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    • 1. 发明授权
    • Aircraft-engine trend monitoring system
    • 飞机发动机趋势监测系统
    • US07979192B2
    • 2011-07-12
    • US11693834
    • 2007-03-30
    • Brian D. MorrisonStephan A. HanveyRonald E. Wilkinson
    • Brian D. MorrisonStephan A. HanveyRonald E. Wilkinson
    • G01C23/00
    • F02D41/22G05B23/0232G07C5/085Y02T10/40
    • Methods and systems for aircraft engine trend monitoring include periodically recording the outputs of engine-condition sensors and analyzing the results to examine piston-engine performance trends and predict the need for engine maintenance. Various analyses can be performed, separately or in parallel, including comparing the current parameter values with values recorded for that parameter in previous instances of similar operating conditions; comparing parameter values to predetermined nominal ranges; and detecting parameter values that exhibit trends over time that if followed would result in out-of-bound readings. Sensed parameter values can also be used to detect when recommended engine operating conditions are being exceeded. By using the results of the analyses to inform engine maintenance scheduling and provide alerts to the pilot and maintenance staff regarding recommended engine performance trends and/or operating condition exceedances, the methods and systems contribute to enhancing the level of safety that can be achieved despite significant maintenance-budget reductions.
    • 飞机发动机趋势监测的方法和系统包括定期记录发动机状态传感器的输出并分析结果,以检查活塞发动机性能趋势并预测发动机维护的需要。 可以单独地或并行地执行各种分析,包括将当前参数值与在先前相似操作条件下的该参数记录的值进行比较; 将参数值与预定的标称范围进行比较; 并检测出随时间呈现趋势的参数值,如果遵循,将导致超限读数。 传感参数值也可用于检测何时超过推荐的发动机工作条件。 通过使用分析结果来通知发动机维护计划,并向飞行员和维护人员提供关于推荐的发动机性能趋势和/或运行状况超标的警报,该方法和系统有助于提高尽可能实现的安全性水平 维护预算削减。
    • 3. 发明授权
    • Electro-statically-shielded processing module
    • US06600972B2
    • 2003-07-29
    • US10039044
    • 2002-01-03
    • Brian D. MorrisonPaul A. Connolly
    • Brian D. MorrisonPaul A. Connolly
    • G05D1100
    • G05D9/12G01F23/0069G01F23/263G01F23/266
    • A fuel measuring system includes a package adapted for mounting to a fuel storage vessel. The package includes an electro-statically shielded enclosure. A processor element is disposed in the enclosure and is adapted for coupling to a fuel sensor disposed in the storage vessel. A communication interface is provided for coupling data through the enclosure between the processor and a processor external to the package through a dielectric transmission media passing through the enclosure. A power supply for the processor element disposed in the enclosure, such power supply being adapted to generate power for the processing element in response to input energy. An energy interface is provided for coupling the input energy from a source external to the enclosure through dielectric transmission media passing through the enclosure. With such an arrangement both data to the electro-statically shielded processor and energy to the electro-statically shielded power supply are coupled to the electro-statically shielded enclosure through dielectric media. Therefore, electrical disturbances external to the enclosure will not be carried by conductive wires into the enclosure and then into the fuel tank which might thereby cause a hazardous condition in the fuel in the tank.
    • 6. 发明授权
    • Electro-statically shielded processing module
    • 静电屏蔽处理模块
    • US06356809B1
    • 2002-03-12
    • US09330405
    • 1999-06-11
    • Brian D. MorrisonPaul A. Connolly
    • Brian D. MorrisonPaul A. Connolly
    • G05D1100
    • G05D9/12G01F23/0069G01F23/263G01F23/266
    • A fuel measuring system includes a package adapted for mounting to a fuel storage vessel. The package includes an electro-statically shielded enclosure. A processor element is disposed in the enclosure and is adapted for coupling to a fuel sensor disposed in the storage vessel. A communication interface is provided for coupling data through the enclosure between the processor and a processor external to the package through a dielectric transmission media passing through the enclosure. A power supply for the processor element disposed in the enclosure, such power supply being adapted to generate power for the processing element in response to input energy. An energy interface is provided for coupling the input energy from a source external to the enclosure through dielectric transmission media passing through the enclosure. With such an arrangement both data to the electro-statically shielded processor and energy to the electro-statically shield power supply are coupled to the electro-statically shielded enclosure though dielectric media. Therefore, electrical disturbances external to the enclosure will not be carried by conductive wires into the enclosure and then into the fuel tank which might thereby cause a hazardous condition in the fuel in the tank.
