CN209935937U - Be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device - Google Patents
Be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device Download PDFInfo
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- CN209935937U CN209935937U CN201920775897.3U CN201920775897U CN209935937U CN 209935937 U CN209935937 U CN 209935937U CN 201920775897 U CN201920775897 U CN 201920775897U CN 209935937 U CN209935937 U CN 209935937U
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Abstract
The utility model discloses a be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device, including bottom plate, internal and external screw thread screw, guide post, ears layer board auto-lock nut bushing plate, monaural layer board auto-lock nut bushing plate, angular form layer board auto-lock nut bushing plate and unmanned aerial vehicle machine equipment fixing frame, first mounting hole and first fixed orifices have been seted up to the bottom plate upper surface, and the bottom plate upper surface is located first mounting hole and has seted up first hole groove, second hole groove, third hole groove, fourth hole groove and fifth hole groove of drawing all around, first external screw thread has been seted up to internal and external screw thread screw surface, and the internal surface of internal and external screw thread screw has seted up the internal thread, the surface of internal and external screw thread screw has cup jointed the axle, and the upper surface of internal and external screw thread screw has seted up a word groove. The utility model relates to a simply, easily master, the cost is with low costs, and the facilitate promotion has reduced the operation degree of difficulty, improves work efficiency, saves manufacturing cost for the company.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle airborne equipment's technical field specifically is a be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole to draw hole device.
Background
Certain environmental monitoring unmanned aerial vehicle airborne equipment installation need use layer board auto-lock nut, and operation flow is as follows: and manufacturing a screw hole of the supporting plate self-locking nut, fixing the supporting plate self-locking nut by using the same type of supporting plate self-locking nut as a template, and manufacturing a rivet hole for connecting the supporting plate self-locking nut and the structure. The method has low working efficiency, the same splint self-locking nut is repeatedly used, and the thread is easily damaged after being disassembled and assembled for many times, thereby causing unnecessary loss. And, the rivet hole on the layer board self-locking nut is through drawing the hole to the structure many times, acts as the bushing plate function, leads to the rivet hole on the layer board self-locking nut to receive the wearing and tearing of drill bit and grow, and the rivet hole site of making also has great error, causes the layer board self-locking nut to take the inclined state after putting into the rivet when riveting, seriously influences product quality.
Therefore, a drilling template capable of replacing a common supporting plate self-locking nut is needed, and the drilling template can be suitable for rivet hole making of supporting plate self-locking nuts of different types and specifications, so that the working efficiency is improved, and the product quality is guaranteed.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a be used for environmental monitoring unmanned aerial vehicle layer board self-locking nut rivet hole to draw hole device, it is simple to possess the design, easily masters, and the cost is with low costs, and the facilitate promotion has reduced the operation degree of difficulty, improves work efficiency, for the advantage that the company saved manufacturing cost, has solved that same layer board self-locking nut recycles, many times dismouting back thread is very easy to be damaged, causes the unnecessary loss. And, the rivet hole on the layer board self-locking nut is through drawing the hole to the structure many times, acts as the bushing plate function, leads to the rivet hole on the layer board self-locking nut to receive the wearing and tearing of drill bit and grow, and the rivet hole site of making also has great error, causes the layer board self-locking nut to take the inclined state after putting into the rivet when riveting, seriously influences product quality's problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device, includes bottom plate, internal and external screw thread screw, guide post, ears layer board auto-lock nut bushing plate, monaural layer board auto-lock nut bushing plate, angular form layer board auto-lock nut bushing plate and unmanned aerial vehicle machine carries equipment fixing frame, first mounting hole and second mounting hole have been seted up to the upper surface of bottom plate, and the upper surface of bottom plate lies in first mounting hole and has seted up first draw hole groove, second draw hole groove, third draw hole groove, fourth draw hole groove and fifth draw hole groove all around, first external screw thread has been seted up to the surface of internal and external screw thread screw, and the internal surface of internal and external screw thread screw has seted up the internal thread, the surface of internal and external screw thread screw has cup jointed the axle, and the upper surface of internal and external screw thread screw.
Preferably, the outer surface of the guide post is provided with second external threads, the lower surface of the guide post is welded with a guide pin, and the second external threads are meshed with the internal threads.
