CN218967172U

CN218967172U - Unmanned aerial vehicle horn installation mechanism

Info

Publication number: CN218967172U
Application number: CN202223145434.XU
Authority: CN
Inventors: 黄赛
Original assignee: Guangdong Runjin Industrial Co ltd
Current assignee: Guangdong Runjin Industrial Co ltd
Priority date: 2022-11-26
Filing date: 2022-11-26
Publication date: 2023-05-05
Anticipated expiration: 2032-11-26

Abstract

The utility model discloses an unmanned aerial vehicle horn mounting mechanism which comprises an unmanned aerial vehicle, four horns and eight connecting blocks. Through setting up unmanned aerial vehicle, the horn, the connecting block, the standing groove, positioning mechanism and drive mechanism's cooperation is used, drive positioning mechanism through drive mechanism and remove to suitable position after, dock horn and unmanned aerial vehicle, the in-process that dock needs to make horn and two connecting blocks laminating, after the laminating is accomplished, loosen drive mechanism, positioning mechanism can be quick fix the horn through the connecting block at the in-process that resets, the quick installation to the horn has been accomplished, current unmanned aerial vehicle fuselage and horn are connected fixedly through a plurality of thread components, it all needs to expend certain time at every turn to assemble and demolish horn and fuselage at the in-process of equipment and demolish, therefore the comparatively loaded down with trivial details problem of inconvenient user quick installation to the horn of installation horn mode.

Description

Unmanned aerial vehicle horn installation mechanism

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle horn installation, and particularly relates to an unmanned aerial vehicle horn installation mechanism.

Background

Unmanned aerial vehicle is low altitude flight device, can reach different purposes through the equipment with multiple different equipment, need fly through the installation horn all around of fuselage at the in-process of using, accomodate the aircraft for convenient, dismantle the horn and fuselage after using, thereby reduce unmanned aerial vehicle's volume and reach the purpose of being convenient for accomodate, and can prevent that unmanned aerial vehicle horn flabellum from breaking the condition of damage from appearing, but unmanned aerial vehicle fuselage and horn are connected fixedly through a plurality of thread components, every turn all need expend certain time with horn and fuselage equipment and demolish at the in-process of equipment and demolish, consequently the comparatively loaded down with trivial details and inconvenient user of installation horn mode installs the horn fast, the problem that prior art exists is: unmanned aerial vehicle fuselage and horn are connected fixedly through a plurality of thread components, all need expend certain time at the in-process of equipment and demolishment at every turn and assemble horn and fuselage and demolish, therefore install the horn mode comparatively loaded down with trivial details inconvenient user quick to the horn installation.

Disclosure of Invention

Aiming at the problems in the prior art, the utility model provides the unmanned aerial vehicle horn mounting mechanism which has the advantage of rapid mounting of the horn, and solves the problems that the prior unmanned aerial vehicle body and the horn are connected and fixed through a plurality of thread assemblies, and a certain time is consumed for assembling and disassembling the horn and the body each time in the assembling and disassembling process, so that the horn mounting mode is complicated and inconvenient for a user to rapidly mount the horn.

The utility model discloses an unmanned aerial vehicle horn mounting mechanism, which comprises an unmanned aerial vehicle, four horns and eight connecting blocks, wherein the eight connecting blocks are respectively positioned around the unmanned aerial vehicle, one side of each connecting block, which is opposite to the other side of each connecting block, is contacted with the surface of the corresponding horn, a placing groove is formed in the inner cavity of each horn, a positioning mechanism matched with the unmanned aerial vehicle is arranged in the inner cavity of each placing groove, and a transmission mechanism matched with the positioning mechanism is arranged in the inner cavity of each placing groove.

As the utility model is preferable, the positioning mechanism comprises two positioning rods, the opposite sides of the two positioning rods are fixedly connected with first tension springs, one side of each first tension spring, which is close to the inner wall of the placing groove, is fixedly connected with the inner wall of the placing groove, and the front side of each positioning rod is fixedly connected with a stress rod.

