WO2025112079A1 - Dynamic balancing test method for outer rotor of permanent magnet direct drive motor - Google Patents
Dynamic balancing test method for outer rotor of permanent magnet direct drive motor Download PDFInfo
- Publication number
- WO2025112079A1 WO2025112079A1 PCT/CN2023/136206 CN2023136206W WO2025112079A1 WO 2025112079 A1 WO2025112079 A1 WO 2025112079A1 CN 2023136206 W CN2023136206 W CN 2023136206W WO 2025112079 A1 WO2025112079 A1 WO 2025112079A1
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- WIPO (PCT)
- Prior art keywords
- dynamic balancing
- rotor
- dummy shaft
- expansion sleeve
- rear end
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/14—Determining imbalance
- G01M1/16—Determining imbalance by oscillating or rotating the body to be tested
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/02—Details of balancing machines or devices
Definitions
- the invention relates to the technical field of dynamic balance verification, and in particular to a dynamic balance test method for an outer rotor of a permanent magnet direct-drive motor.
- the rotor of conventional permanent magnet direct-drive motor is an inner rotor structure, and the dynamic balancing of the rotor is carried out by adding a weight method with a balancing block to ensure that the imbalance of the rotor meets the design requirements after dynamic balancing.
- This method is only applicable to rotors with a rotating shaft, which is convenient for the dynamic balancing machine to support, and the balancing block mounting grooves or mounting screw holes are processed on the pressure plates at both ends of the rotor.
- the existing method cannot be used for dynamic balancing verification. How to achieve this new structure of motor rotor to complete the dynamic balancing test reliably, safely and efficiently is a problem that must be solved in motor manufacturing technology.
- the present invention provides a method for dynamic balancing an outer rotor of a permanent magnet direct-drive motor.
- a method for dynamic balancing an outer rotor of a permanent magnet direct drive motor comprises the following steps:
- Step A Install the front end cover and the rear end cover to the corresponding positions at both ends of the rotor and tighten the bolts, and mark A at the same time;
- Step B Install the left expansion sleeve and the right expansion sleeve on the rear end cover and the front end cover respectively, install the front outer cover on the front end cover and tighten the bolts, and mark B at the same time;
- Step C Lift the assembled rotor vertically and place it on a vertical support table with the front end facing downwards.
- Lift the dynamic balancing dummy shaft to the top of the rotor align it with the center of the rotor and slowly drop it until the front and rear conical surfaces of the dynamic balancing dummy shaft abut against the right expansion sleeve and the left expansion sleeve respectively.
- mark C mark C.
- Step D After disassembling the dummy shaft, front end outer cover, locking nut and right expansion sleeve assembled on the rotor, reinstall the right expansion sleeve on the front end conical surface of the dummy shaft according to mark C, and re-tighten the locking nut in place according to mark C. Hoist the reassembled dummy shaft, right expansion sleeve and locking nut onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter S, start the automatic weight removal dynamic balancing machine to complete the overall dynamic balancing test of the dummy shaft and record the final imbalance on both sides. , ;
- Step E Remove the locking nut and right expansion sleeve on the dynamic balancing dummy shaft. Reassemble the disassembled right expansion sleeve, dynamic balancing dummy shaft and the front end outer cover removed in step D with the rotor according to mark B and mark C respectively. Then tighten and install the locking nut according to mark C. Lift the assembled rotor as a whole onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter Q, start the automatic weight removal dynamic balancing machine to complete the rotor weight removal dynamic balancing test and record the final imbalance on both sides. , ;
- Step F hoist the rotor as a whole onto the vertical support platform, remove the locking nut, dynamic balancing dummy shaft, left expansion sleeve and right expansion sleeve, turn the rotor over and place it horizontally, and remove the front outer cover, rear outer cover, front end cover and rear end cover.
- the mark A in step A includes an identification line A marked at the connection between the rotor and the front end cover corresponding to the position of the front end cover and an identification line B marked at the connection between the rotor and the rear end cover corresponding to the position of the rear end cover.
- the mark A in step A also includes a number marked on the head of each bolt, and the same number marked on the position of the corresponding bolt on the front end cover and the rear end cover.
- the mark B in step B includes an identification line C marked at the connection between the left expansion sleeve and the rear end cover and corresponding to the position of the rear end cover, and an identification line D marked at the connection between the right expansion sleeve and the front end cover and corresponding to the position of the front end cover, and also includes an identification line E marked at the connection between the front outer cover and the front end cover and corresponding to the position of the front end cover.
- step C the dynamic balancing dummy shaft is hoisted through the process screw holes provided at the rear end.
- the mark C in step C includes an identification line F marked at the connection between the rear end conical surface of the dynamic balancing dummy shaft and the left expansion sleeve, and an identification line G marked at the connection between the front end conical surface of the dynamic balancing dummy shaft and the right expansion sleeve.
- the mark C in step C also includes an anti-loosening marking line marked at the connection between the dynamic balancing dummy shaft and the locking nut.
- the dynamic balancing machine parameters S in step D include the distance a from the dynamic balancing machine roller support point to the rear end dummy shaft deweighting point, the distance b from the rear end dummy shaft deweighting point to the front end dummy shaft deweighting point, the distance c from the front end dummy shaft deweighting point to the dynamic balancing machine roller support point, the working radius of the front end dummy shaft deweighting point, and the distance c from the front end dummy shaft deweighting point to the dynamic balancing machine roller support point.
- the working radius of the rear end dummy shaft weight removal The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G1.0. , set up,
- middle Preferably, middle, .
- the dynamic balancing machine parameter Q in step E includes the distance A from the dynamic balancing machine roller support point to the rear end weight removal boss, the distance B from the rear end weight removal boss to the front end weight removal boss, the distance C from the front end weight removal boss to the dynamic balancing machine roller support point, and the working radius of the front end weight removal boss.
- the working radius of the rear end de-weighting boss The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G2.5. , set up,
- middle Preferably, middle, .
- step E uniform numbers are marked on the surfaces of the rotor and the joints of each component.
- the taper of the front end tapered surface and the rear end tapered surface is the same as the taper of the tapered surface A in the left expansion sleeve and the tapered surface B in the right expansion sleeve, and the taper ranges from 15 degrees to 20 degrees.
- the roughness of the front end conical surface and the rear end conical surface is no more than 1.6 microns.
- the contact rate between the left expansion sleeve and the rear end conical surface and the contact rate between the right expansion sleeve and the front end conical surface are not less than 85%.
- the axial width of the front end conical surface is greater than the width of the corresponding mounting groove A in the front end end cover, and the axial width of the rear end conical surface is greater than the width of the corresponding mounting groove B in the rear end end cover.