Preferably, the upper surface of the double-lug supporting plate self-locking nut drill plate is provided with a first through hole, a second through hole and a third through hole, the lower surface of the double-lug supporting plate self-locking nut drill plate is welded with a first positioning pin, and the first through hole and the shaft are equal in size.
Preferably, the upper surface of the single-lug supporting plate self-locking nut drill plate is provided with a first fixing hole and a second fixing hole, the lower surface of the single-lug supporting plate self-locking nut drill plate is welded with a second positioning pin, and the size of the second positioning pin is equal to that of a second hole guiding groove in the upper surface of the bottom plate.
Preferably, the upper surface of the angular support plate self-locking nut drill plate is provided with a first connecting hole, a second connecting hole and a third connecting hole, the lower surface of the angular support plate self-locking nut drill plate is welded with a third positioning pin, and the first connecting hole is equal to the shaft in size.
Preferably, the upper surface of the unmanned aerial vehicle airborne equipment mounting frame is provided with a guide hole.
Compared with the prior art, the beneficial effects of the utility model are as follows: the utility model discloses a set up the bottom plate, interior external screw thread screw, the guide post, two ears layer board self-locking nut bushing plate, single ear layer board self-locking nut bushing plate, angular form layer board self-locking nut bushing plate and unmanned aerial vehicle airborne equipment mounting bracket, reached the design simple, easily master, the cost is with low costs, be convenient for promote, reduced the operation degree of difficulty, improve work efficiency, the effect of saving manufacturing cost for the company, layer board self-locking nut bushing plate fixes on the bottom plate through interior external screw thread screw, make the screw hole on the unmanned aerial vehicle airborne equipment mounting bracket of required installation layer board self-locking nut, put the guide post on the bushing plate into the screw hole on the unmanned aerial vehicle airborne equipment mounting bracket, draw the rivet hole to unmanned aerial vehicle airborne equipment mounting bracket according to the rivet hole on the layer board self-locking nut bushing plate, make layer, corresponding layer board self-locking nut jig is selected according to layer board self-locking nut type to select the guide post of corresponding diameter to put into unmanned aerial vehicle airborne equipment mounting bracket screw hole, draw forth the rivet hole that layer board self-locking nut and unmanned aerial vehicle airborne equipment mounting bracket are connected, this scheme structural design is simple, easily masters, and the cost is with low costs, and the facilitate promotion has reduced the operation degree of difficulty, improves work efficiency, saves manufacturing cost for the company.
Drawings
FIG. 1 is a schematic structural view of a rivet hole guiding device of a double-lug supporting plate self-locking nut of the utility model;
FIG. 2 is a schematic structural view of a rivet hole guiding device of a single-lug supporting plate self-locking nut of the present invention;
FIG. 3 is a schematic structural view of the rivet hole guiding device of the self-locking nut of the angular supporting plate of the present invention;
FIG. 4 is a schematic view of the bottom plate structure of the present invention;
FIG. 5 is a schematic view of the structure of the internal and external screw thread screw of the present invention;
fig. 6 is a schematic structural view of the guide post of the present invention;
FIG. 7 is a schematic view of the double-lug supporting plate self-locking nut drill plate structure of the present invention;
FIG. 8 is a schematic structural view of a single-lug supporting plate self-locking nut drill plate of the present invention;
FIG. 9 is a schematic view of the angle-shaped supporting plate self-locking nut drill plate structure of the present invention;
fig. 10 is a view of the present invention from direction a of fig. 9;
fig. 11 is a schematic view of the structure of the present invention.
