知搜-全球专利检索

  1. Login
  2. Sign Up

Search Results

20 records (took 0.014 seconds)

    Rotor with relief features and one-sided load slots
    1.
    发明授权
    Rotor with relief features and one-sided load slots 有权

    公开(公告)号：US10704401B2

    公开(公告)日：2020-07-07

    申请号：US16100615

    申请日：2018-08-10

    Applicant: United Technologies Corporation

    Inventor： Nicholas Aiello ,  James Cosby

    IPC: F01D5/32 ,  F01D5/30

    Abstract: An exemplary turbomachine rotor assembly includes a pair of spaced rails that extend around a cylindrical surface to define a rotor hub. The rails define a space for receiving blades. Load slots are formed in one of the rails. A relief feature is formed in an opposite surface of an opposing rail. The load slots and relief feature utilized to move at least one of the blades into the space.

    Rotor With Blades Secured by Woven Fiber Attachment System
    2.
    发明申请
    Rotor With Blades Secured by Woven Fiber Attachment System 审中-公开
    带有叶片的转子由机织纤维附着系统固定

    公开(公告)号：US20160146023A1

    公开(公告)日：2016-05-26

    申请号：US14933129

    申请日：2015-11-05

    Applicant: United Technologies Corporation

    Inventor： Anthony R. Bifulco ,  Damon K. Brown ,  Nicholas Aiello

    IPC: F01D5/30 ,  F01D5/14

    CPC classification number: B23P15/006 ,  F01D5/282 ,  F01D5/34 ,  F05D2300/6033

    Abstract: A propulsive engine rotor configured for operation within a gas turbine includes a plurality of spaced airfoil blades circumferentially affixed to an outer hoop-style rim. At least two of the airfoil blades have an integral root configured to extend either through or at least radially inwardly from the rim. A woven fiber system provides that the blade roots are interdigitally wrapped by a plurality of woven fibers before impregnation and/or encapsulation of the fibers and wrapped roots within a ceramic or other composite matrix material to form a composite ring. The composite ring defines the interior body of the rotor, includes a bore through which passes the rotational axis of the rotor, and has a lower mass than the rotor rim. The woven fiber interface between the roots increases the tensile load capacity of the airfoil blades relative to the composite ring, and increases the self-sustaining radius of the rotor.

    Abstract translation: 构造成用于在燃气涡轮机内操作的推进式发动机转子包括多个间隔开的叶片叶片，周向地固定在外箍型轮缘上。 至少两个翼型叶片具有构造成从轮缘延伸穿过或至少径向向内延伸的整体根部。 编织纤维系统规定，在将纤维和包裹的根部浸入陶瓷或其它复合基质材料中以形成复合环之前，叶片根部被多个编织纤维叉指地包裹。 复合环限定转子的内部主体，包括通过转子的旋转轴线并且具有比转子轮辋更低的质量的孔。 根部之间的机织纤维界面增加了翼型相对于复合环的拉伸载荷能力，并提高了转子的自维持半径。

    GAS TURBINE ENGINE ROTOR SEAL
    4.
    发明申请
    GAS TURBINE ENGINE ROTOR SEAL 审中-公开
    气体涡轮发动机转子密封

    公开(公告)号：US20140127007A1

    公开(公告)日：2014-05-08

    申请号：US13671205

    申请日：2012-11-07

    Applicant: United Technologies Corporation

    Inventor： Nicholas Aiello ,  Carney R. Anderson

    IPC: F01D11/00

    CPC classification number: F01D11/001

    Abstract: A rotary seal for sealing a bladed rotor of a gas turbine engine to a stator thereof comprises a sealing element and a sealing element support comprising a radially outer edge portion on which the sealing element is fixed, a radially inner mounting portion adapted to be attached to a supported rotor hub, and a flexible, medial web portion extending between the radially outer edge portion and the radially inner mounting portion.

    Abstract translation: 用于将燃气涡轮发动机的叶片转子密封到其定子的旋转密封件包括密封元件和密封元件支撑件，所述密封元件和密封元件支撑件包括固定密封元件的径向外边缘部分，适于附接到 支撑的转子轮毂和在径向外边缘部分和径向内部安装部分之间延伸的柔性内侧腹板部分。

    TURBOMACHINE ROTOR GROOVE
    5.
    发明申请
    TURBOMACHINE ROTOR GROOVE 有权
    涡轮转子槽

    公开(公告)号：US20140086742A1

    公开(公告)日：2014-03-27

    申请号：US13627036

    申请日：2012-09-26

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Nicholas Aiello ,  Raji Mali

    IPC: F01D5/30 ,  B21D53/78

    CPC classification number: F01D5/3038 ,  Y10T29/49332

    Abstract: An example turbomachine rotor provides a groove that is annular and is configured to receive a root of an airfoil, the groove having a radial cross-sectional area. A ratio of the radial cross-sectional area of the groove to a radial cross-sectional area of the root received within the annular groove is from 2 to 5.

