MASS-FLOW THROTTLE FOR LARGE NATURAL GAS ENGINES

    公开(公告)号:US20220136451A1

    公开(公告)日:2022-05-05

    申请号:US17434520

    申请日:2020-02-28

    Abstract: A mass-flow throttle for highly accurate control of gaseous supplies of fuel and/or air to the combustion chambers for a large engine in response to instantaneous demand signals from the engine's engine control module (ECM), especially for large spark-ignited internal combustion engines. With a unitary block assembly and a throttle blade driven by a non-articulated rotary actuator shaft, in combination with control circuitry including multiple pressure sensors as well as sensors for temperature and throttle position, the same basic throttle concepts are suited to be used for both mass-flow gas (MFG) and mass-flow air (MFA) throttles in industrial applications, to achieve highly accurate mass-flow control despite pressure fluctuations while operating in non-choked flow. The throttle, in combination with the sensors and ECM, enable detection of backfire events, with the throttle system further being enabled to take operative measures to prevent damage to the throttle components resulting from a backfire event.

    System and method for airport surface management

    公开(公告)号:US08554457B2

    公开(公告)日:2013-10-08

    申请号:US13236248

    申请日:2011-09-19

    CPC classification number: G08G5/06 G08G5/065

    Abstract: Described herein are systems and methods for surface management of an airport. One embodiment of the disclosure of this application is related to a method including receiving airport data from an airport network, receiving surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight. Another embodiment of the disclosure of this application is related to a system comprising a user interface displaying information related to flight plan data and airport data received from an airport network, and a surface management module receiving the airport data and surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight.

    System and Method for Predicting Aircraft Gate Arrival Times
    13.
    发明申请
    System and Method for Predicting Aircraft Gate Arrival Times 审中-公开
    预计飞机门到达时间的系统和方法

    公开(公告)号:US20130041575A1

    公开(公告)日:2013-02-14

    申请号:US13368947

    申请日:2012-02-08

    Applicant: James Cole

    Inventor: James Cole

    CPC classification number: G08G5/06

    Abstract: A system and method for receiving an estimated ON time for an aircraft, determining an estimated ON to IN time for the aircraft and determining an estimated gate arrival time for the aircraft based on the estimated ON time and the estimated ON to IN time. The system including a calculation engine for performing the steps of the calculation.

    Abstract translation: 一种用于接收飞行器的估计接通时间的系统和方法,确定飞机的估计的ON到IN时间,并且基于估计的接通时间和估计的ON到IN时间来确定飞行器的估计的门到达时间。 该系统包括用于执行计算步骤的计算引擎。

    System and Method for Airport Surface Management
    14.
    发明申请
    System and Method for Airport Surface Management 有权
    机场地面管理系统与方法

    公开(公告)号:US20120245836A1

    公开(公告)日:2012-09-27

    申请号:US13236248

    申请日:2011-09-19

    CPC classification number: G08G5/06 G08G5/065

    Abstract: Described herein are systems and methods for surface management of an airport. One embodiment of the disclosure of this application is related to a method including receiving airport data from an airport network, receiving surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight. Another embodiment of the disclosure of this application is related to a system comprising a user interface displaying information related to flight plan data and airport data received from an airport network, and a surface management module receiving the airport data and surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight.

    Abstract translation: 这里描述的是用于机场的表面管理的系统和方法。 本申请的公开的一个实施例涉及一种方法,包括从机场网络接收机场数据,接收机场区域的特定段的表面监视数据,基于机场数据和表面监视识别段内的预测冲突 数据和分配出租车时间段的航班。 该应用的公开的另一实施例涉及一种系统,其包括显示与飞行计划数据有关的信息的用户界面和从机场网络接收的机场数据的系统,以及接收机场数据和表面监视数据的表面管理模块, 机场区域,基于机场数据和表面监视数据来识别其中一个段内的预测冲突,以及为飞行分配出租车时隙。

    System and method for multi-stage tail number acquisition
    15.
    发明授权
    System and method for multi-stage tail number acquisition 有权
    多级尾号采集系统及方法

    公开(公告)号:US08145612B2

    公开(公告)日:2012-03-27

    申请号:US11590423

    申请日:2006-10-31

    CPC classification number: G06F17/30286

    Abstract: A system and method for receiving data on an aircraft, the data including a tail number of the aircraft, storing the data in a database, receiving a request including further data, the further data being related to the aircraft, querying the data in the database using the further data and returning the tail number of the aircraft.

    Abstract translation: 一种用于在飞行器上接收数据的系统和方法,所述数据包括飞行器的尾部号码,将数据存储在数据库中,接收包括进一步数据的请求,与飞机相关的另外的数据,查询数据库中的数据 使用进一步的数据并返回飞机的尾部号码。

    Flight track display system using data from a plurality of sources
    16.
    发明授权
    Flight track display system using data from a plurality of sources 有权
    使用来自多个源的数据的飞行轨迹显示系统

    公开(公告)号:US08068039B2

    公开(公告)日:2011-11-29

    申请号:US11226785

    申请日:2005-09-14

    CPC classification number: G01C23/005 G09B29/006

    Abstract: Described is a system and method for displaying flight track data. The system and method include a data feed arrangement to receive target data points from a first data source and a second data source, a data receiving arrangement correlating target data points from the first data source with corresponding target data points received from the second data source, the correlation being based on location and time information in the target data points, a data analyzing arrangement to analyze the target data points and correlated data points and store each target data point and correlating data point in a target flight record, the target flight record corresponding to a target aircraft, a data generation arrangement to generate a flight track for the target aircraft using the data stored in the target flight record, wherein the flight track includes a first portion generated from the first data source and a second portion generated from the correlated target data points and a data distribution arrangement to organize the flight track into a displayable file and distribute the file to users of the system, wherein the displayable file is displayed on a graphical user interface including the flight track information.

