Invention Grant
- Patent Title: Aero engine rotor assembling method and device based on concentricity and verticality measurement
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Application No.: US15118312Application Date: 2014-12-26
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Publication No.: US09709392B2Publication Date: 2017-07-18
- Inventor: Lei Wang , Bo Zhao , Jiubin Tan , Chuanzhi Sun
- Applicant: HARBIN INSTITUTE OF TECHNOLOGY
- Applicant Address: CN Harbin, Heilongjiang
- Assignee: HARBIN INSTITUTE OF TECHNOLOGY
- Current Assignee: HARBIN INSTITUTE OF TECHNOLOGY
- Current Assignee Address: CN Harbin, Heilongjiang
- Agency: Nixon & Vanderhye P.C.
- Priority: CN201410052148 20140214
- International Application: PCT/CN2014/095050 WO 20141226
- International Announcement: WO2015/120744 WO 20150820
- Main IPC: G01B7/30
- IPC: G01B7/30 ; G01B21/24 ; G01M15/02 ; G01B21/02 ; G01B9/02 ; F01D5/02 ; F01D5/30

Abstract:
An aero engine rotor assembling method and device based on concentricity and verticality measurement belongs to mechanical assembly technology. The present invention effectively solves the problem of poor coaxality after the aero engine rotor is assembled and has the characteristics of high coaxality after the rotor is assembled, reduced vibration, mounting easiness, high flexibility and improved engine performance. The measurement and device is: determining rotary reference; determining the angular positioning of a rotary table; extracting the radial error of the radial mounting plane and the inclination error of the axial mounting plane of the rotor based on the four-probe measuring device to obtain the influencing weight of this rotor to the assembled rotor on coaxality; measuring respectively all the rotors to obtain the influencing weight of each rotor to the assembled rotor on coaxality; vector optimizing the weight of each rotor to obtain the assembling angle of each rotor.
Public/Granted literature
- US20170167866A1 AERO ENGINE ROTOR ASSEMBLING METHOD AND DEVICE BASED ON CONCENTRICITY AND VERTICALITY MEASUREMENT Public/Granted day:2017-06-15
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