CN112392825A - Light riveting bolt for aviation - Google Patents
Light riveting bolt for aviation Download PDFInfo
- Publication number
- CN112392825A CN112392825A CN201910745858.3A CN201910745858A CN112392825A CN 112392825 A CN112392825 A CN 112392825A CN 201910745858 A CN201910745858 A CN 201910745858A CN 112392825 A CN112392825 A CN 112392825A
- Authority
- CN
- China
- Prior art keywords
- aviation
- riveting bolt
- bin
- riveting
- main body
- 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
- 230000005540 biological transmission Effects 0.000 claims abstract description 18
- 230000001050 lubricating effect Effects 0.000 claims abstract description 17
- 239000013585 weight reducing agent Substances 0.000 claims abstract description 11
- 230000003014 reinforcing effect Effects 0.000 claims description 19
- 238000005192 partition Methods 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 4
- 238000002955 isolation Methods 0.000 claims description 2
- 230000000149 penetrating effect Effects 0.000 claims 1
- 239000007788 liquid Substances 0.000 description 8
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 3
- 238000005461 lubrication Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
- F16B35/04—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16N—LUBRICATING
- F16N1/00—Constructional modifications of parts of machines or apparatus for the purpose of lubrication
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
The invention discloses a light riveting bolt for aviation, which comprises an aviation riveting bolt main body, wherein a weight reduction bin is arranged inside the aviation riveting bolt main body, springs are connected and arranged on the right sides of the upper end and the lower end of the aviation riveting bolt main body, a piston is sleeved on the surface of a transmission rod, oil outlets are arranged on the upper end and the lower end of the aviation riveting bolt main body, a moving bin is arranged on the left side of the aviation riveting bolt main body, and the right side of the transmission rod penetrates through a lubricating bin and extends into the moving bin to be welded and fixed with a push plate. According to the invention, the weight reduction bin is arranged in the main body of the aviation riveting bolt, so that the mass of the device is reduced, the load burden in aviation is reduced, the aviation efficiency is improved, the strength of the device is increased, the practicability of the device is improved, the device is clamped, the device is prevented from falling off due to long-time vibration, the potential safety hazard is avoided, and the device is prevented from rusting, being incapable of being disassembled and influencing the use of the aviation device.
Description
Technical Field
The invention relates to the technical field of light riveting bolts for aviation, in particular to a light riveting bolt for aviation.
Background
The riveting bolt is a bolt used for connecting and fixing objects, has stable connection and convenient disassembly, has higher strength and stability, but the riveting bolt needed to be used in the field of aviation needs to limit the weight of the riveting bolt at the present stage, and the riveting bolt for aviation often contacts with water vapor, is easy to rust, leads to being difficult to disassemble, and the light riveting bolt on the market at the present stage can not ensure the strength and the stability of the bolt after the quality is lightened. We have therefore proposed an aerospace lightweight clinch bolt to address the above problems.
Disclosure of Invention
The invention aims to provide a light riveting bolt for aviation, which aims to solve the problems that in the background technology, the weight of the riveting bolt needs to be limited in the stages such as the aviation field, the riveting bolt for aviation often contacts with water vapor, is easy to rust and difficult to disassemble, and the light riveting bolt on the market at the present stage cannot ensure the strength and the stability of the light riveting bolt after the quality is reduced.
In order to achieve the purpose, the invention provides the following technical scheme: a light weight riveting bolt for aviation comprises an aviation riveting bolt main body, wherein a weight reduction bin is arranged inside the aviation riveting bolt main body, and the interior of the weight reduction bin is provided with a first reinforcing rib, the right sides of the upper end and the lower end of the aviation riveting bolt main body are connected with springs, and the inside of the spring is provided with fixed blocks, the surface of the aviation riveting bolt main body is uniformly provided with external threads, the aviation riveting bolt main body is provided with lubricating bins at the upper end and the lower end, a transmission rod is inserted at the left side of the lubricating bins, a piston is sleeved on the surface of the transmission rod, and the pistons are divided into three groups, the upper end and the lower end of the aviation riveting bolt main body are both provided with oil outlets which are communicated with the transmission rod, the left side of the aviation riveting bolt main body is provided with a movable bin, and the inside push pedal that is provided with in the storehouse moves, the right side of transfer line all passes lubricated storehouse and extends to the storehouse of moving inside and push pedal welded fastening.
Preferably, the surface of the first reinforcing rib is symmetrically welded with five groups of second reinforcing ribs, and the second reinforcing ribs are welded and fixed with the inner wall of the weight reduction bin.
