CN212195923U - Quick-release structure for mounting of unmanned aerial vehicle - Google Patents
Quick-release structure for mounting of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212195923U CN212195923U CN202020773023.7U CN202020773023U CN212195923U CN 212195923 U CN212195923 U CN 212195923U CN 202020773023 U CN202020773023 U CN 202020773023U CN 212195923 U CN212195923 U CN 212195923U
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- unmanned aerial
- aerial vehicle
- shaft body
- regulation pole
- accommodating part
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- 210000001503 joint Anatomy 0.000 claims description 2
- 230000004308 accommodation Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a quick-release structure for unmanned aerial vehicle mounting, which belongs to the technical field of unmanned aerial vehicles, and comprises a second accommodating part, wherein one side of the second accommodating part is provided with a strip hole, and the other side of the second accommodating part is provided with a mounting hole, two auxiliary mounting plates are arranged on both sides of the top end of the second accommodating part, a plurality of auxiliary mounting holes are arranged on the two auxiliary mounting plates, the two auxiliary mounting plates are connected with the second accommodating part through an adjusting structure, one side below the second accommodating part is provided with a connecting rod, and the other side below the second accommodating part is provided with a first accommodating part; the utility model discloses the top both sides of second holding portion are equipped with auxiliary mounting panel, are equipped with auxiliary mounting hole on two auxiliary mounting panels, and compared prior art, can increase the connection area between rapid disassembly structure and the unmanned aerial vehicle to can strengthen the joint strength between rapid disassembly structure and the unmanned aerial vehicle, improve rapid disassembly structure's connection stability.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to quick detach structure of unmanned aerial vehicle carry.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing radio remote control equipment and a self-contained program control device, and the quick-release structure is used for accommodating the mounting device on the unmanned aerial vehicle.
Chinese patent application number is 201920473292.9 discloses quick detach structure and unmanned aerial vehicle, the second holding portion articulates on first holding portion and forms the accommodation space at lock position and first holding portion, make the second holding portion can open and shut for first holding portion, conveniently treat getting of carry and put, and the accommodation space that forms can be along with the opening of second holding portion and crescent, the application scope of quick detach structure has been increased, in addition, the lock piece can be with the second holding portion locking that is in the lock position, in order to prevent that second holding portion and first holding portion from separating, lead to treating that the carry deviates from the accommodation space.
The above patent has the following problems: above-mentioned rapid disassembly structure only fixes holding portion top on unmanned aerial vehicle through construction bolt, and area of connection is less for joint strength between rapid disassembly structure and the unmanned aerial vehicle is relatively weak, reduces rapid disassembly structure's connection stability.
SUMMERY OF THE UTILITY MODEL
To solve the problems set forth in the background art described above. The utility model provides an unmanned aerial vehicle carries rapid disassembly structure has the joint strength between strong rapid disassembly structure and the unmanned aerial vehicle, improves the characteristics of rapid disassembly structural connection stability.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a quick detach structure of unmanned aerial vehicle carry, includes the second holding portion, rectangular hole has been seted up to one side on the second holding portion, and the mounting hole has been seted up to the opposite side on the second holding portion, the top both sides of second holding portion all are provided with supplementary mounting panel, two a plurality of supplementary mounting hole has been seted up on the supplementary mounting panel, two supplementary mounting panel is connected through adjusting the structure with the second holding portion, below one side of second holding portion is provided with the connecting rod, and the below opposite side of second holding portion is provided with first holding portion, the one end that the second holding portion was kept away from to the connecting rod is provided with the handle, second holding portion and connecting rod, connecting rod and handle and second holding portion rotate through the pivot structure with first holding portion and are connected.
Preferably, the adjusting structure comprises a connecting hole, a connecting bolt, a first adjusting rod and a second adjusting rod, one end of the first adjusting rod is fixed on the second accommodating portion, the second adjusting rod is connected inside the first adjusting rod in a sliding mode, one end, far away from the first adjusting rod, of the second adjusting rod is fixed on the auxiliary mounting plate, a plurality of connecting holes are formed in the first adjusting rod and the second adjusting rod, and the connecting hole is connected with the second adjusting rod through the connecting bolt.
