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    BRACKETS FOR GAS TURBINE ENGINE COMPONENTS
    4.
    发明申请
    BRACKETS FOR GAS TURBINE ENGINE COMPONENTS 审中-公开
    气体涡轮发动机组件支架

    公开(公告)号：US20160348587A1

    公开(公告)日：2016-12-01

    申请号：US15116408

    申请日：2015-01-15

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Jonas S. Banhos ,  Joo Sub Rhee

    IPC: F02C7/20 ,  F01D11/24 ,  F02C7/12

    CPC classification number: F02C7/20 ,  F01D11/24 ,  F02C7/12 ,  F05D2220/32 ,  F05D2240/14 ,  F05D2260/20 ,  F05D2260/30 ,  F05D2260/94

    Abstract: A bracket includes a rigid member and a resilient member for coupling a coolant collector to a coolant supply manifold. The coolant collector is movable between a first position and a second position with respect to the coolant supply manifold due to thermal heating. The resilient member defines an anchoring portion and a cantilevered portion. The anchoring portion couples the cantilevered portion to a midsection of the rigid member for urging the coolant collector toward the coolant supply manifold in the first and second positions.

    Abstract translation: 支架包括刚性构件和用于将冷却剂收集器连接到冷却剂供应歧管的弹性构件。 由于热加热，冷却剂收集器可相对于冷却剂供应歧管在第一位置和第二位置之间移动。 弹性构件限定锚固部分和悬臂部分。 锚定部分将悬臂部分连接到刚性构件的中部，用于在第一和第二位置中将冷却剂收集器朝向冷却剂供应歧管推动。

    Brackets for gas turbine engine components
    5.
    发明授权
    Brackets for gas turbine engine components 有权

    公开(公告)号：US10330012B2

    公开(公告)日：2019-06-25

    申请号：US15116408

    申请日：2015-01-15

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Jonas S. Banhos ,  Joo Sub Rhee

    IPC: F01D11/24 ,  F02C7/12 ,  F02C7/20

    Abstract: A bracket includes a rigid member and a resilient member for coupling a coolant collector to a coolant supply manifold. The coolant collector is movable between a first position and a second position with respect to the coolant supply manifold due to thermal heating. The resilient member defines an anchoring portion and a cantilevered portion. The anchoring portion couples the cantilevered portion to a midsection of the rigid member for urging the coolant collector toward the coolant supply manifold in the first and second positions.

    Duct assembly for a gas turbine engine
    6.
    发明授权
    Duct assembly for a gas turbine engine 有权

    公开(公告)号：US10975730B2

    公开(公告)日：2021-04-13

    申请号：US16460002

    申请日：2019-07-02

    Applicant: United Technologies Corporation

    Inventor： Jonas S. Banhos ,  Anthony Prainito

    IPC: F02C7/20 ,  F01D25/28 ,  F02K3/02 ,  F02K3/04

    Abstract: A gas turbine engine duct assembly includes a composite duct body that includes at least one rim. A flanged bracket includes a radially extending portion that defines a flange. An axially extending portion has an inner duct rim recess for accepting a portion of the at least one rim. At least one attachment plate has a projection recess for accepting a projection on the flanged bracket and an outer rim recess for accepting a portion of the at least one rim.

    SEAL PLATE WITH FLUID BYPASS CONTROL
    7.
    发明申请
    SEAL PLATE WITH FLUID BYPASS CONTROL 审中-公开
    具有流体旁路控制的密封板

    公开(公告)号：US20160356220A1

    公开(公告)日：2016-12-08

    申请号：US14623309

    申请日：2015-02-16

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： William Meyst ,  Jonas S. Banhos ,  Andre Herman Troughton

    IPC: F02C7/06 ,  F02C7/28

    CPC classification number: F02C7/06 ,  F01D25/18 ,  F01D25/183 ,  F02C7/28 ,  F05D2220/32 ,  F05D2240/55 ,  F05D2260/98

    Abstract: The present disclosure relates generally to a manifold including a plurality of manifold channels disposed therethrough, each manifold channel including a manifold channel opening, and a seal plate, including a plurality of seal plate apertures disposed thereon, operably coupled to the manifold, wherein the seal plate includes at least one seal plate channel extending between at least two of the plurality of seal plate apertures.

    Abstract translation: 本公开总体上涉及一种包括多个歧管通道的歧管，每个歧管通道设置在其中，每个歧管通道包括歧管通道开口和密封板，密封板包括可操作地联接到歧管的多个密封板孔，其中密封件 板包括在多个密封板孔中的至少两个之间延伸的至少一个密封板通道。

    DUCT ASSEMBLY FOR A GAS TURBINE ENGINE
    8.
    发明申请
    DUCT ASSEMBLY FOR A GAS TURBINE ENGINE 有权

    公开(公告)号：US20210003038A1

    公开(公告)日：2021-01-07

    申请号：US16460002

    申请日：2019-07-02

    Applicant: United Technologies Corporation

    Inventor： Jonas S. Banhos ,  Anthony Prainito

    IPC: F01D25/28 ,  F02K3/02 ,  F02K3/04

    Abstract: A gas turbine engine duct assembly includes a composite duct body that includes at least one rim. A flanged bracket includes a radially extending portion that defines a flange. An axially extending portion has an inner duct rim recess for accepting a portion of the at least one rim. At least one attachment plate has a projection recess for accepting a projection on the flanged bracket and an outer rim recess for accepting a portion of the at least one rim.

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