CN101463856A - Bearing ring - Google Patents

Bearing ring Download PDF

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Publication number
CN101463856A
CN101463856A CNA2008100366031A CN200810036603A CN101463856A CN 101463856 A CN101463856 A CN 101463856A CN A2008100366031 A CNA2008100366031 A CN A2008100366031A CN 200810036603 A CN200810036603 A CN 200810036603A CN 101463856 A CN101463856 A CN 101463856A
Authority
CN
China
Prior art keywords
ring
grooves
retaining ring
bearing
end ring
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.)
Pending
Application number
CNA2008100366031A
Other languages
Chinese (zh)
Inventor
马宝发
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.)
Shanghai Ri Yong Jea Gate Electric Co Ltd
Original Assignee
Shanghai Ri Yong Jea Gate Electric Co Ltd
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 Shanghai Ri Yong Jea Gate Electric Co Ltd filed Critical Shanghai Ri Yong Jea Gate Electric Co Ltd
Priority to CNA2008100366031A priority Critical patent/CN101463856A/en
Publication of CN101463856A publication Critical patent/CN101463856A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a retaining ring for a bearing, which is a notched circular and flaky structural member. On both sides of the midpoint of a circle, the outer side of the retaining ring is symmetrically provided with two identical grooves; on both sides of the midpoint of the circle, the inner side of the retaining ring is symmetrically provided with two identical grooves; and the grooves of the inner side and the grooves of the outer side are respectively correspondingly arranged, and the grooves of the inner side are narrower than the grooves of the outer side. Compared with the existing retaining ring, the contact area of the retaining ring for the bearing of the invention and a shaft shoulder is increased by 70 percent; the problems of deformation of the shaft shoulder and the deformation of the retaining ring for the bearing, which are caused by the axial tight locking force, can be avoided; the problem of deformation of the retaining ring for the bearing, which is caused by the axial fluctuation force of the rotation of a wind blade, can be avoided; and the retaining ring for the bearing can replace the double-ring (bead ring and retaining ring for the bearing) combined structure in the prior art, and has the advantages of simple assembly and high safety and reliability.

Description

End ring
Technical field
The present invention relates to a kind of component of machine, particularly a kind of end ring.
Background technique
The motor bearings back-up ring is the axial position that is used for fixing bearing.The structure of the end ring 1 of prior art as shown in Figure 1, it is a notched ring sheet structure, its internal diameter is less than the internal diameter of the bearing that is connected, ring outer side 11 is continuous arc-shaped structure, the inboard mid point both sides at ring of ring respectively are provided with a groove 12,13 that size is identical, and the width of this groove and groove are suitable to the distance of the breach of ring.Gross distortion even back-up ring, can take place and break away from the shaft shoulder during greater than 6.5N in axial locking power (impact) in the end ring of this structure.In order to address this problem, when axial locking power during greater than 6.5N, prior art generally adopt steel traveler+end ring two the circle fabricated structures, its installment state as shown in Figure 2, shown in Fig. 2,1 is the end ring of prior art, 3 is locking nut, and 4 is the fan blade inserts, and 5 is bearing, 6 is axle, and 7 is steel traveler.But this construction cost is high and the assembling trouble, particularly when assembling such as end ring place not in placely, end ring has crushed risk.
Summary of the invention
Purpose of the present invention is to overcome the problem that above-mentioned prior art exists, and a kind of end ring of new structure is provided.
The object of the present invention is achieved like this: a kind of end ring, it is a notched ring sheet structure, be characterized in, the outside of described back-up ring is provided with two grooves that size is identical in the mid point bilateral symmetry of ring, the inboard of back-up ring is provided with two grooves that size is identical in the mid point bilateral symmetry of ring, inboard groove and the corresponding setting respectively of outside groove, and the width of inboard groove is less than the width of outside groove.
Described two inboard grooves are separated into three sections with the internal diameter circular arc of back-up ring, and three sections arc length are roughly the same, and all greater than the arc length of groove institute cutout portion.
Described inboard groove is narrow outer wide trapezoidal in being.
End ring of the present invention is owing to adopted above technological scheme, back-up ring increases by 70% with the area of contact of the shaft shoulder than existing back-up ring, improved the axial strength of back-up ring greatly, shaft locking power can be born, the shaft shoulder distortion and the end ring problem on deformation that cause because of axial locking power can be improved smaller or equal to 10N; Can improve the end ring problem on deformation that causes because of fan blade rotation axial float power; Reliability obviously is better than existing back-up ring.Two circle fabricated structures of the steel traveler+end ring of the alternative prior art of end ring of the present invention, cost is original 1/10, assembling is simple, and is safe and reliable, can reduce neglected loading, helps mistake proofing.
Description of drawings
Fig. 1 is the structural representation of prior art end ring;
Fig. 2 is the user mode schematic representation of prior art end ring;
Fig. 3 is the structural representation of end ring of the present invention;
Fig. 4 is the user mode schematic representation of end ring of the present invention;
Fig. 5 is the contact condition schematic representation of the prior art end ring and the shaft shoulder;
Fig. 6 is the contact condition schematic representation of the end ring of the present invention and the shaft shoulder.
Embodiment
Referring to Fig. 3, end ring 2 of the present invention, it is a notched ring sheet structure, the outside of back-up ring is provided with two grooves 21,22 that size is identical in the mid point bilateral symmetry of ring, the inboard of back-up ring is provided with two grooves 23,24 that size is identical in the mid point bilateral symmetry of ring, inboard groove and the corresponding setting respectively of outside groove, and the width of inboard groove is less than the width of outside groove.Two inboard grooves are narrow outer wide trapezoidal in being, and two inboard grooves are separated into three sections with the internal diameter circular arc of back-up ring, and three sections arc length are roughly the same, and all greater than the arc length of groove institute cutout portion.
Referring to Fig. 4, Fig. 4 is the user mode schematic representation of end ring of the present invention.Shown in the figure, 2 is end ring of the present invention, and 3 is locking nut, and 4 is the fan blade inserts, and 5 is bearing, and 6 is axle.As seen comparison diagram 4 and Fig. 2 adopt end ring of the present invention, two circle fabricated structures of the steel traveler+end ring of alternative prior art.
Fig. 5 is the contact condition schematic representation of the prior art end ring and the shaft shoulder.Shown in the figure, 61 is the shaft shoulder, and A indication oblique line partly is the area of contact of the prior art end ring 1 and the shaft shoulder 61.Fig. 6 is the contact condition schematic representation of the end ring of the present invention and the shaft shoulder.Shown in the figure, 61 is the shaft shoulder, and B indication oblique line partly is the area of contact of end ring 2 of the present invention with the shaft shoulder 61.By Fig. 5, Fig. 6 as seen, adopt end ring 2 of the present invention, its area of contact with the shaft shoulder 61 is more much bigger with the area of contact of the shaft shoulder 61 than adopting prior art end ring 1, area of contact has approximately increased by 70%, can improve the problem that the shaft shoulder is out of shape and end ring is out of shape that axial locking power causes thus greatly, also can improve the end ring problem on deformation that causes because of fan blade rotation axial float power.

