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    Ring seal arrangement
    11.
    发明授权
    Ring seal arrangement 有权

    公开(公告)号：US10392953B2

    公开(公告)日：2019-08-27

    申请号：US15623835

    申请日：2017-06-15

    Applicant: United Technologies Corporation

    Inventor： Jonathan Logan Miller ,  Colin D. Craig

    IPC: F01D11/00 ,  F16J15/16 ,  F16J15/44 ,  F01D25/16

    Abstract: A ring seal assembly includes a first ring seal that is symmetrical with respect to a radially extending plane. A second ring seal is separated axially from the first ring seal by a spring. The second ring seal includes a first inner circumferential surface. An interference feature extends radially inward from the first inner circumferential surface to a second inner circumferential surface.

    RADIAL COVERAGE PISTON RING GROOVE ARRANGEMENT
    12.
    发明申请
    RADIAL COVERAGE PISTON RING GROOVE ARRANGEMENT 有权
    径向覆盖活塞环格栅布置

    公开(公告)号：US20160208923A1

    公开(公告)日：2016-07-21

    申请号：US14600858

    申请日：2015-01-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Jonathan Logan Miller

    IPC: F16J15/32 ,  F01D11/00

    CPC classification number: F16J15/3208 ,  F01D11/003 ,  F16J15/3252 ,  F16J15/3268 ,  F16J15/441

    Abstract: A main shaft bearing compartment seal system is described herein. The modified ring groove geometry creates two distinct cavities or steps for a piston ring and a wave spring. This concept provides a separate groove cavity for the spring independent of the fool-proofing and clearance cavity. This modified ring groove geometry increases first face coverage and reduces exposure risk for eccentricity of wave spring to piston ring, to avoid potential disengagement and improve function and performance of the seal assembly and engine.

    Abstract translation: 这里描述了主轴承舱室密封系统。 改进的环槽几何为活塞环和波形弹簧形成两个不同的腔或台阶。 这个概念为弹簧提供了独立的凹槽，独立于傻瓜和间隙空腔。 这种改进的环槽几何增加了第一面覆盖并且降低了波形弹簧对活塞环偏心的暴露风险，以避免潜在的分离并改善密封组件和发动机的功能和性能。

    Slotted Distribution Sleeve for a Seal Plate
    14.
    发明申请
    Slotted Distribution Sleeve for a Seal Plate 有权
    用于密封板的开槽分配套管

    公开(公告)号：US20150152746A1

    公开(公告)日：2015-06-04

    申请号：US14459988

    申请日：2014-08-14

    Applicant: United Technologies Corporation

    Inventor： Alexander J. Maret ,  James B. Coffin ,  Jonathan Logan Miller

    IPC: F01D25/18 ,  F16J15/16

    CPC classification number: F01D25/186 ,  F01D25/183 ,  F05D2260/98 ,  F16C33/6677 ,  F16J15/162 ,  F16J15/324

    Abstract: A seal assembly for a gas turbine engine, may be manufactured in two pieces, the first piece is a seal plate with a cavity around its inner wall and the second piece is a sleeve that mounts in the cavity of the seal plate. The sleeve may have oil distribution channels that deliver oil to subsequent components and apertures that deliver oil to the seal plate. The volume of oil delivered to the seal plate can be set by the number of apertures and related radial holes in the sleeve. Because the sleeve delivers oil through the apertures and radial holes to an annulus in the cavity of the seal plate, cooling bores in the seal plate need only be drilled into the annulus and the number of cooling bores can be independent of the number of radial holes in the sleeve.

