CN201412429Y - Spherical high-locking nut - Google Patents
Spherical high-locking nut Download PDFInfo
- Publication number
- CN201412429Y CN201412429Y CN2009203024854U CN200920302485U CN201412429Y CN 201412429 Y CN201412429 Y CN 201412429Y CN 2009203024854 U CN2009203024854 U CN 2009203024854U CN 200920302485 U CN200920302485 U CN 200920302485U CN 201412429 Y CN201412429 Y CN 201412429Y
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- CN
- China
- Prior art keywords
- locking nut
- spherical
- closely locking
- nut
- closely
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- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a spherical high-locking nut, comprising a high-locking nut with internal thread, wherein a convex spherical surface is arranged on one end of the high-locking nut, a spherical washer is arranged on the convex spherical surface of the high-locking nut, a concave spherical surface is arranged on the spherical washer in fit with the convex spherical surface of the high-locking nut; neck breaking groove on the outside surface of the high-locking nut. A slotting and locking structure on the high-locking nut and the spherical washer are used and a certain twisting momentis applied on the twisting area of the high-locking nut to twist off the neck breaking groove of the nut, thus pre-tightening force is generated and the nut is connected with a sandwich plate by spherical washer adjustment. The spherical high-locking nut is quickly assembled and the reliability of the assembled nut is good and the loosening prevention function is very good. The spherical high-locking nut has advantages of simple structure, easy production and good use effect.
Description
Technical field
The utility model relates to a kind of sphere Closely locking nut, belongs to nut technical field in the fastening piece.
Background technique
At present, some of aircraft interlayer are local because interlayer itself has gradient, adjust angle when needing assembling, avoid that bolts and nuts can not vertically connect on the inclined-plane.Can not satisfy the requirement of this assembly structure with the Closely locking nut of conventional structure, though and traveling self-locking nut can be adjusted angle, assembling speed is slow, assembly precision requires high, and maintenance is inconvenient, and anti-loosening property and load performance are good inadequately, volume is bigger, and has increased the weight of aircraft assembling.Therefore, nut of the prior art still can not satisfy the needs of use
The model utility content
The purpose of this utility model is: providing a kind of can carry out the rapid adjustment assembling on less than 7 ° inclined-plane and have reliable and stable tightness and good fatigue resistance and the sphere Closely locking nut that volume is little, weight is lighter at aircraft interlayer gradient α, to overcome the deficiencies in the prior art.
The utility model is achieved in that the utility model is to improve to form on the existing Closely locking nut basis that is provided with internal thread, promptly the end at Closely locking nut is provided with protruding sphere, and on the position of the protruding sphere of Closely locking nut, be provided with a spherical washer, on spherical washer, be provided with the concave spherical surface that matches with the protruding sphere of Closely locking nut.
On the outer side surface of above-mentioned Closely locking nut, be provided with cut-off neck slot.
The both sides of cut-off neck slot also are respectively equipped with locking mechanism and twist into two parts structure on the outer side surface of above-mentioned Closely locking nut.
The internal thread of above-mentioned Closely locking nut is the self-locking type fine thread of bottom made in U.S.A band circular arc.
Above-mentioned Closely locking nut and spherical washer are the stainless steel material structure.
Owing to adopted technique scheme, the utility model can be installed on interlayer inclination α is less than or equal to 7 ° inclined-plane, when high locked bolts being passed spherical washer and enters the threaded portion of Closely locking nut, apply rational twisting moment (this moment, twisting moment was determined by the cut-off neck slot size) by the twisting structure of twisting into two parts partly to Closely locking nut cut-off neck slot one end, cut-off neck slot is twisted into two parts, be that Closely locking nut just obtains corresponding pretightening force when cut-off neck slot is twisted into two parts, Closely locking nut is in this rotary course, its protruding land portions is partly passed through being connected of high locked bolts with the concave spherical surface of spherical washer, spherical washer is just adjusted to Closely locking nut and high locked bolts on the direction connected vertically this moment, because the locking mechanism that the screw thread of Closely locking nut has has stoped the mutual rotation of bolts and nuts.Therefore the utility model compared with prior art, the utility model not only has can realize the fast advantage of assembling, but also have simple in structure, easy production, easy for installation, volume is little, reliability in light weight, after installing is high and have advantages such as good fatigue resistance and locking effect.Simultaneously, the utility model has solved the aircraft interlayer and has had the problem that gradient is difficult to install.