Preferably, the rotating shaft structure comprises a first shaft body, a second shaft body and a boss, wherein the second shaft body is connected to one end of the first shaft body, and the bosses are fixed to one end of the first shaft body, which is far away from the second shaft body, and one end of the second shaft body, which is far away from the first shaft body.
Preferably, ring channel and square groove have been seted up respectively to the inside of first axis body, the outside of square groove is provided with the ring channel, the internal connection of square groove has square piece, the internal connection of ring channel has annular block, square piece keeps away from the one end of square groove and the one end that the ring channel was kept away from to annular block all is connected on the second axis body.
Preferably, the side walls of the annular groove and the square groove are provided with internal threads, and the side walls of the square block and the annular block are provided with external threads.
Preferably, when the square groove is embedded in the square block for connection and the annular block is embedded in the annular groove for connection, the first shaft body and the second shaft body are in seamless butt joint.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses the top both sides of second holding portion are equipped with auxiliary mounting panel, are equipped with auxiliary mounting hole on two auxiliary mounting panels, and compared prior art, can increase the connection area between rapid disassembly structure and the unmanned aerial vehicle to can strengthen the joint strength between rapid disassembly structure and the unmanned aerial vehicle, improve rapid disassembly structure's connection stability.
2. The utility model discloses the top of auxiliary mounting panel and second holding portion is through adjusting the structural connection, and the mounting area that the regulation structure can provide according to unmanned aerial vehicle carries out corresponding regulation to the position of auxiliary mounting panel to make quick detach structure can be applicable to the unmanned aerial vehicle use of equidimension not.
3. The utility model discloses pivot structure divide into first axis body and second axis body, and first axis body and second axis body realize fixedly through square piece and square groove and the threaded connection of annular ring piece and ring channel, and this kind of structure need not also can go on with the help of the screwdriver of external specialty when the dismouting, easy dismouting makes things convenient for later stage maintenance simultaneously.
Drawings
Fig. 1 is a front view of the present invention;
fig. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic cross-sectional view of the structure of FIG. 2 according to the present invention;
FIG. 4 is a schematic structural view of a section of the rotating shaft structure of the present invention;
FIG. 5 is a schematic diagram of the present invention in a separated state shown in FIG. 4;
in the figure: 1. an auxiliary mounting plate; 2. a rotating shaft structure; 21. a first shaft body; 22. a second shaft body; 23. a boss; 24. an annular groove; 25. an internal thread; 26. a square groove; 27. an external thread; 28. a square block; 29. a ring block; 3. a first receptacle portion; 4. a handle; 5. a connecting rod; 6. a second receptacle portion; 7. a strip hole; 8. mounting holes; 9. an adjustment structure; 91. connecting holes; 92. a connecting bolt; 93. a first adjusting lever; 94. a second adjusting lever; 10. and (5) auxiliary mounting 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.
Referring to fig. 1-5, the present invention provides the following technical solutions: the utility model provides a quick detach structure of unmanned aerial vehicle carry, including second holding portion 6, rectangular hole 7 has been seted up to one side on the second holding portion 6, and mounting hole 8 has been seted up to the opposite side on the second holding portion 6, the top both sides of second holding portion 6 all are provided with supplementary mounting panel 1, a plurality of supplementary mounting hole 10 has been seted up on two supplementary mounting panels 1, two supplementary mounting panel 1 are connected through adjusting structure 9 with second holding portion 6, below one side of second holding portion 6 is provided with connecting rod 5, and the below opposite side of second holding portion 6 is provided with first holding portion 3, the one end that second holding portion 6 was kept away from to connecting rod 5 is provided with handle 4, second holding portion 6 and connecting rod 5, connecting rod 5 and handle 4 and second holding portion 6 rotate through pivot structure 2 with first holding portion 3 and are connected.
