Intelligent detection device and method for compressor stator guide vane setting angle

The technology of a guide vane and a detection method is applied in the field of intelligent detection of the installation angle of the guide vane of the stator of the compressor, which can solve the problems of inconvenient and intelligent use, low accuracy and the like, and achieve high measurement accuracy, high efficiency and convenient use. Effect

Active Publication Date: 2019-05-21
CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC +1
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0003] At present, the existing detection device for the installation angle of the casing blade is completely mechanical, relying on manual reading records. This detection method is highly dependent on the experience and attitude of the operator, and the accuracy is low. It is not convenient and intelligent to use.

Method used

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  • Intelligent detection device and method for compressor stator guide vane setting angle
  • Intelligent detection device and method for compressor stator guide vane setting angle
  • Intelligent detection device and method for compressor stator guide vane setting angle

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Embodiment Construction

[0022] The radial distance of the inclinometer described in this embodiment is 260 mm for the 0-stage blade, 240 mm for the 1-stage blade, 230 mm for the 2-stage blade, and 226 mm for the 3-stage blade.

[0023] The number of stages of blades in the casing described in this embodiment is 4, and each stage has 100 blades.

[0024] Such as Figure 1-4 As shown, the steps of the method for detecting the installation angle of the compressor stator guide vane described in this embodiment are:

[0025] 1. Fix the special measuring and positioning tool on the upper end surface of the compressor casing 15 to be tested through the positioning pin 6, attach the magnetic gauge frame to the depth axis 5 of the measuring tool, and rotate through the high-precision turntable 4 in the center of the measuring tool Drive the dial indicator to beat the outer circle of the casing 15, adjust the two-dimensional sliding table 3 on the center of the measuring tool, and find the axis of the casing ...

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Abstract

The invention relates to an intelligent detection device and method for a compressor stator guide vane setting angle. A measuring and positioning tool is composed of a tool cross beam (1), supportingbases (2), a two-dimensional sliding table (3), a high-precision rotary table (4), a depth shaft (5) and positioning pins (6), wherein the two-dimensional sliding table (3) and the high-precision rotary table (4) are sequentially installed on the lower end face of the middle of the tool cross beam (1), and the depth shaft (5) is fixed to the high-precision rotary table (4); the two supporting bases (2) are located on the two sides of the tool cross beam (1) respectively, the positioning pins (6) are arranged on the supporting bases (2), and the measuring and positioning tool is fixedly placedon a to-be-detected compressor case (15) through the positioning pins (6). Detection results can be displayed in real time, detection result data storage and export functions are provided, and the defects of manual misreading, complex data recording and the like are overcome; the detection method is high in measurement precision, high in efficiency and convenient to use.

Description

technical field [0001] The invention relates to the measurement design of the vane installation angle, and provides an intelligent detection method for the installation angle of the compressor stator guide vane. Background technique [0002] In the field of aviation, the installation angle of the guide vane of the compressor stator has a great influence on the secondary flow loss of the engine, especially the installation angle of the guide vane after the assembly of the high-pressure compressor stator directly affects its energy conversion efficiency. In aero-engines, the direction of the outlet angle of the guide vanes is usually controlled to keep the angle of attack of the airflow flowing into the first-stage rotor blades at a proper position, thereby avoiding the occurrence of engine surge. Therefore, the installation angle of the blades in the casing has a great influence on the performance of the engine, and determining the change of the installation angle of the blad...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B5/24
Inventor 徐昌语郭霞庞长涛吕玉红曹艳刘超
Owner CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC
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