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    FLOATING, NON-CONTACT SEAL WITH AT LEAST THREE BEAMS
    31.
    发明公开
    FLOATING, NON-CONTACT SEAL WITH AT LEAST THREE BEAMS 审中-公开
    浮动，非接触式密封，至少有三个横梁

    公开(公告)号：EP3290755A1

    公开(公告)日：2018-03-07

    申请号：EP17178170.1

    申请日：2017-06-27

    Applicant: United Technologies Corporation

    Inventor： PAULINO, Jose R. ,  CHUONG, Conway ,  WONG, Joey ,  PETERS, Christopher J. ,  WILSON, Ross

    IPC: F16J15/44 ,  F01D11/02

    CPC classification number: F01D11/025 ,  F01D5/02 ,  F01D25/24 ,  F04D29/053 ,  F04D29/083 ,  F04D29/321 ,  F04D29/522 ,  F05D2220/32 ,  F05D2240/60 ,  F05D2260/38 ,  F16J15/442 ,  F16J15/445

    Abstract: A floating, non-contact seal (318) comprises: a shoe (336), and at least three beams (330a,b,c), each beam (330a,b,c) having a first axial end (340a,b,c) and a second axial end (346a,b,c), where the first axial ends (340a,b,c) are coupled to the shoe (336) and the second axial ends (346a,b,c) are coupled to a ring structure (288). An engine comprises: a first structure, a second structure configured to rotate relative to the first structure, and the floating, non-contact seal (318), where the seal (318) interfaces the first structure and the second structure.

    Abstract translation: 浮动非接触密封件（318）包括：鞋（336）和至少三个梁（330a，b，c），每个梁（330a，b，c）具有第一轴向端部（340a，b， c）和第二轴向端部（346a，b，c），其中第一轴向端部（340a，b，c）联接到滑靴（336）并且第二轴向端部（346a，b，c）联接到 环结构（288）。 发动机包括：第一结构，构造成相对于第一结构旋转的第二结构以及浮动非接触式密封件（318），其中密封件（318）与第一结构和第二结构接合。

    RETAINING ASSEMBLY WITH TABS AND RETAINING RING
    32.
    发明公开
    RETAINING ASSEMBLY WITH TABS AND RETAINING RING 审中-公开
    用挡板和挡圈固定组件

    公开(公告)号：EP3290640A1

    公开(公告)日：2018-03-07

    申请号：EP17188824.1

    申请日：2017-08-31

    Applicant: United Technologies Corporation

    Inventor： CHUONG, Conway ,  WILSON, Ross

    IPC: F01D5/30 ,  F01D5/34 ,  F01D9/04

    CPC classification number: F01D5/30 ,  F01D5/3007 ,  F01D5/3015 ,  F01D5/34 ,  F01D9/042 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/30 ,  F05D2260/30

    Abstract: A component retaining assembly (65) includes a housing (62) including a circumferential slot (76). A component (64) is mated to the housing (62). The component (64) includes a first face (86) including at least two tabs (78). The at least two tabs (78) extending at outward from the first face (86) at least partially past a portion of the circumferential slot (76). A retaining ring (66) is disposed within the circumferential slot (76) and abuts the first face (86) of the component (64). The at least two tabs (78) overlap a portion of the retaining ring (66). A gas turbine engine (20) and a method are also disclosed.

    Abstract translation: 部件保持组件（65）包括具有周向槽（76）的壳体（62）。 部件（64）与壳体（62）配合。 部件（64）包括具有至少两个突片（78）的第一面（86）。 从第一面（86）向外延伸的至少两个突出部（78）至少部分地越过周向槽（76）的一部分。 保持环（66）设置在周向槽（76）内并邻接部件（64）的第一面（86）。 该至少两个突出部（78）与保持环（66）的一部分重叠。 燃气涡轮发动机（20）和方法也被公开。

    FLOATING, NON-CONTACT SEAL WITH OFFSET BUILDING CLEARANCE FOR LOAD IMBALANCE
    33.
    发明公开
    FLOATING, NON-CONTACT SEAL WITH OFFSET BUILDING CLEARANCE FOR LOAD IMBALANCE 审中-公开
    浮动非接触式密封，带有偏置建筑间隙，用于加载不平衡

    公开(公告)号：EP3287674A1

    公开(公告)日：2018-02-28

    申请号：EP17176490.5

    申请日：2017-06-16

    Applicant: United Technologies Corporation

    Inventor： WILSON, Ross ,  CHUONG, Conway ,  MECKLENBURG, Dwayne K.

    IPC: F16J15/44 ,  F01D11/02

    CPC classification number: F01D11/025 ,  F01D5/02 ,  F01D25/24 ,  F04D29/083 ,  F04D29/102 ,  F04D29/321 ,  F04D29/522 ,  F05D2220/32 ,  F05D2240/60 ,  F16J15/442 ,  F16J15/445

    Abstract: Aspects of the disclosure are directed to an engine (10) comprising: a first structure (206), a second structure (212) configured to rotate relative to the first structure (206), and a floating, non-contact seal (218) that interfaces the first structure (206) and the second structure (212), where the seal (218) includes: a shoe (236), a first beam (230a) coupled to the shoe (236), and a second beam (230b) coupled to the shoe (236), where during a non-operational state of the engine (10) a reference point (398) of the shoe (236) is substantially centered within a range of radial deflections (394a, 396a) of the reference point (398) of the shoe (236) over the operating range of the engine (10).