As the preferable mode of the utility model, the transmission mechanism comprises the movable rod, the rear sides of the left side and the right side of the bottom of the movable rod are contacted with the surface of the stressed rod, the top of the movable rod is fixedly connected with the transmission rod, the front side of the movable rod is fixedly connected with the second tension spring, the front side of the second tension spring is fixedly connected with the inner wall of the placing groove, and the movable rod plays a role of quickly driving the positioning rod to move through the stressed rod by arranging the transmission mechanism, so that the condition that the horn cannot be separated from a fixed state when the horn needs to be dismantled is avoided.

As the utility model is preferable, the inner cavity of the stress rod is movably connected with the limiting plates, one opposite sides of the two limiting plates are fixedly connected with the inner wall of the placing groove, and the limiting plates play a role in limiting the stress rod and the positioning rod by arranging the limiting plates, so that the dislocation of the stress rod and the positioning rod in the moving process is avoided.

As the utility model is preferable, the left side and the right side of the top of the movable rod are fixedly connected with the movable column, the surface of the movable column is sleeved with the supporting block, the front side of the supporting block is fixedly connected with the inner wall of the placing groove, and the movable column and the supporting block are arranged to enable the movable rod to keep a certain movable track for movement, so that the movable rod is prevented from falling in the moving process.

As the preferable mode of the utility model, the left side and the right side of the inner cavity of the horn are respectively provided with a connecting hole, one side opposite to the two connecting blocks is respectively provided with a positioning groove, one side opposite to the two positioning rods respectively penetrates through the connecting holes and extends to the inner cavity of the positioning groove, and the connecting holes play a role in enabling the positioning rods to be quickly abutted with the positioning grooves through the arrangement of the connecting holes and the positioning grooves.

As the preferable mode of the utility model, the top of the horn is provided with the movable hole, the top of the transmission rod passes through the movable hole and extends to the top of the horn, and the movable hole avoids the situation that the transmission rod contacts with the inner wall of the horn to generate friction when moving through the movable hole.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the utility model, through the matched use of the unmanned aerial vehicle, the horn, the connecting block, the placing groove, the positioning mechanism and the transmission mechanism, the problems that the prior unmanned aerial vehicle body and the horn are connected and fixed through a plurality of thread assemblies, a certain time is consumed for assembling and disassembling the horn and the body in the assembling and disassembling processes each time, and therefore, the horn mounting mode is complicated and the rapid mounting of the horn is inconvenient for a user are solved.

2. According to the utility model, the unmanned aerial vehicle, the horn, the connecting blocks, the placing grooves, the positioning mechanism and the transmission mechanism are arranged, the transmission mechanism drives the positioning mechanism to move to a proper position, then the horn is abutted with the unmanned aerial vehicle, the horn is required to be attached to the two connecting blocks in the abutting process, after the attaching is completed, the transmission mechanism is released, the positioning mechanism can be fast fixed to the horn through the connecting blocks in the resetting process, and the fast installation of the horn is completed.

Drawings

FIG. 1 is a schematic diagram of a structure provided by an embodiment of the present utility model;

FIG. 2 is a cross-sectional view of an embodiment of the present utility model providing a perspective;

fig. 3 is a schematic diagram showing connection of the internal structure of the placement tank according to the embodiment of the utility model.

In the figure: 1. unmanned plane; 2. a horn; 3. a connecting block; 4. a placement groove; 5. a positioning mechanism; 6. a transmission mechanism; 501. a positioning rod; 502. a first tension spring; 503. a force-bearing rod; 601. a movable rod; 602. a transmission rod; 603. a second tension spring; 7. a limiting plate; 8. a moving column; 9. a support block; 10. a connection hole; 11. a positioning groove; 12. a movable hole.

Detailed Description

For a further understanding of the utility model, its features and advantages, reference is now made to the following examples, which are illustrated in the accompanying drawings.

The structure of the present utility model will be described in detail with reference to the accompanying drawings.