- the surface roughness of the left expansion sleeve and the right expansion sleeve is not greater than 1.6 microns.
- the left expansion sleeve and the rear end cover adopt a transition fit
- the right expansion sleeve and the front end cover adopt a transition fit
- the locking nut includes a large end circular ring portion and a small head portion, the outer diameter of the large end circular ring portion is smaller than the inner diameter of the front end outer cover, the inner diameter of the large end circular ring portion is larger than the minimum diameter of the tapered surface B, and the small head portion is processed into a hexagonal nut shape.
- the beneficial effects of the present invention are: realizing dynamic balancing verification of an outer rotor without a rotating shaft structure and without balancing block mounting grooves or mounting screw holes at both ends; the device has a simple and reliable structure, strong practicality, convenient operation and maintenance, low cost, and is easy to disassemble and assemble, and is suitable for small-batch manufacturing of new outer rotors.
- FIG1 is a schematic diagram of the overall structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture with the rotor of the present invention.
- FIG. 2 is a reference diagram of overall dynamic balancing parameters of the rotor of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
- FIG3 is a schematic diagram of the vertical installation structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
- FIG. 4 is a schematic diagram of the structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
- FIG. 5 is a reference diagram of test parameters of a tooling test for a permanent magnet direct drive motor outer rotor dynamic balancing test according to the present invention.
- FIG. 6 is a cross-sectional view of the dynamic balancing dummy shaft structure of the present invention.
- FIG. 7 is a schematic structural diagram of the locking nut of the present invention.
- FIG8 is a cross-sectional view of the locking nut structure of the present invention.
- FIG. 9 is a schematic diagram of the left expansion sleeve of the present invention.
- Fig. 10 is a schematic diagram of a rotational cross-section taken along the line A-A in Fig. 9 .
- Fig. 11 is a schematic cross-sectional view of the B-B section of Fig. 10 .
- FIG. 12 is a schematic diagram of the right expansion sleeve of the present invention.
- Fig. 13 is a schematic diagram of a rotational cross-section taken at C-C in Fig. 12 .
- Fig. 14 is a schematic cross-sectional view of the D-D section of Fig. 13 .
- a method for dynamic balancing the outer rotor of a permanent magnet direct-drive motor includes the following steps: Step A: Install the front end cover 8 and the rear end cover 6 to the corresponding positions at both ends of the rotor 7, use a marker pen to mark the position corresponding to the front end cover 8 at the connection between the rotor 7 and the front end cover 8, and mark the position corresponding to the rear end cover 6 at the connection between the rotor 7 and the rear end cover 6. Mark the line A, tighten the bolts, mark the number on each bolt head with a marker pen, and mark the same position on the front end cover 8 and the rear end cover 6 with a marker pen.
- Step B Install the left expansion sleeve 2 and the right expansion sleeve 3 onto the rear end cover 6 and the front end cover 8 respectively, use a marker pen to mark the position identification line C corresponding to the rear end cover 6 at the connection between the left expansion sleeve 2 and the rear end cover 6, and mark the position identification line D corresponding to the front end cover 8 at the connection between the right expansion sleeve 3 and the front end cover 8, install the front end outer cover 9 onto the front end cover 8 and tighten the bolts, and use a marker pen to mark the position identification line E corresponding to the front end cover 8 at the connection between the front end outer cover 9 and the front end cover 8;
- Step C Lift the assembled rotor 7 vertically and place it on the vertical support platform 1 with the front end facing downward 0, lift the dynamic balancing dummy shaft 1 to the top of the rotor 7 through the process screw hole 11 set at the rear end, align it with the center of the rotor 7 and slowly drop it until the front end conical surface 13 and
- Step D After disassembling the dynamic balancing dummy shaft 1, the front end outer cover 9, the locking nut 4 and the right expansion sleeve 3 assembled on the rotor 7, reinstall the right expansion sleeve 3 on the front end conical surface 13 of the dynamic balancing dummy shaft 1 according to the mark C, and re-tighten the locking nut 4 in place according to the mark C, and hoist the reassembled dynamic balancing dummy shaft 1, the right expansion sleeve 3 and the locking nut 4 as a whole onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter S, start the automatic weight removal dynamic balancing machine to complete the overall dynamic balancing test of the dynamic balancing dummy shaft and record the final imbalance on both sides ; Step E: Remove the locking nut 4 and the right expansion sleeve 3 on the dynamic balancing dummy shaft 1, reassemble the disassembled right expansion s
- the dynamic balancing machine parameters S in step D include the distance a from the dynamic balancing machine roller support point to the rear end dummy shaft weight removal point, the distance b from the rear end dummy shaft weight removal point to the front end dummy shaft weight removal point, the distance c from the front end dummy shaft weight removal point to the dynamic balancing machine roller support point, and the working radius of the front end dummy shaft weight removal point. And the working radius of the rear end dummy shaft weight removal
- the speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G1.0. set up,
- the dynamic balancing machine parameters Q in step E include the distance A from the dynamic balancing machine roller support point to the rear end weight removal boss, the distance B from the rear end weight removal boss to the front end weight removal boss, the distance C from the front end weight removal boss to the dynamic balancing machine roller support point, and the working radius of the front end weight removal boss. And the working radius of the rear end de-weighting boss
- the speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G2.5. , set up,
- the taper of the front end conical surface 13 and the rear end conical surface 12 is the same as the taper of the taper surface A in the left expansion sleeve 2 and the taper surface B in the right expansion sleeve 3, and the taper range is 15 degrees to 20 degrees.
- the roughness of the front end conical surface 13 and the rear end conical surface 12 is not greater than 1.6 microns.
- the contact rate between the left expansion sleeve 2 and the rear end conical surface 12 and the contact rate between the right expansion sleeve 3 and the front end conical surface 13 are not less than 85%.
- the axial width of the front end conical surface 13 is greater than the width of the corresponding mounting groove A in the front end cover 8.
- the axial width of the rear end conical surface 12 is greater than the width of the corresponding mounting groove B in the rear end cover 6.
- the surface roughness of the left expansion sleeve 2 and the right expansion sleeve 3 is not greater than 1.6 microns.
- the left expansion sleeve 2 and the rear end cover 6 adopt a transition fit, and the right expansion sleeve 3 and the front end cover 8 adopt a transition fit.
- the locking nut 4 includes a large end annular portion and a small head.
- the outer diameter of the large end annular portion is smaller than the inner diameter of the front end outer cover 9, and the inner diameter of the large end annular portion is greater than the minimum diameter of the tapered surface B.
- the small head is processed into a hexagonal nut shape.
- the dynamic balancing dummy shaft 1 and the rotor 7 may be fixed by means of bolts or the like.
- the rotor unweighting dynamic balancing test can be verified by welding the balancing block using the weight-adding method.
