CN103899626A - Hexagonal surface self-locking nut - Google Patents
Hexagonal surface self-locking nut Download PDFInfo
- Publication number
- CN103899626A CN103899626A CN201410146850.2A CN201410146850A CN103899626A CN 103899626 A CN103899626 A CN 103899626A CN 201410146850 A CN201410146850 A CN 201410146850A CN 103899626 A CN103899626 A CN 103899626A
- Authority
- CN
- China
- Prior art keywords
- locking
- self
- deformation
- locking nut
- micro
- 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
Links
Images
Landscapes
- Connection Of Plates (AREA)
Abstract
A hexagonal surface self-locking nut is provided with a hexagonal nut body provided with a threaded hole. The hexagonal surface self-locking nut is characterized in that micro-deformation portions distributed at intervals along the circumference of the hexagonal nut body are evenly arranged on the hexagonal nut body, the micro-deformation portions are produced by exerting radial deformation pressure on the side wall of the hexagonal nut body, and the micro-deformation portions enable the hexagonal surface self-locking nut to achieve self-locking. According to the hexagonal surface self-locking nut, the side wall of the hexagonal nut body is extruded in a three-point extrusion mode, so that the hexagonal nut body and a thread in the threaded hole generate micro-deformation so as to achieve the stable and reliable self-locking effect, a technological portion in a high-lock nut can be replaced, the reliable self-locking effect is achieved, raw materials can be greatly saved, and manufacturing cost is lowered. In addition, the hexagonal surface self-locking nut has the advantages of being simple in structure, convenient to install, capable of being used repeatedly, light in weight, wide in application range and the like.
Description
[technical field]
The present invention relates to self-locking nut, particularly relate to a kind of for aerospace hex surface self-locking nut.
[background technique]
General nut in use can get loose due to reasons such as vibrations, and in order to solve the problem that gets loose occurring in nut use, people have invented self-locking nut.The working principle of self-locking nut is by increasing the frictional force of screw connection point to realize antivibration locking functions.The type of self-locking nut is more, at the bottom of it mainly contains and embeds nylon ring, special thread tooth and add the types such as metal locking device.For aerospace field, in the linkage structure of aircraft, for meeting its flight requirement, conventionally need operating weight light, and the high link of fatigue strength.Now in aerospace field, conventionally be all to use Closely locking nut to carry out structure connection, although Closely locking nut can meet the self-locking requirement connecting, but its structure is more complicated, is conventionally all used by process portion and the supporting connection of working portion, and can only dismantle by means of destruction after installing, after dismounting, can not reuse, this just makes it use comparatively trouble, and easily causes the waste of lot of materials resource, is unfavorable for cost-saving.
[summary of the invention]
The present invention is intended to address the above problem, and provide, a kind of self-locking property is good, simple in structure, easy to use, quality light and reusable hex surface self-locking nut.
For achieving the above object, the invention provides a kind of hex surface self-locking nut, it is provided with hexagon nut body with threaded hole, it is characterized in that, on described hexagon nut body, be evenly provided with the micro-deformation portion along its circumferentially-spaced, described micro-deformation portion is that this micro-deformation portion makes hex surface self-locking nut realize self-locking by the sidewall of this hexagon nut body being applied to radial deformation pressure and producing.
Described micro-deformation portion is on 120 degree even angle hexagon nut body spaced apart and described.
Described micro-deformation portion is formed at the end of described hexagon nut body.
The radial-deformation of described micro-deformation portion is 0.6～1mm, and its axial deflection is 1.5～2.5mm, and tangential deformation amount is 1.2～1.8mm.
The radial-deformation of described micro-deformation portion is 0.8mm, and its axial deflection is 2mm, and its tangential deformation amount is 1.5mm.
The end, one end that deviates from described micro-deformation portion at described hexagon nut body is provided with outward extending extension part, and this extension part and described this body by integral forming of hexagon nut are provided with the through hole with described tapped hole perforation in this extension part.
