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    • 1. 发明授权
    • Measurement and machining of engineering components
    • 工程部件的测量和加工
    • US4755952A
    • 1988-07-05
    • US841311
    • 1986-03-19
    • Antony Johns
    • Antony Johns
    • G01B21/02G01B21/00G01B21/20G05B19/18G05B19/416G06F15/46
    • G05B19/18G05B19/4166G05B2219/36523G05B2219/37075G05B2219/37194G05B2219/37196G05B2219/37525G05B2219/37574G05B2219/49362G05B2219/50063G05B2219/50391G05B2219/50399
    • A method and apparatus are described for the automatic gauging of engineering components. The apparatus includes a clamp for holding a component to be gauged, probes for scanning a surface of the component, drives to provide relative motion between the component and the probes in three mutually perpendicular axes, measuring transducers associated with the drives and the probes to generate signals to measure the degree of movement between the component and the probes, computer memory for storing data relating to a reference profile having dimensions which it is desired to achieve, computer apparatus for comparing signals generated by the measuring transducers with the corresponding signals in the memory, computer apparatus for calculating any error between the stored data and signals generated by the measuring transducers to stack the component to maximize desired coincidence between the dimensions of the reference profile and the actual component. The method and apparatus are described with reference to the gauging of components having aerofoils.
    • 描述了用于自动测量工程组件的方法和装置。 该装置包括用于保持要测量的部件的夹具,用于扫描部件表面的探针,驱动以在三个相互垂直的轴线上提供部件和探针之间的相对运动,测量与驱动器相关联的传感器和探针以产生 用于测量部件和探头之间的移动程度的信号,计算机存储器,用于存储与期望达到的具有尺寸的参考轮廓有关的数据;计算机装置,用于将由测量换能器产生的信号与存储器中的相应信号进行比较 计算机装置,用于计算存储的数据与由测量传感器产生的信号之间的任何误差,以堆叠该组件以最大化参考分布图和实际分量的尺寸之间的期望重合。 参考具有机翼的部件的测量来描述该方法和装置。
    • 3. 发明授权
    • Method and apparatus for the measurement of airfoils
    • 用于测量翼型的方法和装置
    • US4811253A
    • 1989-03-07
    • US841511
    • 1986-03-19
    • Antony Johns
    • Antony Johns
    • G01B21/02G01B21/00G01B21/20G05B19/401G05B19/42G01B5/20G06F15/46
    • G05B19/4207G05B19/401G05B2219/36523G05B2219/37075G05B2219/37194G05B2219/37196G05B2219/37574G05B2219/37617G05B2219/50063G05B2219/50358G05B2219/50391G05B2219/50399
    • A method and apparatus are described for the automatic gauging of engineering components. The apparatus includes a clamp for holding a component to be gauged, probes for scanning a surface of the component, drives to provide relative motion between the component and the probes in three mutually perpendicular axes, measuring transducers associated with the drives and the probes to generate signals to measure the degree of movement between the component and the probes, computer memory for storing data relating to a reference profile having dimensions which it is desired to achieve, computer apparatus for comparing signals generated by the measuring transducers with the corresponding signals in the memory, computer apparatus for calculating any error between the stored data and signals generated by the measuring transducers to stack the component to maximize desired coincidence between the dimensions of the reference profile and the actual component. The method and apparatus are described with reference to the gauging of components having aerofoils.
    • 描述了用于自动测量工程组件的方法和装置。 该装置包括用于保持要测量的部件的夹具,用于扫描部件表面的探针,驱动以在三个相互垂直的轴线上提供部件和探针之间的相对运动,测量与驱动器相关联的传感器和探针以产生 用于测量部件和探头之间的移动程度的信号,计算机存储器,用于存储与期望达到的具有尺寸的参考轮廓有关的数据;计算机装置,用于将由测量换能器产生的信号与存储器中的相应信号进行比较 计算机装置,用于计算存储的数据与由测量传感器产生的信号之间的任何误差,以堆叠该组件以最大化参考分布图和实际分量的尺寸之间的期望重合。 参考具有机翼的部件的测量来描述该方法和装置。
    • 4. 发明授权
    • Process for the curvilinear formation of holes
    • 孔的曲线形成过程
    • US4769118A
    • 1988-09-06
    • US095571
    • 1987-07-13
    • Antony Johns
    • Antony Johns
    • B23B5/36B23H9/14B23H3/04
    • B23B5/365B23H9/14F05B2220/302
    • A process is described for the production of holes having curvilinear paths in engineering components. The process comprises the steps of producing relative motion along a curvilinear path between a workpiece in which it is desired to form a curved hole and a drill bit wherein the drill bit comprises a curved delivery tube of an ECM apparatus, the curved tube passing through an aperture in a guidance member which is positioned adjacent the workpiece, the aperture length being less than the diameter of the tube. An example is described of the production of curved holes in a gas turbine engine blade.
    • PCT No.PCT / GB86 / 00751 Sec。 371日期1987年7月13日 102(e)日期1987年7月13日PCT提交1986年12月9日PCT公布。 第WO87 / 03522号公报 日期1987年6月18日。描述了在工程组件中生产具有曲线路径的孔的过程。 该方法包括沿着期望形成弯曲孔的工件之间的曲线路径产生相对运动的步骤和钻头,其中钻头包括ECM装置的弯曲输送管,弯曲管穿过 位于邻近工件的引导构件中的孔径,孔的长度小于管的直径。 描述了在燃气涡轮发动机叶片中产生弯曲孔的实例。