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Method and device for magnetic levitation assembly of pneumatic grabbing clamping type aeroengine rotors on basis of inductosyn angle measurement

An inductive synchronizer, pneumatic grab-type technology, applied in measuring devices, electrical devices, instruments, etc., can solve problems such as low coaxiality, and achieve the effects of reducing noise pollution, reducing vibration, and saving fuel consumption

Inactive Publication Date: 2014-05-14
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0010] Aiming at the deficiencies in the above-mentioned existing technologies, a method and device for maglev assembly of the aero-engine rotor with pneumatic gripping based on the angle measurement of the induction synchronizer is proposed to solve the problem of low coaxiality of the aero-engine rotor after assembly, and to achieve High coaxiality, reduced vibration, easy installation, high flexibility, and improved engine performance

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  • Method and device for magnetic levitation assembly of pneumatic grabbing clamping type aeroengine rotors on basis of inductosyn angle measurement
  • Method and device for magnetic levitation assembly of pneumatic grabbing clamping type aeroengine rotors on basis of inductosyn angle measurement

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Embodiment Construction

[0020] Below in conjunction with accompanying drawing, the present invention is described in further detail:

[0021] A method and device for maglev assembly of a pneumatic gripper type aeroengine rotor based on angle measurement by an inductive synchronizer. The method and device are as follows: a three-jaw pneumatic chuck 4 is arranged at the center of a centering and tilting workbench 3 . The left column 5 a and the right column 5 b are symmetrically distributed on both sides of the maglev shafting 2 and fixed on the base 1 . On the left column 5a, the left upper column connector 7c and the left lower column connector 7a are movably adjusted sequentially from top to bottom, and the left upper horizontal measuring rod 6c is horizontally nested on the left upper column connector 7c. The sensor 8b is fixedly connected with the upper left lateral measuring rod 6c; the lower left lateral measuring rod 6a is horizontally nested on the lower left pole connecting piece 7a, and the ...

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Abstract

The invention discloses a method and device for magnetic levitation assembly of pneumatic grabbing clamping type aeroengine rotors on the basis of inductosyn angle measurement, and belongs to the mechanical assembly technologies. According to the method and device, the rotation base is determined on the basis of a magnetic levitation rotary shaft system; angle location of a rotary platform is determined through an inductosyn; radial errors of a radial assembly surface and inclination errors of an axial assembly surface of each rotor are extracted on the basis of a measuring device with four measuring heads, and the weight of influence, caused by each rotor, on the coaxiality of the assembled corresponding rotor is obtained; all the rotors needing assembly are measured to obtain the weights of influence, caused by the rotors, on the coaxiality of the assembled corresponding rotors are obtained; vector optimization is carried out on the weights of the rotors to obtain assembly angles of the rotors. The method and device for magnetic levitation assembly of the pneumatic grabbing clamping type aeroengine rotors on the basis of inductosyn angle measurement can effectively solve the problem that coaxiality of assembled aeroengine rotors is low, and have the advantages that the coaxiality of the assembled rotors is high, the vibration amplitude is reduced, installation is easy, flexibility is high, and engine performance is improved.

Description

technical field [0001] The invention belongs to the mechanical assembly technology, and mainly relates to a method and device for maglev assembly of aero-engine rotors with pneumatic grippers based on angle measurement by an induction synchronizer. 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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B7/30G01B7/305G01B7/312
Inventor 王雷谭久彬杨文国金国良
Owner HARBIN INST OF TECH