Title:
AIRCRAFT ENGINE ROTOR AIR FLOTATION ASSEMBLY METHOD AND DEVICE BASED ON GANTRY STRUCTURE
Document Type and Number:
WIPO Patent Application WO2015120745
Kind Code:
A1
Abstract:
An aircraft engine rotor air flotation assembly method and device based on a gantry structure, belonging to the field of mechanical assembly technology. The present invention effectively solves the problem that aircraft engine rotors have low coaxiality after being assembled, and has the advantages that rotors have high coaxiality after being assembled, vibration is reduced, installation is easy, flexibility is high, and engine performance is improved. A measurement method and device are based on an air flotation rotary shaft system determining a rotary reference. According to a grating ruler (2f), angular positioning of a turntable is determined. Based on a measurement device having four measuring heads, a radial error of a rotor radial assembly surface and a tilt error of an axial mounting surface are extracted, and an influence weight value of the rotor on the coaxiality of assembled rotors is obtained. All the rotors required for assembly are measured respectively, and an influence weight value of each rotor on the coaxiality of the assembled rotors is obtained. Vector optimisation is performed on the weight value of each rotor and an assembly angle of each rotor is obtained.
Inventors:
TAN JIUBIN (CN)
SUN CHUANZHI (CN)
WANG LEI (CN)
ZHAO BO (CN)
SUN CHUANZHI (CN)
WANG LEI (CN)
ZHAO BO (CN)
Application Number:
PCT/CN2014/095057
Publication Date:
August 20, 2015
Filing Date:
December 26, 2014
Export Citation:
Assignee:
HARBIN INST OF TECHNOLOGY (CN)
International Classes:
G01B7/312; G01B7/305
Foreign References:
| CN103808252A | 2014-05-21 | |||
| CN101799354A | 2010-08-11 | |||
| US20060112577A1 | 2006-06-01 | |||
| CN1635589A | 2005-07-06 |
Attorney, Agent or Firm:
KINGSOUND & PARTNERS (CN)
北京金信知识产权代理有限公司 (CN)
北京金信知识产权代理有限公司 (CN)
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