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Abstract
Description
本发明涉及动平衡校验技术领域,尤其涉及一种永磁直驱电机外转子动平衡试验方法。The invention relates to the technical field of dynamic balance verification, and in particular to a dynamic balance test method for an outer rotor of a permanent magnet direct-drive motor.
现阶段常规永磁直驱电机转子是内转子结构,转子动平衡采用加平衡块的加重法进行动平衡校验,从而确保动平衡后转子不平衡量满足设计要求,这种方法只适用于有转轴的转子,便于动平衡机支撑,并且该转子两端压板上加工好平衡块安装槽或安装螺孔,而对于新型的无转轴结构且两端无平衡块安装槽或安装螺孔的外转子则无法用现有方法进行动平衡校验,如何实现这种新型结构的电机转子可靠、安全、高效完成动平衡试验是电机制造技术中一个必须解决的问题。At present, the rotor of conventional permanent magnet direct-drive motor is an inner rotor structure, and the dynamic balancing of the rotor is carried out by adding a weight method with a balancing block to ensure that the imbalance of the rotor meets the design requirements after dynamic balancing. This method is only applicable to rotors with a rotating shaft, which is convenient for the dynamic balancing machine to support, and the balancing block mounting grooves or mounting screw holes are processed on the pressure plates at both ends of the rotor. However, for the new outer rotor with no rotating shaft structure and no balancing block mounting grooves or mounting screw holes at both ends, the existing method cannot be used for dynamic balancing verification. How to achieve this new structure of motor rotor to complete the dynamic balancing test reliably, safely and efficiently is a problem that must be solved in motor manufacturing technology.
基于此,申请人提出了一种永磁直驱电机外转子动平衡试验方法来解决以上技术问题。Based on this, the applicant proposed a permanent magnet direct drive motor outer rotor dynamic balancing test method to solve the above technical problems.
本发明针对现有技术中的不足,提供了一种永磁直驱电机外转子动平衡试验方法。In view of the deficiencies in the prior art, the present invention provides a method for dynamic balancing an outer rotor of a permanent magnet direct-drive motor.
本发明通过下述技术方案得以解决:The present invention is solved by the following technical solutions:
一种永磁直驱电机外转子动平衡试验方法,包括以下几个步骤:A method for dynamic balancing an outer rotor of a permanent magnet direct drive motor comprises the following steps:
步骤A:将前端端盖和后端端盖分别安装到转子两端对应位置并紧固好螺栓,同时做好标记A;Step A: Install the front end cover and the rear end cover to the corresponding positions at both ends of the rotor and tighten the bolts, and mark A at the same time;
步骤B:将左胀套和右胀套分别安装到后端端盖和前端端盖上,将前端外盖安装到前端端盖上并紧固好螺栓,同时做好标记B;Step B: Install the left expansion sleeve and the right expansion sleeve on the rear end cover and the front end cover respectively, install the front outer cover on the front end cover and tighten the bolts, and mark B at the same time;
步骤C:将装配好的转子立式吊起后前端朝下放置在立式支撑台上,将动平衡假轴吊运到转子正上方,对齐转子中心后缓慢下落直至动平衡假轴的前端锥面和后端锥面分别与右胀套和左胀套抵接,将锁紧螺母安装到动平衡假轴前端对应的螺纹上并完成紧固,同时做好标记C;Step C: Lift the assembled rotor vertically and place it on a vertical support table with the front end facing downwards. Lift the dynamic balancing dummy shaft to the top of the rotor, align it with the center of the rotor and slowly drop it until the front and rear conical surfaces of the dynamic balancing dummy shaft abut against the right expansion sleeve and the left expansion sleeve respectively. Install the locking nut on the corresponding thread at the front end of the dynamic balancing dummy shaft and tighten it. At the same time, mark C.
步骤D:将装配到转子上的动平衡假轴、前端外盖、锁紧螺母及右胀套拆卸后,按照标记C将右胀套重新安装到动平衡假轴的前端锥面上,并按照标记C重新将锁紧螺母紧固到位,将重新组装好的动平衡假轴、右胀套和锁紧螺母组成的整体吊装到自动去重动平衡机上,设置好动平衡机参数S,启动自动去重动平衡机完成动平衡假轴整体动平衡试验并记录两侧最终不平衡量 、 ; Step D: After disassembling the dummy shaft, front end outer cover, locking nut and right expansion sleeve assembled on the rotor, reinstall the right expansion sleeve on the front end conical surface of the dummy shaft according to mark C, and re-tighten the locking nut in place according to mark C. Hoist the reassembled dummy shaft, right expansion sleeve and locking nut onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter S, start the automatic weight removal dynamic balancing machine to complete the overall dynamic balancing test of the dummy shaft and record the final imbalance on both sides. , ;
步骤E:将动平衡假轴上的锁紧螺母和右胀套进行拆卸,拆卸后的右胀套、动平衡假轴以及步骤D中拆卸下来的前端外盖分别按照标记B和标记C与转子重新组装,随后将锁紧螺母按照标记C紧固安装,将组装好的转子整体吊装到自动去重动平衡机上,设置好动平衡机参数Q,启动自动去重动平衡机完成转子去重动平衡试验并记录两侧最终不平衡量 、 ; Step E: Remove the locking nut and right expansion sleeve on the dynamic balancing dummy shaft. Reassemble the disassembled right expansion sleeve, dynamic balancing dummy shaft and the front end outer cover removed in step D with the rotor according to mark B and mark C respectively. Then tighten and install the locking nut according to mark C. Lift the assembled rotor as a whole onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter Q, start the automatic weight removal dynamic balancing machine to complete the rotor weight removal dynamic balancing test and record the final imbalance on both sides. , ;
步骤F:将转子整体吊运到立式支撑台上,拆卸锁紧螺母、动平衡假轴、左胀套及右胀套后,将转子翻身卧式放置,拆卸前端外盖、后端外盖、前端端盖及后端端盖。Step F: hoist the rotor as a whole onto the vertical support platform, remove the locking nut, dynamic balancing dummy shaft, left expansion sleeve and right expansion sleeve, turn the rotor over and place it horizontally, and remove the front outer cover, rear outer cover, front end cover and rear end cover.
优选的,步骤A中的标记A包括在转子和前端端盖连接处标画的与前端端盖对应位置标识线A以及在转子和后端端盖连接处标画的与后端端盖对应位置标识线B。Preferably, the mark A in step A includes an identification line A marked at the connection between the rotor and the front end cover corresponding to the position of the front end cover and an identification line B marked at the connection between the rotor and the rear end cover corresponding to the position of the rear end cover.