    Abstract translation: 涡轮机转子的一个实例提供了一个环形槽，并被构造为容纳翼型的根部，该槽具有径向横截面积。 槽的径向横截面积与在环形槽内容纳的根部的径向横截面积的比为2〜5。

    Rotor with blades secured by woven fiber attachment system
    6.
    发明授权
    Rotor with blades secured by woven fiber attachment system 有权

    公开(公告)号：US10029336B2

    公开(公告)日：2018-07-24

    申请号：US14933129

    申请日：2015-11-05

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Anthony R. Bifulco ,  Damon K. Brown ,  Nicholas Aiello

    IPC: B23P15/00 ,  F01D5/34 ,  F01D5/28

    Abstract: A propulsive engine rotor configured for operation within a gas turbine includes a plurality of spaced airfoil blades circumferentially affixed to an outer hoop-style rim. At least two of the airfoil blades have an integral root configured to extend either through or at least radially inwardly from the rim. A woven fiber system provides that the blade roots are interdigitally wrapped by a plurality of woven fibers before impregnation and/or encapsulation of the fibers and wrapped roots within a ceramic or other composite matrix material to form a composite ring. The composite ring defines the interior body of the rotor, includes a bore through which passes the rotational axis of the rotor, and has a lower mass than the rotor rim. The woven fiber interface between the roots increases the tensile load capacity of the airfoil blades relative to the composite ring, and increases the self-sustaining radius of the rotor.

    Reinforced Gas Turbine Engine Rotor Disk
    7.
    发明申请
    Reinforced Gas Turbine Engine Rotor Disk 审中-公开
    增强燃气轮机发动机转盘

    公开(公告)号：US20160138399A1

    公开(公告)日：2016-05-19

    申请号：US14929771

    申请日：2015-11-02

    Applicant: United Technologies Corporation

    Inventor： Anthony R. Bifulco ,  Damon K. Brown ,  Nicholas Aiello

    IPC: F01D5/02 ,  F01D5/34 ,  F02C3/04

    CPC classification number: F01D5/02 ,  F01D5/06 ,  F01D5/34 ,  F02C3/04 ,  F05D2220/32 ,  F05D2230/31 ,  F05D2230/60 ,  F05D2240/20 ,  F05D2240/35 ,  F05D2300/224 ,  F05D2300/48 ,  F05D2300/603 ,  F05D2300/6032 ,  F05D2300/614 ,  Y02T50/672

    Abstract: A structurally-reinforced rotor disk for a gas turbine engine is disclosed. The rotor disk may comprise a body including a rim configured to support airfoils (which may be separate or integral with the airfoils), an axially-extending bore disposed radially inward of the rim, and a radially-extending web connecting the rim and the bore. The bore may include an axial outer edge and at least one circumferentially-extending annular recess formed axially between the outer edge and the web. The rotor disk may further comprise an annular ring retained in the annular recess, and the annular ring may be formed from a different material than the body of the rotor disk so as to increase a self-sustaining radius of the rotor disk.

    Abstract translation: 公开了一种用于燃气涡轮发动机的结构增强转子盘。 转子盘可以包括主体，其包括构造成支撑翼型件（其可以与翼型件分离或一体的）的边缘，设置在轮辋径向内侧的轴向延伸的孔以及连接轮辋和钻孔的径向延伸的腹板 。 孔可以包括轴向外边缘和在外边缘和腹板之间轴向形成的至少一个周向延伸的环形凹部。 转子盘还可以包括保持在环形凹部中的环形圈，并且环形圈可以由与转子盘的主体不同的材料形成，以便增加转子盘的自维持半径。

    Fiber reinforced spacer for a gas turbine engine
    10.
    发明授权
    Fiber reinforced spacer for a gas turbine engine 有权

    公开(公告)号：US10648481B2

    公开(公告)日：2020-05-12

    申请号：US14929701

    申请日：2015-11-02

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Anthony R. Bifulco ,  Damon K. Brown ,  Nicholas Aiello

    IPC: F02C1/00 ,  F04D29/32 ,  F01D5/02 ,  F01D25/28 ,  F02C3/06

    Abstract: A spacer of a gas turbine engine is reinforced with a fiber. The fiber can be cured with a substrate to form a fiber reinforced composite material. As a gas turbine engine operates, the rotation creates forces which can deform, expand, contract or translate certain gas turbine engine components, including spacers. These forces can adversely affect gas turbine engine performance and reliability, particularly when they are either unpredictable or difficult to control. Reinforcing a spacer with a fiber may allow a lower system weight, more compact or configurable internal packaging or a high degree of reinforcement.

Patent Agency Ranking