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1.发明授权Method and a device for detecting an electrical failure affecting an electric control system of a hydraulic actuator of variable geometries of an aeroengine 有权用于检测影响航空发动机的可变几何形状的液压致动器的电气控制系统的电气故障的方法和装置公开(公告)号：US09116518B2
公开(公告)日：2015-08-25
申请号：US13069999
申请日：2011-03-23
CPC分类号： G05B23/0235 , G05B9/03
摘要： After the control system has been started, which system has two control paths that are used as alternatives for delivering a control electric current to an electrohydraulic member for transforming said current into hydraulic power that is delivered to the actuator, and before powering a starter-generator of the engine, the detection method comprises implementing the following steps for each of the control paths in succession: delivering a predetermined test electric current over said path; evaluating a difference between the test electric current and a measurement of the electric current as transformed into hydraulic power by the electrohydraulic member; and if said difference is greater than a predefined threshold, detecting an electrical failure on said path.
摘要翻译： 在控制系统已经启动之后，哪个系统具有两个控制路径，作为用于将控制电流传递到电动液压构件的替代方案，用于将所述电流转换成输送到致动器的液压动力，并且在起动发电机 所述检测方法包括对所述控制路径中的每一个依次执行以下步骤：在所述路径上传送预定的测试电流; 评估由电动液压构件转换为液压动力的测试电流和电流测量值之间的差异; 并且如果所述差值大于预定阈值，则检测所述路径上的电气故障。
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2.发明授权Method and a device for real time monitoring of a system for measuring a fuel flow rate 有权用于实时监测用于测量燃料流量的系统的方法和装置公开(公告)号：US09021854B2
公开(公告)日：2015-05-05
申请号：US13511816
申请日：2010-11-26
CPC分类号： G01F25/0007 , F02C9/28 , F02D41/222 , F02D2200/0614 , G01F1/82
摘要： A device and method of monitoring the measurement of a fuel flow rate fed to an airplane engine includes delivering the measurement from a mass flowmeter. The monitoring also includes evaluating whether at least the following conditions are satisfied: a signal delivered by the flowmeter is less than a given value; and the engine is running on its own. The measurement is invalidated if these conditions are satisfied simultaneously.
摘要翻译： 监测馈送到飞机发动机的燃料流量的测量的装置和方法包括从质量流量计输送测量值。 监测还包括评估是否满足以下条件：由流量计传递的信号小于给定值; 发动机自身运行。 如果同时满足这些条件，则测量无效。
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3.发明申请METHOD AND A DEVICE FOR REAL TIME MONITORING OF A SYSTEM FOR MEASURING A FUEL FLOW RATE 有权用于实时监测燃料流量的系统的方法和装置公开(公告)号：US20120272710A1
公开(公告)日：2012-11-01
申请号：US13511816
申请日：2010-11-26
IPC分类号： G01F25/00
CPC分类号： G01F25/0007 , F02C9/28 , F02D41/222 , F02D2200/0614 , G01F1/82
摘要： A device and method of monitoring the measurement of a fuel flow rate fed to an airplane engine includes delivering the measurement from a mass flowmeter. The monitoring also includes evaluating whether at least the following conditions are satisfied: a signal delivered by the flowmeter is less than a given value; and the engine is running on its own. The measurement is invalidated if these conditions are satisfied simultaneously.
摘要翻译： 监测馈送到飞机发动机的燃料流量的测量的装置和方法包括从质量流量计输送测量值。 监测还包括评估是否满足以下条件：由流量计传递的信号小于给定值; 发动机自身运行。 如果同时满足这些条件，则测量无效。
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4.发明申请METHOD OF TESTING A SYSTEM FOR PROTECTING A TURBOMACHINE AGAINST OVERSPEED WHILE STARTING 有权测试在起动过程中保护涡轮调制剂的系统的方法公开(公告)号：US20120085101A1
公开(公告)日：2012-04-12
申请号：US13377225
申请日：2010-06-02
IPC分类号： F02C9/28
CPC分类号： F01D21/003 , F01D21/02 , F01D21/20 , F05D2270/021
摘要： In a testing overspeed protection system: a) on receiving an order to start a turbomachine, an electronic regulation system (ERS) of the turbomachine sends an order to a control circuit of a fuel cutoff member to close the fuel cutoff member or to keep it in the closed position; b) the closed state of the FCM is verified on the basis of information transmitted to the ERS and representative of the position of the FCM; c) if the result of the verification in b) is positive, the ERS sends an order to the FCM control circuit to authorize opening of the FCM and enable the starting procedure to continue; and d) if the result of the verification in b) is negative, the ERS issues fault information concerning the overspeed protection system.