    Abstract translation: 用于燃气涡轮发动机的密封组件可以制造成两片，第一件是围绕其内壁的空腔的密封板，第二件是安装在密封板的空腔中的套筒。 套筒可以具有将油输送到向密封板输送油的后续部件和孔的油分配通道。 输送到密封板的油的体积可以通过套筒中的孔的数量和相关的径向孔来设定。 因为套管将油通过孔和径向孔传递到密封板的空腔中的环形空间，所以密封板中的冷却孔仅需要钻入环形空间中，并且冷却孔的数量可以与径向孔的数量无关 在袖子里。

    RADIAL SEAL ARRANGEMENT WITH AXIALLY ELONGATED OIL COOLED RUNNER
    15.
    发明申请
    RADIAL SEAL ARRANGEMENT WITH AXIALLY ELONGATED OIL COOLED RUNNER 有权

    公开(公告)号：US20210054755A1

    公开(公告)日：2021-02-25

    申请号：US16546436

    申请日：2019-08-21

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Jonathan Logan Miller ,  M Rifat Ullah

    IPC: F01D11/00 ,  F02C7/28

    Abstract: A seal includes a seal runner, at least one seal ring, and a seal housing. The runner extends in an axial direction to a runner end face that faces a bearing. The ring is fixed to a static structure and has an inner surface engaging the seal runner and a first face that faces the bearing. The seal housing is fixed to the static structure and includes a first portion extending in an axial direction from the first face of the seal ring to a housing face that faces the bearing. The first portion has a first length extending from the first face of the seal ring to the housing face. The seal runner has a first runner portion with a second length that extends from the first face of the seal ring to the runner end face. The second length is at least 35% longer than the first length.

    BEARING COMPARTMENT SEAL CONFIGURATION FOR A GAS TURBINE ENGINE
    16.
    发明申请
    BEARING COMPARTMENT SEAL CONFIGURATION FOR A GAS TURBINE ENGINE 审中-公开

    公开(公告)号：US20200325788A1

    公开(公告)日：2020-10-15

    申请号：US16383018

    申请日：2019-04-12

    Applicant: United Technologies Corporation

    Inventor： Jonathan Logan Miller ,  M. Rifat Ullah

    IPC: F01D11/00 ,  F16J15/44 ,  F04D29/12

    Abstract: A bearing compartment seal for a gas turbine engine includes at least one seal ring defining an axis and having a radially inward facing sealing surface and a seal runner having a support constructed of a first material and an interface portion constructed of a second material. The interface portion includes a radially outward facing surface. A first coefficient of thermal expansion of the second material is at most approximately equal to a second coefficient of thermal expansion of the at least one seal ring.

    Ring seal arrangement
    17.
    发明授权
    Ring seal arrangement 有权

    公开(公告)号：US10208610B2

    公开(公告)日：2019-02-19

    申请号：US15481164

    申请日：2017-04-06

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Jonathan Logan Miller

    IPC: F16J15/44 ,  F01D11/00 ,  F01D25/16 ,  F01D25/18 ,  F16J15/34

    Abstract: A ring seal assembly is provided. The ring seal assembly may comprise an air side ring seal and an oil side ring seal. The air side ring seal may have one or more axial and radial grooves. The oil side ring seal may also have one or more axial and radial grooves, and may have circumferential slots in fluid communication with one or more of the grooves. The oil side ring seal may have an extended leg protruding towards the air side ring seal. The extended leg and a forward outer surface of the oil side ring seal and an aft outer surface of the air side ring seal may define a spring cavity.

    RING SEAL ARRANGEMENT WITH INSTALLATION FOOLPROOFING
    18.
    发明申请
    RING SEAL ARRANGEMENT WITH INSTALLATION FOOLPROOFING 审中-公开

    公开(公告)号：US20190017605A1

    公开(公告)日：2019-01-17

    申请号：US15650171

    申请日：2017-07-14

    Applicant: United Technologies Corporation

    Inventor： Jonathan Logan Miller ,  Joseph G. Colucci ,  Colin D. Craig ,  Aneil S. Hegde ,  Michael M. Davis

    IPC: F16J15/3296 ,  F16J15/3268

    Abstract: A ring seal in a gas turbine engine includes a ring seal body, an axial sealing dam, a radial sealing dam, and at least one bleed slot. The ring seal body is annular in shape and has a first axial side, a second axial side, a radially outer side, and a radially inner side. The axial sealing dam is on the first axial side and is configured to provide a first sealing surface with a first component. The radial sealing dam is on the radially outer side and is configured to provide a second sealing surface with a second component radially outward from the radially outer side. The at least one bleed slot is on the second axial side and configured to allow fluid to pass through when the ring seal is incorrectly oriented such that the at least one bleed slot is adjacent to the first component.

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