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1. 发明申请

US20210408699A1 CRIMP PIN ELECTRICAL CONNECTOR 有权
公开(公告)号：US20210408699A1
公开(公告)日：2021-12-30
申请号：US16912956
申请日：2020-06-26
申请人： GE AVIATION SYSTEMS LLC
发明人： Brian Matthew Maupin , John S. Mears
IPC分类号： H01R4/20 , H01R13/52 , H01R13/622
摘要： A crimp pin electrical connector comprising a shell defining an interior with a first and a second opening, a flange circumscribing the shell, an insert located within the interior and extending through the first opening. The insert comprising at least one crimp pin including a crimp and a pin provided within at least one passage included within the interior of the shell.

2. 发明申请

US20200217250A1 ELECTRIC MACHINE WITH NON-CONTACT INTERFACE 审中-公开
公开(公告)号：US20200217250A1
公开(公告)日：2020-07-09
申请号：US16240245
申请日：2019-01-04
申请人： GE AVIATION SYSTEMS LLC
发明人： Samuel Robert Hathaway , Clifford D. Westerlund , Jason D. Wilkening , Robert D. Grennan , Michael George Schneider , John S. Mears
IPC分类号： F02C7/18 , F01D5/08 , F02C3/08
摘要： An apparatus and method for a generator for generating power having a rotary union between a rotor and a stator, the rotary union comprising a first fluid passage having a converging nozzle and located within the stator having a first inlet and a first outlet, a second fluid passage having a diverging nozzle and located within the rotor and having a second inlet and a second outlet, the second inlet is aligned with the first outlet and at least one gap located between the rotor and stator.

3. 发明授权

US10720728B2 Electrical connector sealing system 有权
公开(公告)号：US10720728B2
公开(公告)日：2020-07-21
申请号：US16189523
申请日：2018-11-13
申请人： GE AVIATION SYSTEMS LLC
发明人： John S. Mears , Samuel Robert Hathaway , Daniel Alan Niergarth , David George Kloos
IPC分类号： H01R13/52 , H02G3/36 , B23P11/00 , B64D41/00
摘要： A method and apparatus for a crimp pin electrical connector can include a body with a first face and a second face, with openings extending through the body from the first face to the second face. A grommet can connect to the body with grommet holes aligned with the openings. A cap having a set of cap holes can align with the grommet holes. A nut can threadably engage with the body to compress the grommet via the cap to seal wires connected to the body with an interference.

4. 发明授权

US10348162B1 Method and assembly of an electric machine 有权
公开(公告)号：US10348162B1
公开(公告)日：2019-07-09
申请号：US15850719
申请日：2017-12-21
申请人： GE AVIATION SYSTEMS, LLC
发明人： Hao Huang , John S. Mears , Xiaochuan Jia , Samuel Robert Hathaway
IPC分类号： F02C7/32 , H02K7/18 , H02K9/19
摘要： A generator includes a housing, a rotor within the housing and rotatable about an axis of rotation, and a coolant sump within the housing and arranged axially parallel with the axis of rotation, wherein an aeroline of the generator can at least partially limit an aeroline of an engine cowling.

5. 发明授权

US10161356B2 Integrated thrust reverser actuation system 有权
公开(公告)号：US10161356B2
公开(公告)日：2018-12-25
申请号：US14293605
申请日：2014-06-02
申请人： GE Aviation Systems LLC
发明人： John S. Mears , George Stephen Billisits , Chad Russell Wentling
IPC分类号： F02K1/72 , F02K1/56 , F02K1/76 , F02K1/15 , F02K1/09 , F02C7/20
摘要： A turbofan engine having a turbine engine, a nacelle surrounding a portion of the turbine engine, and a thrust reverser. The thrust reverser comprises a movable control surface movable to and from a reversing position and a thrust reverser actuation system having at least one actuator operably coupled to the movable control surface to move the movable control surface into and out of the reversing position. A guide comprising a rail and a bogie having at least one rotatable bearing surface coupled to the rail for relative translational movement between the rail and bogie connects the turbine engine to the movable control surface such that operation of the at least one actuator moves the movable control surface by translation movement between the rail and the bogie.