The diameter of described through hole is greater than the diameter of described tapped hole.
Useful contribution of the present invention is, it efficiently solves the problems referred to above.The present invention is by applying radial deformation pressure to the end of hexagon nut body sidewall, carrying out at 3 pushes and makes the screw thread in hexagon nut body and tapped hole produce micro-distortion and reach self-locking effect, thereby can replace the process portion in Closely locking nut, in realizing reliable self-locking effect, also can greatly save material, reduce manufacture cost.Compare and existing Closely locking nut, tool of the present invention has the following advantages:
1, simple in structure, be convenient to produce, and easy for installation, only need utilize torque spanner just can to assemble and dismantle.And Closely locking nut need be installed supporting process portion and working portion.
2, reusable, can reduce costs.And Closely locking nut need carry out damage type dismounting, disposable use, cost is higher.
3, according to the characteristic distributions of nut bearing capacity, adopt equal strength design, in the situation that bearing same load, materials are minimum, both save material, and also can alleviate nut weight, are applicable to the installation requirement of aerospace field.
4, applied widely, applicable to screw, also applicable to bolt.
[brief description of the drawings]
Fig. 1 is structural representation of the present invention.
Fig. 2 is plan view of the present invention.
Fig. 3 is the half sectional view of A-A in Fig. 2.
Fig. 4 is the half sectional view of B-B in Fig. 2.
Fig. 5 is the distribution map that radial deformation pressure applies, and wherein, the stain in figure represents the location point applying.
Fig. 6 is the distribution schematic diagram of axial deflection, wherein, and the height of the height of black square signal axial deflection in figure, the width of its width indication tangential deformation amount.
Wherein, outer-hexagonal face 22, triangular facet 23, the circumference wall body 24 of hexagon nut body 10, tapped hole 11, outer-hexagonal face 12, extension part 20, inclination.
[embodiment]
The following example is to further explanation of the present invention and supplements, the present invention is not constituted any limitation.
As shown in Fig. 1～Fig. 6, hex surface self-locking nut of the present invention, comprises the extension part 20 that is provided with the hexagon nut body 10 of tapped hole 11 and is connected with these hexagon nut body 10 one.
Specifically, as shown in Figure 1, described hexagon nut body 10 is provided with outer-hexagonal face 12.Described extension part 20 is tilted to extension from the underpart of hexagon nut body 10 and forms.This extension part 20 has the outer-hexagonal face 22 of inclination.The outer-hexagonal face 22 of this inclination and the outer-hexagonal face 12 of the described hexagon nut body 10 crossing angle that is one by one respectively.In the present embodiment, it intersects and is 150 degree angles.Between two adjacent faces of the outer-hexagonal face 22 of described inclination, be respectively equipped with triangular facet 23, this triangular facet 23 and described adjacent hex surface and outer-hexagonal face 12 summit altogether, thus make described extension part 20 and described hexagon nut body 10 there are altogether 6 common summits.
As shown in Figure 1, the outer-hexagonal face 22 of described inclination and the outer edge of triangular facet 23 vertically extend vertically and form circumference wall body 24, and it forms described extension part 20 jointly.
As shown in Figure 3, Figure 4, be provided with axial through hole 21 in the central authorities of described extension part 20, this through hole 21 connects with the tapped hole 11 of described hexagon nut body 10.The conventional outer-hexagonal self-locking nut tapped hole 11 that normally intended diameter is consistent, it is only applicable to attachment screw.And in the present embodiment, in described through hole 21, be not provided with internal thread, and its diameter is greater than tapped hole 11 diameters of described hexagon nut body 10, thereby make hex surface self-locking nut of the present invention can meet aerospace multiple connection requirement, for example, it is both applicable to screw, also applicable to bolt.
