CN211805834U - 737 wing body radome fairing riveting piece specialized tool - Google Patents
737 wing body radome fairing riveting piece specialized tool Download PDFInfo
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- CN211805834U CN211805834U CN201922332642.2U CN201922332642U CN211805834U CN 211805834 U CN211805834 U CN 211805834U CN 201922332642 U CN201922332642 U CN 201922332642U CN 211805834 U CN211805834 U CN 211805834U
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Abstract
The utility model discloses an 737 wing body radome fairing riveting spare specialized tool, its structure includes the instrument body, be provided with fixed plate, spliced pole and riveting axle on the instrument body, the fixed plate pass through the rivet with the left side of instrument body is connected, the spliced pole pass through the rivet with the inboard left wall of instrument body is connected mutually, the riveting axle pass through the rivet with the inboard right wall of instrument body is connected mutually, be provided with fixing bolt on the fixed plate, the right-hand member of spliced pole is provided with the riveting cover, the left end of riveting axle is provided with draw-in groove and cover axle, the draw-in groove is located the inside of riveting axle, the cover axle through weld in the centre department of riveting axle is connected, the right side of riveting cover is provided with the riveting spare. The utility model discloses speed when having accelerated the riveting piece dismouting, time when having saved the riveting piece dismouting has reduced the intensity of labour of operating personnel when to the riveting piece dismouting, has improved the convenience when special-purpose tool uses.
Description
Technical Field
The utility model relates to a specialized tool technical field specifically is 737 wing body radome fairing riveting specialized tool.
Background
Currently, the existing special tool for the 737 wing body fairing riveting piece has some defects, for example; the speed of the existing 737 wing body fairing riveting piece special tool is slower when the riveting piece is disassembled and assembled, the time of disassembling and assembling the riveting piece is prolonged, the labor intensity of operators when the riveting piece is disassembled and assembled is improved, and the convenience of the special tool when the special tool is used is reduced. For this reason, new technical solutions need to be designed to solve the problem.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide 737 wing body radome fairing riveting specialized tool, solved the problem that proposes among the background art.
In order to achieve the above object, the utility model provides a following technical scheme: 737 wing body radome fairing riveting spare specialized tool, including the instrument body, be provided with fixed plate, spliced pole and riveting axle on the instrument body, the fixed plate pass through the rivet with the left side of instrument body is connected, the spliced pole pass through the rivet with the inboard left wall of instrument body is connected mutually, the riveting axle pass through the rivet with the inboard right wall of instrument body is connected mutually, be provided with fixing bolt on the fixed plate, the right-hand member of spliced pole is provided with the riveting cover, the left end of riveting axle is provided with draw-in groove and sleeve shaft, the draw-in groove is located the inside of riveting axle, the sleeve shaft through weld in the centre department of riveting axle is connected, the right side of riveting cover is provided with the riveting spare.
As a preferred embodiment of the present invention, the upper surface of the fixing plate and the upper surface of the tool body are on the same horizontal plane, and are fixedly connected to each other through a fixing bolt.
As a preferred embodiment of the present invention, the riveting sleeve is connected to the right end of the connecting column through a rivet, and the right end of the riveting sleeve corresponds to the position of the riveting shaft.
As an optimized embodiment of the present invention, the length of the sleeve shaft is 1mm, and the depth of the slot is 1.5 mm.
As a preferred embodiment of the present invention, the size of the riveting member is identical to the size of the riveting sleeve and the riveting shaft.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model discloses a riveting axle and the combination of riveting cover, the effectual speed when accelerating the riveting piece dismouting, the time when having saved the riveting piece dismouting has reduced the intensity of labour of operating personnel when to the riveting piece dismouting, has improved the convenience when special-purpose tool uses.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
FIG. 1 is a front view of a 737 special tool for a fairing rivet of a wing body of the present invention;
fig. 2 is a side view of the riveting shaft of the special tool for the 737 wing body fairing riveting piece of the present invention.
In the figure: the riveting tool comprises a tool body 1, a fixing plate 2, a connecting column 3, a riveting shaft 4, a fixing bolt 5, a riveting sleeve 6, a clamping groove 7, a sleeve shaft 8 and a riveting piece 9.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
In the description of the present invention, it should be noted that unless otherwise explicitly stated or limited, the terms "mounted," "connected" and "disposed" are to be construed broadly, and may for example be fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. To the ordinary technical personnel in this field, can understand the specific meaning in the utility model of above-mentioned term with the concrete condition, the utility model provides an electrical apparatus's model is the reference only, can be through changing different models electrical apparatus that the function is the same according to the actual use condition.