6. 发明申请

US20160186688A1 INTEGRATED THRUST REVERSER ACTUATION SYSTEM 审中-公开
标题翻译：集成式逆变器启动系统
公开(公告)号：US20160186688A1
公开(公告)日：2016-06-30
申请号：US14293605
申请日：2014-06-02
申请人： GE Aviation Systems LLC
发明人： John S. Mears , George Stephen Billisits , Chad Russell Wentling
IPC分类号： F02K1/56 , F02C7/20
CPC分类号： F02K1/56 , F02C7/20 , F02K1/09 , F02K1/15 , F02K1/72 , F02K1/763 , F05D2250/34 , F05D2260/57 , F05D2270/60 , F05D2270/62 , F05D2270/64 , F05D2270/66
摘要： A turbofan engine having a turbine engine, a nacelle surrounding a portion of the turbine engine, and a thrust reverser. The thrust reverser comprises a movable control surface movable to and from a reversing position and a thrust reverser actuation system having at least one actuator operably coupled to the movable control surface to move the movable control surface into and out of the reversing position. A guide comprising a rail and a bogie having at least one rotatable bearing surface coupled to the rail for relative translational movement between the rail and bogie connects the turbine engine to the movable control surface such that operation of the at least one actuator moves the movable control surface by translation movement between the rail and the bogie.
摘要翻译：具有涡轮发动机，围绕涡轮发动机的一部分的机舱和推力反向器的涡轮风扇发动机。推力反向器包括可移动到可逆位置的可移动控制表面和推力反向器致动系统，其具有可操作地联接到可移动控制表面的至少一个致动器，以将可移动控制表面移入和移出反转位置。包括轨道和转向架的引导件具有联接到轨道的至少一个可旋转支承表面，用于在轨道和转向架之间的相对平移运动将涡轮发动机连接到可移动控制表面，使得至少一个致动器的操作使可移动控制器轨道与转向架之间的平移运动。

7. 发明授权

US11381142B2 Rotor assembly 有权
公开(公告)号：US11381142B2
公开(公告)日：2022-07-05
申请号：US16298131
申请日：2019-03-11
申请人： GE AVIATION SYSTEMS LLC
发明人： John S. Mears , Austin Michael Cobert , Todd Eric Rook
IPC分类号： H02K15/02 , H02K3/51
摘要： A rotor assembly for an electric machine includes a cylindrical rotor core, a set of posts extending radially outward from the rotor core defining a set of slots between adjacent posts, a set of windings formed by conductive wire wound in the set of slots having end turns extending axially beyond the rotor core, and a retention case overlying the end turns.

8. 发明授权

US11002191B2 Electric machine with non-contact interface 有权
公开(公告)号：US11002191B2
公开(公告)日：2021-05-11
申请号：US16240245
申请日：2019-01-04
申请人： GE AVIATION SYSTEMS LLC
发明人： Samuel Robert Hathaway , Clifford D. Westerlund , Jason D. Wilkening , Robert D. Grennan , David George Kloos , John S. Mears
IPC分类号： F16L27/00 , F02C7/18 , F01D5/08 , H02K1/32 , H02K9/19 , F01L5/08 , F02C3/08
摘要： An apparatus and method for a generator for generating power having a rotary union between a rotor and a stator, the rotary union comprising a first fluid passage having a converging nozzle and located within the stator having a first inlet and a first outlet, a second fluid passage having a diverging nozzle and located within the rotor and having a second inlet and a second outlet, the second inlet is aligned with the first outlet and at least one gap located between the rotor and stator.

9. 发明申请

US20200295636A1 ROTOR ASSEMBLY 审中-公开
公开(公告)号：US20200295636A1
公开(公告)日：2020-09-17
申请号：US16298131
申请日：2019-03-11
申请人： GE AVIATION SYSTEMS LLC
发明人： John S. Mears , Austin Michael Cobert , Todd Eric Rook
IPC分类号： H02K15/02 , H02K3/51
摘要： A rotor assembly for an electric machine includes a cylindrical rotor core, a set of posts extending radially outward from the rotor core defining a set of slots between adjacent posts, a set of windings formed by conductive wire wound in the set of slots having end turns extending axially beyond the rotor core, and a retention case overlying the end turns.

10. 发明申请

US20150089936A1 AIRCRAFT HYDRAULIC SYSTEM 有权
标题翻译：飞机液压系统
公开(公告)号：US20150089936A1
公开(公告)日：2015-04-02
申请号：US14038911
申请日：2013-09-27
申请人： GE Aviation Systems LLC
发明人： John S. Mears
IPC分类号： F15B21/04
CPC分类号： F15B21/041 , B64C13/36
摘要： An aircraft hydraulic system for operating a plurality of hydraulically-operated actuators in the aircraft having a hydraulic reservoir in which hydraulic fluid is stored, a hydraulic distribution system coupling the hydraulic reservoir to the actuators and having a main flow line coupled to the hydraulic reservoir, a hydraulic pump fluidly coupled to the main flow line and the hydraulic reservoir to pump hydraulic fluid from the reservoir to the main flow line, a main filtration system fluidly coupled to the main flow line upstream of at least some of the actuators, and a self-cleaning filter fluidly coupled upstream of the main filtration system.
摘要翻译：一种用于在飞行器中操作多个液压操作致动器的飞行器液压系统，具有存储液压流体的液压储存器，将液压储存器连接到致动器并且具有联接到液压储存器的主流线的液压分配系统，液压泵，其流体地联接到所述主流线和所述液压储存器以将液压流体从所述储存器泵送到所述主流动管线;主过滤系统，其流体地联接到至少一些所述致动器的主流线上游，以及自身 - 清洗过滤器，流体耦合在主过滤系统的上游。

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