As shown in fig. 1 to 3, the unmanned aerial vehicle horn installation mechanism provided by the embodiment of the utility model comprises an unmanned aerial vehicle 1, four horns 2 and eight connecting blocks 3, wherein the eight connecting blocks 3 are respectively positioned around the unmanned aerial vehicle 1, one opposite sides of the two connecting blocks 3 are in contact with the surfaces of the horns 2, a placing groove 4 is formed in an inner cavity of the horns 2, a positioning mechanism 5 matched with the unmanned aerial vehicle 1 is arranged in the inner cavity of the placing groove 4, and a transmission mechanism 6 matched with the positioning mechanism 5 is arranged in the inner cavity of the placing groove 4.

Referring to fig. 3, the positioning mechanism 5 includes two positioning rods 501, wherein opposite sides of the two positioning rods 501 are fixedly connected with a first tension spring 502, one side of the first tension spring 502, which is close to the inner wall of the placement groove 4, is fixedly connected with the inner wall of the placement groove 4, and the front side of the positioning rod 501 is fixedly connected with a stress rod 503.

The scheme is adopted: through setting up positioning mechanism 5, locating lever 501 has played the effect that can be quick fixes horn 2 through connecting block 3, has avoided the condition that horn 2 can't be fixed fast after the butt joint of connecting block 3.

Referring to fig. 3, the transmission mechanism 6 includes a movable rod 601, wherein the rear sides of the left and right sides of the bottom of the movable rod 601 are in contact with the surface of the stressed rod 503, the top of the movable rod 601 is fixedly connected with a transmission rod 602, the front side of the movable rod 601 is fixedly connected with a second tension spring 603, and the front side of the second tension spring 603 is fixedly connected with the inner wall of the placement groove 4.

The scheme is adopted: through setting up drive mechanism 6, movable rod 601 has played the effect that can be quick through atress pole 503 drive locating lever 501 and remove, has avoided when need demolish horn 2 unable messenger's horn 2 break away from the condition of fixed state.

Referring to fig. 3, the inner cavity of the stress rod 503 is movably connected with a limiting plate 7, and opposite sides of the two limiting plates 7 are fixedly connected with the inner wall of the placement groove 4.

The scheme is adopted: through setting up limiting plate 7, limiting plate 7 has played the effect that can carry out spacingly to atress pole 503 and locating lever 501, has avoided atress pole 503 and locating lever 501 to appear the condition of dislocation at the in-process that removes.

Referring to fig. 3, the left and right sides of the top of the movable rod 601 are fixedly connected with a movable column 8, the surface of the movable column 8 is sleeved with a supporting block 9, and the front side of the supporting block 9 is fixedly connected with the inner wall of the placement groove 4.

The scheme is adopted: through setting up movable column 8 and supporting shoe 9, supporting shoe 9 has played the effect that can make movable rod 601 keep certain activity orbit to remove through movable column 8, has avoided movable rod 601 to appear dropping the condition at the in-process that removes.

Referring to fig. 2, connecting holes 10 are formed on both left and right sides of an inner cavity of the arm 2, positioning grooves 11 are formed on opposite sides of the two connecting blocks 3, and opposite sides of the two positioning rods 501 penetrate through the connecting holes 10 and extend to the inner cavity of the positioning grooves 11.

The scheme is adopted: by providing the connection hole 10 and the positioning groove 11, the connection hole 10 plays a role in enabling the positioning rod 501 to be quickly docked with the positioning groove 11.

Referring to fig. 1 and 2, a movable hole 12 is formed at the top of the horn 2, and the top of the transmission rod 602 passes through the movable hole 12 and extends to the top of the horn 2.

The scheme is adopted: by providing the movable hole 12, the movable hole 12 avoids the situation that the transmission rod 602 contacts with the inner wall of the horn 2 when moving, thereby generating friction.

