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    Electric system architecture for more-electric engine accessories
    22.
    发明授权
    Electric system architecture for more-electric engine accessories 有权
    更多电动发动机配件的电气系统结构

    公开(公告)号：US09573539B2

    公开(公告)日：2017-02-21

    申请号：US14461927

    申请日：2014-08-18

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Gregory I. Rozman ,  Jacek F. Gieras ,  Lubomir A. Ribarov

    IPC: H02P9/00 ,  B60R16/03 ,  H02P9/30 ,  H02K7/18

    CPC classification number: B60R16/03 ,  H02K7/1823 ,  H02P9/302 ,  H02P9/307

    Abstract: An electric system and method includes a flux regulated permanent magnet generator configured to provide power for an accessory electric system. The accessory electric system includes an engine accessory and a voltage regulator. The engine accessory includes an induction motor that receives power from the flux regulated permanent magnet generator. The voltage regulator is configured to control an output of the flux regulated permanent magnet generator to maintain a constant voltage-to-frequency ratio.

    Abstract translation: 电气系统和方法包括被配置为为附件电气系统提供电力的磁通调节永久磁铁发生器。 附件电气系统包括发动机附件和电压调节器。 发动机配件包括从磁通调节永磁发电机接收电力的感应电动机。 电压调节器被配置为控制通量调节永磁发电机的输出以保持恒定的电压 - 频率比。

    Wound-field generator including electrically isolated engine alternator
    23.
    发明授权
    Wound-field generator including electrically isolated engine alternator 有权
    包括电隔离发动机交流发电机的励磁发电机

    公开(公告)号：US09467083B1

    公开(公告)日：2016-10-11

    申请号：US14718431

    申请日：2015-05-21

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Leo J. Veilleux, Jr. ,  Lubomir A. Ribarov

    IPC: H02P9/10 ,  H02P9/14 ,  H02P9/38 ,  H02P11/00

    CPC classification number: H02P9/38 ,  H02J7/16 ,  Y02T50/54

    Abstract: An isolated power management system includes at least one electronic power generator with a stationary side and a rotational side. The stationary side has an exciter field stator winding, a main field stator winding, and an isolator stator winding. The rotational side rotates with respect to the stationary side and includes a rotor power converting unit. At least one digital engine microcontroller generates a first electrical excitation current and excites the exciter field stator winding to generate a first electromagnetic field. The rotor power converting unit generates a second electromagnetic field in response to being energized by the first electromagnetic field. The main field stator winding and the isolator stator winding output first and second power signals, respectively, in response to being energized by the second electromagnetic field, where the second power signal is independent and isolated from the first power signal.

    Abstract translation: 隔离式电力管理系统包括具有固定侧和旋转侧的至少一个电子发电机。 固定侧具有励磁场定子绕组，主场定子绕组和隔离器定子绕组。 旋转侧相对于固定侧旋转，并且包括转子功率转换单元。 至少一个数字引擎微控制器产生第一电激励电流并激励励磁机励磁定子绕组以产生第一电磁场。 转子功率转换单元响应于被第一电磁场激励而产生第二电磁场。 主场定子绕组和隔离器定子绕组分别响应于由第二电磁场激励而输出第一和第二功率信号，其中第二功率信号是独立的并且与第一功率信号隔离。

    GENERATORS WITH OPEN LOOP ACTIVE COOLING
    25.
    发明申请
    GENERATORS WITH OPEN LOOP ACTIVE COOLING 有权
    具有开环活动冷却的发电机

    公开(公告)号：US20150048699A1

    公开(公告)日：2015-02-19

    申请号：US14172074

    申请日：2014-02-04

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Lubomir A. Ribarov ,  Robert S. Downing ,  Richard A. Himmelmann

    IPC: H02K9/197

    CPC classification number: H02K9/197 ,  H02K1/32 ,  H02K9/19

    Abstract: A rotor body for a high-speed generator includes a rotor body with interior and exterior surfaces, a coolant inlet and outlet, and a rotor cooling path for actively cooling the rotor body. The coolant inlet and outlet extend between the interior and exterior surfaces. An interior segment of the rotor cooling path fluidly couples the coolant inlet and coolant outlet and is bounded by the rotor body interior surface. An exterior segment of the cooling path is bounded by the rotor body exterior surface and fluidly couples the coolant outlet an environment external to the rotor body.

