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    SEGMENTED SEAL WITH SHIP LAP ENDS
    1.
    发明申请
    SEGMENTED SEAL WITH SHIP LAP ENDS 审中-公开
    SEGMENTED密封与船尾拉链

    公开(公告)号：WO2013180899A1

    公开(公告)日：2013-12-05

    申请号：PCT/US2013/039643

    申请日：2013-05-06

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： AIELLO, Nicholas ,  LEE, Conor

    IPC: F02C7/28 ,  F01D5/20 ,  F02C7/00 ,  F01D5/00

    CPC classification number: F01D11/001 ,  F01D11/005 ,  F04D29/083 ,  F04D29/164 ,  Y10T29/49321

    Abstract: A segment for a knife edge seal includes an arcuate segment with a first end with a first end surface and a second end with a second end surface. The first end surface and the second end surface are complementary and overlapping when the first end surface and the second end surface interface with ends of adjacent segments.

    Abstract translation: 用于刀刃密封件的段包括弓形段，其具有带有第一端面的第一端和具有第二端面的第二端。 当第一端面和第二端面与相邻段的端部相接触时，第一端面和第二端表面是互补和重叠的。

    FLOATING SEGMENTED SEAL
    2.
    发明申请
    FLOATING SEGMENTED SEAL 审中-公开

    公开(公告)号：WO2014025439A3

    公开(公告)日：2014-02-13

    申请号：PCT/US2013/041496

    申请日：2013-05-17

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： AIELLO, Nicholas ,  LEE, Conor

    IPC: F02C7/28 ,  F01D11/00

    Abstract: A gas turbine engine rotor section includes a rotor body with a ledge extending axially from a location on the rotor body. The ledge defines a radially inner surface radially inwardly of the ledge, and a hub extends axially from the rotor, and beyond the ledge. The hub has a radially outer surface spaced from the ledge radially inner surface. A first distance is defined between the radially inner surface of the ledge and the radially outer surface of the hub. A knife edge seal has at least one pointed knife seal portion at a radially outer end. A radially inwardly extending arm portion extends from the seal, and an axially inwardly extending portion extends axially inwardly from the radially inwardly extending portion. The axially inwardly extending portion has a radially outer face and a radially inner face, which are spaced by a second distance. The second distance is less than the first distance. The axially inwardly extending portion is received between the radially inner face of the rotor and the radially outer face of the hub, such that the knife edge seal is free floating between the ledge and the hub.

    FLOATING SEGMENTED SEAL
    6.
    发明公开
    FLOATING SEGMENTED SEAL 有权
    浮动分段式密封件

    公开(公告)号：EP2855890A2

    公开(公告)日：2015-04-08

    申请号：EP13828300.7

    申请日：2013-05-17

    Applicant: United Technologies Corporation

    Inventor： AIELLO, Nicholas ,  LEE, Conor

    IPC: F02C7/28 ,  F01D11/00

    CPC classification number: F01D11/02 ,  F01D11/001

    Abstract: A gas turbine engine rotor section includes a rotor body with a ledge extending axially from a location on the rotor body. The ledge defines a radially inner surface radially inwardly of the ledge, and a hub extends axially from the rotor, and beyond the ledge. The hub has a radially outer surface spaced from the ledge radially inner surface. A first distance is defined between the radially inner surface of the ledge and the radially outer surface of the hub. A knife edge seal has at least one pointed knife seal portion at a radially outer end. A radially inwardly extending arm portion extends from the seal, and an axially inwardly extending portion extends axially inwardly from the radially inwardly extending portion. The axially inwardly extending portion has a radially outer face and a radially inner face, which are spaced by a second distance. The second distance is less than the first distance. The axially inwardly extending portion is received between the radially inner face of the rotor and the radially outer face of the hub, such that the knife edge seal is free floating between the ledge and the hub.

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