    Abstract translation: 描述了用于显示飞行轨迹数据的系统和方法。 该系统和方法包括从第一数据源和第二数据源接收目标数据点的数据馈送装置,将来自第一数据源的目标数据点与从第二数据源接收的相应目标数据点相关联的数据接收装置, 相关性基于目标数据点中的位置和时间信息,数据分析装置,用于分析目标数据点和相关数据点,并存储每个目标数据点并将目标飞行记录中的数据点相关联,目标飞行记录对应 使用存储在目标飞行记录中的数据为目标飞行器生成飞行轨迹的数据生成装置,其中飞行轨迹包括从第一数据源产生的第一部分和从相关联的第二部分生成的第二部分 目标数据点和数据分配安排,以将飞行轨迹组织成可显示的文件 e并将文件分发到系统的用户,其中可显示文件显示在包括航迹信息的图形用户界面上。

    ELECTRICAL CONNECTOR HAVING ALIGNMENT MECHANISM
    17.
    发明申请
    ELECTRICAL CONNECTOR HAVING ALIGNMENT MECHANISM 有权
    具有对准机构的电气连接器

    公开(公告)号:US20110256746A1

    公开(公告)日:2011-10-20

    申请号:US13081767

    申请日:2011-04-07

    CPC classification number: H01R13/53 H01R2101/00

    Abstract: An electrical connector assembly may include a connector body having a conductor receiving end and first and second connector ends formed substantially perpendicularly to an axial direction of the conductor receiving end. The connector body includes a first axial bore that communicates with each of a second axial bore and a third axial bore in the first and second connector ends, respectively. The electrical connector assembly may include a conductor spade assembly received in the first axial bore, wherein the conductor spade assembly includes a spade portion extending between the second axial bore and the third axial bore. A removeable contact may be received within the second axial bore to conductively engage the spade portion of the conductor spade assembly.

    Abstract translation: 电连接器组件可以包括具有导体接收端的连接器主体,以及基本上垂直于导体接收端的轴向方向形成的第一和第二连接器端。 连接器主体包括分别与第一和第二连接器端部中的第二轴向孔和第三轴向孔中的每一个连通的第一轴向孔。 电连接器组件可以包括容纳在第一轴向孔中的导体铲形组件,其中导体铲形组件包括在第二轴向孔和第三轴向孔之间延伸的铲形部分。 可以在第二轴向孔内容纳可移除的接触件以导电地接合导体铲形组件的铲形部分。

    SODIUM/MOLYBDENUM POWDER COMPACTS AND METHODS FOR PRODUCING THE SAME
    18.
    发明申请
    SODIUM/MOLYBDENUM POWDER COMPACTS AND METHODS FOR PRODUCING THE SAME 有权
    SODIUM / MOLYBDENUM POWDER COMPACTS AND METHODS FOR PRODUCTING THE SAME

    公开(公告)号:US20090188789A1

    公开(公告)日:2009-07-30

    申请号:US12392792

    申请日:2009-02-25

    Abstract: A method for producing a metal article according to one embodiment may include: Providing a supply of a sodium/molybdenum composite metal powder; compacting the sodium/molybdenum composite metal powder under sufficient pressure to form a preformed article; placing the preformed article in a sealed container; raising the temperature of the sealed container to a temperature that is lower than a sintering temperature of molybdenum; and subjecting the sealed container to an isostatic pressure for a time sufficient to increase the density of the article to at least about 90% of theoretical density.

    Abstract translation: 根据一个实施方案的金属制品的制造方法可以包括:提供钠/钼复合金属粉末; 在足够的压力下压制钠/钼复合金属粉末以形成预制制品; 将预制制品放置在密封容器中; 将密封容器的温度提高到低于钼的烧结温度的温度; 并将密封的容器经受等静压力足以将制品的密度增加至理论密度的至少约90%的时间。

    Ladle
    20.
    发明申请
    Ladle 有权
    钢包

    公开(公告)号:US20050206052A1

    公开(公告)日:2005-09-22

    申请号:US10803891

    申请日:2004-03-19

    CPC classification number: F27D1/0006

    Abstract: A liner for a ladle is formed of a body of refractory material defining a hollow interior which is bounded by a continuous sidewall. Within the interior is a barrier of refractory material which faces the interior surface of part of the sidewall and is spaced inwardly therefrom in the hollow interior of the body to define with said facing part of said sidewall a spout for discharging molten metal, in use, from the ladle. The barrier has two longitudinal edge surfaces received at two facing inner portions of the sidewall respectively which are extended inwardly. By providing these inward extensions the barrier can be positioned within the interior of the liner thereby obviating the need for an outward extension from the liner body to define a spout. This enables the liner to be used with ladle shells without the shell requiring modification to accommodate such an outward extension.

    Abstract translation: 用于钢包的衬里由限定由连续侧壁限定的中空内部的耐火材料体形成。 在内部是耐火材料的屏障,其面向侧壁的一部分的内表面并且在主体的中空内部中向内间隔开,以限定所述侧壁的所述面对部分,用于在使用中排出熔融金属的喷口, 从钢包。 屏障具有两个纵向边缘表面,其分别容纳在侧壁的两个相对的内部部分,其向内延伸。 通过设置这些向内的延伸部分,阻挡件可以定位在衬套的内部内,从而避免需要从衬套主体向外延伸以限定喷口。 这使得衬套能够与钢包壳一起使用,而壳体不需要修改以适应这种向外延伸。

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