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    • 1. 发明授权
    • Engine fuel control system and method
    • 发动机燃油控制系统及方法
    • US6148601A
    • 2000-11-21
    • US75130
    • 1998-05-08
    • Anthony Charles JonesMark M. HarrisDavid R. RipleyMalcolm J. McArthur
    • Anthony Charles JonesMark M. HarrisDavid R. RipleyMalcolm J. McArthur
    • F02C9/26F02C9/28
    • F02C9/263F02C9/28
    • Accuracy and predictability are provided in a fuel control system for an engine system including a fuel supply and a combustion chamber. The fuel control system includes at least one fuel injector having a calibrated nozzle to direct a fuel flow from the fuel supply into the combustion chamber of the engine, a servo valve connected between the fuel supply and the calibrated nozzle to meter the fuel flow from the fuel supply to the calibrated nozzle, a pressure transducer operably associated with the calibrated nozzle to measure a pressure drop in the fuel flow across the calibrated nozzle, and a controller operably associated with the pressure transducer and the servo valve to control the metering of the fuel flow by the servo valve. The calibrated nozzle has a known fuel flow vs. pressure drop characteristic. The controller controls the metering of the fuel flow by the servo valve based on the pressure drop measured by the pressure transducer and the known fuel flow vs. pressure drop characteristic of the calibrated nozzle.
    • 在包括燃料供应和燃烧室的发动机系统的燃料控制系统中提供了精度和可预测性。 燃料控制系统包括至少一个具有校准喷嘴的燃料喷射器,用于将来自燃料供应的燃料流引导到发动机的燃烧室中,连接在燃料供应和校准喷嘴之间的伺服阀, 燃料供应到校准喷嘴,与校准喷嘴可操作地相关联的压力传感器,以测量穿过校准喷嘴的燃料流中的压降;以及与压力传感器和伺服阀可操作地相关联以控制燃料计量的控制器 由伺服阀流动。 校准喷嘴具有已知的燃料流量对压降特性。 控制器基于由压力传感器测量的压降和已知的燃料流量对校准喷嘴的压降特性来控制由伺服阀计量燃料流量的计量。
    • 2. 发明授权
    • Turbojet engine lubrication system
    • 涡轮喷气发动机润滑系统
    • US07216473B1
    • 2007-05-15
    • US09350552
    • 1999-07-09
    • Malcolm J. McArthurAnthony C. Jones
    • Malcolm J. McArthurAnthony C. Jones
    • F02C7/06
    • F01D25/18
    • A lubrication system for an expendable gas turbine engine (20) having a rotatable shaft (26) is provided. Bearings (28) journal the shaft (26) for rotation about an axis. The system includes a vessel (46) for containing lubricating oil, a conduit (58) extending from the vessel (46) to the bearings (28), and a solenoid operated valve (70,76) in the conduit (58) and operable to only either fully open or fully closed. A control circuit (16) is provided for pulsing the solenoid (70) at a controlled rate to alternatingly (a) allow oil flow and (b) halt oil flow to the bearings (28) for a time insufficient to cause oil starvation of the bearings (28).
    • 提供了一种具有可旋转轴(26)的消耗式燃气涡轮发动机(20)的润滑系统。 轴承(28)使轴(26)轴颈旋转。 该系统包括用于容纳润滑油的容器(46),从容器(46)延伸到轴承(28)的导管(58)以及导管(58)中的电磁阀(70,76),并可操作 只能完全打开或完全关闭。 提供控制电路(16),用于以受控的速率脉动螺线管(70),以交替地(a)允许油流动,和(b)停止油流到轴承(28)一段不足以引起油不足的时间 轴承(28)。
    • 5. 发明授权
    • Multiple parameter sensor and method of operation thereof
    • 多参数传感器及其操作方法
    • US5747680A
    • 1998-05-05
    • US630572
    • 1996-04-10
    • Malcolm J. McArthur
    • Malcolm J. McArthur
    • F01D17/02G01D5/20G01D21/02G01M15/00
    • F01D17/02G01D21/02G01D5/2013F05D2220/30F05D2220/50
    • A multiple parameter sensor is disclosed having a preferred application in a turbine used in an auxiliary power unit. The multiple parameter sensor includes a first part (12) for rotation with a rotating member (14) having a speed of rotation to be measured; a second part (20) mounted in a fixed position adjacent the first part to respond to the speed of rotation of the first part to produce a first periodic signal (22), the second part in response to the first periodic signal producing a second signal representing the speed of rotation of the rotating member and comprising electrical winding (26) in which the first periodic signal is magnetically induced by rotation of the first part with the rotating member; and wherein the second part produces at least one additional signal with each additional signal representing one additional parameter of operation of the device associated with the rotating member.
