公开(公告)号：US11348717B2

公开(公告)日：2022-05-31

申请号：US16176600

申请日：2018-10-31

Applicant: Hamilton Sundstrand Corporation

Inventor： Ashutosh Joshi ,  Debabrata Pal ,  Mark W. Metzler ,  Richard L. Downing ,  Charles Patrick Shepard

IPC: H01F27/10 ,  H01F27/02 ,  H01F27/12 ,  H01F27/16 ,  H01F27/28

Abstract: An inductor assembly includes a housing including a base, a sidewall, and an insert. The base and the sidewall define a cavity and the insert being positioned within the cavity. A core assembly is positioned within the cavity. The core assembly includes a core and a plurality of windings wrapped about the core and disposed between the sidewall and the insert. A flow path is formed in the housing for receiving a coolant to remove heat from the core assembly.

公开(公告)号：US09561861B2

公开(公告)日：2017-02-07

申请号：US14792050

申请日：2015-07-06

Applicant: Hamilton Sundstrand Corporation

Inventor： Jeffrey T. Wavering ,  Richard L. Downing

IPC: B64D41/00 ,  H02B1/21

CPC classification number: B64D41/00 ,  B64D2221/00 ,  H02B1/056 ,  H02B1/21

Abstract: A power-distribution panel has a circuit-breaker panel that is completely separable from an aircraft and from a back chassis connected to the aircraft. The back chassis is mechanically mounted to the aircraft and electrically connected to both a power-supply bus and a power-distribution harness of the aircraft. The circuit-breaker panel can be removably coupled to the back chassis to complete a plurality of circuits from the power supply bus to a plurality the plurality of circuits that receive power via the power-distribution harness. In some embodiments, the circuit-breaker panel can be slideably coupled to the back chassis without the use of tools. Electrical connectors may provide electrically connectivity between the circuit-breaker panel and the back chassis. The electrical connectors may have back chassis portions that align with circuit-breaker panel portions so as to provide such electrically connectivity automatically when the circuit-breaker panel is coupled to the back chassis.

Abstract translation: 配电盘具有与飞机完全分离的断路器面板和与飞机相连的背板。 后底盘机械地安装在飞行器上并与飞机的电源总线和配电线束电连接。 断路器面板可以可拆卸地耦合到后机架，以完成从电源总线到经由配电线束接收电力的多个电路的多个电路。 在一些实施例中，断路器面板可以在不使用工具的情况下可滑动地联接到后机架。 电连接器可以在断路器面板和后机架之间提供电连接。 电连接器可以具有与断路器面板部分对准的背部底座部分，以便当断路器面板耦合到后机架时自动提供这种电连接。

公开(公告)号：US10923983B2

公开(公告)日：2021-02-16

申请号：US16048873

申请日：2018-07-30

Applicant: Hamilton Sundstrand Corporation

Inventor： Craig J. Wojcik ,  Ted A. Martin ,  Mark W. Metzler ,  Richard L. Downing

IPC: H02K5/20 ,  F02C7/06 ,  H02K7/18 ,  H02K9/19

Abstract: Generator housings for generators of aircraft are provided. The generator housings include a mounting pad at a first end, the generator housing extending to a second end, and a base arranged to connect to an electronics module. The generator housing defines a generator cavity and a flow path to supply a working fluid through the generator housing, the flow path extending between an inlet formed in the mounting pad and at least one outlet formed in the mounting pad. One or more electronics flow ports enable fluid connection between the flow path within the generator housing and the electronic module when connected and one or more inductor ports enable fluid connection between the flow path within the generator housing and one or more inductors when mounted to the generator housing.

公开(公告)号：US20170008638A1

公开(公告)日：2017-01-12

申请号：US14792050

申请日：2015-07-06

Applicant: Hamilton Sundstrand Corporation

Inventor： Jeffrey T. Wavering ,  Richard L. Downing

IPC: B64D41/00 ,  H02B1/21

CPC classification number: B64D41/00 ,  B64D2221/00 ,  H02B1/056 ,  H02B1/21

Abstract: A power-distribution panel has a circuit-breaker panel that is completely separable from an aircraft and from a back chassis connected to the aircraft. The back chassis is mechanically mounted to the aircraft and electrically connected to both a power-supply bus and a power-distribution harness of the aircraft. The circuit-breaker panel can be removably coupled to the back chassis to complete a plurality of circuits from the power supply bus to a plurality the plurality of circuits that receive power via the power-distribution harness. In some embodiments, the circuit-breaker panel can be slideably coupled to the back chassis without the use of tools. Electrical connectors may provide electrically connectivity between the circuit-breaker panel and the back chassis. The electrical connectors may have back chassis portions that align with circuit-breaker panel portions so as to provide such electrically connectivity automatically when the circuit-breaker panel is coupled to the back chassis.

Abstract translation: 配电盘具有与飞机完全分离的断路器面板和与飞机相连的背板。 后底盘机械地安装在飞行器上并与飞机的电源总线和配电线束电连接。 断路器面板可以可拆卸地耦合到后机架，以完成从电源总线到经由配电线束接收电力的多个电路的多个电路。 在一些实施例中，断路器面板可以在不使用工具的情况下可滑动地联接到后机架。 电连接器可以在断路器面板和后机架之间提供电连接。 电连接器可以具有与断路器面板部分对准的背部底座部分，以便当断路器面板耦合到后机架时自动提供这种电连接。