CN210958111U - High-rotation-speed end-face magnetic coupling structure - Google Patents

High-rotation-speed end-face magnetic coupling structure Download PDF

Info

Publication number
CN210958111U
CN210958111U CN201922001973.8U CN201922001973U CN210958111U CN 210958111 U CN210958111 U CN 210958111U CN 201922001973 U CN201922001973 U CN 201922001973U CN 210958111 U CN210958111 U CN 210958111U
Authority
CN
China
Prior art keywords
magnetic
mounting seat
disk mounting
magnetic disk
rotational speed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201922001973.8U
Other languages
Chinese (zh)
Inventor
吴进军
李�荣
章曙
王海朋
陈强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rongtong Aviation Engine Technology Co ltd
Original Assignee
No 60 Institute of Headquarters of General Staff of PLA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by No 60 Institute of Headquarters of General Staff of PLA filed Critical No 60 Institute of Headquarters of General Staff of PLA
Priority to CN201922001973.8U priority Critical patent/CN210958111U/en
Application granted granted Critical
Publication of CN210958111U publication Critical patent/CN210958111U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The utility model discloses a high rotational speed terminal surface magnetic coupling structure solves the technical problem of current high rotational speed vibration isolation, transmission power, belongs to the flexible shaft coupling field of high rotational speed. A high-rotation-speed end face magnetic coupling structure comprises a driving shaft, a driving end disk mounting seat, a magnetic ring, a spacer, a driven end disk mounting seat, a driven shaft and a gap adjusting gasket. The magnetic disk mounting seat is fixed with the shaft, and a dynamic balance weight-removing area is reserved in the magnetic disk mounting seat; the magnetic ring is arranged in the magnetic disk mounting seat and is in interference fit with the magnetic disk mounting seat; the magnetic pole between the N pole and the S pole in the magnetic ring; and a clearance of about 0.5mm is reserved between the driving end disk and the driven end disk, and the clearance is adjusted by a clearance adjusting gasket. The utility model discloses can use at high rotational speed, refer in particular to 60000r/min and above transmission field, realize the flexible hookup of high rotational speed, the utility model discloses under the operating condition, the vibration is little, can stabilize the transmission moment of torsion, and life is high, and is with low costs.