The working principle of the utility model is as follows:

when using, pulling transfer line 602, transfer line 602 can drive movable rod 601 and remove and carry out tensile to second extension spring 603, movable rod 601 can with the surface contact of atress pole 503 and carry out the atress to atress pole 503 at the in-process that removes, atress pole 503 can drive locating lever 501 after the atress moves, locating lever 501 can carry out tensile to first extension spring 502 at the in-process that removes, after locating lever 501 moves to suitable position, dock horn 2 and unmanned aerial vehicle 1, need make horn 2 and laminating of two connecting blocks 3 at the in-process of docking, after the laminating is accomplished, loosen transfer line 602, the pulling force of second extension spring 603 contracts and can drive movable rod 601 fast and reset, movable rod 601 can make atress pole 503 break away from the state of atress at the in-process that resets, after atress pole 503 breaks away from the state, the pulling force of first extension spring 502 contracts and can be quick drive locating lever 501 and inserts the inner chamber of constant head tank 11 and fix horn 2 through connecting block 3, the quick installation to horn 2 has been accomplished.

To sum up: this unmanned aerial vehicle horn installation mechanism uses through setting up unmanned aerial vehicle 1, horn 2, connecting block 3, standing groove 4, positioning mechanism 5 and drive mechanism 6's cooperation, has solved current unmanned aerial vehicle fuselage and horn and has connected fixedly through a plurality of thread components, all need expend certain time at the in-process of equipment and demolishd at every turn and assemble horn and fuselage and demolish, therefore the comparatively loaded down with trivial details problem of inconvenient user quick installation to the horn of installation horn mode.

It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Unmanned aerial vehicle horn installation mechanism, including unmanned aerial vehicle (1), four horn (2) and eight connecting blocks (3), its characterized in that: eight connecting blocks (3) are located around unmanned aerial vehicle (1) respectively, and two opposite one sides of connecting block (3) all with the surface contact of horn (2), standing groove (4) have been seted up to the inner chamber of horn (2), the inner chamber of standing groove (4) is provided with positioning mechanism (5) that use with unmanned aerial vehicle (1) cooperation, the inner chamber of standing groove (4) is provided with drive mechanism (6) that use with positioning mechanism (5) cooperation.

2. The unmanned aerial vehicle horn mounting mechanism of claim 1, wherein: the positioning mechanism (5) comprises two positioning rods (501), wherein one sides of the two positioning rods (501) opposite to each other are fixedly connected with a first tension spring (502), one side, close to the inner wall of the placing groove (4), of the first tension spring (502) is fixedly connected with the inner wall of the placing groove (4), and the front side of each positioning rod (501) is fixedly connected with a stress rod (503).

3. The unmanned aerial vehicle horn mounting mechanism of claim 2, wherein: the transmission mechanism (6) comprises a movable rod (601), the rear sides of the left side and the right side of the bottom of the movable rod (601) are in contact with the surface of a stressed rod (503), the top of the movable rod (601) is fixedly connected with a transmission rod (602), the front side of the movable rod (601) is fixedly connected with a second tension spring (603), and the front side of the second tension spring (603) is fixedly connected with the inner wall of a placing groove (4).

4. A drone arm mounting mechanism according to claim 3, wherein: the inner cavity of the stress rod (503) is movably connected with limiting plates (7), and one opposite sides of the two limiting plates (7) are fixedly connected with the inner wall of the placing groove (4).

5. A drone arm mounting mechanism according to claim 3, wherein: the movable rod is characterized in that the left side and the right side of the top of the movable rod (601) are fixedly connected with movable columns (8), supporting blocks (9) are sleeved on the surfaces of the movable columns (8), and the front sides of the supporting blocks (9) are fixedly connected with the inner walls of the placing grooves (4).

6. The unmanned aerial vehicle horn mounting mechanism of claim 2, wherein: connecting holes (10) are formed in the left side and the right side of the inner cavity of the horn (2), positioning grooves (11) are formed in the opposite sides of the two connecting blocks (3), and the opposite sides of the two positioning rods (501) penetrate through the connecting holes (10) and extend to the inner cavity of the positioning grooves (11).

7. A drone arm mounting mechanism according to claim 3, wherein: the top of horn (2) has seted up movable hole (12), the top of transfer line (602) passes movable hole (12) and extends to the top of horn (2).