In the figure: 1. a base plate; 11. a first mounting hole; 12. a second mounting hole; 13. a first lead hole groove; 14. a second lead hole groove; 15. a third lead hole groove; 17. a fourth lead hole groove; 2. an internal and external thread screw; 21. a first external thread; 22. an internal thread; 23. a shaft; 24. a straight slot; 3. a guide post; 31. a first external thread; 32. a guide pin; 4. a double-lug supporting plate self-locking nut drilling template; 41. a first through hole; 42. a second through hole; 43. a third through hole; 44. a first positioning pin; 5. a single-lug supporting plate self-locking nut drill plate; 51. a first fixing hole; 52. a second fixing hole; 53. a second positioning pin; 6. the angular supporting plate is self-locked with a nut drilling template; 61. a first connection hole; 62. a second connection hole; 63. a third connection hole; 64. a third positioning pin; 7. an unmanned aerial vehicle airborne equipment mounting frame; 71. and (4) leading holes.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" 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 simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1 to fig. 11, the present invention provides an embodiment: a self-locking nut rivet hole leading device for an environment monitoring unmanned aerial vehicle supporting plate comprises a bottom plate 1, an internal and external thread screw 2, a guide post 3, a double-lug supporting plate self-locking nut drill plate 4, a single-lug supporting plate self-locking nut drill plate 5, an angular supporting plate self-locking nut drill plate 6 and an unmanned aerial vehicle onboard equipment mounting frame 7, wherein the upper surface of the bottom plate 1 is provided with a first mounting hole 11 and a second mounting hole 12, the upper surface of the bottom plate 1 is positioned around the first mounting hole 11 and is provided with a first leading hole groove 13, a second leading hole groove 14, a third leading hole groove 15, a fourth leading hole groove 16 and a fifth leading hole groove 17, the outer surface of the internal and external thread screw 2 is provided with a first external thread 21, the inner surface of the internal and external thread screw 2 is provided with an internal thread 22, the outer surface of the internal and external thread screw 2 is sleeved with a shaft 23, the upper surface of the internal and external thread screw 2 is provided with, and a guide pin 32 is welded to the lower surface of the guide post 3, and the second external thread 31 is engaged with the internal thread 22.
The upper surface of the double-lug supporting plate self-locking nut drill plate 4 is provided with a first through hole 41, a second through hole 42 and a third through hole 43, the lower surface of the double-lug supporting plate self-locking nut drill plate 4 is welded with a first positioning pin 44, the first through hole 41 and the shaft 23 are equal in size, the second through hole 42 penetrates through a first lead-out hole groove 13 and a fourth lead-out hole groove 16 on the upper surface of the bottom plate 1 to lead out a double-lug supporting plate self-locking nut rivet hole to the unmanned aerial vehicle airborne equipment mounting rack 7, the double-lug supporting plate self-locking nut drill plate 4 is fixed on the bottom plate 1 through an internal thread screw 2 to manufacture a screw hole on the unmanned aerial vehicle airborne equipment mounting rack 7, a guide post 3 on the double-lug supporting plate self-locking nut drill plate 4 is put into the screw hole on the unmanned aerial vehicle airborne equipment mounting rack 7, the rivet hole is led out to the unmanned aerial vehicle airborne equipment mounting, and selecting a corresponding double-lug supporting plate self-locking nut drill plate 4 according to the type of the supporting plate self-locking nut, selecting a guide post 3 with a corresponding diameter, putting the guide post into a screw hole of an unmanned aerial vehicle airborne equipment mounting frame 7, and leading out a rivet hole for connecting the supporting plate self-locking nut with the unmanned aerial vehicle airborne equipment mounting frame 7.
The upper surface of the single-lug supporting plate self-locking nut drill plate 5 is provided with a first fixing hole 51 and a second fixing hole 52, the lower surface of the single-lug supporting plate self-locking nut drill plate 5 is welded with a second positioning pin 53, the size of the second positioning pin 53 is equal to that of a second guide hole groove 14 on the upper surface of the bottom plate 1, the second fixing hole 52 penetrates through the second guide hole groove 14 on the upper surface of the bottom plate 1 to lead out a single-lug supporting plate self-locking nut rivet hole to an unmanned aerial vehicle airborne equipment mounting rack 7, the single-lug supporting plate self-locking nut drill plate 5 is fixed on the bottom plate 1 through an internal thread screw 2, a screw hole is formed in the unmanned aerial vehicle airborne equipment mounting rack 7 required to be provided with a supporting plate self-locking nut, a guide post 3 on the single-lug supporting plate self-locking nut drill plate 5 is placed in the screw hole on the unmanned aerial vehicle airborne equipment mounting rack 7, a supporting plate self-locking nut screw hole is manufactured through the unmanned aerial vehicle airborne equipment mounting frame 7, a corresponding single-lug supporting plate self-locking nut drill plate 5 is selected according to the type of the supporting plate self-locking nut, the guide column 3 with the corresponding diameter is selected to be placed into the screw hole of the unmanned aerial vehicle airborne equipment mounting frame 7, and a rivet hole formed by the supporting plate self-locking nut and the unmanned aerial vehicle airborne equipment mounting frame 7 is led out.
