Aero-engine rotor assembly method and device based on aligning and tilt adjusting rotary platform

A technology for assembly of aero-engines and rotors, applied in measuring devices, electrical devices, instruments, etc., can solve problems such as low coaxiality, and achieve the effects of reducing noise pollution, saving fuel consumption, and reducing vibration

Inactive Publication Date: 2014-05-14
HARBIN INST OF TECH
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Problems solved by technology

[0010] In view of the deficiencies in the above existing technologies, an aeroengine rotor assembly method and device based on a self-aligning and tilting turntable is proposed to solve the problem of low coaxi

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  • Aero-engine rotor assembly method and device based on aligning and tilt adjusting rotary platform
  • Aero-engine rotor assembly method and device based on aligning and tilt adjusting rotary platform

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[0020] The present invention will be described in further detail below in conjunction with the accompanying drawings:

[0021] An aeroengine rotor assembly method and device based on a centering and tilting turntable. The method and device are as follows: a three-jaw hydraulic chuck 4 is arranged on the center position of the centering and tilting table 3. The left upright 5a and the right upright 5b are symmetrically distributed on both sides of the maglev shaft system 2 and fixedly mounted on the base 1; the left upright 5a is movably and adjustablely sleeved from top to bottom on the left upright pole connecting piece 7c and the left downright pole The rod connector 7a, the upper left lateral measuring rod 6c is horizontally nested on the upper left pillar connecting piece 7c, the upper sensor adapter 10b is fixedly connected with the upper left lateral measuring rod 6c, the upper axial eddy current sensor 8b and the upper sensor adapter 10b fixed connection; the lower left la...

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Abstract

The invention discloses an aero-engine rotor assembly method and device based on an aligning and tilt adjusting rotary platform, and belongs to the mechanical assembly technology. According to the assembly method and device, rotation reference is determined based on a magnetic levitation rotation shaft system, angle location of the rotary platform is determined through an inductosyn, the radial error of the radial assembly face and the inclination error of the axial assembly face of each rotor are extracted through a four-measuring-head measurement device, and the weight of influence on the coaxiality of the assembled rotors from the rotors is obtained; all the rotors needed by assembly are measured, and the weight of influence on the coaxiality of the assembled rotors from the rotors is obtained; vector optimization is carried out on the weight of each rotor, and then the assembly angle of each rotor is obtained. The aero-engine rotor assembly method and device based on the aligning and tilt adjusting rotary platform can effectively solve the problem of the low coaxiality after the aero-engine rotors are assembled, and have the advantages that the coaxiality achieved after the rotors are assembled is high, vibration is reduced, installation is easy, the flexibility is high, and performance of an engine is improved.

Description

technical field [0001] The invention belongs to mechanical assembly technology, and mainly relates to an aeroengine rotor assembly method and device based on a self-aligning and tilting turntable. Background technique [0002] Aeroengine assembly is the last link in the manufacturing process of aeroengine, and it is also one of the most important manufacturing links. Under the conditions of the existing aero-engine design scheme and processing technology level, the quality of assembly and work efficiency have an important impact on the quality, performance and production efficiency of the engine. Therefore, in the assembly process, the coaxiality of the installed rotor should be improved as much as possible, so as to reduce the vibration of the aero-engine and improve the performance of the aero-engine. However, in actual production, the assembly of aero-engines is completely manual assembly. The level of assembly accuracy and stability depends entirely on the experience an...

Claims

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Application Information

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IPC IPC(8): G01B7/30G01B7/305G01B7/312
Inventor 赵勃谭久彬王雷
Owner HARBIN INST OF TECH
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