Claims (3)

1, a kind of end ring, it is a notched ring sheet structure, it is characterized in that: the outside of described back-up ring is provided with two grooves that size is identical in the mid point bilateral symmetry of ring, the inboard of back-up ring is provided with two grooves that size is identical in the mid point bilateral symmetry of ring, inboard groove and the corresponding setting respectively of outside groove, and the width of inboard groove is less than the width of outside groove.
2, end ring as claimed in claim 1 is characterized in that: described two inboard grooves are separated into three sections with the internal diameter circular arc of back-up ring, and three sections arc length are roughly the same, and all greater than the arc length of groove institute cutout portion.
3, end ring according to claim 1 is characterized in that: narrow outer wide trapezoidal in described inboard groove is.
CNA2008100366031A 2008-04-24 2008-04-24 Bearing ring Pending CN101463856A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA2008100366031A CN101463856A (en) 2008-04-24 2008-04-24 Bearing ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA2008100366031A CN101463856A (en) 2008-04-24 2008-04-24 Bearing ring

Publications (1)

Publication Number Publication Date
CN101463856A true CN101463856A (en) 2009-06-24

Family

ID=40804582

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2008100366031A Pending CN101463856A (en) 2008-04-24 2008-04-24 Bearing ring

Country Status (1)

Country Link
CN (1) CN101463856A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102562821A (en) * 2012-02-29 2012-07-11 杨丽萍 Split combined retainer ring used on inner side of bearing outer ring
CN104475355A (en) * 2014-12-18 2015-04-01 合肥安晶龙电子有限公司 Gas-blowing system of color selector
CN104659989A (en) * 2015-01-09 2015-05-27 广东威灵电机制造有限公司 Motor and split washer thereof
CN112211912A (en) * 2020-09-17 2021-01-12 东风汽车集团有限公司 Bearing limiting retainer ring
CN112564352A (en) * 2020-12-24 2021-03-26 贵阳万江航空机电有限公司 Baffle structure for fixing motor rotor part and assembling method
CN112943801A (en) * 2021-03-18 2021-06-11 常州克劳诺斯特种轴承制造有限公司 Integrated middle clamp spring, double-row outer-ring-free bearing and planetary speed reduction mechanism

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102562821A (en) * 2012-02-29 2012-07-11 杨丽萍 Split combined retainer ring used on inner side of bearing outer ring
CN104475355A (en) * 2014-12-18 2015-04-01 合肥安晶龙电子有限公司 Gas-blowing system of color selector
CN104659989A (en) * 2015-01-09 2015-05-27 广东威灵电机制造有限公司 Motor and split washer thereof
CN112211912A (en) * 2020-09-17 2021-01-12 东风汽车集团有限公司 Bearing limiting retainer ring
CN112211912B (en) * 2020-09-17 2021-11-16 东风汽车集团有限公司 Bearing limiting retainer ring
CN112564352A (en) * 2020-12-24 2021-03-26 贵阳万江航空机电有限公司 Baffle structure for fixing motor rotor part and assembling method
CN112943801A (en) * 2021-03-18 2021-06-11 常州克劳诺斯特种轴承制造有限公司 Integrated middle clamp spring, double-row outer-ring-free bearing and planetary speed reduction mechanism

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C02 Deemed withdrawal of patent application after publication (patent law 2001)
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Open date: 20090624