Description of drawings
Structural representation when accompanying drawing 1 makes up for the utility model;
Accompanying drawing 2 is a Closely locking nut structural representation of the present utility model;
Accompanying drawing 3 is a spherical washer structural representation of the present utility model;
Structural representation when accompanying drawing 4 is installed and used for the utility model.
Embodiment
Embodiment of the present utility model: as Fig. 1, Fig. 2, shown in Figure 3, the utility model is made up of Closely locking nut 1 that is provided with internal thread 5 and spherical washer 2, during making, produce protruding sphere 4 simultaneously at an end of Closely locking nut 1, and on the position of the protruding sphere 4 of Closely locking nut 1, be provided with a spherical washer 2, the one side of spherical washer 2 is made into the plane, on the another side of spherical washer 2, produce the concave spherical surface 8 that matches with the protruding sphere 4 of Closely locking nut 1, Closely locking nut 1 and spherical washer 2 can adopt conventional metallic material to make, but when using on the aircraft, preferably adopt stainless steel material to make; On the outer side surface of Closely locking nut 1, make a circle cut-off neck slot 3 then, and the both sides of cut-off neck slot 3 are produced locking mechanism 6 respectively and are twisted into two parts structure 7 on the outer side surface of Closely locking nut 1; The internal thread 5 of Closely locking nut 1 is made into the self-locking type fine thread of bottom made in U.S.A band circular arc.
When using the utility model, in assembling, to pack in the sandwich plate 10 with the high locked bolts 9 that Closely locking nut 1 of the present utility model is used, spherical washer 2 is penetrated high locked bolts 9 to be contacted with sandwich plate 10, Closely locking nut 1 is screwed on the high locked bolts 9, apply certain twisting moment by special tool and twisting into two parts on the structure 7, thereby cut-off neck slot 3 is twisted into two parts, this moment, protruding sphere 4 parts of Closely locking nut 1 were connected with spherical washer 2 adjustment.
The environment that Closely locking nut 1 uses has determined Closely locking nut 1 that pretightening force and coupling mechanism force preferably will be arranged, and pretightening force is to be determined by the moment of twisting into two parts of twisting into two parts groove 3, if Closely locking nut 1 twist into two parts groove 3 to twist into two parts moment too small, the pretightening force that produces just can not make Closely locking nut 1 and spherical washer 2 or sandwich plate 10 be connected firmly, if Closely locking nut 1 twist into two parts groove 3 to twist into two parts moment excessive, during the pretightening force that produces can make Closely locking nut 1 and spherical washer 2 is connected sandwich plate 10 is applied excessive pressure, make sandwich plate 10 be in stress for a long time and be out of shape.The locking torque of Closely locking nut 1 produces by internal thread 5 region deformations, the size of locking torque has determined the locking property and the vibration resistance of nut, and excessive locking torque also can cause damage to the screw thread of high locked bolts 9, have only distortion could guarantee the mechanical property requirement, and then satisfy the clamping needs by effective control internal thread 5 zones.
Claims (4)
1. sphere Closely locking nut, comprise the Closely locking nut (1) that is provided with internal thread (5), it is characterized in that: the end at Closely locking nut (1) is provided with protruding sphere (4), and on the position of the protruding sphere (4) of Closely locking nut (1), be provided with a spherical washer (2), on spherical washer (2), be provided with the concave spherical surface (8) that matches with the protruding sphere (4) of Closely locking nut (1); On the outer side surface of Closely locking nut (1), be provided with cut-off neck slot (3).
