CN218401002U - Unmanned aerial vehicle mounting connector - Google Patents
Unmanned aerial vehicle mounting connector Download PDFInfo
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- CN218401002U CN218401002U CN202222329809.1U CN202222329809U CN218401002U CN 218401002 U CN218401002 U CN 218401002U CN 202222329809 U CN202222329809 U CN 202222329809U CN 218401002 U CN218401002 U CN 218401002U
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- aerial vehicle
- unmanned aerial
- connecting piece
- locking
- block
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Abstract
The utility model discloses an unmanned aerial vehicle mounting connector, which is used for connecting an unmanned aerial vehicle and expanding functional parts, and comprises a connecting piece and a main body, wherein the connecting piece is provided with a mounting hole, the unmanned aerial vehicle is detachably connected with the connecting piece, and the unmanned aerial vehicle covers one end of the mounting hole; a convex block is arranged on the inner side wall of the mounting hole, and a locking groove is formed in the convex block; the main part is provided with a locking block, and the locking block is locked in the locking groove. The main part stretches into in the mounting hole along the lug and rotates, and the bulge card that is the lock block of type after having rotated certain angle is held in locking groove department, makes the lock block lock smoothly at the locking inslot, and the simple structure of unmanned aerial vehicle carry connector, the installation is all more simple and convenient with the dismantlement, the last daily maintenance and the change of expanding functional unit of being convenient for on the unmanned aerial vehicle. The connecting piece can be dismantled with unmanned aerial vehicle and be connected with and do benefit to the connecting piece of changing the damage to when unmanned aerial vehicle need not the carry and extends the functional unit, lift the connecting piece off and can reduce the windage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle carries connector.
Background
The existing unmanned aerial vehicle is widely applied to the fields of military affairs, scientific research, civil use and the like. In order to extend the service function of unmanned aerial vehicle, often mount various types of extension functional unit on unmanned aerial vehicle for unmanned aerial vehicle can carry out various complicacies, dangerous task, but the fixed degree of difficulty that extends the functional unit on unmanned aerial vehicle is usually great, and the coupling mechanism structure of conventional setting is numerous and diverse, complex operation, the installation is more difficult with dismantling the extension functional unit, is unfavorable for unmanned aerial vehicle's daily maintenance and the functional unit of change different grade type.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem that will solve is: the utility model provides a loading and unloading make things convenient for unmanned aerial vehicle to carry connector.
In order to solve the technical problem, the utility model discloses a technical scheme be: an unmanned aerial vehicle mounting connector is used for connecting an unmanned aerial vehicle and expanding functional parts and comprises a connecting piece and a main body, wherein the connecting piece is provided with a mounting hole, and the unmanned aerial vehicle is detachably connected with the connecting piece; a convex block is arranged on the inner side wall of the mounting hole, and a locking groove is formed in the convex block; the main part is provided with a locking block, and the locking block is locked in the locking groove.
Further, the connecting piece with unmanned aerial vehicle passes through bolted connection.
Furthermore, the outer side wall of the connecting piece is provided with a convex lug, and the lug is provided with a bolt hole.
Further, the number of the lugs is multiple, and the lugs are uniformly distributed around the circumference of the connecting piece.
Furthermore, the number of the convex blocks is two, and the two convex blocks are arranged at intervals.
Further, the locking groove is arranged close to the center of the lug.
Furthermore, the cross section of the locking block is convex.
Furthermore, a chamfer is arranged at the end part of the bump.
Further, still including hindering the ring, hinder the ring cover and locate in the main part, hinder the ring and be used for contradicting the connecting piece is kept away from unmanned aerial vehicle's one side.
The beneficial effects of the utility model reside in that: the main part stretches into in the mounting hole along the lug and rotates, and the bulge card that is the locking piece of type after having rotated certain angle is held in locking groove department, makes the locking piece locking smoothly at the locking inslot, and the simple structure of unmanned aerial vehicle carry connector, the installation is all more simple and convenient with the dismantlement, the last expansion functional component's of unmanned aerial vehicle of being convenient for daily maintenance and change. The connecting piece can be dismantled with unmanned aerial vehicle and be connected with the connecting piece that does benefit to the change damage, when unmanned aerial vehicle need not the carry and extends the functional unit, lift the connecting piece off and can reduce the windage.
Drawings
Fig. 1 is a schematic structural view of an unmanned aerial vehicle mounting connector according to a first embodiment of the present invention;
FIG. 2 is an enlarged detail view of portion A of FIG. 1;
fig. 3 is the utility model discloses a cross-sectional view of connecting piece in unmanned aerial vehicle carries connector.
Description of reference numerals:
1. a connecting member; 11. mounting holes; 12. a bump; 121. a locking groove; 13. a lug; 131. bolt holes;
2. a main body; 21. a locking block; 22. and (4) blocking the ring.
Detailed Description
In order to explain the technical content, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
Referring to fig. 1 to 3, the mounting connector for the unmanned aerial vehicle is used for connecting the unmanned aerial vehicle and expanding functional components, and comprises a connecting piece 1 and a main body 2, wherein the connecting piece 1 is provided with a mounting hole 11, and the unmanned aerial vehicle is detachably connected with the connecting piece 1; a convex block 12 is arranged on the inner side wall of the mounting hole 11, and a locking groove 121 is arranged on the convex block 12; the main body 2 is provided with a locking block 21, and the locking block 21 is locked in the locking groove 121.