摘要翻译： 在测试超速保护系统中：a）在接收到启动涡轮机的命令时，涡轮机的电子调节系统（ERS）向燃料切断构件的控制电路发送命令以关闭燃料切断构件或保持 处于关闭状态; b）FCM的关闭状态是根据发送给ERS的信息并代表FCM的位置进行验证的; c）如果b）中的验证结果为正，则ERS向FCM控制电路发送命令以授权开启FCM并使启动过程继续; 和d）如果b）中的验证结果为否定，则ERS会发出有关超速保护系统的故障信息。
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5.发明授权Method of testing a system for protecting a turbomachine against overspeed while starting 有权在起动时测试涡轮机械防止超速的系统的方法公开(公告)号：US08925329B2
公开(公告)日：2015-01-06
申请号：US13377225
申请日：2010-06-02
CPC分类号： F01D21/003 , F01D21/02 , F01D21/20 , F05D2270/021
摘要： In a testing overspeed protection system: a) on receiving an order to start a turbomachine, an electronic regulation system (ERS) of the turbomachine sends an order to a control circuit of a fuel cutoff member to close the fuel cutoff member or to keep it in the closed position; b) the closed state of the FCM is verified on the basis of information transmitted to the ERS and representative of the position of the FCM; c) if the result of the verification in b) is positive, the ERS sends an order to the FCM control circuit to authorize opening of the FCM and enable the starting procedure to continue; and d) if the result of the verification in b) is negative, the ERS issues fault information concerning the overspeed protection system.
摘要翻译： 在测试超速保护系统中：a）在接收到启动涡轮机的命令时，涡轮机的电子调节系统（ERS）向燃料切断构件的控制电路发送命令以关闭燃料切断构件或保持 处于关闭状态; b）FCM的关闭状态是根据发送给ERS的信息进行验证的，并代表FCM的位置; c）如果b）中的验证结果为正，则ERS向FCM控制电路发送命令以授权开启FCM并使启动过程继续; 和d）如果b）中的验证结果为否定，则ERS会发出有关超速保护系统的故障信息。
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公开(公告)号：US09021870B2
公开(公告)日：2015-05-05
申请号：US14003391
申请日：2012-02-24
CPC分类号： G01M15/14 , F15B9/09 , F15B19/005 , F15B21/087 , F16K37/0041 , F16K37/0083 , G05B23/0235 , G05B23/0283 , G05B2219/42271
摘要： A method for monitoring a system for actuating variable geometries of a turbojet engine, the actuation system including a control device, a servovalve, and an actuator controlled by the servovalve, the control device configured to determine a control current according to a set position value and to a measured position of the actuator and to provide the control current to the servovalve. The monitoring method includes: detecting a stabilized condition; determining an average value of the control current during the detecting the stabilized condition; and comparing the average value with a predetermined threshold.
摘要翻译： 一种用于监测用于驱动涡轮喷气发动机的可变几何的系统的方法，所述致动系统包括控制装置，伺服阀和由所述伺服阀控制的致动器，所述控制装置被配置成根据设定的位置值确定控制电流， 到致动器的测量位置并且向伺服阀提供控制电流。 监测方法包括：检测稳定状态; 在检测稳定状态期间确定控制电流的平均值; 以及将所述平均值与预定阈值进行比较。
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公开(公告)号：US20140000352A1
公开(公告)日：2014-01-02
申请号：US14003391
申请日：2012-02-24
IPC分类号： G01M15/14
CPC分类号： G01M15/14 , F15B9/09 , F15B19/005 , F15B21/087 , F16K37/0041 , F16K37/0083 , G05B23/0235 , G05B23/0283 , G05B2219/42271
摘要： A method for monitoring a system for actuating variable geometries of a turbojet engine, the actuation system including a control device, a servovalve, and an actuator controlled by the servovalve, the control device configured to determine a control current according to a set position value and to a measured position of the actuator and to provide the control current to the servovalve. The monitoring method includes: detecting a stabilized condition; determining an average value of the control current during the detecting the stabilized condition; and comparing the average value with a predetermined threshold.