For making hex surface self-locking nut of the present invention there is excellent self-locking property, on described hexagon nut body 10, be evenly provided with the micro-deformation portion along its circumferentially-spaced.This micro-deformation portion is by the sidewall of this hexagon nut body 10 being applied to radial deformation pressure and producing.By the sidewall of self-locking nut body is applied to radial deformation pressure, all can there is micro-distortion in the screw thread of this hexagon nut body 10 and tapped hole 11, just can realize good self-locking effect by the micro-deformation of screw thread.As shown in Figure 5, Figure 6, the present embodiment is to apply described radial deformation pressure in the upper end portion of described hexagon nut body 10, and this radial deformation pressure is to be uniformly applied on the same circumferential side wall of hexagon nut body 10 in the mode at 120Du angle, interval.The radial-deformation of described micro-deformation portion is 0.6～1mm, preferably 0.8mm.The axial deflection of this micro-deformation portion is 1.5～2.5mm, preferably 2mm.The tangential deformation amount of this micro-deformation portion is 1.2～1.8mm, preferably 1.5mm.When concrete enforcement, utilize fixture pushing apart from the position at hexagon nut body 10 1.5～2.5mm places, upper-end surface, hexagon nut body 10 sidewalls of tangential wide approximately 1.2～1.8mm are extruded, and towards the deformation quantity that radially produces 0.6～1mm, make therefrom the screw thread in tapped hole 11 produce distortion, and then reach the object of self-locking.
By this, just formed hex surface self-locking nut of the present invention.The present invention makes the screw thread of tapped hole 11 produce distortion by extrusion-deformation, thereby can realize reliable and stable self-locking effect, while installing and using, only need to use the mounting torque of regulation to coordinate with screw or bolt, just can realize reliable self-locking effect, both easy for installation, and simple in structure, and reusable, can greatly reduce user cost, should widely popularize.
Although the present invention is disclosed by above embodiment, scope of the present invention is not limited to this, is not departing under the condition of the present invention's design, and the similar or equivalent element that above each member can be understood with affiliated technical field personnel is replaced.
Claims (7)
1. a hex surface self-locking nut, it is provided with the hexagon nut body (10) of (11) with threaded hole, it is characterized in that, on described hexagon nut body (10), be evenly provided with the micro-deformation portion along its circumferentially-spaced, described micro-deformation portion is that this micro-deformation portion makes hex surface self-locking nut realize self-locking by the sidewall of this hexagon nut body (10) is applied radial deformation pressure and produced.
2. hex surface self-locking nut as claimed in claim 1, is characterized in that, described micro-deformation portion is on 120 degree even angle hexagon nut bodies spaced apart and described (10).
3. hex surface self-locking nut as claimed in claim 2, is characterized in that, described micro-deformation portion is formed at the end of described hexagon nut body (10).
4. hex surface self-locking nut as claimed in claim 3, is characterized in that, the radial-deformation of described micro-deformation portion is 0.6～1mm, and its axial deflection is 1.5～2.5mm, and tangential deformation amount is 1.2～1.8mm.
5. hex surface self-locking nut as claimed in claim 4, is characterized in that, the radial-deformation of described micro-deformation portion is 0.8mm, and its axial deflection is 2mm, and its tangential deformation amount is 1.5mm.
6. hex surface self-locking nut as claimed in claim 5, it is characterized in that, the end, one end that deviates from described micro-deformation portion at described hexagon nut body (10) is provided with outward extending extension part (20), this extension part (20) is one-body molded with described hexagon nut body (10), is provided with the through hole (21) connecting with described tapped hole (11) in this extension part (20).