优选的,步骤A中的标记A还包括在每个螺栓头部标记好的编号,以及在前端端盖和后端端盖上对应螺栓的位置标记好的同样的编号。Preferably, the mark A in step A also includes a number marked on the head of each bolt, and the same number marked on the position of the corresponding bolt on the front end cover and the rear end cover.
优选的,步骤B中的标记B包括在左胀套和后端端盖连接处标画的与后端端盖对应位置标识线C以及在右胀套和前端端盖连接处标画的与前端端盖对应位置标识线D,还包括在前端外盖与前端端盖连接处标画的与前端端盖对应位置标识线E。Preferably, the mark B in step B includes an identification line C marked at the connection between the left expansion sleeve and the rear end cover and corresponding to the position of the rear end cover, and an identification line D marked at the connection between the right expansion sleeve and the front end cover and corresponding to the position of the front end cover, and also includes an identification line E marked at the connection between the front outer cover and the front end cover and corresponding to the position of the front end cover.
优选的,步骤C中通过后端设置的工艺螺孔将动平衡假轴进行吊运。Preferably, in step C, the dynamic balancing dummy shaft is hoisted through the process screw holes provided at the rear end.
优选的,步骤C中的标记C包括在动平衡假轴的后端锥面与左胀套连接处标画的标识线F以及在动平衡假轴的前端锥面与右胀套连接处标画的标识线G。Preferably, the mark C in step C includes an identification line F marked at the connection between the rear end conical surface of the dynamic balancing dummy shaft and the left expansion sleeve, and an identification line G marked at the connection between the front end conical surface of the dynamic balancing dummy shaft and the right expansion sleeve.
优选的,步骤C中的标记C还包括在动平衡假轴与锁紧螺母连接处标画的防松标线。Preferably, the mark C in step C also includes an anti-loosening marking line marked at the connection between the dynamic balancing dummy shaft and the locking nut.
优选的,步骤D中的动平衡机参数S包括动平衡机滚轮支撑点至后端假轴去重处的距离a、后端假轴去重处至前端假轴去重处的距离b、前端假轴去重处至动平衡机滚轮支撑点的距离c、前端假轴去重处工作半径 以及后端假轴去重处工作半径 ,动平衡机转速按电机额定转速N设置,最大允许不平衡量按国标G1.0要求的计算值 、 设置, Preferably, the dynamic balancing machine parameters S in step D include the distance a from the dynamic balancing machine roller support point to the rear end dummy shaft deweighting point, the distance b from the rear end dummy shaft deweighting point to the front end dummy shaft deweighting point, the distance c from the front end dummy shaft deweighting point to the dynamic balancing machine roller support point, the working radius of the front end dummy shaft deweighting point, and the distance c from the front end dummy shaft deweighting point to the dynamic balancing machine roller support point. And the working radius of the rear end dummy shaft weight removal The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G1.0. , set up,
根据刚性转子动平衡计算,According to the rigid rotor dynamic balance calculation,
, ,
, ,
以及不平衡量计算公式,And the unbalance calculation formula,
, ,
式中, 表示转子单位质量的许用不平衡度( ), 表示转子工作角速度, ,其中 为转子转速, 表示平衡等级,共分11个平衡等级, 表示转子许用不平衡量, 表示转子质量, 表示每个校正平面的许用剩余不平衡量, 表示工作半径, In the formula, Indicates the permissible unbalance per unit mass of the rotor ( ), represents the rotor operating angular velocity, ,in is the rotor speed, Indicates the balance level, which is divided into 11 levels. Indicates the allowable unbalance of the rotor. represents the rotor mass, Indicates the permissible residual unbalance for each correction plane, Indicates the working radius,
得到,get,
, ,
。 .
优选的, 中, 。 Preferably, middle, .
优选的,步骤E中的动平衡机参数Q包括动平衡机滚轮支撑点至后端去重凸台的距离A、后端去重凸台至前端去重凸台的距离B、前端去重凸台至动平衡机滚轮支撑点的距离C、前端去重凸台工作半径 以及后端去重凸台工作半径 ,动平衡机转速按电机额定转速N设置,最大允许不平衡量按国标G2.5要求的计算值 、 设置, Preferably, the dynamic balancing machine parameter Q in step E includes the distance A from the dynamic balancing machine roller support point to the rear end weight removal boss, the distance B from the rear end weight removal boss to the front end weight removal boss, the distance C from the front end weight removal boss to the dynamic balancing machine roller support point, and the working radius of the front end weight removal boss. And the working radius of the rear end de-weighting boss The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G2.5. , set up,
根据刚性转子动平衡计算,According to the rigid rotor dynamic balance calculation,
, ,
, ,
以及不平衡量计算公式,And the unbalance calculation formula,
, ,
式中, 表示转子单位质量的许用不平衡度( ), 表示转子工作角速度, ,其中 为转子转速, 表示平衡等级,共分11个平衡等级, 表示转子许用不平衡量, 表示转子质量, 表示每个校正平面的许用剩余不平衡量, 表示工作半径, In the formula, Indicates the permissible unbalance per unit mass of the rotor ( ), represents the rotor operating angular velocity, ,in is the rotor speed, Indicates the balance level, which is divided into 11 levels. Indicates the allowable unbalance of the rotor. represents the rotor mass, Indicates the permissible residual unbalance for each correction plane, Indicates the working radius,
得到,get,
, ,
。 .
优选的, 中, 。 Preferably, middle, .
优选的,步骤E中完成转子去重动平衡试验后,在转子及各个部件连接处表面标记统一编号。Preferably, after the rotor weight removal dynamic balancing test is completed in step E, uniform numbers are marked on the surfaces of the rotor and the joints of each component.
优选的,所述前端锥面以及所述后端锥面的锥度与所述左胀套内的锥度面A以及所述右胀套内的锥度面B的锥度相同,所述锥度的范围在15度~20度。Preferably, the taper of the front end tapered surface and the rear end tapered surface is the same as the taper of the tapered surface A in the left expansion sleeve and the tapered surface B in the right expansion sleeve, and the taper ranges from 15 degrees to 20 degrees.
优选的,所述前端锥面和所述后端锥面的粗糙度不大于1.6微米。Preferably, the roughness of the front end conical surface and the rear end conical surface is no more than 1.6 microns.
优选的,所述左胀套与所述后端锥面的接触率以及所述右胀套与所述前端锥面的接触率均不低于85%。Preferably, the contact rate between the left expansion sleeve and the rear end conical surface and the contact rate between the right expansion sleeve and the front end conical surface are not less than 85%.
优选的,所述前端锥面的轴向宽度大于所述前端端盖内对应的安装槽A的宽度,所述后端锥面的轴向宽度大于所述后端端盖内对应的安装槽B的宽度。Preferably, the axial width of the front end conical surface is greater than the width of the corresponding mounting groove A in the front end end cover, and the axial width of the rear end conical surface is greater than the width of the corresponding mounting groove B in the rear end end cover.