Preferably, the left and right sides of fixed block all is the inclined plane form, the fixed block is kept away from the one end of aviation riveting bolt main part and is all extended to fixed storehouse outside.
Preferably, the lubricating bin is divided into three parts by a partition plate, and the partition plate is welded and fixed with the inner walls of the upper end and the lower end of the lubricating bin.
Preferably, the joint of the transmission rod and the isolation plate is glued with a sealing gasket, and the sealing gasket is abutted to the transmission rod.
Compared with the prior art, the invention has the beneficial effects that: the weight reduction bin is arranged in the main body of the aviation riveting bolt, so that the mass of the device is reduced, the load burden in aviation is reduced, the aviation efficiency is improved, the mass of the device is reduced through the first reinforcing rib and the second reinforcing rib, the compressive strength of the device is enhanced through the first reinforcing rib and the strength of the device is increased, the practicability of the device is improved, the device is clamped, the device is prevented from falling off due to long-time vibration, potential safety hazards are caused, and the device is prevented from rusting, being incapable of being disassembled and influencing the use of the aviation device;
(1) the weight reduction bin is arranged in the main body of the aviation riveting bolt, so that the mass of the device is reduced, the load burden in aviation is reduced, and the aviation efficiency is improved;
(2) by arranging the fixing bin and the fixing block, when a user uses the device, the device is inserted into the bolt hole, the fixing block is abutted against the bolt hole, then the fixing block moves towards the inside of the fixing bin to compress the spring, then the device moves towards the bolt hole through the external thread by rotating the aviation riveting bolt main body, when the right side of the device passes through the bolt hole, the fixing block is not abutted against the bolt hole any more, then the fixing block is driven by the spring to reset, the device is clamped, and the device is prevented from falling off due to long-time vibration and potential safety hazards are avoided;
(3) through setting up lubricated storehouse, transfer line, piston, removal storehouse and push pedal, the user is when regularly examining aviation flying device, through pressing the push pedal for transfer line and piston move rightly, then pass through the lubricated liquid of piston with lubricated storehouse inside and promote between the oil outlet to the external screw thread, and external thread lubrication between the continuous inflow external screw thread of lubricated liquid avoids the device to rust, and unable dismantlement influences aviation device's use.
Description of the drawings:
in order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic sectional elevation view of the structure of the present invention;
FIG. 2 is a schematic top sectional view of the first and second ribs of the present invention;
FIG. 3 is an enlarged view of the structure A in FIG. 1 according to the present invention;
fig. 4 is a schematic front view of the structure of the present invention.
In the figure: 1. an aviation riveting bolt body; 2. a weight reduction bin; 3. a first reinforcing rib; 4. a spring; 5. fixing the bin; 6. a fixed block; 7. an external thread; 8. a lubrication bin; 9. a transmission rod; 10. a piston; 11. an oil outlet hole; 12. moving the bin; 13. pushing the plate; 14. and a second reinforcing rib.
The specific implementation mode is as follows:
the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, an embodiment of the present invention is shown: a light weight riveting bolt for aviation comprises an aviation riveting bolt main body 1, wherein a weight reducing bin 2 is arranged inside the aviation riveting bolt main body 1, a first reinforcing rib 3 is arranged inside the weight reducing bin 2, second reinforcing ribs 14 are symmetrically welded on the surface of the first reinforcing rib 3, five groups of the second reinforcing ribs 14 are arranged, the second reinforcing ribs 14 are fixedly welded with the inner wall of the weight reducing bin 2 and are used for improving the strength of the device and avoiding the strength reduction caused by the mass reduction, a spring 4 is connected and arranged on the right side of the upper end and the lower end of the aviation riveting bolt main body 1, a fixing block 6 is arranged inside the spring 4, the left side and the right side of the fixing block 6 are in an inclined plane shape, one end, far away from the aviation riveting bolt main body 1, of the fixing block 6 extends to the outside of a fixing bin 5 and is used for passing through the inclined plane shape, when the rest bolt holes of the fixing block 6 are abutted against, external threads 7 are uniformly formed on the surface of the aviation riveting bolt body 1;
the aviation riveting bolt comprises a main body 1, a lubricating bin 8, a lubricating liquid, a baffle plate, a transmission rod 9, a sealing gasket, a transmission rod 9, a piston 10, three groups of pistons 10, oil outlets 11, a lubricating liquid, a lubricating liquid, a liquid, and the oil outlet 11 is linked together with the transfer line 9, and the removal storehouse 12 has been seted up to the left side of aviation riveting bolt main part 1, and removes the inside push pedal 13 that is provided with of storehouse 12, and the right side of transfer line 9 all passes lubricated storehouse 8 and extends to and remove the storehouse 12 inside and push pedal 13 welded fastening.
