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47 条记录 (耗时 0.015 秒)

    FUEL CUTOFF TESTING SYSTEM
    1.
    发明授权
    FUEL CUTOFF TESTING SYSTEM 有权
    燃料切断试验系统

    公开(公告)号：EP2974965B1

    公开(公告)日：2017-11-01

    申请号：EP15176775.3

    申请日：2015-07-15

    申请人： The Boeing Company

    发明人： McDONALD, Darren Gordon ,  WELSH, Bryan Douglas

    IPC分类号： B64D37/00 ,  B64F5/00 ,  F02C9/44

    CPC分类号： F02C9/26 ,  B64D37/005 ,  B64F5/60 ,  F01D21/20 ,  F02C9/44 ,  F05D2270/095 ,  F05D2270/12 ,  Y02T50/671

    摘要： A method and apparatus for controlling operation of an engine (226) in an aircraft (202). A time (244) when a cutoff speed (246) for the aircraft (202) will be reached at which a flow of fuel (224) is to be stopped is identified. A delay (248) between sending a command (250) to move a switch (214) to an off position (222) and the time (244) at which the engine (226) ceases operation is also identified. The command (250) is sent based on the predicted time (244) and the delay (248). The command (250) causes the switch (214) to move to the off position (222) moving a fuel control switch (238) for the engine (226) of the aircraft (202) to a shut off position (242) to stop the flow of fuel (224) to the engine (226).

    JET ENGINE, FLYING VEHICLE, AND METHOD FOR OPERATING JET ENGINE
    3.
    发明公开
    JET ENGINE, FLYING VEHICLE, AND METHOD FOR OPERATING JET ENGINE 审中-公开
    斯德哥尔摩，FLUGZEUG UND VERFAHREN ZUM BETRIEB EINES STRAHLTRIEBWERKS

    公开(公告)号：EP3098420A1

    公开(公告)日：2016-11-30

    申请号：EP15773405.4

    申请日：2015-02-18

    申请人： Mitsubishi Heavy Industries, Ltd.

    发明人： UENO, Yoshihiko ,  FURUYA, Shojiro

    IPC分类号： F02C9/28 ,  B64D33/02 ,  F02C7/228 ,  F02C7/232 ,  F02C9/44 ,  F02K7/18 ,  F23R3/28

    CPC分类号： F02C9/32 ,  B64D33/02 ,  F02C7/04 ,  F02C7/222 ,  F02C7/232 ,  F02C9/44 ,  F02K7/00 ,  F02K7/14 ,  F02K7/18 ,  F05D2220/323 ,  F05D2220/80 ,  F05D2240/35 ,  F05D2250/90 ,  F05D2270/306 ,  F23N1/002 ,  F23N2037/02 ,  F23N2037/10 ,  F23N2041/20 ,  F23R3/28

    摘要： A jet engine has an inlet which takes in air, a combustor (12) which combusts fuel by using the air, and a fuel control section (37) which controls supply of the fuel. The combustor (12) has a fuel supplying section (22) which supplies the fuel, injectors (20) which inject the fuel. Each injector (20) contains openings (30-1 to 30-5) which inject the fuel. The fuel supplying section (22) supplies the fuel to the injector (20) in a flow rate according to a command of an autopilot. The fuel control section (37) controls the injectors (20) such that the number of the openings (30) which inject the fuel or flow-path cross-section areas of the pipes which send the fuel in case of the low-speed is more than the number of the openings (30) which inject the fuel or the flow-path cross-section areas of the pipes which send the fuel in case of the high-speed.

    摘要翻译： 喷气发动机具有吸入空气的入口，利用空气燃烧燃料的燃烧器（12）和控制燃料供给的燃料控制部（37）。 燃烧器（12）具有供给燃料的燃料供给部（22），喷射燃料的喷射器（20）。 每个喷射器（20）包含喷射燃料的开口（30-1至30-5）。 燃料供给部（22）根据自动驾驶员的指令，以流量将燃料供给到喷射器（20）。 燃料控制部（37）控制喷射器（20），使得在低速的情况下喷射发送燃料的管道的燃料或流路横截面积的开口（30）的数量为 大于喷射燃料的开口（30）的数量或在高速情况下发送燃料的管道的流路横截面积的数量。

    Methods for controlling fuel mixing
    5.
    发明公开
    Methods for controlling fuel mixing 有权
    一种用于控制将燃料混合物的方法

    公开(公告)号：EP2333280A3

    公开(公告)日：2014-05-21

    申请号：EP10191494.3

    申请日：2010-11-17

    申请人： General Electric Company

    发明人： Loeven II, Robert J.

