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    SYSTEM FOR PACKAGING ELECTRONIC COMPONENTS IN A ROTATABLE SHAFT
    41.
    发明申请
    SYSTEM FOR PACKAGING ELECTRONIC COMPONENTS IN A ROTATABLE SHAFT 有权
    用于在可旋转轴中包装电子部件的系统

    公开(公告)号：US20170058694A1

    公开(公告)日：2017-03-02

    申请号：US15347879

    申请日：2016-11-10

    Applicant: General Electric Company

    Inventor： Donald W. Shaw ,  Kurt Kramer Schleif ,  Zachary John Snider

    IPC: F01D21/00 ,  F03D80/80

    CPC classification number: F01D21/003 ,  F03D7/042 ,  F03D80/82 ,  F05D2220/31 ,  F05D2220/32 ,  F05D2240/60 ,  F05D2260/80 ,  Y02E10/72

    Abstract: A system for packaging electronic components in a rotatable shaft includes an annular carrier shaft having a first end that is axially spaced from a second end and an inner surface that is radially spaced from an outer surface, and a plurality of transmitter assemblies annularly arranged within the carrier shaft. Each transmitter assembly includes a transmitter housing radially supported within the carrier shaft via a pair of circumferentially spaced rail members. Each transmitter assembly comprises a daughter board that extends laterally and longitudinally across a bottom portion of the transmitter housing and at least one electronic component electrically coupled to the daughter board. The electronic component extends substantially perpendicular to the daughter board within the transmitter housing.

    Abstract translation: 一种用于将可旋转轴中的电子部件包装的系统包括环形载体轴，其具有与第二端轴向间隔开的第一端和与外表面径向间隔开的内表面，以及多个发射器组件， 载体轴。 每个发射器组件包括经由一对周向间隔的导轨构件径向支撑在载体轴内的变送器壳体。 每个发射器组件包括子板，该子板横向延伸穿过变送器壳体的底部部分和至少一个电耦合到子板的电子部件。 电子部件基本上垂直于发射机外壳内的子板延伸。

    SYSTEM FOR PACKAGING ELECTRONIC COMPONENTS IN A ROTATABLE SHAFT
    42.
    发明申请
    SYSTEM FOR PACKAGING ELECTRONIC COMPONENTS IN A ROTATABLE SHAFT 有权
    用于在可旋转轴中包装电子部件的系统

    公开(公告)号：US20160138426A1

    公开(公告)日：2016-05-19

    申请号：US14541196

    申请日：2014-11-14

    Applicant: General Electric Company

    Inventor： Donald W. Shaw ,  Kurt Kramer Schleif ,  Zachary John Snider

    IPC: F01D25/28 ,  F01D21/00 ,  F03D7/04 ,  H05K5/00

    CPC classification number: F01D21/003 ,  F03D7/042 ,  F03D80/82 ,  F05D2220/31 ,  F05D2220/32 ,  F05D2240/60 ,  F05D2260/80 ,  Y02E10/72

    Abstract: A system for packaging electronic components in a rotatable shaft includes an annular carrier shaft having a first end that is axially spaced from a second end and an inner surface that is radially spaced from an outer surface, and a plurality of transmitter assemblies annularly arranged within the carrier shaft. Each transmitter assembly includes a transmitter housing radially supported within the carrier shaft via a pair of circumferentially spaced rail members. Each transmitter assembly comprises a daughter board that extends laterally and longitudinally across a bottom portion of the transmitter housing and at least one electronic component electrically coupled to the daughter board. The electronic component extends substantially perpendicular to the daughter board within the transmitter housing.

    Abstract translation: 一种用于将可旋转轴中的电子部件包装的系统包括环形载体轴，其具有与第二端轴向间隔开的第一端和与外表面径向间隔开的内表面，以及多个发射器组件， 载体轴。 每个发射器组件包括经由一对周向间隔的导轨构件径向支撑在载体轴内的变送器壳体。 每个发射器组件包括子板，该子板横向延伸穿过变送器壳体的底部部分和至少一个电耦合到子板的电子部件。 电子部件基本上垂直于发射机外壳内的子板延伸。

    SYSTEMS AND METHODS FOR ATTACHING A PROBE TO A CASING OF A GAS TURBINE ENGINE
    43.
    发明申请
    SYSTEMS AND METHODS FOR ATTACHING A PROBE TO A CASING OF A GAS TURBINE ENGINE 有权
    将探测器连接到气体涡轮发动机的系统和方法

    公开(公告)号：US20160084736A1

    公开(公告)日：2016-03-24

    申请号：US14489759

    申请日：2014-09-18

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Kurt Kramer Schleif ,  Zachary John Snider ,  Nathan Lee Brown ,  Andrea Booher Kretschmar ,  Michael Allen Ball

    IPC: G01M15/14 ,  G01D11/18 ,  G01D11/30

    CPC classification number: G01M15/14 ,  F01D17/02 ,  G01D11/30

    Abstract: A system for attaching a probe to a casing of a gas turbine engine is disclosed. The system may include a probe receptacle attachable to the casing. The probe receptacle may include an internal bore, a bayonet slot, a spring disposed within the internal bore adjacent to the bayonet slot, and a sealing surface within the internal bore. The system also may include a probe attachment assembly disposed about the probe and configured to engage the probe receptacle. The probe attachment assembly may include at least one bayonet positionable within the bayonet slot and a seal positionable adjacent to the sealing surface within the internal bore.

