公开(公告)号：US09890661B2

公开(公告)日：2018-02-13

申请号：US15118322

申请日：2014-12-26

Applicant: HARBIN INSTITUTE OF TECHNOLOGY

Inventor： Jiubin Tan ,  Chuanzhi Sun ,  Lei Wang ,  Bo Zhao

IPC: F01D25/28 ,  G01B7/31 ,  G01C9/06

CPC classification number: F01D25/28 ,  F01D5/027 ,  F01D25/285 ,  F05D2230/60 ,  F05D2260/83 ,  G01B7/31 ,  G01C9/06 ,  G01C2009/064

Abstract: An aero engine rotor air floatation assembling method and device based on a gantry structure belong to mechanical assembling technology. The present invention can effectively solve 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 measuring method and device are: determining rotary reference based on a rotary air bearing; determining the angular positioning of a rotary table according to a grating ruler; 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 required for assembling 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.

公开(公告)号：US20150260255A1

公开(公告)日：2015-09-17

申请号：US14421610

申请日：2014-02-19

Applicant: HARBIN INSTITUTE OF TECHNOLOGY

Inventor： Jiubin Tan ,  Junning Cui ,  Lei Wang

IPC: F16F15/03 ,  G01L19/00 ,  G01D5/20 ,  F16F15/00 ,  H02K41/035

CPC classification number: F16F15/03 ,  F16F15/002 ,  F16F15/0232 ,  G01D5/20 ,  G01L19/0061 ,  H02K41/0356

Abstract: A magnetically suspended vibration isolator with zero stiffness whose angle degree of freedom is decoupled with a joint ball bearing has a main body, in which a sleeve and a lower mounting plate are supported with a magnetically suspended thrust bearing, a piston cylinder and the sleeve are lubricated and supported with a cylinder air bearing surface, and the angle degree of freedom between a upper mounting plate and the lower mounting plate is decoupled with a joint ball bearing; a position close-loop control system comprising voice coil motors, displacement sensors, limit switches, a controller and a driver is introduced, and the relative position between the upper mounting plate and the lower mounting plate is precisely controlled.

Abstract translation: 具有零刚度的磁悬浮隔振器，其角度自由度用接头球轴承解耦具有主体，其中套筒和下安装板由磁悬浮推力轴承，活塞缸和套筒支撑 通过气缸空气轴承表面进行润滑和支撑，上安装板和下安装板之间的角度自由度用接头球轴承分离; 引入了包括音圈电机，位移传感器，限位开关，控制器和驱动器的位置闭环控制系统，并且精确地控制了上安装板和下安装板之间的相对位置。

公开(公告)号：US20150219179A1

公开(公告)日：2015-08-06

申请号：US14421378

申请日：2014-02-19

Applicant: HARBIN INSTITUTE OF TECHNOLOGY

Inventor： Junning Cui ,  Jiubin Tan ,  Lei Wang

IPC: F16F15/03 ,  F16F15/00 ,  G03F7/20 ,  G01D5/20 ,  G01L19/00 ,  H02K41/035 ,  F16C32/06 ,  G01B7/00

CPC classification number: F16F15/03 ,  F16C32/0614 ,  F16F15/002 ,  G01B7/003 ,  G01D5/20 ,  G01L19/00 ,  G03F7/70833 ,  H02K41/0356

Abstract: A vibration isolator with zero stiffness whose angle degree of freedom is decoupled with a spherical air bearing has a main body, in which a sleeve and a lower mounting plate, a piston cylinder and the sleeve are both lubricated and supported with air bearing surfaces respectively, and the angle degree of freedom between a upper mounting plate and the lower mounting plate is decoupled with a spherical air bearing; a position close-loop control system comprising voice coil motors, displacement sensors, limit switches, a controller and a driver is introduced, and the relative position between the upper mounting plate and the lower mounting plate is precisely controlled.

Abstract translation: 具有零刚度的隔振器，其角度自由度用球形空气轴承解耦，其主体具有主体，其中套筒和下安装板，活塞缸和套筒分别被润滑并支撑在空气轴承表面上， 上安装板和下安装板之间的角度自由度用球形空气轴承分离; 引入了包括音圈电机，位移传感器，限位开关，控制器和驱动器的位置闭环控制系统，并且精确地控制了上安装板和下安装板之间的相对位置。