The working principle is as follows: when a user uses the device, the device is inserted into a bolt hole, the fixing block 6 is abutted against the bolt hole, then the fixing block 6 moves towards the inside of the fixing bin 5 to compress the spring 4, then the device moves towards the bolt hole through the external thread 7 by rotating the aviation riveting bolt main body 1, when the right side of the device passes through the bolt hole, the fixing block 6 is not abutted against the bolt hole any more, then the fixing block 6 is driven to reset through the spring 4, and the device is clamped, the device is prevented from falling off due to long-time vibration, so that potential safety hazards are avoided;
when a user regularly checks the aviation flight device, the push plate 13 is pressed to push the transmission rod 9 and the piston 10 to move rightwards, then the piston 10 pushes lubricating liquid in the lubricating bin 8 to the outside between the threads 7 through the oil outlet 11, the lubricating liquid continuously flows into the outside between the threads 7 to lubricate the threads 7, and the phenomenon that the device is rusted and cannot be disassembled to influence the use of the aviation flight device is avoided.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (5)
1. The utility model provides a light riveting bolt for aviation, includes aviation riveting bolt main part (1), its characterized in that: the aviation riveting bolt is characterized in that a weight reduction bin (2) is arranged in the aviation riveting bolt body (1), a first reinforcing rib (3) is arranged in the weight reduction bin (2), springs (4) are connected to the right sides of the upper end and the lower end of the aviation riveting bolt body (1), fixing blocks (6) are arranged in the springs (4), external threads (7) are uniformly arranged on the surface of the aviation riveting bolt body (1), lubricating bins (8) are arranged at the upper end and the lower end of the aviation riveting bolt body (1), transmission rods (9) are inserted in the left sides of the lubricating bins (8), a partition plate is inserted in the right sides of the transmission rods (9) in a penetrating manner, pistons (10) are sleeved on the surface of the transmission rods (9), the pistons (10) are in three groups, oil outlet holes (11) are formed in the upper end and the lower end of the aviation riveting bolt body (1), and the oil outlet holes (11) are communicated with the transmission rods (, the aviation riveting bolt is characterized in that a moving bin (12) is arranged on the left side of the aviation riveting bolt main body (1), a push plate (13) is arranged inside the moving bin (12), and the right side of the transmission rod (9) penetrates through the lubricating bin (8) and extends to the inside of the moving bin (12) to be welded and fixed with the push plate (13).
2. The light weight rivet bolt for aviation according to claim 1, wherein: the surface of the first reinforcing rib (3) is symmetrically welded with second reinforcing ribs (14), the number of the second reinforcing ribs (14) is five, and the second reinforcing ribs (14) are welded and fixed with the inner wall of the weight reduction bin (2).
3. The light weight rivet bolt for aviation according to claim 1, wherein: the left side and the right side of the fixing block (6) are all inclined planes, and one end, far away from the aviation riveting bolt main body (1), of the fixing block (6) extends to the outside of the fixing bin (5).
4. The light weight rivet bolt for aviation according to claim 1, wherein: the lubricating bin (8) is divided into three parts by the partition board, and the partition board is welded and fixed with the inner walls of the upper end and the lower end of the lubricating bin (8).
5. The light weight rivet bolt for aviation according to claim 1, wherein: and sealing gaskets are glued at the joints of the transmission rod (9) and the isolation plate and are abutted against the transmission rod (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910745858.3A CN112392825A (en) | 2019-08-13 | 2019-08-13 | Light riveting bolt for aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910745858.3A CN112392825A (en) | 2019-08-13 | 2019-08-13 | Light riveting bolt for aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112392825A true CN112392825A (en) | 2021-02-23 |
Family
ID=74602715
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910745858.3A Pending CN112392825A (en) | 2019-08-13 | 2019-08-13 | Light riveting bolt for aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112392825A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113685415A (en) * | 2021-08-20 | 2021-11-23 | 宁波九龙紧固件制造有限公司 | Flexible high-strength bolt and production process thereof |
-
2019
- 2019-08-13 CN CN201910745858.3A patent/CN112392825A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113685415A (en) * | 2021-08-20 | 2021-11-23 | 宁波九龙紧固件制造有限公司 | Flexible high-strength bolt and production process thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20210223 |