Shape measuring apparatus
    51.
    发明授权

    公开(公告)号:US09829303B2

    公开(公告)日:2017-11-28

    申请号:US15497722

    申请日:2017-04-26

    发明人: Yasuhiro Yamauchi

    IPC分类号: G01B5/20 G01B5/012 G01B5/28

    摘要: In a shape measuring apparatus for measuring the roughness and/or contour of a surface of a workpiece by sliding a sensing pin on a tip end side of an arm on the workpiece, the arm is provided with an engagement mechanism that makes a sensing pin side of the arm removable to a base end side of the arm. The engagement mechanism has two engagement surfaces which face each other and attract each other by a magnetic force. One of the engagement surfaces includes a linear first groove that is in parallel to an axis of the arm and another engagement part that is different from the first groove, and the other of the engagement surfaces includes a first fitting pin that is positioned to be fitted into the first groove and a second fitting pin that is fitted into the other engagement part.

    Gear Measurement Method and Gear Measurement Apparatus

    公开(公告)号:US20170292822A1

    公开(公告)日:2017-10-12

    申请号:US15472590

    申请日:2017-03-29

    申请人: JTEKT CORPORATION

    IPC分类号: G01B5/20

    CPC分类号: G01B5/202 G01B5/166

    摘要: A gear measurement method and a gear measurement apparatus capable of evaluating meshing and fitting of a gear are provided. A measurement method for a gear includes a measurement step of measuring an actual movement locus of a ball that is moved along a tooth groove of the gear as a shape evaluation index for the gear. In the case of a VGR rack, tooth surfaces of rack teeth are constituted of curved surfaces. Thus, a reference pin for use in OPD cannot be disposed so as to be in line contact with the tooth surfaces, and the rack teeth cannot be measured. However, the ball can be disposed so as to be in point contact with the tooth surfaces, which enables a measurement of the rack teeth.

    Measurement method
    57.
    发明授权

    公开(公告)号:US09689655B2

    公开(公告)日:2017-06-27

    申请号:US13122499

    申请日:2009-10-29

    IPC分类号: G01B5/008 G01B5/20 G01B21/04

    CPC分类号: G01B5/008 G01B5/20 G01B21/042

    摘要: This invention relates to a method for measuring a feature of an object that comprises obtaining a representation of at least the feature on the object by acquiring multiple data points via surface measurement of at least the feature. A model substantially replicating at least the feature of the object is fitted to the representation. The model comprises parameters defining at least two independently alterable portions that are linked at a common point. The fitting comprises changing the form of the model by altering at least one of the at least two independently alterable portions. The method also comprises obtaining information regarding at least the feature from the fitted model.

    AIRCRAFT ENGINE ROTOR ASSEMBLY METHOD AND DEVICE
    60.
    发明申请
    AIRCRAFT ENGINE ROTOR ASSEMBLY METHOD AND DEVICE 有权
    飞机发动机转子总成方法和装置

    公开(公告)号:US20170050275A1

    公开(公告)日:2017-02-23

    申请号:US15118803

    申请日:2014-12-26

    摘要: Aircraft engine rotors traditionally have low coaxiality after assembly. This is solved by the methods and devices described herein, having advantages that the rotors have high coaxiality after assembly, reduced vibration, easy installation, high flexibility, and improved engine performance. A measurement method and device use an air flotation rotary shaft system determining a rotary reference. An induction synchronizer determines angular positioning of a turntable. Using a four probe measurement device, a radial error of a rotor radial assembly surface and an inclination error of an axial mounting surface are extracted and an influence weight value of the rotor on the coaxiality of assembled rotors is obtained. All rotors required for assembly are measured and an influence weight value of each on the coaxiality of the assembled rotors is obtained. Vector optimization is performed on the weight value of each rotor and an assembly angle of each rotor is obtained.

    摘要翻译: 飞机发动机转子在组装后传统上具有低同轴度。 这通过本文所述的方法和装置来解决,其优点在于转子在组装之后具有高的同轴度,减少的振动,易于安装,高灵活性和改进的发动机性能。 测量方法和装置使用确定旋转参考的空气浮选旋转轴系统。 感应同步器确定转台的角度定位。 使用四探头测量装置,提取转子径向组件表面的径向误差和轴向安装表面的倾斜误差,并且获得转子对组装转子同轴度的影响重量值。 测量组装所需的所有转子,并且获得各组合转子的同轴度的影响重量值。 对每个转子的重量值执行向量优化,并获得每个转子的组装角度。