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    Pneumatic compressor bleed valve
    15.
    发明授权
    Pneumatic compressor bleed valve 有权
    气动压缩机排气阀

    公开(公告)号：US06755025B2

    公开(公告)日：2004-06-29

    申请号：US10200461

    申请日：2002-07-23

    Applicant: Andreas Eleftheriou ,  Vittorio Bruno ,  Ian William Chandler

    Inventor： Andreas Eleftheriou ,  Vittorio Bruno ,  Ian William Chandler

    IPC: F02C918

    CPC classification number: F04D27/0215 ,  F01D17/105 ,  F04D27/023

    Abstract: A pneumatically operated compressor bleed valve communicating between a compressor housing and a bypass duct of a gas turbine engine. The valve has an annular piston slidably mounted within an annular chamber concentric the longitudinal engine axis. An annular valve plug on the piston and an annular valve seat on the compressor housing defining a valve seal interface. A control air pressure conduit communicates between a portion of the annular chamber bounded by the piston and a source of control air pressure. Guide bearings mounted to the periphery of the piston and the housing have a helical guide surface concentric the engine axis.

    Abstract translation: 气动操作的压缩机放气阀，其在压缩机壳体和燃气涡轮发动机的旁路管道之间连通。 阀具有可滑动地安装在与纵向发动机轴线同心的环形室内的环形活塞。 活塞上的环形阀塞和压缩机壳体上的环形阀座，限定阀密封接口。 控制空气压力导管在由活塞限定的环形室的一部分与控制气压源之间连通。 安装到活塞和壳体周边的导向轴承具有与发动机轴线同心的螺旋引导表面。

    Diffuser pipe assembly
    16.
    发明授权
    Diffuser pipe assembly 有权
    扩散管总成

    公开(公告)号：US6123506A

    公开(公告)日：2000-09-26

    申请号：US233023

    申请日：1999-01-20

    Applicant: Joseph Horace Brand ,  Andreas Eleftheriou

    Inventor： Joseph Horace Brand ,  Andreas Eleftheriou

    IPC: F04D29/44

    CPC classification number: F04D29/441

    Abstract: The invention provides a diffuser assembly constructed of internal and external concentrically nested bowl-shaped shells for directing an outward flow of compressed air from a centrifugal compressor impeller to an axially rearward diffused annular flow. The shells can be easily manufactured from nested metal castings thereby eliminating much of the cost and time involved in fabricating prior art diffusers of multiple formed tubes brazed to a separately machined hub. The novel diffuser assembly has two concentrically nested bowl-shaped shells, each shell having an inner peripheral compressor impeller casing about a central opening, and an outer edge. Opposing nested surfaces of the shells have an array of mating grooves separated by abutting seam edges thus defining individual diffuser ducts extending from the compressor impeller casings to the outer shell edges when the shells are secured together.

    Abstract translation: 本发明提供了一种由内部和外部同心嵌套的碗形壳体构成的扩散器组件，用于将离心式压缩机叶轮向外的压缩空气流引导到轴向向后扩散的环形流。 壳可以容易地由嵌套的金属铸件制造，从而消除了制造现有技术的多个成形管钎焊到单独加工的毂的扩散器所花费的大量成本和时间。 新型扩散器组件具有两个同心嵌套的碗形壳，每个壳体具有围绕中心开口的内周边压缩机叶轮壳体和外边缘。 壳体的相对的嵌套表面具有由邻接的接缝边缘分开的配合凹槽的阵列，从而限定当壳体固定在一起时从压缩机叶轮壳体延伸到外壳边缘的各个扩散器管道。

    Rotor assembly
    20.
    发明授权
    Rotor assembly 有权
    转子总成

    公开(公告)号：US09353626B2

    公开(公告)日：2016-05-31

    申请号：US13614584

    申请日：2012-09-13

    Applicant: Andreas Eleftheriou ,  Richard Ivakitch

    Inventor： Andreas Eleftheriou ,  Richard Ivakitch

    IPC: F01D5/02 ,  F02K3/06 ,  F04D29/26 ,  F16D1/09

    CPC classification number: F01D5/025 ,  F02K3/06 ,  F04D29/266 ,  F05D2230/60 ,  F05D2250/292 ,  F05D2260/30 ,  F16D2001/0903 ,  Y10T29/49316

    Abstract: A rotor assembly for a gas turbine engine, with an annular sleeve having an inner member connected around the shaft to rotate together therewith and having an outer member with a first end connected to the inner member, the outer member defining an annular continuous frustoconical inner surface angled such as to extend closer to the central axis near the first end. A rotor disc includes an annular protuberance extending radially inwardly of the outer member and forced toward the first end, and having an annular continuous frustoconical outer surface complementary to the inner surface of the outer member and in torque-transmitting engagement therewith. The assembly includes means for axially pressing the sleeve and the disc against one another to maintain the complementary frustoconical surfaces in torque-transmitting engagement. A method of engaging a rotor disc to a driving shaft in a gas turbine engine is also provided.

    Abstract translation: 一种用于燃气涡轮发动机的转子组件，其具有环形套筒，该内部构件围绕轴连接以与其一起旋转并具有外部构件，第一端连接到内部构件，外部构件限定环形连续的截头圆锥形内表面 成角度的，以便靠近第一端的中心轴线延伸。 转子盘包括沿着外部构件的径向向内延伸并被迫朝向第一端的环形突起，并且具有与外部构件的内表面互补的环形连续的截头圆锥形外表面和与其成扭矩传递接合。 组件包括用于将套筒和盘片彼此轴向按压以保持互补的截头圆锥形表面在扭矩传递接合中的装置。 还提供了一种将转子盘接合到燃气涡轮发动机中的驱动轴的方法。

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