    • 燃料测量系统包括适于安装到燃料储存容器的包装。 该包装包括一个静电屏蔽的外壳。 处理器元件设置在外壳中并且适于联接到设置在存储容器中的燃料传感器。 提供通信接口,用于通过穿过外壳的电介质传输介质将数据通过外壳之间的数据耦合到处理器与处理器外部的处理器之间。 一种用于设置在外壳中的处理器元件的电源,该电源适于响应于输入能量而产生用于处理元件的功率。 提供能量接口,用于通过介质传输介质通过外壳将输入能量从外部的外部源耦合到外壳。 通过这样的布置,电静电屏蔽处理器的数据和电静电屏蔽电源的能量通过介电介质耦合到静电屏蔽的外壳。 因此,外壳外部的电气干扰将不会被导线进入外壳,而是进入燃料箱,从而可能导致油箱内的燃油中的危险状况。
    • 9. 发明授权
    • Optical ring architecture
    • 光环架构
    • US07657330B2
    • 2010-02-02
    • US10373272
    • 2003-02-24
    • Brian D. Morrison
    • Brian D. Morrison
    • H04B10/20G02F1/00H04J14/00
    • G01F23/266G01F23/0069G01F23/263G05D9/12H04L12/437
    • A system and method for providing a network that includes at least two microprocessor-controlled devices that include a first microprocessor-controlled device and a distinct second microprocessor-controlled device, and at least two bi-directional fiber optic cables to provide a communicative ring amongst the at least two microprocessor controlled devices by connecting the at least two microprocessor-controlled devices in a daisy-chain, where the first microprocessor-controlled device and the distinct second microprocessor-controlled device communicate via at least two of the bi-directional fiber optic cables.
    • 一种用于提供包括至少两个微处理器控制的设备的网络的系统和方法,所述设备包括第一微处理器控制的设备和不同的第二微处理器控制的设备,以及至少两个双向光纤电缆,以在 所述至少两个微处理器控制的设备通过以菊链形式连接所述至少两个微处理器控制的设备,其中所述第一微处理器控制的设备和所述不同的第二微处理器控制设备经由所述双向光纤 电缆
    • 10. 发明授权
    • Controlled impedance connector
    • 受控阻抗连接器
    • US4895523A
    • 1990-01-23
    • US268146
    • 1988-11-07
    • Brian D. MorrisonJack J. Rosenberg
    • Brian D. MorrisonJack J. Rosenberg
    • H01R12/71H05K1/02H05K3/32H05K3/36
    • H01R12/714H05K1/0218H05K3/325H05K3/361
    • A very high density, multiple contact connector has low-inductance power and ground planes and gold dot contacts for providing a controlled impedance environment to a module assembly by minimizing undesirable effects such as ground-noise and reflections while assuring operation at interconnect bandwidths up to 6 GHz. The controlled impedance connector connects two printed wiring boards (PWBs) comprising surface mounted devices to a motherboard. The PWBs are bonded to opposite sides of a central heat frame. The connector has two flexible circuits containing a total of 460 gold dot signal connections plus a plurality of separate gold dot power and ground connections. Signal runs between the PWBs and the connector flexible circuits are interconnected using copper fingers soldered to pads on the PWBs. Power and ground planes connect to the PWBs via gold dot contacts on the inside of the flexible circuit surface to pads on the PWBs. The connector is a true zero insertion force design. A clamping mechanism comprising jacking screws pulls the spring-loaded gold dots on the flexible circuit of the connector against the pads on a motherboard. A clamping force of 200 pounds is used to achieve the required connector to motherboard interconnect pressure.
    • 非常高密度的多接触连接器具有低电感功率和接地平面以及金点触点,用于通过最小化诸如接地噪声和反射的不期望的影响,同时确保在互连带宽高达6处工作,从而为模块组件提供受控的阻抗环境 GHz。 受控阻抗连接器将包括表面安装设备的两个印刷电路板(PWB)连接到主板。 PWB结合到中央加热框架的相对侧。 该连接器具有两个柔性电路,其中包含总共460个金点信号连接以及多个单独的金点电源和接地连接。 在PWB和连接器柔性电路之间的信号连接使用焊接到PWB上的焊盘的铜指互连。 电源和接地层通过柔性电路表面内部的金点触点连接到PWB上的PWB上的焊盘。 连接器是真正的零插入力设计。 包括顶起螺钉的夹紧机构将连接器的柔性电路上的弹簧加载的金点拉到主板上的焊盘上。 使用200磅的夹紧力来实现主板互连压力所需的连接器。