A first connecting hole 61, a second connecting hole 62 and a third connecting hole 63 are formed in the upper surface of the angle support plate self-locking nut drill plate 6, a third positioning pin 64 is welded on the lower surface of the angle support plate self-locking nut drill plate 6, the first connecting hole 61 is equal to the shaft 23 in size, the third connecting hole 63 penetrates through a third guide hole groove 15 and a fifth guide hole groove 17 in the upper surface of the base plate 1 to lead out an angle support plate self-locking nut rivet hole to the unmanned aerial vehicle airborne equipment mounting frame 7, the angle support plate self-locking nut drill plate 6 is fixed on the base plate 1 through an internal thread screw 2, a screw hole is formed in the unmanned aerial vehicle airborne equipment mounting frame 7 required to be provided with the support plate self-locking nut drill plate, the guide post 3 on the angle support plate self-locking nut drill plate 6 is placed into the screw hole in the unmanned aerial vehicle airborne equipment mounting frame 7, and the rivet hole, a supporting plate self-locking nut screw hole is manufactured through the unmanned aerial vehicle airborne equipment mounting frame 7, a corresponding angular supporting plate self-locking nut drill plate 6 is selected according to the type of the supporting plate self-locking nut, the guide column 3 with the corresponding diameter is selected to be placed into the screw hole of the unmanned aerial vehicle airborne equipment mounting frame 7, and a rivet hole formed by the supporting plate self-locking nut and the unmanned aerial vehicle airborne equipment mounting frame 7 is led out.
The pilot hole 71 has been seted up to the upper surface of unmanned aerial vehicle airborne equipment mounting bracket 7, and this scheme structural design is simple, easily masters, and the cost is with low costs, and the facilitate promotion has reduced the operation degree of difficulty, improves work efficiency, saves manufacturing cost for the company.
The working principle is as follows: a double-lug supporting plate self-locking nut drill plate 4, a single-lug supporting plate self-locking nut drill plate 5 or an angular supporting plate self-locking nut drill plate 6 are fixed on a bottom plate 1 through internal and external thread screws 2, screw holes are manufactured on an unmanned aerial vehicle airborne equipment mounting frame 7 needing to be provided with supporting plate self-locking nuts, guide posts 3 on the double-lug supporting plate self-locking nut drill plate 4, the single-lug supporting plate self-locking nut drill plate 5 or the angular supporting plate self-locking nut drill plate 6 are placed into the screw holes on the unmanned aerial vehicle airborne equipment mounting frame 7, rivet holes are led out of the unmanned aerial vehicle airborne equipment mounting frame 7 according to rivet holes on the double-lug supporting plate self-locking nut drill plate 4, the single-lug supporting plate self-locking nut drill plate 5 or the angular supporting plate self-locking nut drill plate 6, supporting plate self-locking nut screw holes are manufactured, The single-lug supporting plate self-locking nut drill plate 5 or the angular supporting plate self-locking nut drill plate 6 is selected, the guide columns 3 with corresponding diameters are selected to be placed into screw holes of an unmanned aerial vehicle airborne equipment mounting frame 7, and rivet holes for connecting the supporting plate self-locking nuts with the unmanned aerial vehicle airborne equipment mounting frame 7 are led out.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented 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.
Claims (6)
1. The utility model provides a be used for environmental monitoring unmanned aerial vehicle layer board self-locking nut rivet hole draw hole device, includes bottom plate (1), internal and external screw thread screw (2), guide post (3), ears layer board self-locking nut bushing plate (4), monaural layer board self-locking nut bushing plate (5), angular form layer board self-locking nut bushing plate (6) and unmanned aerial vehicle airborne equipment mounting bracket (7), its characterized in that: the upper surface of the bottom plate (1) is provided with a first mounting hole (11) and a second mounting hole (12), the upper surface of the bottom plate (1) is located on the periphery of the first mounting hole (11) and is provided with a first hole leading groove (13), a second hole leading groove (14), a third hole leading groove (15), a fourth hole leading groove (16) and a fifth hole leading groove (17), the outer surface of the internal and external thread screw (2) is provided with a first external thread (21), the inner surface of the internal and external thread screw (2) is provided with an internal thread (22), the outer surface of the internal and external thread screw (2) is sleeved with a shaft (23), and the upper surface of the internal and external thread screw (2) is provided with a straight groove (24).