2. sphere Closely locking nut according to claim 1 is characterized in that: the both sides of cut-off neck slot on the outer side surface of Closely locking nut (1) (3) are respectively equipped with locking mechanism (6) and twist into two parts structure (7).
3. sphere Closely locking nut according to claim 1 is characterized in that: the internal thread (5) of Closely locking nut (1) is the self-locking type fine thread of bottom made in U.S.A band circular arc.
4. sphere Closely locking nut according to claim 1 is characterized in that: Closely locking nut (1) and spherical washer (2) are the stainless steel material structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203024854U CN201412429Y (en) | 2009-04-23 | 2009-04-23 | Spherical high-locking nut |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203024854U CN201412429Y (en) | 2009-04-23 | 2009-04-23 | Spherical high-locking nut |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201412429Y true CN201412429Y (en) | 2010-02-24 |
Family
ID=41714313
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009203024854U Expired - Fee Related CN201412429Y (en) | 2009-04-23 | 2009-04-23 | Spherical high-locking nut |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201412429Y (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103541957A (en) * | 2012-07-16 | 2014-01-29 | 富泰华工业（深圳）有限公司 | Locking assembly |
| CN104314948A (en) * | 2014-11-11 | 2015-01-28 | 贵州航天精工制造有限公司 | Light controllable pretightening force self-locking swing nut assembly |
| CN105156445A (en) * | 2015-10-20 | 2015-12-16 | 贵州航天精工制造有限公司 | Double-lug spherical multifunctional hi-lock nut |
| CN105387050A (en) * | 2015-12-11 | 2016-03-09 | 南京金龙新能源汽车研究院有限公司 | Wheel nut |
| CN106704339A (en) * | 2016-12-30 | 2017-05-24 | 东方蓝天钛金科技有限公司 | Self-adjusting detachable high-locking nut assembly |
| CN108412884A (en) * | 2018-03-22 | 2018-08-17 | 贵州航天精工制造有限公司 | One kind is light-duty to wave self locking nut connector and its manufacturing method |
| CN108457968A (en) * | 2017-12-21 | 2018-08-28 | 河南航天精工制造有限公司 | Screwed assembly and its nut |
-
2009
- 2009-04-23 CN CN2009203024854U patent/CN201412429Y/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103541957A (en) * | 2012-07-16 | 2014-01-29 | 富泰华工业（深圳）有限公司 | Locking assembly |
| CN103541957B (en) * | 2012-07-16 | 2016-03-16 | 富泰华工业（深圳）有限公司 | Locked assembly |
| CN104314948A (en) * | 2014-11-11 | 2015-01-28 | 贵州航天精工制造有限公司 | Light controllable pretightening force self-locking swing nut assembly |
| CN105156445A (en) * | 2015-10-20 | 2015-12-16 | 贵州航天精工制造有限公司 | Double-lug spherical multifunctional hi-lock nut |
| CN105387050A (en) * | 2015-12-11 | 2016-03-09 | 南京金龙新能源汽车研究院有限公司 | Wheel nut |
| CN106704339A (en) * | 2016-12-30 | 2017-05-24 | 东方蓝天钛金科技有限公司 | Self-adjusting detachable high-locking nut assembly |
| CN108457968A (en) * | 2017-12-21 | 2018-08-28 | 河南航天精工制造有限公司 | Screwed assembly and its nut |
| CN108412884A (en) * | 2018-03-22 | 2018-08-17 | 贵州航天精工制造有限公司 | One kind is light-duty to wave self locking nut connector and its manufacturing method |
| CN108412884B (en) * | 2018-03-22 | 2020-07-14 | 贵州航天精工制造有限公司 | Light swinging self-locking nut connecting piece and manufacturing method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100224 Termination date: 20140423 |