优选的,所述左胀套和所述右胀套的表面粗糙度不大于1.6微米。Preferably, the surface roughness of the left expansion sleeve and the right expansion sleeve is not greater than 1.6 microns.
优选的,所述左胀套与所述后端端盖采用过渡配合,所述右胀套与所述前端端盖采用过渡配合。Preferably, the left expansion sleeve and the rear end cover adopt a transition fit, and the right expansion sleeve and the front end cover adopt a transition fit.
优选的,所述锁紧螺母包括大端圆环部和小头部,所述大端圆环部外径小于所述前端外盖内径,所述大端圆环部内径大于所述锥度面B的最小直径,所述小头部加工成六角螺母状。Preferably, the locking nut includes a large end circular ring portion and a small head portion, the outer diameter of the large end circular ring portion is smaller than the inner diameter of the front end outer cover, the inner diameter of the large end circular ring portion is larger than the minimum diameter of the tapered surface B, and the small head portion is processed into a hexagonal nut shape.
本发明的有益效果在于:实现新型的无转轴结构且两端无平衡块安装槽或安装螺孔的外转子的动平衡校验;装置结构简单可靠、实用性强、操作及维护方便、成本低,便于拆装,适用于新型外转子小批量制造。The beneficial effects of the present invention are: realizing dynamic balancing verification of an outer rotor without a rotating shaft structure and without balancing block mounting grooves or mounting screw holes at both ends; the device has a simple and reliable structure, strong practicality, convenient operation and maintenance, low cost, and is easy to disassemble and assemble, and is suitable for small-batch manufacturing of new outer rotors.
为了更清楚地说明本发明实施例或现有技术中的技术方案,以下将对实施例或现有技术描述中所需要使用的附图进行论述,显然,在结合附图进行描述的技术方案仅仅是本发明的一些实施例,对于本领域普通技术人员而言,在不付出创造性劳动的前提下,还可以根据这些附图所示实施例得到其它的实施例及其附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be discussed below. Obviously, the technical solutions described in conjunction with the drawings are only some embodiments of the present invention. For ordinary technicians in this field, other embodiments and their drawings can be obtained based on the embodiments shown in these drawings without paying creative work.
图1是本发明的永磁直驱电机外转子动平衡试验工装带转子整体结构示意图。FIG1 is a schematic diagram of the overall structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture with the rotor of the present invention.
图2是本发明的永磁直驱电机外转子动平衡试验工装带转子整体动平衡参数参考图。FIG. 2 is a reference diagram of overall dynamic balancing parameters of the rotor of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
图3是本发明的永磁直驱电机外转子动平衡试验工装立式安装结构示意图。FIG3 is a schematic diagram of the vertical installation structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
图4是本发明的永磁直驱电机外转子动平衡试验工装部分结构示意图。FIG. 4 is a schematic diagram of the structure of the permanent magnet direct drive motor outer rotor dynamic balancing test fixture of the present invention.
图5是本发明的永磁直驱电机外转子动平衡试验工装试验参数参考图。FIG. 5 is a reference diagram of test parameters of a tooling test for a permanent magnet direct drive motor outer rotor dynamic balancing test according to the present invention.
图6是本发明的动平衡假轴结构剖面图。FIG. 6 is a cross-sectional view of the dynamic balancing dummy shaft structure of the present invention.
图7是本发明的紧锁紧螺母结构示意图。FIG. 7 is a schematic structural diagram of the locking nut of the present invention.
图8是本发明的紧锁紧螺母结构剖面图。FIG8 is a cross-sectional view of the locking nut structure of the present invention.
图9是本发明的左胀套示意图。FIG. 9 is a schematic diagram of the left expansion sleeve of the present invention.
图10是图9的A-A处旋转剖剖面示意图。Fig. 10 is a schematic diagram of a rotational cross-section taken along the line A-A in Fig. 9 .
图11是图10的B-B处剖面示意图。Fig. 11 is a schematic cross-sectional view of the B-B section of Fig. 10 .
图12是本发明的右胀套示意图。FIG. 12 is a schematic diagram of the right expansion sleeve of the present invention.
图13是图12的C-C处旋转剖剖面示意图。Fig. 13 is a schematic diagram of a rotational cross-section taken at C-C in Fig. 12 .
图14是图13的D-D处剖面示意图。Fig. 14 is a schematic cross-sectional view of the D-D section of Fig. 13 .
图中:1、动平衡假轴,2、左胀套,3、右胀套,4、锁紧螺母,5、后端外盖,6、后端端盖,7、转子,8、前端端盖,9、前端外盖,10、立式支撑台,11、工艺螺孔,12、后端锥面,13、前端锥面,14、螺纹。In the figure: 1. dynamic balancing dummy shaft, 2. left expansion sleeve, 3. right expansion sleeve, 4. locking nut, 5. rear end outer cover, 6. rear end end cover, 7. rotor, 8. front end cover, 9. front end outer cover, 10. vertical support platform, 11. process screw hole, 12. rear end cone, 13. front end cone, 14. thread.
