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78 条记录 (耗时 0.019 秒)

    SPEED OR TORQUE PROBE FOR GAS TURBINE ENGINES
    4.
    发明公开
    SPEED OR TORQUE PROBE FOR GAS TURBINE ENGINES 审中-公开
    汽轮机发动机转速或转矩探头

    公开(公告)号：EP3267207A1

    公开(公告)日：2018-01-10

    申请号：EP17186205.5

    申请日：2011-06-16

    申请人： Weston Aerospace Limited

    发明人： Bodin, Robert Michael George

    IPC分类号： G01P3/488 ,  G01P1/02 ,  G01L3/10

    摘要： The invention comprises a variable reluctance sensor for sensing the speed or torque of a shaft in a gear box or gas turbine engine, comprising a magnetic pole piece; a conductive wire wrapped around the pole piece; a housing surrounding the pole piece, the housing having a front face and at least one side wall, wherein, in use, the front face is positioned proximate to an object to be sensed, wherein the pole piece extends through the front face of the housing and the front face of the housing is substantially less rigid than the side wall of the housing by forming the front face substantially thinner and less massive than the sidewalls of the housing. By having a front face that is able to flex, less stress is exerted on the pole piece under external vibration, when the pole piece is firmly connected to the front face.

    摘要翻译： 本发明包括用于感测齿轮箱或燃气涡轮发动机中的轴的速度或转矩的可变磁阻传感器，其包括磁极件; 缠绕在极靴周围的导线; 围绕所述极靴的外壳，所述外壳具有前表面和至少一个侧壁，其中，在使用中，所述前表面定位成靠近待感测物体，其中所述极片延伸穿过所述外壳的前表面 并且通过形成比壳体的侧壁明显更薄并且质量更小的前表面，壳体的前表面的刚性比壳体的侧壁小得多。 通过具有能够弯曲的前表面，当极片牢固地连接到正面时，在外部振动下施加在极片上的应力较小。

    SYSTEM FOR DETECTING ABNORMAL MOVEMENT OF A SHAFT IN A GAS TURBINE ENGINE
    5.
    发明授权
    SYSTEM FOR DETECTING ABNORMAL MOVEMENT OF A SHAFT IN A GAS TURBINE ENGINE 有权
    用于检测燃气涡轮发动机中轴的异常运动的系统

    公开(公告)号：EP3106626B1

    公开(公告)日：2018-01-03

    申请号：EP16168763.7

    申请日：2016-05-09

    申请人： WESTON AEROSPACE LIMITED

    发明人： OATES, Ray

    IPC分类号： F01D21/04

    CPC分类号： F01D21/04 ,  F01D21/003 ,  F01D21/045 ,  F05D2230/21 ,  G01M15/14

    摘要： The present invention provides a system for detecting abnormal axial movement of a shaft in a gas turbine engine. The system comprises a detection circuit including a detector element including a frangible link portion (32) forming part of an electrical detection circuit and a plunger (38) integral with the frangible link portion (32). The plunger (38) is arranged such that it is displaced by abnormal axial movement of the gas turbine shaft to break the frangible link portion (32) from the remainder of the detection circuit and thereby break the electrical detection circuit. The system includes two connection blocks (33, 35) each having a connection at a respective first portion for electrical connection to a signal sensing unit, and being connected at respective second portions to opposite ends of the frangible link portion such that the electrical circuit running through the detector element and a signal sensing unit is modified when the frangible link portion (32) is broken by movement of the plunger (38).

    Sensor for detecting abnormal movement of a gas turbine shaft
    6.
    发明公开
    Sensor for detecting abnormal movement of a gas turbine shaft 审中-公开
    用于检测燃气轮机轴的异常运动的传感器

    公开(公告)号：EP2570618A3

    公开(公告)日：2017-08-16

    申请号：EP12184130.8

    申请日：2012-09-12

    申请人： WESTON AEROSPACE LIMITED

    发明人： Kulczyk, Wojciech Konrad

    IPC分类号： F01D21/04 ,  F01D17/02 ,  F02B51/04

    CPC分类号： F02B51/04 ,  F01D17/02 ,  F01D21/045 ,  F02B51/06 ,  F02G2254/10 ,  F05D2260/80 ,  F05D2270/09 ,  Y02T10/126

    摘要： A sensor element for use in a backing sensor to monitor a gas turbine shaft. The sensor includes an oscillator circuit (30) having an oscillator and a resonance circuit (42), and a frequency detector (31) for monitoring the frequency of the ossilation circuit. Abnormal movement of the shaft cuts the circuit in the sensor along a cutting line (15). The cutting of the sensor changes the capacitance and/or inductance of the resonance circuit and thereby changes the frequency of oscillation.

    摘要翻译： 传感器元件用于后备传感器以监测燃气轮机轴。 该传感器包括具有振荡器和谐振电路（42）的振荡器电路（30），以及用于监测该ossilation电路的频率的频率检测器（31）。 轴的异常移动沿着切割线（15）切割传感器中的电路。 传感器的切割改变了谐振电路的电容和/或电感，从而改变了振荡的频率。

    Thermocouple probe
    9.
    发明授权
    Thermocouple probe 有权
    热电偶探头

    公开(公告)号：EP2818839B1

    公开(公告)日：2016-08-03

    申请号：EP14173345.1

    申请日：2014-06-20

    申请人： WESTON AEROSPACE LIMITED

    发明人： Ewing, James ,  Loveless, Daniel

    IPC分类号： G01K1/12 ,  G01K7/04 ,  G01K13/02

    CPC分类号： G01K7/02 ,  G01K1/12 ,  G01K1/20 ,  G01K7/04 ,  G01K13/02 ,  G01K2205/00

    摘要： A cooled thermocouple arrangement (1) including a thermocouple (2) comprising two wires (3,4) joined at a first sensing end (5) to define a hot thermocouple function. At least a portion of the wires (3,4) are in thermal communication with a cooling arrangement, and the cooling arrangement has an inlet (14) for coolant and an outlet (15) for coolant. The thermocouple probe arrangement (1) includes a first inlet temperature sensor (21) for determining the temperature of the coolant as it enters the cooling arrangement, and a flow rate sensor (20) for determining the flow rate of coolant passing through the cooling arrangement. The thermocouple probe arrangement (1) includes connectors for connecting the outputs from the thermocouple (2), first inlet temperature sensor (21) and the flow rate sensor (20) to a correction data processor (23) whereby the data processor can correct the temperature sensed by the thermocouple to take account of the effect of the cooling arrangement. The pair of thermocouple wires (3,4) are arranged inside a sheath or casing, and a cooling jacket (12) is provided around the thermocouple probe. The cooling jacket (12) includes a pair of concentric tubes (16,17) defining a return coolant circuit from the end of the probe proximal the connectors (8), to a portion of the probe distal from the connectors, and then back to the proximal end (8) of the probe, and the portion of the thermocouple probe containing the sensing end (5) of the thermocouple projects from the distal end of the cooling jacket (12).