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Aero-engine rotor air floatation assembling method and device based on inductance measurement

An aero-engine, inductance measurement technology, applied in the field of mechanical assembly, 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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Problems solved by technology

[0010] Aiming at the deficiencies in the above existing technologies, a method and device for air-floating assembly of aero-engine rotors based on inductance measurement is proposed to solve the problem of low coaxiality of aero-engine rotors after assembly, and to achieve high coaxiality and reduce Small vibration, easy installation, high flexibility, purpose of improving engine performance

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  • Aero-engine rotor air floatation assembling method and device based on inductance measurement
  • Aero-engine rotor air floatation assembling method and device based on inductance measurement

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Embodiment Construction

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

[0021] An air-floating assembly method and device for an aero-engine rotor based on inductance measurement, the method and device are as follows: a three-jaw hydraulic chuck 4 is arranged on the center position 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 air bearing 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 lower lever type inductive ...

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Abstract

The invention discloses an aero-engine rotor air floatation assembling method and device based on inductance measurement, and belongs to the machine assembling technology. The measuring method and device are based on an air flotation rotating shaft system to determine a rotary benchmark. The method comprises the steps that the angle positioning of a rotary table is determined according to a circular grating; the radial error of a radial assembling face and the inclined error of an axial assembling face of rotors are extracted based on a four-measuring-head measuring device, and the influence weight of the rotors on the assembled rotor coaxiality is obtained; all the required rotors are measured and assembled respectively, and the influence weight of the rotors on the assembled rotor coaxiality is obtained; vector optimization is carried out on the weights of the rotors, and the assembling angles of the rotors are obtained. The method and device can effectively solve the problem that the rotors of an aero-engine are low in coaxiality after being assembled, and have the advantages of being high in coaxiality after the rotors are assembled, reducing vibration, being easy to mount, being high in flexibility, and improving the engine performance.

Description

technical field [0001] The invention belongs to mechanical assembly technology, and mainly relates to an air-floating assembly method and device for an aero-engine rotor based on inductance measurement. 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 experie...

Claims

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Application Information

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IPC IPC(8): G01B7/30G01B7/312G01B7/305
Inventor 谭久彬孙传智王雷
Owner HARBIN INST OF TECH
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