    • 公开了一种在辅助动力单元中使用的涡轮机中具有优选应用的多参数传感器。 多参数传感器包括用于与具有要测量的旋转速度的旋转构件(14)一起旋转的第一部分(12) 安装在与所述第一部分相邻的固定位置以响应所述第一部分的旋转速度以产生第一周期性信号(22)的第二部分(20),所述第二部分响应于所述第一周期性信号产生第二信号 代表旋转构件的旋转速度并且包括电绕组(26),其中第一周期信号由第一部分与旋转构件的旋转磁力引起; 并且其中所述第二部分产生至少一个附加信号,其中每个附加信号表示与所述旋转部件相关联的装置的操作的一个附加参数。
    • 7. 发明授权
    • Power unit fuel pressurization system
    • 动力装置燃油加压系统
    • US5184458A
    • 1993-02-09
    • US439684
    • 1989-11-21
    • Steven W. LampeMalcolm J. McArthur
    • Steven W. LampeMalcolm J. McArthur
    • B64D41/00F02C7/272F02C7/277F02C7/32
    • F02C7/32B64D41/00F02C7/272F02C7/277F05D2220/50F05D2260/4023Y02T50/44Y02T50/671
    • A power generating unit in accordance with the present invention comprises a pressurized gas source (44) providing pressurized gas containing oxygen to be used in combustion of a fuel; a combustor (42) for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply (48); a first turbine (68) driven by pressurized gas produced by the combustor; a gear box (70) driven by the turbine having an output shaft (72); a fuel pump (46) disposed within the fuel supply having a pair of input shafts (64 and 76) for providing pressurized fuel to the combustor in response to rotation of either of the input shafts; a motor (58) coupled to the pressurized gas source having a drive shaft (60) which rotates in response to the pressurized gas applied from the gas source; and a coupling mechanism (62 and 74), coupled to the shafts, for applying driving torque to the fuel pump during rotation of the pressurized gas to the combustor from the input shaft which is rotating at a higher velocity.
    • 根据本发明的发电单元包括加压气体源(44),其提供用于燃料燃烧的含氧的加压气体; 燃烧器(42),用于通过由加压气体源提供给燃烧器的加压气体的混合物燃烧产生的加压气体和通过燃料供给装置(48)提供给燃烧器的燃料; 由燃烧器产生的加压气体驱动的第一涡轮机(68); 由所述涡轮机驱动的齿轮箱(70)具有输出轴(72); 设置在燃料供给装置内的燃料泵(46)具有一对输入轴(64和76),用于响应于任一个输入轴的转动而向燃烧器提供加压燃料; 耦合到加压气体源的马达(58)具有响应于从气体源施加的加压气体而旋转的驱动轴(60); 以及联接到所述轴的联接机构(62和74),用于在从所述输入轴以更高速度旋转的状态下将所述加压气体旋转到所述燃烧器期间向所述燃料泵施加驱动扭矩。
    • 8. 发明授权
    • Fluid control valve for a hydraulic system operating with variable
viscosity, contaminated, fluid
    • 用于液压系统的流体控制阀,其操作具有可变的粘度,被污染的流体
    • US5499650A
    • 1996-03-19
    • US335272
    • 1994-11-07
    • Malcolm J. McArthurHarvey Jansen
    • Malcolm J. McArthurHarvey Jansen
    • G05D16/20
    • G05D16/2093Y10T137/2409Y10T137/2607Y10T137/7737Y10T137/86574Y10T137/86622Y10T137/86855
    • Problems such as slow frequency response and low reliability when operating with contaminated fluids of variable viscosity are alleviated in a low pressure hydraulic system (10) which utilizes a single stage, electro-hydraulic, clevis-type pressure control valve (40). The valve (40)includes a control piston (106) referenced to a control pressure within a control pressure cavity (60) to provide a feedback of control pressure which converts the valve (40) from an integral to a proportional control device, thereby enhancing stability of the hydraulic system (10). Compensation for changes in fluid viscosity, as a result of changes in fluid temperature, is provided by fabricating a bifurcated portion (98) and/or a metering bridge portion (62) of the valve (10) from materials having dissimilar coefficients of thermal expansion. Exemplary embodiments of a hydraulic system (10) suitable for use in either vehicular or stationary applications involving pressure actuated devices, such as a clutch (16), automatic transmissions or anti-lock brakes, are provided.
