APPARATUS AND METHOD FOR TEMPERATURE MAPPING A TURBINE COMPONENT IN A HIGH TEMPERATURE COMBUSTION ENVIRONMENT
    1.
    发明申请
    APPARATUS AND METHOD FOR TEMPERATURE MAPPING A TURBINE COMPONENT IN A HIGH TEMPERATURE COMBUSTION ENVIRONMENT 有权
    在高温燃烧环境中温度测量涡轮机组件的装置和方法

    公开(公告)号:US20120200698A1

    公开(公告)日:2012-08-09

    申请号:US13023774

    申请日:2011-02-09

    IPC分类号: H04N7/18

    摘要: Method and system for calibrating a thermal radiance map of a turbine component in a combustion environment. At least one spot (18) of material is disposed on a surface of the component. An infrared (IR) imager (14) is arranged so that the spot is within a field of view of the imager to acquire imaging data of the spot. A processor (30) is configured to process the imaging data to generate a sequence of images as a temperature of the combustion environment is increased. A monitor (42, 44) may be coupled to the processor to monitor the sequence of images of to determine an occurrence of a physical change of the spot as the temperature is increased. A calibration module (46) may be configured to assign a first temperature value to the surface of the turbine component when the occurrence of the physical change of the spot is determined.

    摘要翻译: 用于在燃烧环境中校准涡轮机部件的热辐射图的方法和系统。 至少一个材料点(18)设置在部件的表面上。 红外线(IR)成像器(14)被布置成使得该点位于成像器的视场内以获取该点的成像数据。 处理器(30)被配置为当燃烧环境的温度增加时,处理成像数据以产生图像序列。 监视器(42,44)可以耦合到处理器以监视图像序列,以确定当温度升高时点的物理变化的发生。 校准模块(46)可以被配置为当确定点的物理变化的发生时,将第一温度值分配给涡轮机部件的表面。

    Specimen coordinate automated measuring machine/fiducial automated
measuring machine
    2.
    发明授权
    Specimen coordinate automated measuring machine/fiducial automated measuring machine 失效
    标准坐标自动测量机/基准自动测量机

    公开(公告)号:US5050112A

    公开(公告)日:1991-09-17

    申请号:US390852

    申请日:1989-08-08

    IPC分类号: G01B21/04 G05B19/401

    摘要: The Specimen coordinate Automated Measuring Machine (SCAMM) and the Fiducial Automated Measuring Machine (FAMM) is a computer controlled metrology system capable of measuring length, width, and thickness, and of locating fiducial marks. SCAMM and FAMM have many similarities in their designs, and they can be converted from one to the other without taking them out of the hot cell. Both have means for: supporting a plurality of samples and a standard; controlling the movement of the samples in the +/- X and Y directions; determining the coordinates of the sample; compensating for temperature effects; and verifying the accuracy of the measurements and repeating as necessary. SCAMM and FAMM are designed to be used in hot cells.

    摘要翻译: 样品坐标自动测量机(SCAMM)和基准自动测量机(FAMM)是一种能够测量长度,宽度和厚度以及定位基准标记的计算机控制测量系统。 SCAMM和FAMM在设计上有很多相似之处,它们可以从一个转换到另一个,而不必将它们从热电池中取出。 两者都具有:支持多个样本和标准的手段; 控制样品在+/- X和Y方向的移动; 确定样品的坐标; 补偿温度影响; 并验证测量的准确性并根据需要进行重复。 SCAMM和FAMM设计用于热电池。

    Robotic processing and inspection system
    3.
    发明授权
    Robotic processing and inspection system 失效
    机器人加工检验系统

    公开(公告)号:US5390128A

    公开(公告)日:1995-02-14

    申请号:US44701

    申请日:1993-04-12

    IPC分类号: G05B19/408 G06F15/46

    摘要: Automated system for trimming and inspecting complex composite aircraft parts. A straight firing abrasive water jet head with integral catcher mounted on a first Z axis slide is numerically controlled on a six axis gantry/water jet manipulator (X, Y, Z, C, A, B axes). A touch probe mounted on a second Z axis slide is used to gauge three part points which establish part orientation in the X, Y, Z gantry/robot cell; also to adjust CNC and CMM part trim/inspection programs to actual part orientation and for peripheral dimensional inspection.

    摘要翻译: 用于修整和检查复杂复合飞机部件的自动化系统。 在六轴龙门/喷水机械手(X,Y,Z,C,A,B轴)上数字控制一个具有安装在第一Z轴滑块上的集成捕获器的直喷式磨料水喷头。 安装在第二个Z轴滑块上的探针用于测量在X,Y,Z机架/机器人单元中建立零件取向的三个零件点; 还可以将CNC和CMM零件修整/检验程序调整为实际零件定向和外围尺寸检查。

    Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment
    5.
    发明授权
    Apparatus and method for temperature mapping a turbine component in a high temperature combustion environment 有权
    用于在高温燃烧环境中对涡轮机部件进行温度测绘的装置和方法

    公开(公告)号:US08749629B2

    公开(公告)日:2014-06-10

    申请号:US13023774

    申请日:2011-02-09

    IPC分类号: H04N7/18

    摘要: Method and system for calibrating a thermal radiance map of a turbine component in a combustion environment. At least one spot (18) of material is disposed on a surface of the component. An infrared (IR) imager (14) is arranged so that the spot is within a field of view of the imager to acquire imaging data of the spot. A processor (30) is configured to process the imaging data to generate a sequence of images as a temperature of the combustion environment is increased. A monitor (42, 44) may be coupled to the processor to monitor the sequence of images of to determine an occurrence of a physical change of the spot as the temperature is increased. A calibration module (46) may be configured to assign a first temperature value to the surface of the turbine component when the occurrence of the physical change of the spot is determined.

    摘要翻译: 用于在燃烧环境中校准涡轮机部件的热辐射图的方法和系统。 至少一个材料点(18)设置在部件的表面上。 红外线(IR)成像器(14)被布置成使得该点位于成像器的视场内以获取该点的成像数据。 处理器(30)被配置为当燃烧环境的温度增加时,处理成像数据以产生图像序列。 监视器(42,44)可以耦合到处理器以监视图像序列,以确定当温度升高时点的物理变化的发生。 校准模块(46)可以被配置为当确定点的物理变化的发生时,将第一温度值分配给涡轮机部件的表面。