Description

High-rotation-speed end-face magnetic coupling structure
Technical Field
The utility model relates to a high rotational speed terminal surface magnetic coupling structure for solve the technological problem of the steady transmission power of current high rotational speed, belong to the flexible shaft coupling field of high rotational speed.
Background
The high-speed coupling is a difficult point of research at home and abroad, and is particularly applied to the application field of the rotating speed of more than 60000rpm (the rpm is a rotating speed unit, and 1rpm represents 1 revolution per minute). At present, only the high-precision diaphragm coupling is applied in the field of high-rotating-speed power transmission more mature. The high-precision diaphragm coupler has high requirements on processing and manufacturing errors and application and assembly errors of parts, so that the coupler is high in manufacturing cost and maintenance cost and is difficult to be widely applied to engineering.
The magnetic coupling structure is an important method for realizing non-contact power transmission and torque transmission, and can be operated under the condition of centering error. However, the magnetic coupling structure is rarely applied to the field of high-speed transmission, and the main reasons are as follows: on one hand, the magnetic coupling is used as a part of the rotor, and is easy to generate violent vibration at high rotating speed, so that the system operation is influenced; on the other hand, the magnetic coupling has small tensile stress intensity, and the centrifugal tensile stress at high rotating speed can damage the magnetic coupling.
Chinese patent (granted publication number: CN104795964B) discloses a high-speed permanent magnet coupling. Structurally, this structure is a cartridge-type permanent magnet coupling. Although the patent specification is applicable to the field of 50000rpm high speed motors, as the barrel coupling structure, the greater the power transfer requirement, the longer the magnetic barrel. And the longer magnetic cylinder can generate larger vibration displacement and vibration force to influence the stable operation of the system at high rotating speed.
Disclosure of Invention
The utility model aims to solve the technical problem that, through designing a high rotational speed terminal surface magnetic coupling structure, realize the flexible hookup of initiative axle head and passive axle head, the vibration is little, can stabilize the transmission moment of torsion, and life is high, and is with low costs.
In order to achieve the purpose, the utility model relates to a high rotational speed terminal surface magnetic coupling, including drive end disk mount pad, driven end disk mount pad, drive end disk mount pad set up on the driving shaft, driven end disk mount pad sets up on the driven shaft, sets up the magnetic ring in drive end disk mount pad, driven end disk mount pad respectively, magnetic ring and disk mount pad interference fit, two magnetic ring polarity are opposite, set up the spacer on the face that drive end disk mount pad, driven end disk mount pad are relative, the spacer seals the magnetic ring in the disk mount pad, sets up 0.5mm-0.7 mm's clearance between drive end disk mount pad and the driven end disk mount pad.
The magnetic ring is of a circular ring-shaped integral structure.
The interference magnitude between the magnetic ring and the magnetic disk mounting seat is not less than 0.07 mm.
The spacer is firmly welded with the disk mounting seat.
The gap adjusting device further comprises a gap adjusting gasket, and the gap adjusting gasket is arranged on the driving shaft or the driven shaft.
The utility model firstly selects the end-face type magnetic coupling structure, and avoids the severe vibration of the rotor at high rotating speed caused by overlong cantilever at the end of the magnetic coupling; secondly, a magnetic ring structure is adopted instead of a fan-shaped magnetic sheet structure, so that the phenomenon that unbalance is generated during assembly to cause severe vibration at high rotating speed is avoided; the tensile stress generated by the high-speed rotation of the magnetic ring is offset through the interference fit design, so that the magnetic ring does not bear the tensile stress within the working rotating speed range, and the magnetic ring is prevented from cracking during working; and finally, a dynamic balance weight removing area is designed on the disk mounting seat, and unbalanced vibration at high rotating speed can be reduced by dynamically balancing the disk coupling. The utility model discloses have the function that the installation is simple, the vibration isolation is fallen and is fallen, stabilize transmission power, simultaneously under high rotational speed, especially the rotational speed is in 60000rpm and above rotor system, this shaft coupling operation is stable, and the vibration is little, long service life.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a partial enlarged view of the present invention;
FIG. 3 is a schematic structural view of a disk mounting base according to the present invention;
fig. 4 is a schematic view of the magnetic ring of the present invention.
Wherein: 1-driving shaft; 2-drive end disk mounting seat; 3-a magnetic ring; 4-a spacer; 5-driven end disk mounting base; 6-driven shaft; 7-gap adjusting gasket.
Detailed Description
The following is a detailed description of the present invention:
examples
As shown in fig. 1, the utility model relates to a high rotational speed terminal surface magnetic coupling structure contains driving shaft 1, driving end disk mount pad 2, magnetic ring 3, spacer 4, driven end disk mount pad 5, driven shaft 6, transfers clearance gasket 7. The magnetic disk mounting seat is fixed with the shaft, and a dynamic balance weight-removing area is reserved in the magnetic disk mounting seat; the magnetic ring is arranged in the magnetic disk mounting seat, the magnetic ring is in interference fit with the magnetic disk mounting seat, and a magnetic pole is arranged between the N pole and the S pole in the magnetic ring; the magnetic ring is sealed in the magnetic disk mounting seat by the spacer; and a clearance of about 0.5mm is reserved between the driving end disk and the driven end disk, and the clearance is adjusted by a clearance adjusting gasket. When the driving shaft rotates, the driven shaft is driven to rotate through the magnetic attraction between the magnetic rings.
As shown in fig. 4, the magnet ring 3 is a circular ring-shaped integral structure.
As shown in fig. 2, 3 and 4, the outer annular surface of the magnetic ring 3 is in interference fit with the inner annular surfaces of the disk mounting seats 2 and 5. The magnetic ring is in interference fit with the disk mounting seat, and the design requirement P of the interference magnitude lies in that: the designed interference magnitude counteracts the centrifugal tensile stress generated by the high-speed rotation of the magnetic ring, so that the magnetic ring still does not bear the tensile stress at the maximum working speed. Taking a certain embodiment as an example, the diameter of the magnetic ring is 4.5mm, the diameter of the magnetic ring is 15mm, and the maximum rotating speed is 90000 rpm. According to the conditions, the maximum centrifugal pressure borne by the magnetic ring under the condition of no interference fit is calculated through a formula.
Figure DEST_PATH_GDA0002457249210000031
Figure DEST_PATH_GDA0002457249210000032
F, centrifugal force; m mass; r radius; omega angular velocity; rho material density; d theta single sector infinitesimal; dr radial infinitesimal; l disc axial length; p centrifugal pressure (pressure); a, the centrifugal force action area of a single sector; and f, frequency conversion. And calculating to obtain the maximum centrifugal pressure of the magnetic ring to be 49 MPa. The interference magnitude is designed to be not less than 0.07mm according to the maximum centrifugal pressure and the coordinated deformation of the magnetic ring and the magnetic disk mounting seat.
As shown in fig. 2 and 3, dynamic balance weight removing regions are provided on the back surfaces of the disk mounting base 2 and the disk mounting base 5, and unbalance vibration at a high rotation speed can be reduced by performing dynamic balance on the magnetic coupling.
As shown in fig. 1 and 2, the two spacers 4 are connected to the drive-side disk mount 2 and the driven-side disk mount 5, respectively, by laser welding. The laser welding form is reliable, the heat diffusion range is small, demagnetization of the magnetic ring cannot be caused, and the laser welding method is very effective.
Above embodiment only is for explaining the utility model discloses a technical thought can not be injectd with this the utility model discloses a protection scope, all according to the utility model provides a technical thought, any change of doing on technical scheme basis all falls into the utility model discloses within the protection scope.

