Aero-engine rotor stacking assembly method and device based on capacitance sensing and magnetic levitation supporting
A technology of capacitive sensing and inductive sensing, which is applied in the field of mechanical assembly, can solve the problems of low coaxiality, reduce noise pollution, save installation time and cost, and save fuel consumption
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, a method and device for stacking and assembling aero-engine rotors based on capacitive sensing and maglev support is proposed to solve the problem of low coaxiality of the aero-engine rotors after assembly and to achieve the coaxiality of the rotors after assembly. High, reduce vibration, easy installation, high flexibility, and improve engine performance
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[0020] Below in conjunction with accompanying drawing, the present invention is described in further detail:
[0021] A method and device for stacking and assembling aircraft engine rotors based on capacitive sensing and maglev support. The method and device are as follows: a four-jaw pneumatic chuck 4 is arranged on the center position of a centering and tilting workbench 3 . The left moving guide rail 10a and the right moving guide rail 10b are symmetrically distributed on the base 1 on both sides of the magnetic suspension shaft system 2, the left column 5a is installed on the left moving guide rail, and the right column 5b is installed on the right moving guide rail. 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 l...
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The invention discloses an aero-engine rotor stacking assembly method and device based on capacitance sensing and magnetic levitation supporting and belongs to the mechanical assembly technology. According to a measuring method and device, rotation standards are determined based on a magnetic levitation rotating shaft system; angle positioning of a rotary table is determined according to an inductosyn; based on the four-measuring-head measuring device, the radial error of the radial assembly faces of rotors and the tilt error of the axial assembly faces of the rotors are extracted, and the influence weights of the rotors on the coaxiality obtained after assembly of the rotors are obtained; all the rotors needed during assembly are measured respectively, and the influence weights of the rotors on the coaxiality obtained after assembly of the rotors are obtained; vector optimization is conducted on the weights of the rotors, and the assembly angles of the rotors are obtained. The aero-engine rotor stacking assembly method and device based on capacitance sensing and magnetic levitation supporting can effectively solve the problem that the coaxiality obtained after assembly of the aero-engine rotors is low, and have the advantages that the coaxiality obtained after assembly of the aero-engine rotors is high, vibration is reduced, installation is easy, the flexibility ratio is high, and engine performance is improved.
Description
technical field [0001] The invention belongs to mechanical assembly technology, and mainly relates to an aeroengine rotor stacking assembly method and device based on capacitive sensing and maglev support. 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 expe...
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Login to View More IPC IPC(8): G01B7/30G01B7/305G01B7/312
Inventor 赵勃谭久彬王雷
Owner HARBIN INST OF TECH