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Blade space angle measuring device for blade ring structure part

A technology of space angle and structural parts, applied in the direction of measuring device, mechanical measuring device, angle/taper measurement, etc., can solve the problems of long three-coordinate detection cycle and difficult measurement of blade space angle, and achieve long measurement cycle and wide application foreground effect

Inactive Publication Date: 2021-03-09
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the above-mentioned technical problems, the present invention provides a blade space angle measuring device for the blade ring structural parts, which solves the problems of difficult measurement of the blade space angle and long three-coordinate detection cycle in engine impeller or blade ring parts

Method used

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  • Blade space angle measuring device for blade ring structure part
  • Blade space angle measuring device for blade ring structure part
  • Blade space angle measuring device for blade ring structure part

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Embodiment Construction

[0022] The present invention will be described in detail below in conjunction with the accompanying drawings, but the protection scope of the present invention is not limited by the accompanying drawings.

[0023] figure 1 It is a schematic diagram of the structure of the leaf ring structure, figure 2 It is a schematic diagram of the A-A cross-sectional structure of the leaf ring structure part, as shown in the figure: the blade of the leaf ring part has a space structure at an angle of 17, and L in the figure is the distance from the blade measurement point to the center of the part; Q is the positioning diameter of the part on the limit tooling .

[0024] The blade space angle measuring device of the leaf ring structural part of the present invention includes an angle measuring tool and a limit measuring tool; the limit measuring tool is used to fix the leaf ring type part to be tested and the angle measuring tool, and the angle measuring tool is used to measure the blade ...

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Abstract

The invention relates to the technical field of aero-engine blade ring type part measurement, in particular to a blade space angle measuring device for a blade ring structure part, which comprises anangle measuring tool and a limiting measuring tool. The limiting measuring tool is used for fixing a blade ring type part to be measured and the angle measuring tool, and the angle measuring tool is used for measuring the blade space angle. According to the invention, the problem that the blade space angle in an impeller and a blade ring type structural part is difficult to measure is solved, theblade space angle can be directly and quickly measured and directly read, so that the problem of long blade space angle measurement period of the part is solved, the occupation of three-coordinate equipment can be reduced, the development and production period of the part is shortened, and the device has a wide application prospect.

Description

technical field [0001] The invention relates to the technical field of measuring an aeroengine leaf ring type part, in particular to a blade space angle measuring device for a leaf ring structural part. Background technique [0002] More and more impeller-type and leaf-ring structural parts are used in modern jet aeroengines. The blades of these parts control the direction of air intake, so the requirements for the angle of the blades are relatively strict. The only feasible method of measurement is CMM. The three-coordinate measurement needs to scan the leaf shape points, and the detection cycle is long. After the three-coordinate scanning, manual fitting is required to obtain the angle result, and the leaf ring structure parts have a large number of blades, and the workload is very large, which is difficult to adapt to the mass production of parts. , so it is very inefficient to use three coordinates to detect this size. Contents of the invention [0003] In order to s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B5/24G01B5/00
CPCG01B5/24G01B5/003
Inventor 俸跃伟刘培科郭春艳
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION