CN219056606U - Unmanned aerial vehicle task load - Google Patents

Abstract

The utility model relates to the technical field of unmanned aerial vehicles and discloses an unmanned aerial vehicle task load, which comprises an installation component, a loudspeaker and a searchlight; the mounting assembly comprises a mounting seat and a controller, wherein the mounting seat is used for being mounted on the unmanned aerial vehicle, the controller is fixed on the mounting seat, and the controller is provided with a first interface which is used for being electrically connected with the unmanned aerial vehicle; the loudspeaker is fixed on the mounting assembly and is electrically connected with the controller; the searchlight is fixed on the mounting assembly and is electrically connected with the controller; the utility model integrates two common load horns and searchlight into a whole load, enriches the tasks that can be executed by the unmanned aerial vehicle, reduces the repeated load dismounting operation and is convenient to use.

Description

Unmanned aerial vehicle task load

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a task load of an unmanned aerial vehicle.

Background

The unmanned plane is a flying device in rapid development, has the advantages of flexible maneuvering, rapid response, unmanned flying and low operation requirement, and can be widely applied to the fields of agriculture, exploration, photography, border patrol and the like; unmanned aerial vehicle mission loads are an important component of unmanned aerial vehicle systems, which unmanned aerial vehicles perform missions by loading a variety of different loads.

The current unmanned aerial vehicle's task load is more designs to single load, when carrying out different tasks, need to pull down current load, installs new load again, uses inconveniently.

Disclosure of Invention

The utility model aims to provide a task load of an unmanned aerial vehicle, which integrates two commonly used load horns and searchlight into a whole load, enriches tasks which can be executed by the unmanned aerial vehicle, reduces repeated load dismounting operation and is convenient to use.

In order to achieve the above object, the present utility model provides an unmanned aerial vehicle mission load, comprising a mounting assembly, a horn and a searchlight; the mounting assembly comprises a mounting seat and a controller, wherein the mounting seat is used for being mounted on the unmanned aerial vehicle, the controller is fixed on the mounting seat, and the controller is provided with a first interface which is used for being electrically connected with the unmanned aerial vehicle; the loudspeaker is fixed on the mounting assembly and is electrically connected with the controller; the searchlight is fixed on the installation component and is electrically connected with the controller.

The first interface is a power supply communication interface, and when the power supply communication interface is plugged into the unmanned aerial vehicle, the unmanned aerial vehicle can supply power and communicate with the controller through the power supply communication interface.

In some embodiments, the horn is secured to a side of the controller facing away from the mount.

In some embodiments, the mount comprises a base, and a connecting arm connected to the base; the controller is fixed on the base, and the searchlight is fixed on the connecting arm.

Further, the outer wall of the base is connected with a connecting part, and the connecting part is provided with a first connecting hole.

Further, the base is provided with a second connecting hole.

In some embodiments, the controller is provided with a second interface.

Further, the controller is further provided with an interface cover, the interface cover is connected to the controller, and the interface cover can cover or expose the second interface.

In some embodiments, the horn is a horn.

In some embodiments, the unmanned aerial vehicle mission load further comprises a driving motor electrically connected with the controller, the searchlight is fixed on the mounting base through the driving motor, and the driving motor is used for driving the searchlight to rotate around the rotation axis.

Compared with the prior art, the unmanned aerial vehicle task load has the beneficial effects that: through with loudspeaker with the searchlight is installed to on the installation component, can be with two kinds of load loudspeaker and the searchlight that are used often integrate into an overall load, richen unmanned aerial vehicle can carry out the task, reduced the operation of repeated dismouting load, convenient to use, just unmanned aerial vehicle can be given through first interface controller power supply and communication to control loudspeaker with the searchlight for unmanned aerial vehicle need not through two lines with loudspeaker with the searchlight is connected respectively, has simplified unmanned aerial vehicle with wiring operation between the unmanned aerial vehicle task load.

Drawings

Fig. 1 is a structural diagram of a task load of an unmanned aerial vehicle according to an embodiment of the present utility model;

fig. 2 is an exploded view of a unmanned aerial vehicle task load provided by an embodiment of the present utility model;

fig. 3 is a side view of a unmanned aerial vehicle mission load provided by an embodiment of the present utility model;

fig. 4 is a side view of an unmanned aerial vehicle task load provided by an embodiment of the present utility model after the interface cover is removed;

fig. 5 is a block diagram of a mounting base according to an embodiment of the present utility model.

In the figure, 1, a mounting seat; 11. a base; 12. a connecting arm; 101. a connection part; 102. a first connection hole; 103. a second connection hole;

2. a controller; 21. a first interface; 22. a second interface; 23. an interface cover;

3. a horn; 31. a driving unit; 32. a horn;

4. a searchlight; 41. a searchlight body; 42. a light emitting lamp bead;

5. and driving the motor.

Detailed Description

The following describes in further detail the embodiments of the present utility model with reference to the drawings and examples. The following examples are illustrative of the utility model and are not intended to limit the scope of the utility model.

In the description of the present utility model, it should be understood that the terms "upper," "lower," "vertical," "horizontal," "top," "bottom," and the like indicate an orientation or a positional relationship based on that shown in the drawings, and are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements to be referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present utility model.

The terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature.

In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.

In the present utility model, unless expressly stated or limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, as well as the first and second features not being in direct contact but being in contact with each other through additional features therebetween. Moreover, a first feature being "above," "over" and "on" a second feature includes the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is higher in level than the second feature. The first feature being "under", "below" and "beneath" the second feature includes the first feature being directly under and obliquely below the second feature, or simply means that the first feature is less level than the second feature.

As shown in fig. 1, a preferred unmanned aerial vehicle task load according to an embodiment of the present utility model includes a mounting assembly, a horn 3, and a searchlight 4; the mounting assembly comprises a mounting seat 1 and a controller 2, wherein the mounting seat 1 is used for being mounted on the unmanned aerial vehicle, the controller 2 is fixed on the mounting seat 1, the controller 2 is provided with a first interface 21, and the first interface 21 is used for being electrically connected with the unmanned aerial vehicle; the loudspeaker 3 is fixed on the mounting assembly and is electrically connected with the controller 2; the searchlight 4 is fixed on the mounting assembly and is electrically connected with the controller 2.

Based on this technical scheme, through installing loudspeaker 3 and searchlight 4 to the installation component, can become a whole load with two kinds of load loudspeaker 3 and searchlight 4 that are used often, richen unmanned aerial vehicle can carry out the task, reduced the operation of repeated dismouting load, and unmanned aerial vehicle can be through first interface 21 for controller 2 power supply and communication to control loudspeaker 3 and searchlight 4, convenient to use.

In this embodiment, the first interface 21 is a power supply communication interface, and when the power supply communication interface is plugged into the unmanned aerial vehicle, the unmanned aerial vehicle can supply power and communicate with the controller through the power supply communication interface.

In this embodiment, the horn 3 is fixed to a surface of the controller 2 facing away from the mount 1, and the searchlight 4 is fixed to the mount 1.

The unmanned aerial vehicle task load further comprises a driving motor 5 electrically connected with the controller 2, the searchlight 4 is fixed on the mounting seat 1 through the driving motor 5, and the driving motor 5 is used for driving the searchlight 4 to rotate around the rotation axis; the irradiation range of the searchlight 4 can be enlarged by adopting the driving motor 5 so as to meet the requirement of users on more irradiation.

In this embodiment, the driving motor 5 is a pan-tilt motor.

Referring to fig. 1, 2 and 5, the mounting base 1 includes a base 11 and a connecting arm 12 connected to the base 11; the controller 2 is fixed on the base 11, and the searchlight 4 is fixed on the connecting arm 12.

The outer wall of the base 11 is connected with a connecting part 101, the connecting part 101 is provided with a first connecting hole 102, and the base 11 is connected with the unmanned aerial vehicle through the first connecting hole 102 through bolts.

In this embodiment, four connecting portions 101 are provided, two connecting portions 101 are a first group of connecting portions, and the other two connecting portions 101 are a second group of connecting portions, wherein the first group of connecting portions are disposed on one side of the base 11, and the second group of connecting portions are disposed on the other side of the base 11 and are symmetrical to the first group of connecting portions.

The second connecting hole 103 has been seted up to the base 11, and the base 11 passes through second connecting hole 103 and unmanned aerial vehicle bolted connection.

In the present embodiment, four second connection holes 103 are provided, and four second connection holes 103 are provided at four corners of the base 11, respectively.

Referring to fig. 2, 3 and 4, the controller 2 is provided with a second interface 22.

In the present embodiment, the second interface 22 is a USB interface, which is used to introduce audio into the controller 2.