Referring to fig. 1-2, the present invention provides a technical solution: 737 wing body radome fairing riveting member specialized tool, including tool body 1, be provided with fixed plate 2, spliced pole 3 and riveting axle 4 on tool body 1, fixed plate 2 is connected with the left side of tool body 1 through the rivet, spliced pole 3 is connected with the left wall of tool body 1 inboard through the rivet, riveting axle 4 is connected with the right wall of tool body 1 inboard through the rivet, be provided with fixing bolt 5 on fixed plate 2, the right-hand member of spliced pole 3 is provided with riveting cover 6, the left end of riveting axle 4 is provided with draw-in groove 7 and sleeve shaft 8, draw-in groove 7 is located the inside of riveting axle 4, sleeve shaft 8 is connected through welding in the middle of riveting axle 4, the right side of riveting cover 6 is provided with riveting member 9, in this embodiment as shown in figure 1 and figure 2 through the combination of riveting axle 4 and riveting cover 6, the speed of riveting piece 9 when dismouting has effectually been accelerated, time when having saved riveting piece 9 dismouting, has reduced operating personnel intensity of labour when the dismouting to riveting piece 9, has improved the convenience when special-purpose tool used.
In the embodiment, referring to fig. 1, the upper surface of the fixing plate 2 and the upper surface of the tool body 1 are on the same horizontal plane and are fixedly connected to the inside of the tool body 1 through a fixing bolt 5, which is effective in securing the fixing plate 2 and the tool body 1.
In this embodiment, referring to fig. 1, the riveting sleeve 6 is connected to the right end of the connecting column 3 through a rivet, and the right end of the riveting sleeve 6 corresponds to the position of the riveting shaft 4, so that the stability of the riveting member 9 during assembling and disassembling can be effectively improved.
In this embodiment, referring to fig. 2, the length of the sleeve shaft 8 is 1mm, and the depth of the slot 7 is 1.5mm, which is effective in improving the convenience of the rivet 9 during connection.
In the embodiment, referring to fig. 1, the size of the riveting member 9 is matched with the size of the riveting sleeve 6 and the size of the riveting shaft 4, and the riveting member 9 has an effect of effectively improving the convenience of assembling and disassembling the riveting member 9.
It should be noted that, the 737 special tool for riveting the wing fairing of the present invention includes a tool body 1, a fixing plate 2, a connecting post 3, a riveting shaft 4, a fixing bolt 5, a riveting sleeve 6, a clamping groove 7, a sleeve shaft 8, a riveting member 9, etc. all of which are parts known to those skilled in the art or general standard parts, and the structure and principle of which are known to those skilled in the art through technical manuals or conventional experimental methods, in the idle position of the device, all of the above electric devices, which refer to power components, electric devices, and adaptive monitoring computers, are connected to a power supply through wires, and specific connection means should refer to the following working principle that the electric devices complete electrical connection in sequence, and the detailed connection means is known in the art, and the following working principle and process are mainly introduced without describing electrical control, when 737 wing body radome fairing riveting piece specialized tool uses, through the combination of riveting axle 4 and riveting cover 6, the effectual speed of when accelerating riveting 9 dismouting, time when having saved riveting 9 dismouting, reduced the intensity of labour of operating personnel when the dismouting to riveting 9, improved the convenience when specialized tool uses.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. 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.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (5)
1.737 wing body radome fairing riveting specialized tool, including instrument body (1), its characterized in that: the tool body (1) is provided with a fixed plate (2), a connecting column (3) and a riveting shaft (4), the fixing plate (2) is connected with the left side of the tool body (1) through a rivet, the connecting column (3) is connected with the left wall of the inner side of the tool body (1) through a rivet, the riveting shaft (4) is connected with the right wall of the inner side of the tool body (1) through a rivet, a fixing bolt (5) is arranged on the fixing plate (2), a riveting sleeve (6) is arranged at the right end of the connecting column (3), the left end of the riveting shaft (4) is provided with a clamping groove (7) and a sleeve shaft (8), the clamping groove (7) is located inside the riveting shaft (4), the sleeve shaft (8) is connected with the middle of the riveting shaft (4) through welding, and the right side of the riveting sleeve (6) is provided with a riveting piece (9).
2. The 737 wing body fairing rivet special tool of claim 1, wherein: the upper surface of the fixing plate (2) and the upper surface of the tool body (1) are on the same horizontal plane and fixedly connected with the inside of the tool body (1) through a fixing bolt (5).
3. The 737 wing body fairing rivet special tool of claim 1, wherein: the riveting sleeve (6) is connected with the right end of the connecting column (3) through a rivet, and the right end of the riveting sleeve (6) corresponds to the position of the riveting shaft (4).
4. The 737 wing body fairing rivet special tool of claim 1, wherein: the length of sleeve axle (8) is 1mm, the degree of depth of draw-in groove (7) is 1.5 mm.
5. The 737 wing body fairing rivet special tool of claim 1, wherein: the size of the riveting piece (9) is matched with that of the riveting sleeve (6) and the riveting shaft (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922332642.2U CN211805834U (en) | 2019-12-23 | 2019-12-23 | 737 wing body radome fairing riveting piece specialized tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922332642.2U CN211805834U (en) | 2019-12-23 | 2019-12-23 | 737 wing body radome fairing riveting piece specialized tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211805834U true CN211805834U (en) | 2020-10-30 |
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ID=73032758
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922332642.2U Active CN211805834U (en) | 2019-12-23 | 2019-12-23 | 737 wing body radome fairing riveting piece specialized tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211805834U (en) |
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2019
- 2019-12-23 CN CN201922332642.2U patent/CN211805834U/en active Active
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