    Abstract translation: 本发明的方面涉及一种发动机（10），其包括：第一结构（206），被构造成相对于第一结构（206）旋转的第二结构（212）以及浮动的非接触式密封件（218） ，所述第一结构（206）和所述第二结构（212）接合，其中所述密封件（218）包括：鞋（236），联接到所述鞋（236）的第一梁（230a）和第二梁 ），其中在发动机（10）的非操作状态期间，鞋（236）的参考点（398）基本上对中于所述鞋（236）的径向偏转范围（394a，396a） 鞋（236）的参考点（398）超过发动机（10）的操作范围。

    REDUCED MISALIGNMENT GEAR SYSTEM
    34.
    发明公开
    REDUCED MISALIGNMENT GEAR SYSTEM 审中-公开
    具有减少平行不对传输系统

    公开(公告)号：EP3036411A1

    公开(公告)日：2016-06-29

    申请号：EP14838303.7

    申请日：2014-08-13

    Applicant: United Technologies Corporation

    Inventor： BUDNICK, Matthew ,  CHUONG, Conway

    IPC: F01D25/18

    CPC classification number: F01D25/18 ,  F01D25/16 ,  F02C7/06 ,  F02C7/36 ,  F05D2260/40311 ,  F16H1/28 ,  F16H57/043 ,  F16H57/0471 ,  F16H57/0479 ,  F16H57/0486 ,  Y02T50/671

    Abstract: A lubrication system for a fan drive planetary gear system according to an exemplary aspect of the present disclosure includes, among other things, a stationary first bearing configured to receive a lubricant from a lubricant input, the stationary first bearing is located adjacent a fan drive shaft. A second bearing is configured to rotate with the fan drive shaft, the first bearing engages the second bearing and is configured to transfer the lubricant from the first bearing to the second bearing and into at least one fluid passage in the fan drive shaft. A conduit fluidly connects the at least one passage in the fan drive shaft with at least one component on the fan drive gear system.

    BEARING-SUPPORTED SEAL
    38.
    发明公开
    BEARING-SUPPORTED SEAL 审中-公开

    公开(公告)号：EP3514413A1

    公开(公告)日：2019-07-24

    申请号：EP19152101.2

    申请日：2019-01-16

    Applicant: United Technologies Corporation

    Inventor： DIFRANCESCO, Michael L. ,  CHUONG, Conway

    IPC: F16J15/3216 ,  F16J15/44 ,  F01D11/00 ,  F01D11/02 ,  F16C33/72

    Abstract: A seal (200) according to the present disclosure includes a plate, and a floating shoe (200B) supported with respect to the plate (208) in a first direction. The floating shoe (200B) has a sealing feature (200C) extending in a second direction perpendicular to the first direction. At least one bearing (209) is between the plate (208) and the floating shoe (200B). The bearing (209)is configured to facilitate movement of the floating shoe (200B) with respect to the plate (208) in the second direction.
    A gas turbine engine including the seal and a method of sealing a rotating component with respect to a stationary component are also disclosed.

    DUAL HYDROSTATIC SEAL ASSEMBLY
    39.
    发明公开
    DUAL HYDROSTATIC SEAL ASSEMBLY 审中-公开

    公开(公告)号：EP3462062A1

    公开(公告)日：2019-04-03

    申请号：EP18185831.7

    申请日：2018-07-26

    Applicant: United Technologies Corporation

    Inventor： DiFRANCESCO, Michael L. ,  CHUONG, Conway

    IPC: F16J15/44 ,  F01D11/02 ,  F01D25/22

    Abstract: A seal assembly (10) includes first and second rings (16A,16B). The first ring (16A) includes a first outer ring (18A), a first beam (28A) connected to the first outer ring (18A), and a first shoe (22A). The first shoe (22A) includes free and fixed ends (24A,26A) and is configured to move radially. The second seal ring (16B) is disposed axially adjacent and is attached to the first seal ring (16A). The second seal ring (16B) includes a second outer ring (18B), a second beam (28B) connected to the second outer ring (18B), and a second shoe (22B). The second shoe (22B) includes free and fixed ends (24B,26B) and is configured to move in a generally radial direction. The free end (24B) of the second shoe (22B) is disposed axially adjacent to the fixed end (26A) of the first shoe (22A). The fixed end (26B) of the second shoe (22B) is disposed axially adjacent to the free end (24A) of the first shoe (22A).

    HYDROSTATIC NON-CONTACT SEAL WITH SEAL CARRIER ELIMINATION
    40.
    发明公开
    HYDROSTATIC NON-CONTACT SEAL WITH SEAL CARRIER ELIMINATION 审中-公开

    公开(公告)号：EP3428489A1

    公开(公告)日：2019-01-16

    申请号：EP18172174.7

    申请日：2018-05-14

    Applicant: United Technologies Corporation

    Inventor： CHUONG, Conway ,  D'AMBRUOSO, Tara ,  WONG, Joey

    IPC: F16J15/44 ,  F01D11/02

    Abstract: Aspects of the disclosure are directed to a non-contact seal assembly comprising a plurality of seal shoes (54) arranged about a centerline (22) in an annular array, the seal shoes (54) including a first seal shoe (54) extending axially along the centerline (22) between a first shoe end (70) and a second shoe end (72). The non-contact seal assembly may comprise a seal base (52) circumscribing the annular array of the seal shoes (54), the seal base (52) comprising first, second and third inner radial seal base surfaces (33, 35, 37) where the third inner radial seal base surface (37) is axially between the first and second inner radial seal base surfaces (33, 36) and is radially proximate the centerline (22) with respect to the radially distal first and second inner radial seal base surfaces (33, 35). The non-contact seal assembly may further comprise a plurality of spring elements (56), each of the spring elements (56) radially distal from and connecting to a respective one of the seal shoes (54) and radially proximate the third inner radial seal base surface (37).

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