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Study on measurement of leading and trailing edges of blades based on optical scanning system

机译:基于光学扫描系统的叶片前缘和后缘测量研究

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摘要

In the field of aeronautics, the geometry and dimensional accuracy of the blade edges has a large influence on the aerodynamic performance of aero engine. Therefore, a non-contact optical scanning system is established to realize the measurement of leading and trailing edges of blades in a rapid, precise and efficient manner in the paper. Based on the mechanical framework of a traditional CMM, the system is equipped with a specified sensing device as the scanning probe, which is made up by two new-style laser scanning sensors installed at a certain angle to each other by a holder. In the measuring procedure, the geometric dimensions of the measured blade edges on every contour plane are determined by the contour information on five transversals at the leading or trailing edges, which can be used to determine the machining allowance of the blades. In order to verify the effectiveness and practicality of the system set up, a precision forging blade after grinded is adopted as the measured object and its leading and trailing edges are measured by the system respectively. In the experiment, the thickness of blade edges on three contour planes is measured by the optical scanning system several times. As the experiment results show, the repeatability accuracy of the system can meet its design requirements and the inspecting demands of the blade edges. As a result, the optical scanning system could serve as a component of the intelligent manufacturing system of blades to improve the machining quality of the blade edges.
机译:在航空领域,叶片边缘的几何形状和尺寸精度对航空发动机的空气动力性能具有很大的影响。因此,建立了一种非接触式光学扫描系统,以在纸张中快速,精确和有效地实现叶片前缘和后缘的测量。该系统在传统三坐标测量机的机械框架的基础上,配备了指定的传感设备作为扫描探针,该传感器由两个新型激光扫描传感器组成,两个传感器之间通过一定角度相互安装。在测量过程中,每个轮廓平面上测得的叶片边缘的几何尺寸由前缘或后缘的五个横向轮廓信息确定,这些信息可用于确定叶片的加工余量。为了验证该系统的有效性和实用性,采用磨削后的精密锻造刀片作为被测对象,并分别测量其前缘和后缘。在实验中,通过光学扫描系统多次测量了三个轮廓平面上的刀刃厚度。实验结果表明,该系统的重复精度可以满足设计要求和叶片边缘的检测要求。结果,光学扫描系统可以用作叶片的智能制造系统的组件,以提高叶片边缘的加工质量。

著录项

  • 来源
  • 会议地点 Beijing(CN)
  • 作者单位

    Aviation Key Laboratory of Science and Technology on Precision Manufacturing Technology, Beijing Precision Engineering Institute for Aircraft Industry, Beijing 100076, China;

    Tianjin Institute of Metrological Supervision and Testing, Tianjin 300192, China;

    Aviation Key Laboratory of Science and Technology on Precision Manufacturing Technology, Beijing Precision Engineering Institute for Aircraft Industry, Beijing 100076, China;

    Aviation Key Laboratory of Science and Technology on Precision Manufacturing Technology, Beijing Precision Engineering Institute for Aircraft Industry, Beijing 100076, China;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Leading edge; trailing edge; aero engine; optical scanning sensor;

    机译:前沿;后缘航空发动机光学扫描传感器;

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