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公开(公告)号：US09347579B2
公开(公告)日：2016-05-24
申请号：US14169793
申请日：2014-01-31
Applicant: Hamilton Sundstrand Corporation
Inventor： Jacek F. Gieras , Gary M. McBrien , Leo J. Veilleux, Jr.
CPC classification number: F16K31/0655 , F16K31/0651 , F16K31/0658 , F16K31/0675 , H01F7/081 , H01F7/13 , H01F7/1607 , H01F2007/086
Abstract: An electromagnetic solenoid actuator comprises a ferromagnetic core and a ferromagnetic plunger. The ferromagnetic core supports a plurality of windings, and is oriented along an axis. The ferromagnetic plunger is aligned axially with the ferromagnetic core, and is translatable along the axis to vary a width of an air gap separating the ferromagnetic plunger from the ferromagnetic core. The ferromagnetic plunger and the ferromagnetic core overlap axially at a flux bypass that provides an alternative flux path that diverts increasing flux away from the air gap as the width of air gap decreases.
Abstract translation: 电磁螺线管致动器包括铁磁芯和铁磁柱塞。 铁磁芯支撑多个绕组，并且沿着轴线定向。 铁磁柱塞与铁磁芯轴向对准，并且可沿着轴线平移以改变将铁磁柱塞与铁磁芯分离的气隙的宽度。 铁磁柱塞和铁磁芯在通量旁路处轴向重叠，提供了随着气隙宽度减小而将增加的磁通从气隙转移的替代磁通路径。
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公开(公告)号：US20160047550A1
公开(公告)日：2016-02-18
申请号：US14457373
申请日：2014-08-12
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien
IPC: F23R3/28
CPC classification number: F23R3/28 , F02C7/222 , F02C7/228 , F02C9/263 , F02C9/34 , F05D2240/40 , F05D2270/09 , F05D2270/3015 , F05D2270/304 , F05D2270/306 , Y02T50/672
Abstract: Distributed fuel control system and methods are disclosed. A distributed fuel control system may comprise a controller, a fuel delivery system, and fuel delivery system sensors and combustion sensors. The controller may output a control signal in response to at least one of the fuel delivery system sensor or the combustion sensors. In response, the fuel flow to individual multiplex fuel delivery unit may be controlled according to various methods. One such method includes determining a desired fuel pressure differential, directing a torque motor to set a pressure regulator to a position corresponding to the desired fuel pressure differential, determining a sensed fuel pressure differential, and adjusting the torque motor in response to a difference between the sensed fuel pressure differential and the desired fuel pressure differential.
Abstract translation: 公开了分散燃料控制系统和方法。 分布式燃料控制系统可以包括控制器，燃料输送系统和燃料输送系统传感器和燃烧传感器。 控制器可以响应于燃料输送系统传感器或燃烧传感器中的至少一个输出控制信号。 作为响应，可以根据各种方法来控制到个体多路复用燃料输送单元的燃料流量。 一种这样的方法包括确定期望的燃料压力差，引导扭矩电动机将压力调节器设置到对应于期望燃料压力差的位置，确定感测到的燃料压力差，以及响应于所述燃料压力差之间的差异来调节转矩电动机 感测的燃料压力差和期望的燃料压力差。
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公开(公告)号：US09091212B2
公开(公告)日：2015-07-28
申请号：US13851580
申请日：2013-03-27
Applicant: Hamilton Sundstrand Corporation
Inventor： Leo J. Veilleux, Jr. , Gary M. McBrien
Abstract: A fuel system for an aircraft comprises a boost pump, a main fuel pump and a motive pump. The boost pump receives fuel from a storage unit. The main fuel pump receives fuel from the boost pump and delivers fuel to a distribution system. The motive fuel pump receives fuel from the boost pump, routes fuel through the storage unit, and delivers fuel to an actuator. A method for delivering fuel in an aircraft comprises pumping fuel from a fuel tank to a distribution system using a main pump, pumping fuel from a fuel tank to an actuator using a motive pump, and routing fuel from the actuator to the main pump.
Abstract translation: 用于飞行器的燃料系统包括增压泵，主燃料泵和动力泵。 增压泵从存储单元接收燃料。 主燃料泵从增压泵接收燃料并将燃料输送到分配系统。 动力燃料泵从增压泵接收燃料，将燃料通过存储单元引导，并将燃料输送到致动器。 用于在飞行器中输送燃料的方法包括：使用主泵将燃料从燃料箱泵送到配电系统，使用动力泵从燃料箱向致动器泵送燃料，以及将燃料从致动器引导到主泵。
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公开(公告)号：US20140331773A1
公开(公告)日：2014-11-13
申请号：US13889763
申请日：2013-05-08
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Peter L. Jalbert , Gary M. McBrien
IPC: G01N29/36
CPC classification number: G01N29/36 , G01H9/00 , G10K11/002
Abstract: A vibration sensor includes a probe body with a vibration isolator operatively connected to the probe body for isolation of the probe body from vibrations of a structure to be monitored for vibration. A waveguide is operatively connected to the probe body to convey microwaves to and from a surface for sensing vibration of the structure to be monitored for vibration.