Specifically, the adjusting structure 9 includes a connecting hole 91, a connecting bolt 92, a first adjusting rod 93 and a second adjusting rod 94, one end of the first adjusting rod 93 is fixed on the second accommodating portion 6, the inside of the first adjusting rod 93 is slidably connected with the second adjusting rod 94, one end of the second adjusting rod 94 far away from the first adjusting rod 93 is fixed on the auxiliary mounting plate 1, the first adjusting rod 93 and the second adjusting rod 94 are both provided with a plurality of connecting holes 91, the connecting hole 91 on the first adjusting rod 93 is connected with the connecting hole 91 on the second adjusting rod 94 through the connecting bolt 92,
through adopting above-mentioned technical scheme, can carry out corresponding regulation to the position of auxiliary mounting panel 1 according to the installation area that unmanned aerial vehicle provided to make rapid disassembly structure can be applicable to the unmanned aerial vehicle use of equidimension not.
Specifically, the rotating shaft structure 2 includes a first shaft body 21, a second shaft body 22 and a boss 23, one end of the first shaft body 21 is connected with the second shaft body 22, the boss 23 is fixed on both the end of the first shaft body 21 far away from the second shaft body 22 and the end of the second shaft body 22 far away from the first shaft body 21,
by adopting the technical scheme, the normal rotation of the rotating shaft structure 2 is not influenced, and meanwhile, the rotating shaft structure 2 has the segmented detachable function.
Specifically, the first shaft 21 is provided with an annular groove 24 and a square groove 26 inside, the annular groove 24 is provided outside the square groove 26, the square groove 26 is connected with a square block 28 inside, the annular groove 24 is connected with an annular block 29 inside, one end of the square block 28 away from the square groove 26 and one end of the annular block 29 away from the annular groove 24 are both connected to the second shaft 22,
by adopting the technical scheme, the connection strength of the first shaft body 21 and the second shaft body 22 is improved.
Specifically, the side walls of the annular groove 24 and the square groove 26 are provided with internal threads 25, the side walls of the square block 28 and the annular block 29 are provided with external threads 27,
through adopting above-mentioned technical scheme for first axis body 21 and second axis body 22 need not also to go on with the help of the screwdriver of external specialty when the dismouting, easy dismouting makes things convenient for later stage maintenance simultaneously.
Specifically, when the square groove 26 is embedded in the square block 28 for connection and the annular block 29 is embedded in the annular groove 24 for connection, no gap is abutted between the first shaft body 21 and the second shaft body 22,
through adopting above-mentioned technical scheme, avoid the gap to cause the influence to bearing structure 2's result of use.
The utility model discloses other structures and the principle of well rapid disassembly structure have been disclosed in the rapid disassembly structure and the unmanned aerial vehicle that china patent application number is 201920473292.9 discloses.