    IPC分类号： F02C7/22 ,  F02C9/40 ,  F02C9/44 ,  F23R3/36

    CPC分类号： F02C7/22 ,  F02C9/40 ,  F02C9/44 ,  F23K2900/05004 ,  F23N1/002 ,  F23N2021/10 ,  F23N2037/08 ,  F23R3/36 ,  F23R2900/00002

    摘要： Methods (200) for controlling fuel mixing are provided. One or more parameters associated with the operation of a machine configured to receive a combined fuel is identified. A fuel flow of the combined fuel that is provided to the machine may be determined. Based at least in part on the identified parameters, a ratio of a first fuel type (105) included in the combined fuel to the determined fuel flow may be determined. The first fuel type may have a heating value that is greater than a second fuel type (110) included in the combined fuel. A flow of the first fuel type may be set based at least in part on the ratio. Subsequent to setting the flow of the first fuel type, an energy content of the fuel flow of the combined fuel may be determined, and the flow of the first fuel type may be adjusted based at least in part on the determined energy content.

    Method and Systems for Virtual Sensor Selection and Blending
    7.
    发明公开
    Method and Systems for Virtual Sensor Selection and Blending 有权
    Verfahren und Systeme zur virtuellen Sensorauswahl und Mischung

    公开(公告)号：EP2239441A2

    公开(公告)日：2010-10-13

    申请号：EP10151889.2

    申请日：2010-01-28

    申请人： General Electric Company

    发明人： Nestico, Brian Francis ,  Adibhatla, Sridhar ,  Gutz, David Allen ,  Viassolo, Daniel Edgardo

    IPC分类号： F02C9/28 ,  F02C9/44

    CPC分类号： F02C9/28 ,  F02C9/00 ,  F02C9/44 ,  F05D2270/30 ,  F05D2270/301 ,  F05D2270/3011 ,  F05D2270/3013 ,  F05D2270/303 ,  F05D2270/304 ,  F05D2270/44 ,  G05B17/02 ,  Y02T50/671

    摘要： An engine control system (200) for a vehicle propulsion system includes a plurality of engine model modules (215,216,217) executing independently and programmed to receive engine operating condition values from a plurality of sensors (302) positioned on an engine, each of the plurality of engine model modules programmed to determine an estimate of a process parameter of a location in the engine where at least one of a sensor for the process parameter is not available, a sensor for the process parameter is not present at the location, a sensor at the location has failed, and a sensor at the location is determined to be inaccurate, an estimate source selector configured to determine model blending factors (318), and a model blending module (322) configured to determine an estimated virtual sensor value using the determined estimates from at least two of the plurality of engine model modules and the model blending factors.

    摘要翻译： 用于车辆推进系统的发动机控制系统（200）包括多个发动机模型模块（215,216,217），其独立执行并被编程以从位于发动机上的多个传感器（302）接收发动机操作状态值， 发动机模型模块被编程以确定发动机中的位置的过程参数的估计，其中用于过程参数的传感器中的至少一个不可用，用于过程参数的传感器不存在于位置处，传感器处于 位置已经失败，并且位置处的传感器被确定为不准确，被配置为确定模型混合因子（318）的估计源选择器和被配置为使用所确定的估计值来确定估计的虚拟传感器值的模型混合模块（322） 来自多个发动机模型模块中的至少两个和模型混合因子。

    Aircraft takeoff
    8.
    发明公开
    Aircraft takeoff 有权
    Flugzeugstart

    公开(公告)号：EP1616788A3

    公开(公告)日：2009-01-14

    申请号：EP05253647.1

    申请日：2005-06-14

    申请人： ROLLS-ROYCE PLC

    发明人： Brown, Stephen Geoffrey

    IPC分类号： B64D45/00 ,  B64D31/00 ,  F02C9/00

    CPC分类号： F02C9/44 ,  B64C19/00 ,  B64D31/00

    摘要： The present invention provides a method of operating an aircraft whereby actual acceleration of an aircraft is used as the direct measure of the capability of the aircraft to takeoff. Thus, a minimum takeoff acceleration is determined for an aircraft and then through appropriate sensing means for acceleration, actual acceleration of the aircraft is determined and compared with that predetermined minimum takeoff acceleration. If the actual aircraft acceleration exceeds the minimum takeoff acceleration then an indication such as a buzzer or signal is provided. The present method may also be used in cooperation with existing takeoff determining systems utilising engine thrust as the means of determining aircraft capability to takeoff. The authority of the various aircraft takeoff criteria can be adjusted as required. Furthermore, the present aircraft acceleration regime may be utilised with regard to adjusting existing engine thrust means for determining takeoff or cruise capability.