Abstract translation: 振动传感器包括具有可操作地连接到探针主体的隔振器的探针主体，用于将探针体与用于振动监测的结构的振动隔离。 波导管可操作地连接到探针体，以将微波传送到表面和从表面传送用于感测待监测的结构的振动以进行振动。
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公开(公告)号：US11573130B2
公开(公告)日：2023-02-07
申请号：US16692402
申请日：2019-11-22
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien , Peter A. Dorian
Abstract: A system has a first temperature sensor located at a first location. A second temperature sensor is located at a second location. A control is configured to determine a difference between voltages indicated of a temperature sensed by each of the first and second sensors. A method is also disclosed.
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Patent Agency Ranking
公开(公告)号：US11287154B2
公开(公告)日：2022-03-29
申请号：US16692469
申请日：2019-11-22
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien , Peter A. Dorian
Abstract: A ducting system has a first upstream location is to be connected to a first source of air. A downstream location in the duct is to be connected to a second source of air. The upstream location has a first valve, and the downstream location has a second valve. An end location of the duct is to be connected to a sink. A control for the valves achieves a desired pressure and temperature of air at the end location. The first temperature sensor is located at a position intermediate the upstream location and the downstream location. A second temperature sensor is located at a position intermediate the downstream location and the end location. A control is programmed to determine the health of the first and second valves based upon a difference between temperatures sensed by the first and second sensors. An air use system and a method are also disclosed.
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公开(公告)号：US11047920B2
公开(公告)日：2021-06-29
申请号：US16373182
申请日：2019-04-02
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien , James A. Gosse
Abstract: Disclosed is a short detection system for an aircraft. The system includes a pair of alternating current sources defined by respective frequencies being offset by a predetermined value. The system includes a pair of sensor systems including respective measurement circuits coupled to respective sensor apparatuses to measure at least one parameter of an environment. The system includes an alternating current measurement system that includes a low pass filter having a cutoff frequency greater than the predetermined value such that a beat indicative of a difference between the respective frequencies passed through the pair of sensor systems is isolated by the low pass filter. The system indicates a short among the pair of sensor systems when the beat is present.
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公开(公告)号：US20210156745A1
公开(公告)日：2021-05-27
申请号：US16692402
申请日：2019-11-22
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien , Peter A. Dorian
IPC: G01K5/24
Abstract: A system has a first temperature sensor located at a first location. A second temperature sensor is located at a second location. A control is configured to determine a difference between voltages indicated of a temperature sensed by each of the first and second sensors. A method is also disclosed.
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公开(公告)号：US10987617B2
公开(公告)日：2021-04-27
申请号：US15091023
申请日：2016-04-05
Applicant: Hamilton Sundstrand Corporation
Inventor： Lubomir A. Ribarov , Richard J. Carpenter , Aaron V. Price , Gary M. McBrien , Aaron F. Rickis , Bryan V. Scala
Abstract: A filter assembly for a fluid flow system includes a filter housing, a housing inlet to allow the fluid flow into the filter housing and a housing outlet to allow the fluid flow to exit the filter housing. A filter element is located in the filter housing to collect contaminants from the fluid flow. A pressure sensor is located to measure a pressure drop across the filter element. The pressure sensor includes at least one sense line extending into an interior volume of the filter housing. A method of monitoring a filter assembly for a fluid flow system includes positioning a pressure sensor at a filter assembly, extending at least one sense line from the pressure sensor into an internal volume of a filter housing of the filter assembly, and measuring a pressure drop across a filter element of the filter assembly via the pressure sensor.
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公开(公告)号：US20200319239A1
公开(公告)日：2020-10-08
申请号：US16373182
申请日：2019-04-02
Applicant: Hamilton Sundstrand Corporation
Inventor： Gary M. McBrien , James A. Gosse
Abstract: Disclosed is a short detection system for an aircraft. The system includes a pair of alternating current sources defined by respective frequencies being offset by a predetermined value. The system includes a pair of sensor systems including respective measurement circuits coupled to respective sensor apparatuses to measure at least one parameter of an environment. The system includes an alternating current measurement system that includes a low pass filter having a cutoff frequency greater than the predetermined value such that a beat indicative of a difference between the respective frequencies passed through the pair of sensor systems is isolated by the low pass filter. The system indicates a short among the pair of sensor systems when the beat is present.
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