22

    申请人: Robert J. Kraft

    发明人: Robert J. Kraft

    IPC分类号: F02B500

    CPC分类号: E04H4/06 E04F17/00

    摘要: A novel pool deck structure channel located beneath a swimming pool deck surface is disclosed that incorporates both a drainage device and a pool safety fence support structure. The unique channel design eliminate the need to have separate support holes drilled in a pool deck surface that can be a safety hazard when not in use, cause functional problems due to dirt and debris, and are not otherwise aesthetically pleasing. The unique channel design includes an elongated trough extending beneath the pool deck surface for supporting a drainage device, a plurality of holes in the trough, and a plurality of inserts within the holes that extend into the trough in order to support pool safety fence support posts.

    摘要翻译: 公开了一种位于游泳池甲板表面下方的新颖的游泳池甲板结构通道,其包括排水装置和游泳池安全栅栏支撑结构。 独特的通道设计消除了在游泳池甲板表面上钻出单独的支撑孔的需要,在不使用时可能会导致安全隐患,导致由于污垢和碎屑引起的功能问题,并且在其他方​​面不美观。 唯一的通道设计包括在池甲板表面下方延伸的细长槽,用于支撑排水装置,槽中的多个孔以及在孔内的多个插入物,其延伸到槽中以便支撑游泳池安全栅栏支撑柱 。

    Three degrees of freedom aft mounting system for gas turbine transition duct
    7.
    发明授权
    Three degrees of freedom aft mounting system for gas turbine transition duct 有权
    用于燃气轮机过渡管的三自由度后部安装系统

    公开(公告)号:US06442946B1

    公开(公告)日:2002-09-03

    申请号:US09712735

    申请日:2000-11-14

    IPC分类号: F02C720

    摘要: A multiple directional axes structural support system for use as the aft end mount for a gas turbine transition duct to a turbine inlet is disclosed. The mounting system is configured to withstand high temperature gradients and mechanical loads associated with gas turbine environments while allowing multiple axes adjustment and interface capability between the transition duct and the turbine inlet casing. A spherical ball joint allows for rotation about multiple (three) axes to compensate for relative thermal growth, manufacturing tolerances, and assembly tolerances between mating surfaces. The ball joint is held in place by fitted spacers, bosses, and a through-bolt, that when torqued will dampen out unwanted vibrations in the multi-axis mounting system.

    摘要翻译: 公开了用作用于到涡轮机入口的燃气轮机过渡管道的后端安装件的多方向轴结构支撑系统。 安装系统被配置为承受与燃气轮机环境相关的高温梯度和机械负载,同时允许过渡管道和涡轮机入口套管之间的多个轴线调整和接口能力。 球形球形接头允许围绕多(3)个轴线旋转,以补偿配合表面之间的相对热增长,制造公差和组装公差。 球形接头通过安装的垫片,凸台和贯穿螺栓固定在适当的位置,当扭转时会抑制多轴安装系统中的不必要的振动。

    Airfoil vibration damping device
    8.
    发明授权
    Airfoil vibration damping device 失效
    翼型减振装置

    公开(公告)号:US5820343A

    公开(公告)日:1998-10-13

    申请号:US509259

    申请日:1995-07-31

    IPC分类号: F01D5/16 F01D5/18 F01D5/26

    CPC分类号: F01D5/26 F01D5/16 Y10S416/50

    摘要: A rotor blade for a rotor assembly is provided which includes a root, an airfoil, a platform, and a damper. The airfoil includes at least one cavity. The platform extends laterally outward from the blade between the root and the airfoil, and includes an airfoil side, a root side, and an aperture extending between the root side of the platform and the cavity within the airfoil. The damper, which includes at least one bearing surface, is received within the aperture and the cavity. The bearing surface is in contact with a surface within the cavity and friction between the bearing surface and the surface within the cavity damps vibration of the blade.

    摘要翻译: 提供了一种用于转子组件的转子叶片,其包括根部,翼型件,平台和阻尼器。 翼型件包括至少一个空腔。 平台在叶片和叶片之间从叶片横向向外延伸,并且包括翼型件侧面,根部侧面和在平台的根侧和翼型之间延伸的孔。 包括至少一个支承表面的阻尼器被容纳在孔和腔内。 轴承表面与空腔内的表面接触,并且轴承表面与空腔内的表面之间的摩擦阻碍了叶片的振动。

    Airfoil vibration damping device
    9.
    发明授权
    Airfoil vibration damping device 失效
    翼型减振装置

    公开(公告)号:US5558497A

    公开(公告)日:1996-09-24

    申请号:US509276

    申请日:1995-07-31

    IPC分类号: F01D5/26

    CPC分类号: F01D5/26 Y10S416/50

    摘要: A rotor blade for a rotor assembly is provided comprising a root, an airfoil, and a damper. The airfoil includes a base, a tip, a first cavity, a second cavity, and a passage. The passage includes a pair of walls converging from the first cavity to the second cavity, thereby connecting the first and second cavities. The damper is received within the passage. According to one aspect of the present invention, a difference in gas pressure across the damper biases the damper against the converging walls of the passage. According to another aspect of the present invention, centrifugal force biases the damper against the converging walls of the passage.

    摘要翻译: 提供了一种用于转子组件的转子叶片,其包括根部,翼型件和阻尼器。 翼型件包括基座,尖端,第一腔,第二腔和通道。 通道包括从第一腔体到第二腔室会聚的一对壁,由此连接第一和第二腔体。 阻尼器被接收在通道内。 根据本发明的一个方面,横跨阻尼器的气体压力差使阻尼器抵靠通道的会聚壁偏压。 根据本发明的另一方面,离心力将阻尼器抵靠通道的会聚壁偏压。

    High Output Modular CAES (HOMC)
    10.
    发明申请
    High Output Modular CAES (HOMC) 有权
    高输出模块化CAES(HOMC)

    公开(公告)号:US20140208730A1

    公开(公告)日:2014-07-31

    申请号:US14237200

    申请日:2012-08-13

    申请人: Robert J Kraft

    发明人: Robert J Kraft

    IPC分类号: F15B1/02

    摘要: A compressed air energy storage system integrated with a source of secondary heat, such as a simple cycle gas turbine, to increase power production and to provide power regulation through the use of stored compressed air heated by said secondary heat to provide power augmentation.

    摘要翻译: 与二次热源(例如简单循环燃气轮机)集成的压缩空气能量存储系统,以增加功率产生,并且通过使用由所述次级热量加热的存储的压缩空气提供功率调节以提供功率增加。