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Elastic algorithm for calculating rotor assembly pose based on end jump measurement

A rotor assembly and rotor technology, which is applied in computing, special data processing applications, instruments, etc., can solve the problem of not considering contact deformation, etc., and achieve the effect of improving the assembly qualification rate, improving the coaxiality of the rotor, and accurately predicting

Active Publication Date: 2019-08-02
DALIAN UNIV OF TECH
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Problems solved by technology

[0004] A common flaw of these prediction algorithms is that they assume rigid stacking and do not take into account actual contact deformation

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  • Elastic algorithm for calculating rotor assembly pose based on end jump measurement
  • Elastic algorithm for calculating rotor assembly pose based on end jump measurement
  • Elastic algorithm for calculating rotor assembly pose based on end jump measurement

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Embodiment Construction

[0045] The specific implementation manners of the present invention will be further described below in conjunction with the accompanying drawings and technical solutions.

[0046] An elastic algorithm for calculating the rotor assembly pose based on end jump measurements,

[0047] Basic assumption: the asperities on the mating surface are extruded against each other under the action of external force and undergo elastic deformation. The deformation behavior of the asperities is analyzed according to the Hertz contact theory, and the plastic deformation is not considered.

[0048] as attached figure 1 , with two adjacent disks, the upper and lower centers of rotor A are: A o2 、A o1 , the upper and lower centers of the rotor B are respectively: B O2 , B O1 , the mating surface of the two rotors is the upper end surface A of rotor A 2 And rotor B lower end surface B 1 ; Two contact surfaces A 2 , B 1 Represented by a matrix, the form of the data is a ring, respectively A...

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Abstract

The invention discloses an elastic algorithm for calculating a rotor assembly pose based on end jump measurement. A rotor matching surface is equivalent to a plurality of micro-convex body contact pairs; the contact elastic deformation is calculated by using a Hertz contact rule, contact pairs which actually contact with each other are separated; the final contact state is judged through the energy and torque balance equation, the normal vector of the contact plane is finally solved to represent the contact pose, the rotor assembly pose prediction accuracy is improved, the assembly coaxialitycan be well reflected, and rotor assembly phase prediction and optimization are better achieved. The method is based on actually measured end hop data in actual production; elastic deformation generated in the assembly process is considered; the method has the advantages that the defects of a rigid prediction algorithm are overcome, the accurate prediction of the assembly pose before assembly is realized, the rotor coaxiality after assembly is improved, meanwhile, the one-time assembly qualification rate is greatly improved, and the method has important practical guiding significance for axisprediction and assembly phase adjustment and optimization in the assembly process of the aero-engine rotor piece.

Description

technical field [0001] The invention proposes an elastic algorithm for calculating the axis pose of rotor assembly, which can be applied to axis prediction and assembly phase optimization in the assembly process of important components such as aeroengine high-pressure compressor rotors, high-pressure turbine discs, and low-pressure rotor assemblies. , During the assembly guidance process. Background technique [0002] In the assembly process of high-precision aero-engine components, it is necessary to ensure the coaxiality after assembly. Since "trial and error" assembly requires repeated trial assembly and deployment, in order to improve assembly efficiency, reduce costs, and improve the assembly accuracy of rotor components, it is necessary to accurately predict and optimize the phase before assembly. Therefore, to improve the success rate of an assembly, it is necessary to seek the relationship between the runout shape before assembly and the axis deflection after assemb...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/20
Inventor 孙清超高一超刘鑫马跃李震汪云龙赵斌斌
Owner DALIAN UNIV OF TECH
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