Disc-shaft connection rotor system thermal analysis test bench and thermal deformation measurement method

A technology of thermal deformation and test bench, which is applied in the direction of measuring devices, testing of mechanical components, testing of machine/structural components, etc. It can solve the problems that it is difficult to accurately control the thermal characteristics and the thermal deformation of the spindle system is difficult to achieve accuracy, etc. , to achieve the effect of comprehensive and accurate control of content and results

Active Publication Date: 2019-02-15
NORTHEASTERN UNIV
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

There are many factors that affect the thermal deformation of the disk-shaft connection rotor system. Although many scholars have used the finite element method to conduct quantitative analysis on it, these analyzes are carried out on the basis of simplifying the heat source and the disk-shaft connection structure, so it is difficult Accurate control of thermal characteristics, while using finite element method to analyze the thermal deformation of the spindle system is difficult to achieve accuracy, compared with finite element modeling, experimental method can analyze more accurately and get more accurate results

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  • Disc-shaft connection rotor system thermal analysis test bench and thermal deformation measurement method
  • Disc-shaft connection rotor system thermal analysis test bench and thermal deformation measurement method
  • Disc-shaft connection rotor system thermal analysis test bench and thermal deformation measurement method

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Embodiment Construction

[0039] The specific implementation manners of the present invention will be further described below in conjunction with the drawings and technical solutions.

[0040] Such as figure 1 , 2 As shown, a thermal analysis test bench for a disc-shaft connection rotor system is mainly composed of an electric drive and control system A, an ignition system B, a heat insulation system C, a nonlinear support-rotor system D, a test sensor system E and a base 17 ;

[0041] The base 17 is equipped with a plurality of anchor bolts for fixing the motor support 4, the bearing support a15 and the bearing support b18, and serves as a slideway for the heat shield.

[0042] Such as Figure 4 As shown, the nonlinear support-rotor system D includes a disk structure 7 and a rotating shaft 8, and the two ends of the rotating shaft 8 fix the rotor on the bearing seat a15 and the bearing seat b18 through two bearings and the bearing seat 6 ; Disc shaft connection structure such as Figure 5(a) and ...

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Abstract

The invention belongs to the field of aero-engine disc-shaft connection rotor system thermal effect analysis and thermal deformation measurement, and relates to a disc-shaft connection rotor system thermal analysis test bench and a thermal deformation measurement method. The test bench is mainly composed of an electric drive and control system, an ignition system, a heat insulation system, a nonlinear support-rotor system, a test sensing system and a base. The heating temperature of a disc-shaft connection rotor system can be accurately controlled by an igniter. By adjusting the gas valve of the igniter, the firepower of the igniter can be controlled, and the disc-shaft connection rotor system can be heated within different temperature ranges. The thermal deformation of a disc-shaft connection rotor system in an environment with uniform temperature distribution can be measured, and the thermal deformation in an environment with non-uniform temperature distribution and the thermal deformation under a variable speed condition can be measured.

Description

technical field [0001] The invention belongs to the field of thermal effect analysis and thermal deformation measurement of an aero-engine disk-shaft connection rotor system, and relates to a disk-shaft connection rotor system thermal analysis test bench and a method for measuring thermal deformation thereof. Test rig for thermal deformation of disc-shaft coupled rotor systems in a uniformly distributed environment and under variable speed conditions. Background technique [0002] With the continuous improvement of the performance of aero-engines, more and more of its critical parts adopt the overall structural design, and a large number of difficult-to-machine materials such as titanium alloys and high-temperature alloys are used. The improvement and upgrading of processing technology and equipment is an inevitable trend. The technological research of the integral disk and shaft parts of the new structure is particularly important. Disc shaft parts are rotating parts, whic...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/02
CPCG01M13/022
Inventor 丁喆罗忠李玉奇栗江韩清凯任红军
Owner NORTHEASTERN UNIV
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