以下将结合附图对本发明各实施例的技术方案进行清楚、完整的描述,显然,所描述的实施例仅仅是本发明的一部分实施例,而不是全部实施例。基于本发明中所述的实施例,本领域普通技术人员在不需要创造性劳动的前提下所得到的所有其它实施例,都在本发明所保护的范围内。The following will clearly and completely describe the technical solutions of various embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments described in the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
如图1至图14所示,一种永磁直驱电机外转子动平衡试验方法,包括以下几个步骤:步骤A:将前端端盖8和后端端盖6分别安装到转子7两端对应位置,用记号笔在转子7和前端端盖8连接处标画与前端端盖8对应位置标识线A以及在转子7和后端端盖6连接处标画与后端端盖6对应位置标识线B,并紧固好螺栓,在每个螺栓头部用记号笔标记好编号,以及在前端端盖8和后端端盖6上对应螺栓的位置用记号笔标记好同样的编号;步骤B:将左胀套2和右胀套3分别安装到后端端盖6和前端端盖8上,用记号笔在左胀套2和后端端盖6连接处标画与后端端盖6对应位置标识线C以及在右胀套3和前端端盖8连接处标画与前端端盖8对应位置标识线D,将前端外盖9安装到前端端盖8上并紧固好螺栓,用记号笔在前端外盖9与前端端盖8连接处标画与前端端盖8对应位置标识线E;步骤C:将装配好的转子7立式吊起后前端朝下放置在立式支撑台10上,通过后端设置的工艺螺孔11将动平衡假轴1吊运到转子7正上方,对齐转子7中心后缓慢下落直至动平衡假轴1的前端锥面13和后端锥面12分别与右胀套3和左胀套2抵接,用记号笔在动平衡假轴1的后端锥面12与左胀套2连接处标画标识线F以及在动平衡假轴1的前端锥面13与右胀套3连接处标画标识线G,将锁紧螺母4安装到动平衡假轴1前端对应的螺纹14上并完成紧固,用记号笔在动平衡假轴1与锁紧螺母4连接处标画防松标线;步骤D:将装配到转子7上的动平衡假轴1、前端外盖9、锁紧螺母4及右胀套3拆卸后,按照标记C将右胀套3重新安装到动平衡假轴1的前端锥面13上,并按照标记C重新将锁紧螺母4紧固到位,将重新组装好的动平衡假轴1、右胀套3和锁紧螺母4组成的整体吊装到自动去重动平衡机上,设置好动平衡机参数S,启动自动去重动平衡机完成动平衡假轴整体动平衡试验并记录两侧最终不平衡量 ;步骤E:将动平衡假轴1上的锁紧螺母4和右胀套3进行拆卸,拆卸后的右胀套3、动平衡假轴1以及步骤D中拆卸下来的前端外盖9分别按照标记B和标记C与转子7重新组装,随后将锁紧螺母4按照标记C紧固安装,将组装好的转子7整体吊装到自动去重动平衡机上,设置好动平衡机参数Q,启动自动去重动平衡机完成转子去重动平衡试验并记录两侧最终不平衡量 ,在转子7及各个部件连接处表面用记号笔标记统一编号;步骤F:将转子7整体吊运到立式支撑台10上,拆卸锁紧螺母4、动平衡假轴1、左胀套2及右胀套3后,将转子7翻身卧式放置,拆卸前端外盖9、后端外盖5、前端端盖8及后端端盖6。 As shown in Figures 1 to 14, a method for dynamic balancing the outer rotor of a permanent magnet direct-drive motor includes the following steps: Step A: Install the front end cover 8 and the rear end cover 6 to the corresponding positions at both ends of the rotor 7, use a marker pen to mark the position corresponding to the front end cover 8 at the connection between the rotor 7 and the front end cover 8, and mark the position corresponding to the rear end cover 6 at the connection between the rotor 7 and the rear end cover 6. Mark the line A, tighten the bolts, mark the number on each bolt head with a marker pen, and mark the same position on the front end cover 8 and the rear end cover 6 with a marker pen. Numbering; Step B: Install the left expansion sleeve 2 and the right expansion sleeve 3 onto the rear end cover 6 and the front end cover 8 respectively, use a marker pen to mark the position identification line C corresponding to the rear end cover 6 at the connection between the left expansion sleeve 2 and the rear end cover 6, and mark the position identification line D corresponding to the front end cover 8 at the connection between the right expansion sleeve 3 and the front end cover 8, install the front end outer cover 9 onto the front end cover 8 and tighten the bolts, and use a marker pen to mark the position identification line E corresponding to the front end cover 8 at the connection between the front end outer cover 9 and the front end cover 8; Step C: Lift the assembled rotor 7 vertically and place it on the vertical support platform 1 with the front end facing downward 0, lift the dynamic balancing dummy shaft 1 to the top of the rotor 7 through the process screw hole 11 set at the rear end, align it with the center of the rotor 7 and slowly drop it until the front end conical surface 13 and the rear end conical surface 12 of the dynamic balancing dummy shaft 1 are respectively in contact with the right expansion sleeve 3 and the left expansion sleeve 2, use a marker to mark the identification line F at the connection between the rear end conical surface 12 of the dynamic balancing dummy shaft 1 and the left expansion sleeve 2, and use a marker to mark the identification line G at the connection between the front end conical surface 13 of the dynamic balancing dummy shaft 1 and the right expansion sleeve 3, install the locking nut 4 on the corresponding thread 14 at the front end of the dynamic balancing dummy shaft 1 and complete the tightening, use a marker to mark the dynamic balancing dummy shaft 1 and the locking nut 4. Mark the anti-loosening mark line at the connection of nut 4; Step D: After disassembling the dynamic balancing dummy shaft 1, the front end outer cover 9, the locking nut 4 and the right expansion sleeve 3 assembled on the rotor 7, reinstall the right expansion sleeve 3 on the front end conical surface 13 of the dynamic balancing dummy shaft 1 according to the mark C, and re-tighten the locking nut 4 in place according to the mark C, and hoist the reassembled dynamic balancing dummy shaft 1, the right expansion sleeve 3 and the locking nut 4 as a whole onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter S, start the automatic weight removal dynamic balancing machine to complete the overall dynamic balancing test of the dynamic balancing dummy shaft and record the final imbalance on both sides ; Step E: Remove the locking nut 4 and the right expansion sleeve 3 on the dynamic balancing dummy shaft 1, reassemble the disassembled right expansion sleeve 3, the dynamic balancing dummy shaft 1 and the front end outer cover 9 removed in step D with the rotor 7 according to the mark B and mark C respectively, then tighten and install the locking nut 4 according to the mark C, hoist the assembled rotor 7 as a whole onto the automatic weight removal dynamic balancing machine, set the dynamic balancing machine parameter Q, start the automatic weight removal dynamic balancing machine to complete the rotor weight removal dynamic balancing test and record the final imbalance on both sides , use a marker to mark the surfaces of the rotor 7 and the joints of each component with a uniform number; Step F: hoist the rotor 7 as a whole onto the vertical support platform 10, remove the locking nut 4, the dynamic balancing dummy shaft 1, the left expansion sleeve 2 and the right expansion sleeve 3, turn the rotor 7 over and place it horizontally, and remove the front end outer cover 9, the rear end outer cover 5, the front end end cover 8 and the rear end cover 6.
步骤D中的动平衡机参数S包括动平衡机滚轮支撑点至后端假轴去重处的距离a、后端假轴去重处至前端假轴去重处的距离b、前端假轴去重处至动平衡机滚轮支撑点的距离c、前端假轴去重处工作半径 以及后端假轴去重处工作半径 ,动平衡机转速按电机额定转速N设置,最大允许不平衡量按国标G1.0要求的计算值 设置, The dynamic balancing machine parameters S in step D include the distance a from the dynamic balancing machine roller support point to the rear end dummy shaft weight removal point, the distance b from the rear end dummy shaft weight removal point to the front end dummy shaft weight removal point, the distance c from the front end dummy shaft weight removal point to the dynamic balancing machine roller support point, and the working radius of the front end dummy shaft weight removal point. And the working radius of the rear end dummy shaft weight removal The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G1.0. set up,
根据刚性转子动平衡计算,According to the rigid rotor dynamic balance calculation,
, ,
, ,
以及不平衡量计算公式,And the unbalance calculation formula,
, ,
式中, 表示转子单位质量的许用不平衡度( ), 表示转子工作角速度, ,其中 为转子转速, 表示平衡等级,共分11个平衡等级, 表示转子许用不平衡量, 表示转子质量, 表示每个校正平面的许用剩余不平衡量, 表示工作半径, In the formula, Indicates the permissible unbalance per unit mass of the rotor ( ), represents the rotor operating angular velocity, ,in is the rotor speed, Indicates the balance level, which is divided into 11 balance levels. Indicates the allowable unbalance of the rotor. represents the rotor mass, Indicates the permissible residual unbalance for each correction plane, Indicates the working radius,
得到,get,
,其中 , ,in ,
,其中 。 ,in .