The structure/working principle of the utility model is as follows: installing the connecting piece 1 on the unmanned aerial vehicle, and arranging the main body 2 on an extended functional component to be mounted; locking piece 21 on main part 2 stretches into in the mounting hole 11 and rotates along the lower surface of lug 12, rotates main part 2 until locking piece 21 just to locking groove 121, makes locking piece 21 locking form stable connection in locking groove 121.
From the above description, the beneficial effects of the present invention are: main part 2 stretches into and rotates along lug 12 in the mounting hole 11, makes locking piece 21 lock smoothly in locking groove 121, and the unmanned aerial vehicle carries the connector simple structure, and the installation is all more simple and convenient with the dismantlement, the last daily maintenance and the change of the extension functional unit of being convenient for of unmanned aerial vehicle. Connecting piece 1 can be dismantled with unmanned aerial vehicle and be connected and be favorable to changing connecting piece 1 of damage, when unmanned aerial vehicle need not the carry and extends the functional unit, lift connecting piece 1 off and can reduce the windage.
Further, connecting piece 1 with unmanned aerial vehicle passes through bolted connection.
As can be seen from the above description, the connection mode of the connecting piece 1 and the unmanned aerial vehicle is simple, convenient and stable.
Further, a convex lug 13 is arranged on the outer side wall of the connecting piece 1, and a bolt hole 131 is arranged on the lug 13.
As can be seen from the above description, the provision of the bolt holes 131 on the projecting lugs 13 ensures the structural strength of the body 2 of the connector 1.
Further, the number of the lugs 13 is multiple, and the lugs 13 are evenly distributed around the circumference of the connecting piece 1.
As can be seen from the above description, the plurality of lugs 13 can make the connection of the connector 1 to the body 2 more stable, while balancing the forces applied to the connector 1.
Further, the number of the bumps 12 is two, and the two bumps 12 are arranged at intervals.
As can be seen from the above description, the locking block 21 enters from the gap between the two protrusions 12, and then the two locking blocks 21 are locked in the two locking grooves 121 respectively, so that the connection stability can be improved and the two sides of the main body 2 are balanced in stress.
Further, the locking groove 121 is disposed near the center of the projection 12.
As apparent from the above description, the locking groove 121 provided near the center of the projection 12 effectively prevents the locking piece 21 from falling off the projection 12, improving the reliability of the locked state.
Further, the cross section of the locking block 21 is convex.
As can be seen from the above description, the locking between the locking piece 21 and the locking groove 121 in the shape of a letter of Chinese character 'tu' is effective.
Furthermore, a chamfer is arranged at the end of the bump 12.
As can be seen from the above description, the locking block 21 enters from the lead angle at the end of the projection 12, reducing the resistance encountered when the main body 2 rotates.
Further, still include and hinder ring 22, hinder ring 22 the cover locate on main part 2, hinder ring 22 and be used for contradicting the connecting piece 1 keeps away from the one side of unmanned aerial vehicle.
Known from the above description, hinder ring 22 and can make main part 2 produce the removal trend of keeping away from mounting hole 11, increase the inseparable degree between locking piece 21 and the locking groove 121, ensure unmanned aerial vehicle and carry the stability of connector.
Example one
Referring to fig. 1 to fig. 3, a first embodiment of the present invention is: an unmanned aerial vehicle mounting connector is used for connecting an unmanned aerial vehicle and expanding functional parts (such as mechanical clamping jaws or lamps) and comprises a connecting piece 1 and a main body 2, wherein the connecting piece 1 is provided with a mounting hole 11, the unmanned aerial vehicle is detachably connected with the connecting piece 1, and the unmanned aerial vehicle covers one end of the mounting hole 11; a convex block 12 is arranged on the inner side wall of the mounting hole 11, and a locking groove 121 is formed in the convex block 12; the main body 2 is provided with a locking block 21, and the locking block 21 is locked in the locking groove 121. Specifically, the connecting piece 1 is annular as a whole, and the convex block 12 is arc-shaped; the main body 2 is formed into a cylindrical shape corresponding to the connecting member 1, and the side surface of the main body 2 protrudes outward to form the locking block 21. During the use, install connecting piece 1 on unmanned aerial vehicle, locate expansion functional unit with main part 2 on to make connecting piece 1 be connected with the cooperation of main part 2.
Preferably, the connecting piece 1 is connected with the unmanned aerial vehicle through a bolt. Be equipped with convex lug 13 on the lateral wall of connecting piece 1, be equipped with bolt hole 131 on the lug 13, correspond on the unmanned aerial vehicle bolt hole 131 is equipped with the screw hole. The number of the lugs 13 is multiple, and the lugs 13 are evenly distributed around the circumference of the connecting piece 1. In this embodiment, the number of the lugs 13 is two, and the two lugs 13 are symmetrically arranged. In other embodiments, the number of lugs 13 may be set to one, three, or more.