7. hex surface self-locking nut as claimed in claim 6, is characterized in that, the diameter of described through hole (21) is greater than the diameter of described tapped hole (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410146850.2A CN103899626A (en) | 2014-04-14 | 2014-04-14 | Hexagonal surface self-locking nut |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410146850.2A CN103899626A (en) | 2014-04-14 | 2014-04-14 | Hexagonal surface self-locking nut |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103899626A true CN103899626A (en) | 2014-07-02 |
Family
ID=50991142
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410146850.2A Pending CN103899626A (en) | 2014-04-14 | 2014-04-14 | Hexagonal surface self-locking nut |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103899626A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106151235A (en) * | 2016-06-17 | 2016-11-23 | 浙江吉利罗佑发动机有限公司 | A kind of gas extraction system installs nut |
| CN107461392A (en) * | 2017-08-22 | 2017-12-12 | 苏州威富达精密机械制造有限公司 | It is a kind of can oblique angle fix coupling nut |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201705785U (en) * | 2010-05-28 | 2011-01-12 | 中国航空工业标准件制造有限责任公司 | Flange plate hexagonal nut with self-locking function |
| CN201874958U (en) * | 2010-11-10 | 2011-06-22 | 浙江新东方紧固件有限公司 | Locking nut |
| CN102187105A (en) * | 2008-10-20 | 2011-09-14 | 利斯航空用品公司 | Polygonal driving means with inbuilt collar |
| CN203809478U (en) * | 2014-04-14 | 2014-09-03 | 西安亚太航空技术有限公司 | Hexagonal-face self-locking nut |
-
2014
- 2014-04-14 CN CN201410146850.2A patent/CN103899626A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102187105A (en) * | 2008-10-20 | 2011-09-14 | 利斯航空用品公司 | Polygonal driving means with inbuilt collar |
| CN201705785U (en) * | 2010-05-28 | 2011-01-12 | 中国航空工业标准件制造有限责任公司 | Flange plate hexagonal nut with self-locking function |
| CN201874958U (en) * | 2010-11-10 | 2011-06-22 | 浙江新东方紧固件有限公司 | Locking nut |
| CN203809478U (en) * | 2014-04-14 | 2014-09-03 | 西安亚太航空技术有限公司 | Hexagonal-face self-locking nut |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106151235A (en) * | 2016-06-17 | 2016-11-23 | 浙江吉利罗佑发动机有限公司 | A kind of gas extraction system installs nut |
| CN106151235B (en) * | 2016-06-17 | 2018-03-23 | 浙江吉利罗佑发动机有限公司 | A kind of gas extraction system installs nut |
| CN107461392A (en) * | 2017-08-22 | 2017-12-12 | 苏州威富达精密机械制造有限公司 | It is a kind of can oblique angle fix coupling nut |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7922434B2 (en) | Laminated nut with center tension sleeve | |
| WO2017067324A1 (en) | Threaded-connection anti-loosening locking device | |
| CN203809478U (en) | Hexagonal-face self-locking nut | |
| JP2008051269A (en) | Fastening nut | |
| CN105538206A (en) | Combination wrench for outer hexagon bolts and nuts | |
| US20150174951A1 (en) | Wheel structure for an automobile | |
| CN105065401A (en) | Expansion bolt assembly | |
| CN103899626A (en) | Hexagonal surface self-locking nut | |
| US7789608B2 (en) | Laminated nut with tension indicator | |
| CN204512120U (en) | Connect bearing pin | |
| CN104907999A (en) | Blind hole inner shaft sleeve detachment device | |
| JP3163716U (en) | Fastening structure for locking nut, bolt and nut | |
| US7670092B2 (en) | Laminated nut with center tension sleeve | |
| CN206175448U (en) | Nut fastener | |
| CN211314794U (en) | Quincunx and sleeve combined bolt | |
| CN102555662A (en) | Wheel mounting structure | |
| CN209818497U (en) | Flange surface self-locking bolt | |
| CN105275945A (en) | Slitting snap ring of cylindrical roller bearing belt | |
| CN201554760U (en) | Vehicle wheel hub anti-rotation fastener | |
| CN103899630A (en) | Locking nut | |
| AU2019299616A1 (en) | Mounting sleeve | |
| CN201896845U (en) | Locking nut for underwater pump | |
| CN110345147B (en) | Effective anti-loosening combined nut | |
| CN201554741U (en) | Vehicle wheel hub fastening piece | |
| CN202628744U (en) | Detachable screw anti-looseness component |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140702 |