2. The device of claim 1, wherein the device is used for guiding the rivet hole of the self-locking nut of the supporting plate of the environmental monitoring unmanned aerial vehicle, and is characterized in that: the outer surface of the guide post (3) is provided with a second external thread (31), the lower surface of the guide post (3) is welded with a guide pin (32), and the second external thread (31) is meshed with the internal thread (22).
3. The device of claim 1, wherein the device is used for guiding the rivet hole of the self-locking nut of the supporting plate of the environmental monitoring unmanned aerial vehicle, and is characterized in that: first through-hole (41), second through-hole (42) and third through-hole (43) have been seted up to the upper surface of binaural layer board self-locking nut bushing plate (4), and the lower surface welding of binaural layer board self-locking nut bushing plate (4) has first locating pin (44), and first through-hole (41) and axle (23) size equal.
4. The device of claim 1, wherein the device is used for guiding the rivet hole of the self-locking nut of the supporting plate of the environmental monitoring unmanned aerial vehicle, and is characterized in that: first fixed orifices (51) and second fixed orifices (52) have been seted up to the upper surface of monaural layer board self-locking nut bushing board (5), and the lower surface welding of monaural layer board self-locking nut bushing board (5) has second locating pin (53), and second locating pin (53) draw hole groove (14) size equal with bottom plate (1) upper surface.
5. The device of claim 1, wherein the device is used for guiding the rivet hole of the self-locking nut of the supporting plate of the environmental monitoring unmanned aerial vehicle, and is characterized in that: first connecting hole (61), second connecting hole (62) and third connecting hole (63) have been seted up to the upper surface of angular form layer board self-locking nut bushing plate (6), and the lower surface welding of angular form layer board self-locking nut bushing plate (6) has third locating pin (64), and first connecting hole (61) equals with the size of axle (23).
6. The device of claim 1, wherein the device is used for guiding the rivet hole of the self-locking nut of the supporting plate of the environmental monitoring unmanned aerial vehicle, and is characterized in that: the upper surface of unmanned aerial vehicle airborne equipment mounting bracket (7) has been seted up pilot hole (71).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920775897.3U CN209935937U (en) | 2019-05-28 | 2019-05-28 | Be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920775897.3U CN209935937U (en) | 2019-05-28 | 2019-05-28 | Be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device |
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| Publication Number | Publication Date |
|---|---|
| CN209935937U true CN209935937U (en) | 2020-01-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920775897.3U Active CN209935937U (en) | 2019-05-28 | 2019-05-28 | Be used for environmental monitoring unmanned aerial vehicle layer board auto-lock nut rivet hole draw hole device |
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| CN (1) | CN209935937U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110000413A (en) * | 2019-05-28 | 2019-07-12 | 远望时代(天津)航空技术有限公司 | One kind being used for environmental monitoring unmanned plane supporting plate self-lock nut rivet hole pilot hole device |
-
2019
- 2019-05-28 CN CN201920775897.3U patent/CN209935937U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110000413A (en) * | 2019-05-28 | 2019-07-12 | 远望时代(天津)航空技术有限公司 | One kind being used for environmental monitoring unmanned plane supporting plate self-lock nut rivet hole pilot hole device |
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Effective date of registration: 20211206 Address after: 400000 station 406-081, 4th floor, office building, Luyu advanced manufacturing industrial park, Puli new area, Zhaojia street, Kaizhou District, Chongqing Patentee after: Beiyisen Technology (Chongqing) Co.,Ltd. Address before: 300000 4-1,2-101, dongguyuan, No. 22, Erwei Road, development zone, Dongli District, Tianjin Patentee before: Yuanwang Times (Tianjin) Aviation Technology Co.,Ltd. |
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| TR01 | Transfer of patent right |