The utility model discloses a theory of operation and use flow: the position of two auxiliary mounting panels 1 is adjusted according to the installation area that unmanned aerial vehicle can provide, and the adjustment step is as follows: the second adjusting rod 94 slides inside the first adjusting rod 93, until the second adjusting rod 94 slides to a proper position, the connecting bolt 92 is used for connecting the first adjusting rod 93 with the connecting hole 91 in the second adjusting rod 94, the adjustment work is completed, the top end of the second accommodating part 6 is fixed on the unmanned aerial vehicle through the mounting bolt, then the two auxiliary mounting plates 1 are fixed on the unmanned aerial vehicle through the mounting bolt, the installation work is completed, compared with the prior art, the connecting area between the quick-release structure and the unmanned aerial vehicle can be increased, so that the connecting strength between the quick-release structure and the unmanned aerial vehicle can be enhanced, and the connecting stability of the quick-release structure is improved; when needing to maintain or overhaul the revolution mechanic 2, the counter-rotation second shaft body 22, square piece 28 and annular piece 29 break away from square groove 26 and ring channel 24 gradually under the effect of external screw 27 and internal screw 25, when breaking away from completely, the stall, again respectively from connection structure's both ends take off first shaft body 21 and second shaft body 22, need not also to go on with the help of the screwdriver of external specialty, easy dismouting makes things convenient for later maintenance simultaneously.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle mounted's rapid disassembly structure, includes second holding portion (6), its characterized in that: one side of the second containing part (6) is provided with a long hole (7), the other side of the second containing part (6) is provided with a mounting hole (8), the two sides of the top end of the second containing part (6) are respectively provided with an auxiliary mounting plate (1), a plurality of auxiliary mounting holes (10) are arranged on the two auxiliary mounting plates (1), the two auxiliary mounting plates (1) are connected with the second containing part (6) through an adjusting structure (9), a connecting rod (5) is arranged at one side below the second accommodating part (6), and the other side below the second containing part (6) is provided with a first containing part (3), a handle (4) is arranged at one end of the connecting rod (5) far away from the second accommodating part (6), the second accommodating part (6) is rotatably connected with the connecting rod (5), the connecting rod (5) is rotatably connected with the handle (4), and the second accommodating part (6) is rotatably connected with the first accommodating part (3) through the rotating shaft structure (2).
2. The rapid disassembly structure of unmanned aerial vehicle mount of claim 1, characterized in that: adjust structure (9) including connecting hole (91), connecting bolt (92), first regulation pole (93) and second regulation pole (94), the one end of first regulation pole (93) is fixed on second holding portion (6), the inside sliding connection of first regulation pole (93) has second regulation pole (94), the one end that first regulation pole (93) were kept away from in second regulation pole (94) is fixed on supplementary mounting panel (1), all seted up a plurality of connecting hole (91) on first regulation pole (93) and the second regulation pole (94), first regulation pole (93) are gone up connecting hole (91) and second regulation pole (94) are gone up connecting hole (91) are connected through connecting bolt (92).
3. The rapid disassembly structure of unmanned aerial vehicle mount of claim 1, characterized in that: the rotating shaft structure (2) comprises a first shaft body (21), a second shaft body (22) and a boss (23), wherein the second shaft body (22) is connected to one end of the first shaft body (21), and the boss (23) is fixed to one end, away from the second shaft body (22), of the first shaft body (21) and one end, away from the first shaft body (21), of the second shaft body (22).
4. The rapid disassembly structure of unmanned aerial vehicle mount of claim 3, characterized in that: annular groove (24) and square groove (26) have been seted up respectively to the inside of first axis body (21), the outside of square groove (26) is provided with annular groove (24), the internal connection of square groove (26) has square piece (28), the internal connection of annular groove (24) has annular piece (29), the one end that square groove (26) were kept away from in square piece (28) and the one end that annular piece (29) were kept away from annular groove (24) are all connected on second axis body (22).
5. The rapid disassembly structure that unmanned aerial vehicle mounted of claim 4, its characterized in that: the side walls of the annular groove (24) and the square groove (26) are provided with internal threads (25), and the side walls of the square block (28) and the annular block (29) are provided with external threads (27).
6. The rapid disassembly structure of unmanned aerial vehicle mount of claim 3, characterized in that: when the square groove (26) is embedded in the square block (28) for connection and the annular block (29) is embedded in the annular groove (24) for connection, the first shaft body (21) and the second shaft body (22) are in seamless butt joint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020773023.7U CN212195923U (en) | 2020-05-11 | 2020-05-11 | Quick-release structure for mounting of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020773023.7U CN212195923U (en) | 2020-05-11 | 2020-05-11 | Quick-release structure for mounting of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212195923U true CN212195923U (en) | 2020-12-22 |
Family
ID=73814180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020773023.7U Expired - Fee Related CN212195923U (en) | 2020-05-11 | 2020-05-11 | Quick-release structure for mounting of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212195923U (en) |
-
2020
- 2020-05-11 CN CN202020773023.7U patent/CN212195923U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201222 |
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| CF01 | Termination of patent right due to non-payment of annual fee |