    • 在使用单级电液式U形夹式压力控制阀(40)的低压液压系统(10)中,减轻了在具有可变粘度的污染流体的情况下操作时的频率响应慢和可靠性低的问题。 阀(40)包括以控制压力腔(60)内的控制压力的控制活塞(106),以提供将阀(40)从积分转换成比例控制装置的控制压力的反馈,由此增强 液压系统(10)的稳定性。 通过从具有不同热膨胀系数的材料制造阀(10)的分叉部分(98)和/或计量桥接部分(62)来提供由于流体温度变化而导致的流体粘度变化的补偿 。 提供了适用于涉及压力致动装置(例如离合器(16)),自动变速器或防抱死制动器的车辆或固定应用中的液压系统(10)的示例性实施例。
    • 9. 发明授权
    • Cooling system for auxiliary power unit
    • 辅助动力装置冷却系统
    • US5105875A
    • 1992-04-21
    • US639292
    • 1991-01-10
    • Malcolm J. McArthur
    • Malcolm J. McArthur
    • H05K7/20
    • H05K7/20927
    • A cooling system which utilizes a lubricant for lubricating moving components within the system and a combustible fuel which is to be combusted within the system includes a first circuit (19) which contains at least one circuit element and which operates within a first range of temperatures, a second circuit (21) which contains at least one circuit element and which operates within a second range of temperatures which is lower than the first range of temperatures at which the first circuit operates, a lubricant flow path (25) located adjacent the first circuit for cooling the first circuit by providing a heat flow path between the lubricant and the first circuit when the lubricant is disposed within the lubricant flow path, and a combustible fuel flow path (23) located adjacent the second circuit for cooling the second circuit by providing a heat flow path between the combustible fuel and the second circuit when the combustible fuel is disposed within the combustible fuel flow path. A method associated with the cooling system involves the steps of providing a heat flow path between the first circuit and the lubricant in order to cool the first circuit, and providing a heat flow path between the second circuit and the combustible fuel in order to cool the second circuit.
    • 利用润滑剂来润滑系统内的运动部件的冷却系统和在系统内要燃烧的可燃燃料包括:第一回路(19),其包含至少一个电路元件,并在第一温度范围内运行, 包含至少一个电路元件并且在低于第一电路工作的第一温度范围的第二温度范围内工作的第二电路(21),位于第一电路附近的润滑剂流路(25) 通过在所述润滑剂设置在所述润滑剂流动路径内时在所述润滑剂和所述第一回路之间设置热流路径来冷却所述第一回路;以及位于所述第二回路附近的可燃燃料流路(23),用于通过提供第 当可燃燃料设置在可燃燃料流动路径内时,可燃燃料和第二回路之间的热流路径。 与冷却系统相关联的方法包括以下步骤:在第一回路和润滑剂之间提供热流路,以冷却第一回路,并且在第二回路和可燃燃料之间提供热流路径,以便冷却 第二电路。
    • 10. 发明授权
    • Emergency power unit oxidizing gas bottle heating apparatus
    • 应急动力装置氧化气瓶加热装置
    • US5020317A
    • 1991-06-04
    • US394544
    • 1989-08-16
    • Malcolm J. McArthur
    • Malcolm J. McArthur
    • B64D41/00
    • B64D41/00F05B2220/50
    • An emergency power unit for providing emergency on board power to an aircraft having apparatus for heating the oxidizing gas contained in the oxidizing gas bottle includes a fuel supply source (14) for supplying fuel, and oxidizing gas bottle (12) containing pressurized oxidizing gas, an oxidizing gas heating device (18) and (20) for heating the pressurized oxidizing gas within the oxidizing gas bottle (12) by using heat energy generated by a combustor (16) wherein the combustor (16) causes combustion of a mixture of fuel and oxidizing gas heated by the oxidizing gas heating device (18) and (20). Hot gases resulting from the combustion of the mixture of fuel and heated oxidizing gas drive the blades of a turbine (32) thereby producing emergency on board power to the aricraft.
    • 一种用于向具有用于加热氧化气体瓶中包含的氧化气体的装置的飞行器提供紧急电力的应急动力单元包括用于供应燃料的燃料供应源(14)和包含加压氧化气体的氧化气瓶(12) 氧化气体加热装置(18)和(20),用于通过使用由燃烧器(16)产生的热能来加热氧化气体瓶(12)内的加压氧化气体,其中燃烧器(16)引起燃料混合物燃烧 和由氧化气体加热装置(18)和(20)加热的氧化气体。 由燃料和加热的氧化气体的混合物的燃烧产生的热气体驱动涡轮机(32)的叶片,由此产生对工艺品的紧急电力。