    Abstract translation: 用于高速发电机的转子体包括具有内表面和外表面的转子体，冷却剂入口和出口以及用于主动冷却转子体的转子冷却通路。 冷却剂入口和出口在内表面和外表面之间延伸。 转子冷却路径的内部段流体地联接冷却剂入口和冷却剂出口并且由转子体内表面限定。 冷却通道的外部段由转子主体外表面限定，并将冷却剂出口流体地连接到转子体外部的环境。

    RESISTIVE-INDUCTIVE DE-ICING OF AIRCRAFT FLIGHT CONTROL SURFACES
    26.
    发明申请
    RESISTIVE-INDUCTIVE DE-ICING OF AIRCRAFT FLIGHT CONTROL SURFACES 有权
    航空飞行控制表面的电感式感应检测

    公开(公告)号：US20140319278A1

    公开(公告)日：2014-10-30

    申请号：US13870403

    申请日：2013-04-25

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Lubomir A. Ribarov ,  Jacek F. Gieras

    IPC: B64D15/12

    CPC classification number: B64D15/12 ,  B64D15/00 ,  B64D15/14

    Abstract: Embodiments of the disclosure include a de-icing system for an aircraft. The de-icing system includes a plurality of resistive-inductive heating elements inserted adjacent to a flight control surface and a controller configured to provide a supply current to each of the plurality of resistive-inductive heating elements. Each of the plurality of resistive-inductive heating elements produces an electromagnetic field normal to the flight control surfaces and resistive heat in response to the supply current. The electromagnetic field induces an eddy current in the flight control surface.

    Abstract translation: 本公开的实施例包括用于飞行器的除冰系统。 除冰系统包括与飞行控制表面相邻地插入的多个电阻感应加热元件和被配置为向多个电阻感应加热元件中的每一个提供电源电流的控制器。 多个电阻感应加热元件中的每一个响应于电源电流产生垂直于飞行控制表面的电磁场和电阻热。 电磁场在飞行控制表面中产生涡流。

    Hybrid propulsion systems
    27.
    发明授权
    Hybrid propulsion systems 有权

    公开(公告)号：US12145734B2

    公开(公告)日：2024-11-19

    申请号：US17135800

    申请日：2020-12-28

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Leo J. Veilleux, Jr. ,  Lubomir A. Ribarov

    IPC: B64D27/24 ,  B60L50/60 ,  B64D27/02 ,  B64D27/10 ,  B64D35/06 ,  F02C3/04 ,  F02C6/20 ,  F16H57/02

    Abstract: A hybrid propulsion system can include a turbomachine having a compressor, a combustion chamber, and a compressor turbine. The compressor can be connected to the compressor turbine via a first shaft. The system can include a hybrid drive assembly which can include a power turbine in fluid communication with an outlet of the compressor turbine to be driven by compressor turbine exhaust to drive a second shaft that is disconnected from the first shaft. The hybrid drive assembly can also include an electrical machine mechanically coupled to the second shaft either to convert rotational energy to electrical energy or to convert electrical energy to rotational energy of the second shaft.

    STOWABLE ELECTRIC-HYBRID PROPFAN
    28.
    发明公开
    STOWABLE ELECTRIC-HYBRID PROPFAN 审中-公开

    公开(公告)号：US20230358191A1

    公开(公告)日：2023-11-09

    申请号：US17738543

    申请日：2022-05-06

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Leo J. Veilleux, JR. ,  Lubomir A. Ribarov

    IPC: F02K7/10 ,  B64D27/24 ,  B64D27/10 ,  B64D31/00

    CPC classification number: F02K7/10 ,  B64D27/10 ,  B64D27/24 ,  B64D31/00 ,  B64D2027/026 ,  F05D2220/34 ,  F05D2220/76

    Abstract: An electricity generation and propulsion system of an aircraft is provided. The electricity generation and propulsion system includes a fuselage, a hybrid-electric power generation system operably disposed in the fuselage and a ram air turbine (RAT) device. The RAT device is coupled with the hybrid-electric power generation system and is stowable in the fuselage and deployable to an exterior of the fuselage. The RAT device is operable as a RAT when deployed into an airstream that drives rotations of the RAT from which the hybrid-electric power generation system generates electricity, and the RAT device is operable as a propulsor when deployed and driven by the hybrid-electric power generation system.

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