Preferably, as shown in fig. 2, the number of the protrusions 12 is two, two of the protrusions 12 are arranged at intervals, and the protrusions 12, the locking grooves 121 and the locking blocks 21 are arranged in a one-to-one correspondence manner. When the main body 2 is connected with the connecting piece 1 in a matching way, the locking block 21 on the main body 2 enters from the gap between the two convex blocks 12, and then the main body 2 is rotated, so that the locking block 21 rotates along the lower surface of the convex block 12 until the locking block 21 is opposite to the locking groove 121.
Preferably, the locking groove 121 is located near the center of the projection 12 to reduce the risk of the locking block 21 falling off the projection 12.
Preferably, as shown in fig. 2, the cross section of the locking block 21 is convex, and the convex part of the locking block 21 enters the locking groove 121 to form locking.
Preferably, as shown in fig. 2 and 3, a chamfer is provided on an end of the bump 12. Unmanned aerial vehicle carries connector still includes hinders ring 22, it locates to hinder the ring 22 cover in main part 2, it is used for contradicting to hinder ring 22 connecting piece 1 is kept away from unmanned aerial vehicle's one side. Specifically, between the end of the projection 12 and the locking groove 121, the thickness of the projection 12 gradually decreases from a position near the locking groove 121 toward the end. Locking piece 21 inserts behind the breach between two lugs 12 and carries out directional rotation along the lead angle direction, and at this in-process, main part 2 constantly deepens mounting hole 11 deeply for locking piece 21 and resistance ring 22 take place elastic deformation, thereby make the resistance that locking piece 21 received increase gradually along with rotating, be favorable to increasing the pretightning force between locking piece 21 and the locking groove 121, reduce the risk that locking piece 21 withdraws from locking groove 121.
To sum up, the utility model provides an unmanned aerial vehicle carries connector, the main part stretches into in the mounting hole along the lug and rotates, and the bulge card that is the lock block of type after having turned over certain angle is held in locking groove department, makes the lock block lock smoothly at the locking inslot, simple structure, and the installation is all more simple and convenient with the dismantlement, the last daily overhaul and the change of extending functional unit of unmanned aerial vehicle of being convenient for. The connecting piece can be dismantled with unmanned aerial vehicle and be connected with and do benefit to the connecting piece of changing the damage to when unmanned aerial vehicle need not the carry and extends the functional unit, lift the connecting piece off and can reduce the windage. The bolt holes are arranged on the convex lugs, so that the structural strength of the main body of the connecting piece can be ensured. The locking groove arranged close to the center of the convex block effectively prevents the locking block from falling off from the convex block, and the reliability of the locking state is improved. The locking effect between the convex locking block and the locking groove is good. Hinder the ring and can make the main part produce the removal trend of keeping away from the mounting hole, increase the inseparable degree between locking piece and the locking groove, ensure unmanned aerial vehicle carry the stability of connector.
The above mentioned is only the embodiment of the present invention, and the patent scope of the present invention is not limited thereby, and all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (9)
1. The utility model provides an unmanned aerial vehicle carries connector for connect unmanned aerial vehicle and extend functional unit, its characterized in that: the unmanned aerial vehicle comprises a connecting piece and a main body, wherein the connecting piece is provided with a mounting hole, and the unmanned aerial vehicle is detachably connected with the connecting piece; a convex block is arranged on the inner side wall of the mounting hole, and a locking groove is formed in the convex block; the main part is provided with a locking block, and the locking block is locked in the locking groove.
2. The unmanned aerial vehicle mounting connector of claim 1, wherein: the connecting piece with unmanned aerial vehicle passes through bolted connection.
3. An unmanned aerial vehicle mounting connector according to claim 2, characterized in that: the outer side wall of the connecting piece is provided with a convex lug, and the lug is provided with a bolt hole.
4. An unmanned aerial vehicle mounting connector according to claim 3, characterized in that: the number of the lugs is multiple, and the lugs are uniformly distributed around the circumference of the connecting piece.
5. The unmanned aerial vehicle mounting connector of claim 1, wherein: the number of the convex blocks is two, and the two convex blocks are arranged at intervals.
6. The unmanned aerial vehicle mounting connector of claim 1, wherein: the locking groove is arranged close to the center of the lug.
7. An unmanned aerial vehicle mounting connector according to claim 1, wherein: the cross-section of the locking block is convex.
8. The unmanned aerial vehicle mounting connector of claim 1, wherein: and a guide angle is arranged at the end part of the lug.
9. The unmanned aerial vehicle mounting connector of claim 8, wherein: still including hindering the ring, hinder the ring cover and locate in the main part, hinder the ring and be used for contradicting the connecting piece is kept away from unmanned aerial vehicle's one side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222329809.1U CN218401002U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle mounting connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222329809.1U CN218401002U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle mounting connector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218401002U true CN218401002U (en) | 2023-01-31 |
Family
ID=85030916
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222329809.1U Active CN218401002U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle mounting connector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218401002U (en) |
-
2022
- 2022-09-01 CN CN202222329809.1U patent/CN218401002U/en active Active
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