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    High temperature measurement probe
    1.
    发明授权
    High temperature measurement probe 有权
    高温测量探头

    公开(公告)号：US08992081B2

    公开(公告)日：2015-03-31

    申请号：US13161899

    申请日：2011-06-16

    申请人： Peter Ireland ,  Andrew Wilson ,  Steven Thorpe ,  Damian Martin

    发明人： Peter Ireland ,  Andrew Wilson ,  Steven Thorpe ,  Damian Martin

    IPC分类号： G01K7/02 ,  G01K1/14 ,  G01K1/08 ,  G01K13/02

    CPC分类号： G01K13/02 ,  G01K13/028

    摘要： A high temperature measurement probe comprises an elongate probe body having a measuring head which in use is located in a hot fluid flow. The probe further comprises a thermocouple extending along the interior of the probe body to terminate at a temperature-sensing thermocouple junction inside the measuring head. The probe body has internal passages for circulation of a coolant fluid therein. The measuring head contains a channel, one end of the channel forming an inlet for receiving hot fluid from the hot fluid flow and another end of the channel forming an outlet for discharging the hot fluid received at the inlet. Between the inlet and the outlet a section of the channel extends along the length direction of the probe body. The thermocouple runs along the section of the channel with the thermocouple junction proximate the upstream end of the section.

    摘要翻译： 高温测量探头包括具有测量头的细长探针体，测量头在使用中位于热流体流中。 探头还包括沿着探针本体的内部延伸的热电偶，以终止于测量头内的温度感测热电偶结。 探针体具有用于在其中循环冷却剂流体的内部通道。 测量头包含通道，通道的一端形成用于从热流体流接收热流体的入口，并且通道的另一端形成用于排出在入口处接收的热流体的出口。 在入口和出口之间，通道的一部分沿探头主体的长度方向延伸。 热电偶沿着通道的部分延伸，热电偶接头靠近该部分的上游端。

    Gas turbine engine simulator
    2.
    发明授权
    Gas turbine engine simulator 有权
    燃气轮机发动机模拟器

    公开(公告)号：US07717668B2

    公开(公告)日：2010-05-18

    申请号：US11583068

    申请日：2006-10-19

    申请人： Changmin Son ,  Peter Ireland ,  Steven Thorpe ,  Terence Jones

    发明人： Changmin Son ,  Peter Ireland ,  Steven Thorpe ,  Terence Jones

    IPC分类号： F01D25/00

    CPC分类号： G01M15/14 ,  F05B2230/50 ,  F05B2260/80

    摘要： A gas turbine engine simulator comprising a simulator rotor disc which has substantially the same maximum external dimensions as a rotor disc and is manufactured from a material which has a density of less than 220 kg/m3. The simulator rotor disc is manufactured from a foamed plastic material with a closed cell structure. The simulator rotor disc is provided with a cavity in flow communication with a source of simulator coolant fluid, at least one flow outlet, at least one heater unit and at least one thermocouple mounted within said cavity for the measurement of simulator coolant fluid temperature within said cavity.

    摘要翻译： 一种燃气涡轮发动机模拟器，其包括模拟器转子盘，其具有与转子盘基本上相同的最大外部尺寸，并且由密度小于220kg / m 3的材料制成。 模拟器转子盘由具有闭孔结构的发泡塑料制成。 模拟器转子盘设置有与模拟器冷却剂流体源，至少一个流出口，至少一个加热器单元和安装在所述腔内的至少一个热电偶流动连通的空腔，用于测量所述腔内的模拟器冷却剂流体温度 腔。

    Gas turbine engine simulator
    3.
    发明申请
    Gas turbine engine simulator 有权
    燃气轮机发动机模拟器

    公开(公告)号：US20070207039A1

    公开(公告)日：2007-09-06

    申请号：US11583068

    申请日：2006-10-19

    申请人： Changmin Son ,  Peter Ireland ,  Steven Thorpe ,  Terence Jones

    发明人： Changmin Son ,  Peter Ireland ,  Steven Thorpe ,  Terence Jones

    IPC分类号： F01D5/30

    CPC分类号： G01M15/14 ,  F05B2230/50 ,  F05B2260/80

    摘要： A gas turbine engine simulator comprising a simulator rotor disc which has substantially the same maximum external dimensions as a rotor disc and is manufactured from a material which has a density of less than 220 kg/m3. The simulator rotor disc is manufactured from a foamed plastic material with a closed cell structure. The simulator rotor disc is provided with a cavity in flow communication with a source of simulator coolant fluid, at least one flow outlet, at least one heater unit and at least one thermocouple mounted within said cavity for the measurement of simulator coolant fluid temperature within said cavity.

    摘要翻译： 一种燃气涡轮发动机模拟器，其包括具有与转子盘基本上相同的最大外部尺寸的模拟器转子盘，并且由密度小于220kg / m 3的材料制造。 模拟器转子盘由具有闭孔结构的发泡塑料制成。 模拟器转子盘设置有与模拟器冷却剂流体源，至少一个流出口，至少一个加热器单元和安装在所述腔内的至少一个热电偶流动连通的空腔，用于测量所述腔内的模拟器冷却剂流体温度 腔。

    Gravity gradiometer
    5.
    发明申请
    Gravity gradiometer 有权
    重力梯度计

    公开(公告)号：US20070051175A1

    公开(公告)日：2007-03-08

    申请号：US11494545

    申请日：2006-07-28

    申请人： John French ,  Kieran Carroll ,  Steven Thorpe

    发明人： John French ,  Kieran Carroll ,  Steven Thorpe

    IPC分类号： G01V7/02

    CPC分类号： G01V7/10

    摘要： A gravity gradiometer having quadrupole responders in which a mass quadrupole is supported by a torsional spring forming a flexure allowing rotation of the mass quadrupole about its center of mass. The flexure can be a pair of spaced apart posts. The flexure can be made from glassy metal having at room temperature a high elastic limit, high stiffness, high strength and low internal damping. The flexure can alternatively be a web made of glassy metal.

    摘要翻译： 具有四极响应器的重力梯度计，其中质量四极杆由形成弯曲的扭转弹簧支撑，允许质量四极杆围绕其质心旋转。 挠曲件可以是一对间隔开的柱。 弯曲可以由具有高弹性极限，高刚度，高强度和低内部阻尼的室温玻璃状金属制成。 挠性件也可以是由玻璃状金属制成的网。