当 且 ,则试验合格,反之需继续去重后再次试验直至合格。 when and , the test is qualified, otherwise it is necessary to continue to remove duplicates and test again until it passes.
步骤E中的动平衡机参数Q包括动平衡机滚轮支撑点至后端去重凸台的距离A、后端去重凸台至前端去重凸台的距离B、前端去重凸台至动平衡机滚轮支撑点的距离C、前端去重凸台工作半径 以及后端去重凸台工作半径 ,动平衡机转速按电机额定转速N设置,最大允许不平衡量按国标G2.5要求的计算值 、 设置, The dynamic balancing machine parameters Q in step E include the distance A from the dynamic balancing machine roller support point to the rear end weight removal boss, the distance B from the rear end weight removal boss to the front end weight removal boss, the distance C from the front end weight removal boss to the dynamic balancing machine roller support point, and the working radius of the front end weight removal boss. And the working radius of the rear end de-weighting boss The speed of the dynamic balancing machine is set according to the rated speed N of the motor, and the maximum allowable unbalance is calculated according to the national standard G2.5. , set up,
根据刚性转子动平衡计算,According to the rigid rotor dynamic balance calculation,
, ,
, ,
以及不平衡量计算公式,And the unbalance calculation formula,
, ,
式中, 表示转子单位质量的许用不平衡度( ), 表示转子工作角速度, ,其中 为转子转速, 表示平衡等级,共分11个平衡等级, 表示转子许用不平衡量, 表示转子质量, 表示每个校正平面的许用剩余不平衡量, 表示工作半径, In the formula, Indicates the permissible unbalance per unit mass of the rotor ( ), represents the rotor operating angular velocity, ,in is the rotor speed, Indicates the balance level, which is divided into 11 balance levels. Indicates the allowable unbalance of the rotor. represents the rotor mass, Indicates the permissible residual unbalance for each correction plane, Indicates the working radius,
得到,get,
,其中 , ,in ,
,其中 。 ,in .
当 且 ,则试验合格,反之需继续去重后再次试验直至合格。 when and , the test is qualified, otherwise it is necessary to continue to remove duplicates and test again until it passes.
所述前端锥面13以及所述后端锥面12的锥度与所述左胀套2内的锥度面A以及所述右胀套3内的锥度面B的锥度相同,所述锥度的范围在15度~20度,所述前端锥面13和所述后端锥面12的粗糙度不大于1.6微米,所述左胀套2与所述后端锥面12的接触率以及所述右胀套3与所述前端锥面13的接触率均不低于85%,所述前端锥面13的轴向宽度大于所述前端端盖8内对应的安装槽A的宽度,所述后端锥面12的轴向宽度大于所述后端端盖6内对应的安装槽B的宽度,所述左胀套2和所述右胀套3的表面粗糙度不大于1.6微米,所述左胀套2与所述后端端盖6采用过渡配合,所述右胀套3与所述前端端盖8采用过渡配合,所述锁紧螺母4包括大端圆环部和小头部,所述大端圆环部外径小于所述前端外盖9内径,所述大端圆环部内径大于所述锥度面B的最小直径,所述小头部加工成六角螺母状。The taper of the front end conical surface 13 and the rear end conical surface 12 is the same as the taper of the taper surface A in the left expansion sleeve 2 and the taper surface B in the right expansion sleeve 3, and the taper range is 15 degrees to 20 degrees. The roughness of the front end conical surface 13 and the rear end conical surface 12 is not greater than 1.6 microns. The contact rate between the left expansion sleeve 2 and the rear end conical surface 12 and the contact rate between the right expansion sleeve 3 and the front end conical surface 13 are not less than 85%. The axial width of the front end conical surface 13 is greater than the width of the corresponding mounting groove A in the front end cover 8. The axial width of the rear end conical surface 12 is greater than the width of the corresponding mounting groove B in the rear end cover 6. The surface roughness of the left expansion sleeve 2 and the right expansion sleeve 3 is not greater than 1.6 microns. The left expansion sleeve 2 and the rear end cover 6 adopt a transition fit, and the right expansion sleeve 3 and the front end cover 8 adopt a transition fit. The locking nut 4 includes a large end annular portion and a small head. The outer diameter of the large end annular portion is smaller than the inner diameter of the front end outer cover 9, and the inner diameter of the large end annular portion is greater than the minimum diameter of the tapered surface B. The small head is processed into a hexagonal nut shape.
在其余实施例中,所述动平衡假轴1与所述转子7之间可以通过螺栓等方式进行固定。In other embodiments, the dynamic balancing dummy shaft 1 and the rotor 7 may be fixed by means of bolts or the like.
在其余实施例中,转子去重动平衡试验中可通过加重法焊接平衡块的方式进行校验。In other embodiments, the rotor unweighting dynamic balancing test can be verified by welding the balancing block using the weight-adding method.
对于本领域技术人员而言,显然本发明不限于上述示范性实施例的细节,而且在不背离本发明的精神或基本特征的情况下,能够以其他的具体形式实现本发明。因此,无论从哪一点来看,均应将实施例看作是示范性的,而且是非限制性的。本发明的范围由所附权利要求进行限定,而不是上述说明限定,因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本发明内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。It will be apparent to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be considered exemplary and non-restrictive from any point of view. The scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be considered as limiting the claim to which it relates.
此外,应当理解,虽然本说明书按照实施方式加以描述,但并非每个实施方式仅包含一个独立的技术方案,说明书的这种叙述方式仅仅是为清楚起见,本领域技术人员应当将说明书作为一个整体,各实施例中的技术方案也可以经适当组合,形成本领域技术人员可以理解的其他实施方式。In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.
在此处键入序列表自由内容描述段落。Type your sequence listing free description paragraph here.