Claims (5)

1. The utility model provides a high rotational speed terminal surface magnetic coupling which characterized in that: the magnetic ring magnetic disk drive comprises a drive end magnetic disk mounting seat and a driven end magnetic disk mounting seat, wherein the drive end magnetic disk mounting seat is arranged on a drive shaft, the driven end magnetic disk mounting seat is arranged on a driven shaft, magnetic rings are respectively arranged in the drive end magnetic disk mounting seat and the driven end magnetic disk mounting seat, the magnetic rings are in interference fit with the magnetic disk mounting seats, the polarities of the two magnetic rings are opposite, spacers are arranged on the opposite surfaces of the drive end magnetic disk mounting seat and the driven end magnetic disk mounting seat, the spacers seal the magnetic rings in the magnetic disk mounting seats, and a gap of 0.5-0.7 mm is arranged between the drive end magnetic disk mounting seat and the driven end magnetic disk mounting seat.
2. The magnetic coupling of claim 1, wherein: the magnetic ring is of a circular ring-shaped integral structure.
3. The magnetic coupling of claim 1, wherein: the interference magnitude between the magnetic ring and the magnetic disk mounting seat is not less than 0.07 mm.
4. The magnetic coupling of claim 1, wherein: the spacer is firmly welded with the disk mounting seat.
5. The magnetic coupling of claim 1, wherein: the gap adjusting device further comprises a gap adjusting gasket, and the gap adjusting gasket is arranged on the driving shaft or the driven shaft.
CN201922001973.8U 2019-11-19 2019-11-19 High-rotation-speed end-face magnetic coupling structure Active CN210958111U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922001973.8U CN210958111U (en) 2019-11-19 2019-11-19 High-rotation-speed end-face magnetic coupling structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922001973.8U CN210958111U (en) 2019-11-19 2019-11-19 High-rotation-speed end-face magnetic coupling structure

Publications (1)

Publication Number Publication Date
CN210958111U true CN210958111U (en) 2020-07-07

Family

ID=71376493

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922001973.8U Active CN210958111U (en) 2019-11-19 2019-11-19 High-rotation-speed end-face magnetic coupling structure

Country Status (1)

Country Link
CN (1) CN210958111U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113389750A (en) * 2021-07-29 2021-09-14 深圳飞磁科技有限公司 High-speed contactless magnetic suspension coupling for suspension blower
CN114234003A (en) * 2021-12-03 2022-03-25 徐州新电高科电气有限公司 Cloud platform camera structure suitable for electric power

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113389750A (en) * 2021-07-29 2021-09-14 深圳飞磁科技有限公司 High-speed contactless magnetic suspension coupling for suspension blower
CN114234003A (en) * 2021-12-03 2022-03-25 徐州新电高科电气有限公司 Cloud platform camera structure suitable for electric power

Similar Documents

Publication Publication Date Title
CN210958111U (en) High-rotation-speed end-face magnetic coupling structure
CN202197205U (en) Variable torque and variable speed permanent magnetic coupler
CN102324830B (en) Vertical permanent magnetic variable torque variable speed coupler with radiating device
CN203457028U (en) Coaxial sleeve type permanent magnetic eddy current coupling employing magnet-gathering type magnetic circuit structure
CN111946656A (en) Combined permanent magnetic suspension bearing for pump
CN104506015A (en) Magnetic transmission device
CN107465286B (en) Permanent magnet rotor structure
CN101571161A (en) Magnetic sliding bearing
CN100441891C (en) Permanent magnetism and turbine composite bearing
CN110259952B (en) Rotary dynamic sealing device of centrifugal machine
CN207261255U (en) A kind of Fluorine-lined magnetic centrifugal pump
CN104005797B (en) Gas turbine rotor supporting mechanism and the gas turbine with this supporting mechanism
CN112849383A (en) Sealed rim propeller or generator
CN204156709U (en) A kind of hybrid permanent magnet eddy-current coupling
CN103107679A (en) Permanent magnet eddy coupling with smaller time-lag effects in disc type
CN103490589A (en) Coaxial sleeve type permanent magnet eddy-current coupling with magnetic coagulation type magnetic circuit structure
CN210034331U (en) Permanent magnet flexible transmission gear
CN212407292U (en) Upper driving type main shaft complex for centrifugal supergravity device
CN212868447U (en) Mechanical sealing device for pressure screen
CN205278381U (en) Rotation type multi -spring seal structure
CN210920119U (en) Rotary dynamic sealing device of centrifugal machine
CN104253523A (en) Combined permanent magnet eddy current speed governor
CN210318214U (en) Rotor bearing of horizontal end suction pump
CN204559269U (en) A kind of modular rotor structure of magneto
CN203734504U (en) Plug-in type permanent magnetic driving speed governor

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20230629

Address after: 211299 3rd Floor, Comprehensive Experimental Building, No.1 Science and Technology Innovation Avenue, Lishui Economic Development Zone, Nanjing, Jiangsu Province

Patentee after: Rongtong Aviation Engine Technology Co.,Ltd.

Address before: No. 766, Zhujiang Road, Xuanwu District, Nanjing City, Jiangsu Province, 210016

Patentee before: NO.60 INSTITUTE OF THE HEADQUARTERS OF GENERAL STAFF OF PLA

TR01 Transfer of patent right