    Abstract translation: 公开了一种用于将探头附接到燃气涡轮发动机的壳体的系统。 该系统可以包括可附接到壳体的探针插座。 探针插座可以包括内孔，卡口槽，布置在邻近卡口槽的内孔内的弹簧以及内孔内的密封表面。 该系统还可以包括围绕探针设置的探测器附接组件，并且被配置成接合探针插座。 探针附接组件可以包括可定位在卡口槽内的至少一个卡口和可在内孔内靠近密封表面定位的密封件。

    Vibration damping system for turbine blade or nozzle, retention system therefor, and method of assembly
    46.
    发明授权
    Vibration damping system for turbine blade or nozzle, retention system therefor, and method of assembly 有权

    公开(公告)号：US11519276B1

    公开(公告)日：2022-12-06

    申请号：US17574092

    申请日：2022-01-12

    Applicant: General Electric Company

    Inventor： Zachary John Snider ,  John McConnell Delvaux

    IPC: F01D5/16

    Abstract: A vibration damping element for a vibration damping system for a turbine nozzle or blade includes an elongated body and a wire mesh member that surrounds the elongated body. The wire mesh member has a first outer dimension in an inoperative state and a second, larger outer dimension in an operative state. In the operative state, the wire mesh member frictionally engages with an inner surface of a body opening in the turbine nozzle or blade to damp vibration. In the inoperative state, the wire mesh member slides freely in the body opening in the turbine nozzle or blade. A retention system includes a retention member on the elongated body that fixes the wire mesh member relative to a length of the elongated body in the operative state in the body opening of the turbine nozzle or blade.

    Unitary body turbine shrouds including shot peen screens integrally formed therein and turbine systems thereof
    48.
    发明授权
    Unitary body turbine shrouds including shot peen screens integrally formed therein and turbine systems thereof 有权

    公开(公告)号：US11035248B1

    公开(公告)日：2021-06-15

    申请号：US16693856

    申请日：2019-11-25

    Applicant: General Electric Company

    Inventor： Zachary John Snider ,  Evan John Dozier ,  Claire Fridtjof Lang

    IPC: F01D11/08 ,  F01D25/12 ,  B24C1/10 ,  B24C3/32

    Abstract: Turbine shrouds including shot peen screens integrally formed therein. The shroud may include a unitary body having a support portion coupled directly to a turbine casing of the turbine system, an intermediate portion integral with and extending away from the support portion, and a seal portion integral with the intermediate portion, opposite the support portion. The unitary body may also include an inlet opening(s) formed in the support portion, a plenum(s) in fluid communication with the inlet opening(s), and a cooling passage extending through the seal portion and in fluid communication with the plenum(s). Additionally, the unitary body may include a shot peen screen(s) positioned within the plenum(s) and extending within the intermediate portion. The shot peen screen(s) may include a plurality of voids formed therethrough and may prevents shot from passing through the shot peen screen(s) when performing a shot peening process on the unitary body.

    ADDITIVE MANUFACTURED COMPONENTS INCLUDING INTEGRALLY FORMED PASSAGES, CHANNELS, AND CONDUITS, AND METHODS OF FORMING SAME
    49.
    发明申请
    ADDITIVE MANUFACTURED COMPONENTS INCLUDING INTEGRALLY FORMED PASSAGES, CHANNELS, AND CONDUITS, AND METHODS OF FORMING SAME 有权

    公开(公告)号：US20210154927A1

    公开(公告)日：2021-05-27

    申请号：US16693854

    申请日：2019-11-25

    Applicant: General Electric Company

    Inventor： Zachary John Snider ,  Michael Scott Soden ,  Michael Robert Berry

    IPC: B29C64/188

    Abstract: Additively manufactured components including unitary bodies. The component may include a unitary body having a component section. The component section may include at least one passage extending at least partially through the component section. The unitary body may also include a supplemental section formed integral with the component section. The supplemental section may be disposed over the passage(s) of the component section and may include a channel extending at least partially through the supplemental section. The channel may be in fluid communication with the passage(s) of the component section. Additionally, the unitary body may include a transition conduit positioned within the component section and the supplemental section. The transition conduit may extend between the passage(s) of the component section and the channel of the supplemental section to fluidly couple the passage(s) and the channel.

    Unitary body turbine shrouds including structural breakdown and collapsible features
    50.
    发明授权
    Unitary body turbine shrouds including structural breakdown and collapsible features 有权

    公开(公告)号：US10830050B2

    公开(公告)日：2020-11-10

    申请号：US16263430

    申请日：2019-01-31

    Applicant: General Electric Company

    Inventor： Zachary John Snider

    IPC: F01D5/14 ,  F01D25/14 ,  F01D5/20 ,  F01D11/08

    Abstract: Turbine shrouds including structural breakdown and collapsible features are disclosed. The shrouds may include a unitary body including a support portion coupled directly to a turbine casing of the turbine system, an intermediate portion integral with and extending away from the support portion, and a seal portion integral with the intermediate portion. The unitary body of the shroud may also include two opposing slash faces extending adjacent to and between the support portion and the seal portion, and a plenum extending through the support portion, the intermediate portion, and at least a portion of the seal portion, between the two opposing slash faces. Additionally, the unitary body may include a bridge member(s) formed integral with the intermediate portion, and extending partially through the plenum, and an aperture(s) formed within a portion of the plenum extending through the intermediate portion.

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