Claims (8)
[Corrected 06.12.2023 in accordance with Article 91]
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| CN202311625359.3 | 2023-11-30 | ||
| CN202311625359.3A CN117870960B (en) | 2023-11-30 | 2023-11-30 | A dynamic balancing test method for the outer rotor of a permanent magnet direct drive motor |
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| WO2025112079A1 true WO2025112079A1 (en) | 2025-06-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| PCT/CN2023/136206 Pending WO2025112079A1 (en) | 2023-11-30 | 2023-12-04 | Dynamic balancing test method for outer rotor of permanent magnet direct drive motor |
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| WO (1) | WO2025112079A1 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN117870960B (en) * | 2023-11-30 | 2024-12-06 | 江苏中车电机有限公司 | A dynamic balancing test method for the outer rotor of a permanent magnet direct drive motor |
| CN120721293B (en) * | 2025-09-04 | 2025-11-11 | 中车株洲电机有限公司 | Dynamic balance tool and method for hollow shaft rotor |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4543825A (en) * | 1982-09-25 | 1985-10-01 | Carl Schenck A.G. | Procedure for balancing of rotors without journals |
| JPH0552695A (en) * | 1991-08-22 | 1993-03-02 | Fuji Electric Co Ltd | Rotation testing equipment rotor |
| US20110083505A1 (en) * | 2009-10-08 | 2011-04-14 | Allen Iv George I | Balance Test Indexing Tool for Balance-Testing a Rotor |
| CN105806558A (en) * | 2016-05-13 | 2016-07-27 | 北京精密机电控制设备研究所 | Dynamic balance tool for permanent-magnet shaftless impeller |
| US20170044928A1 (en) * | 2014-10-29 | 2017-02-16 | Harbin Institute Of Technology | Five-degree-of-freedom adjustment and positioning method and apparatus for assembly/measurement of rotor and stator of aircraft engine |
| CN111044223A (en) * | 2019-11-22 | 2020-04-21 | 北京动力机械研究所 | Dynamic balancing device for disc rotor of turbine engine |
| CN114123695A (en) * | 2021-11-17 | 2022-03-01 | 中车株洲电机有限公司 | Dynamic balance auxiliary device of outer rotor structure and dynamic balance detection method |
| CN114184318A (en) * | 2021-11-03 | 2022-03-15 | 东莞市卓茂仪器有限公司 | Design method and structure of externally-supported clamping jaw for dynamic balance test of axis-free rotating body |
| CN217211254U (en) * | 2022-05-18 | 2022-08-16 | 华域汽车电动系统(上海)有限公司 | Dummy shaft device for dynamic balance test of rotor without output shaft |
| CN115752901A (en) * | 2022-10-24 | 2023-03-07 | 北方华锦化学工业股份有限公司 | Six-point balancing method for fan rotor |
| CN115790972A (en) * | 2022-09-14 | 2023-03-14 | 北京动力机械研究所 | Hydraulic dynamic balance device |
| CN218847495U (en) * | 2023-01-29 | 2023-04-11 | 华域汽车电动系统有限公司 | A process shaft device for dynamic balance detection of hollow shaft rotor |
| CN116183108A (en) * | 2023-01-10 | 2023-05-30 | 上海衡望智能科技有限公司 | A balance test device for internally supported rotors |
| CN117870960A (en) * | 2023-11-30 | 2024-04-12 | 江苏中车电机有限公司 | A dynamic balancing test method for the outer rotor of a permanent magnet direct drive motor |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002071503A (en) * | 2000-09-04 | 2002-03-08 | Hitachi Ltd | Unbalance correction mechanism and method, disk device, and information device |
| CN206410823U (en) * | 2017-01-18 | 2017-08-15 | 广州卓玄金机械设备有限公司 | One kind is automatically positioned outer rotor dynamic balancing machine |
| CN107733178B (en) * | 2017-10-23 | 2024-03-12 | 合众新能源汽车股份有限公司 | An electric vehicle wheel hub motor test bench |
| CN217819183U (en) * | 2022-08-22 | 2022-11-15 | 东莞费格斯风机有限公司 | Motor outer rotor balance correction device |
-
2023
- 2023-11-30 CN CN202311625359.3A patent/CN117870960B/en active Active
- 2023-12-04 WO PCT/CN2023/136206 patent/WO2025112079A1/en active Pending
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4543825A (en) * | 1982-09-25 | 1985-10-01 | Carl Schenck A.G. | Procedure for balancing of rotors without journals |
| JPH0552695A (en) * | 1991-08-22 | 1993-03-02 | Fuji Electric Co Ltd | Rotation testing equipment rotor |
| US20110083505A1 (en) * | 2009-10-08 | 2011-04-14 | Allen Iv George I | Balance Test Indexing Tool for Balance-Testing a Rotor |
| US20170044928A1 (en) * | 2014-10-29 | 2017-02-16 | Harbin Institute Of Technology | Five-degree-of-freedom adjustment and positioning method and apparatus for assembly/measurement of rotor and stator of aircraft engine |
| CN105806558A (en) * | 2016-05-13 | 2016-07-27 | 北京精密机电控制设备研究所 | Dynamic balance tool for permanent-magnet shaftless impeller |
| CN111044223A (en) * | 2019-11-22 | 2020-04-21 | 北京动力机械研究所 | Dynamic balancing device for disc rotor of turbine engine |
| CN114184318A (en) * | 2021-11-03 | 2022-03-15 | 东莞市卓茂仪器有限公司 | Design method and structure of externally-supported clamping jaw for dynamic balance test of axis-free rotating body |
| CN114123695A (en) * | 2021-11-17 | 2022-03-01 | 中车株洲电机有限公司 | Dynamic balance auxiliary device of outer rotor structure and dynamic balance detection method |
| CN217211254U (en) * | 2022-05-18 | 2022-08-16 | 华域汽车电动系统(上海)有限公司 | Dummy shaft device for dynamic balance test of rotor without output shaft |
| CN115790972A (en) * | 2022-09-14 | 2023-03-14 | 北京动力机械研究所 | Hydraulic dynamic balance device |
| CN115752901A (en) * | 2022-10-24 | 2023-03-07 | 北方华锦化学工业股份有限公司 | Six-point balancing method for fan rotor |
| CN116183108A (en) * | 2023-01-10 | 2023-05-30 | 上海衡望智能科技有限公司 | A balance test device for internally supported rotors |
| CN218847495U (en) * | 2023-01-29 | 2023-04-11 | 华域汽车电动系统有限公司 | A process shaft device for dynamic balance detection of hollow shaft rotor |
| CN117870960A (en) * | 2023-11-30 | 2024-04-12 | 江苏中车电机有限公司 | A dynamic balancing test method for the outer rotor of a permanent magnet direct drive motor |
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| CN117870960B (en) | 2024-12-06 |
| CN117870960A (en) | 2024-04-12 |
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