摘要翻译： 一种用于监测用于驱动涡轮喷气发动机的可变几何的系统的方法，所述致动系统包括控制装置，伺服阀和由所述伺服阀控制的致动器，所述控制装置被配置成根据设定的位置值确定控制电流， 到致动器的测量位置并且向伺服阀提供控制电流。 监测方法包括：检测稳定状态; 在检测稳定状态期间确定控制电流的平均值; 以及将所述平均值与预定阈值进行比较。
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8.发明申请METHOD OF DETECTING A FAULT WITH THE MEANS FOR DE-ICING A PROBE FOR MEASURING A PHYSICAL PARAMETER 有权用于检测用于测量物理参数的探测器的方法来检测故障的方法公开(公告)号：US20130088249A1
公开(公告)日：2013-04-11
申请号：US13805147
申请日：2011-06-22
申请人： Benoit Biraud , Franck Godel
发明人： Benoit Biraud , Franck Godel
IPC分类号： G01R31/28
CPC分类号： G01R31/2829 , B64D15/20 , F01D17/08 , F05D2260/80 , F05D2260/85 , G01D3/08 , G01K15/00 , G01K15/007
摘要： A method of detecting a fault in a de-icer probe for measuring a physical parameter on an airplane engine, the method including: prior to starting an engine, measuring a first value of the physical parameter with help of the probe; activating the probe de-icer; at an end of a determined duration from a start of de-icing, measuring a second value of the parameter with help of the probe; and comparing the first and second values and generating a fault signal if the difference between the first and second values is less than a determined threshold.
摘要翻译： 一种检测除冰探头中用于测量飞机发动机上的物理参数的故障的方法，所述方法包括：在启动发动机之前，借助所述探针测量所述物理参数的第一值; 激活探头除冰器; 在从除冰开始开始的确定的持续时间结束时，借助探针测量参数的第二值; 以及如果第一和第二值之间的差小于确定的阈值，则比较第一和第二值并产生故障信号。
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9.发明授权公开(公告)号：US08857150B2
公开(公告)日：2014-10-14
申请号：US12742953
申请日：2008-11-18
申请人： Christian Aurousseau , Jonathan Benitah , Xavier Flandrois , Jean-Remi Masse , Mickael Sauzedde , Franck Godel , Julien Maille
发明人： Christian Aurousseau , Jonathan Benitah , Xavier Flandrois , Jean-Remi Masse , Mickael Sauzedde , Franck Godel , Julien Maille
CPC分类号： F02C7/236 , F02C9/263 , F02C9/28 , F02C9/44 , F05D2260/80 , F05D2270/092 , F05D2270/304
摘要： A device and method for monitoring a high-pressure pump in a turbomachine fuel supply circuit by detecting opening of a pressurizing and shut-off valve mounted on an outlet side of a fuel flow regulating valve, by measuring rotational speed of the turbomachine corresponding to the opening of the pressurizing and cut-off valve, and by monitoring change in a value of the rotational speed to propose replacement of the high-pressure pump when the measure value rotational speed reaches a predetermined threshold.
摘要翻译： 一种用于通过检测安装在燃料流量调节阀的出口侧的加压和截止阀的开度来监测涡轮机燃料供应回路中的高压泵的装置和方法，通过测量与该燃料流量调节阀对应的涡轮机的旋转速度 打开加压和截止阀，并且通过监测转速值的变化，以在测量值转速达到预定阈值时提出更换高压泵。
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10.发明授权Method of detecting a fault with the means for de-icing a probe for measuring a physical parameter 有权用用于测量物理参数的探针除冰装置来检测故障的方法公开(公告)号：US08994392B2
公开(公告)日：2015-03-31
申请号：US13805147
申请日：2011-06-22
申请人： Benoit Biraud , Franck Godel
发明人： Benoit Biraud , Franck Godel
CPC分类号： G01R31/2829 , B64D15/20 , F01D17/08 , F05D2260/80 , F05D2260/85 , G01D3/08 , G01K15/00 , G01K15/007
摘要： A method of detecting a fault in a de-icer probe for measuring a physical parameter on an airplane engine, the method including: prior to starting an engine, measuring a first value of the physical parameter with help of the probe; activating the probe de-icer; at an end of a determined duration from a start of de-icing, measuring a second value of the parameter with help of the probe; and comparing the first and second values and generating a fault signal if the difference between the first and second values is less than a determined threshold.
摘要翻译： 一种检测除冰探头中用于测量飞机发动机上的物理参数的故障的方法，所述方法包括：在启动发动机之前，借助所述探针测量所述物理参数的第一值; 激活探头除冰器; 在从除冰开始开始的确定的持续时间结束时，借助探针测量参数的第二值; 以及如果第一和第二值之间的差小于确定的阈值，则比较第一和第二值并产生故障信号。
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