The drone mission load further includes an interface cover 23, the interface cover 23 being connected to the controller 2, and the interface cover 23 being capable of covering the second interface 22 or exposing the second interface 22. The second port 22 can be protected and waterproof by the port cover 23.

It will be appreciated that the interface cover 23 may be connected to the controller 2 by any manner such as a snap connection, a sliding connection, a detachable connection, or a hinge connection, so as to cover the second interface 22 or expose the second interface 22, and the case cover and the case body that implement the function by any manner of connection should be considered as the protection scope of the present utility model without departing from the technical principles of the present utility model.

The horn 3 is a horn including a driving unit 31, and a horn 32 connected to the driving unit 31. The horn has high efficiency, and only a small driving unit and horn part are needed to achieve 120dB sound pressure, so that the horn has light overall weight.

The searchlight 4 comprises a searchlight body 41 connected with the driving motor 5 and light-emitting lamp beads 42 arranged on the searchlight body 41, wherein two light-emitting lamp beads 42 are arranged, the light-emitting lamp beads 42 are high-efficiency light-emitting lamp beads, and the central illuminance of the emitted light of the light-emitting lamp beads 42 at the position 50 meters in front can reach 25lux.

The searchlight of this embodiment adopts no reflector design, lightens weight, reduces luminance loss, and uses high efficiency luminescent light pearl, just can reach required luminance using two luminescent light pearls, required light in weight.

In summary, the unmanned aerial vehicle task load provided by the embodiment of the utility model has the following beneficial effects:

1. adopt installation component, loudspeaker 3 and searchlight 4, can become a whole load with two kinds of load loudspeaker 3 and searchlight 4 that are used often, richened unmanned aerial vehicle can carry out the task, reduced the operation of repeated dismouting load, convenient to use.

2. The controller 2 electrically connected with the horn 3 and the searchlight 4 is adopted and the first interface 21 is arranged, so that the wiring operation between the unmanned aerial vehicle and the whole load can be simplified.

3. The use of the second interface 22 enables a user to direct audio into the controller 2 to meet different shouting needs of the user.

4. The second port 22 can be protected and waterproof by the port cover 23.

5. Adopt the horn loudspeaker can make whole unmanned aerial vehicle mission load have lighter weight, avoid increasing too much load for unmanned aerial vehicle.

6. The adoption of the high-power luminous lamp beads can enable the searchlight 4 to have lighter weight, so that the task load of the whole unmanned aerial vehicle has lighter weight, and too much load is prevented from being added to the unmanned aerial vehicle.

7. The irradiation range of the searchlight 4 can be enlarged by adopting the driving motor 5 so as to meet more irradiation requirements of users.

The foregoing is merely a preferred embodiment of the present utility model, and it should be noted that modifications and substitutions can be made by those skilled in the art without departing from the technical principles of the present utility model, and these modifications and substitutions should also be considered as being within the scope of the present utility model.

Claims (9)

1. An unmanned aerial vehicle mission load, comprising:

the installation assembly comprises an installation seat and a controller, wherein the installation seat is used for being installed on the unmanned aerial vehicle, the controller is fixed on the installation seat, and the controller is provided with a first interface which is used for being electrically connected with the unmanned aerial vehicle;

the loudspeaker is fixed on the mounting assembly and is electrically connected with the controller;

and the searchlight is fixed on the mounting assembly and is electrically connected with the controller.

2. The unmanned aerial vehicle mission load of claim 1, wherein the horn is secured to a face of the controller facing away from the mount.

3. The unmanned aerial vehicle mission load of claim 1, wherein the mount comprises a base, and a connecting arm connected to the base; the controller is fixed on the base, and the searchlight is fixed on the connecting arm.

4. A unmanned aerial vehicle mission load as claimed in claim 3, wherein the outer wall of the base is connected with a connecting portion, the connecting portion being provided with a first connecting hole.

5. A unmanned aerial vehicle mission load as claimed in claim 3, wherein the base is provided with a second attachment aperture.

6. The unmanned aerial vehicle mission load of claim 1, wherein the controller is configured with a second interface.

7. The unmanned aerial vehicle mission load of claim 6, further comprising an interface cover coupled to the controller, the interface cover capable of covering or exposing the second interface.

8. The unmanned aerial vehicle mission load of claim 1, wherein the horn is a horn.

9. The unmanned aerial vehicle mission load of any of claims 1-8, further comprising a drive motor electrically connected to the controller, the searchlight being secured to the mount via the drive motor, the drive motor being configured to drive the searchlight to rotate about an axis of rotation.

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