阅读说明：本技术 无人机系统 (Unmanned aerial vehicle system ) 是由 王成皓 周海峰 黄海鹏 周云 于 2020-06-05 设计创作，主要内容包括：本申请涉及一种无人机系统,包括：所述无人机、所述容置槽、所述定位装置和所述控制装置。本申请实施例所述无人机系统通过将所述定位装置设置于与所述无人机相连的所述容置槽内,所述定位装置与所述无人机相互独立,当所述无人机被破坏而无法正常工作时,所述定位装置还可以继续正常工作。通过所述控制装置获取所述定位装置的输出信号即可确定所述无人机的具体位置。本申请实施例提供的所述无人机系统解决了现有技术中存在的操作人员在无人机坠毁时无法获得无人机具体位置的技术问题,达到了提高操作人员对于所述无人机的可操控性。(The application relates to an unmanned aerial vehicle system, include: the unmanned aerial vehicle, the storage tank, positioner and controlling means. This application embodiment the unmanned aerial vehicle system through with positioner set up in with unmanned aerial vehicle links to each other in the storage tank, positioner with unmanned aerial vehicle mutual independence works as unmanned aerial vehicle is destroyed and during unable normal work, positioner can also continue normal work. The specific position of the unmanned aerial vehicle can be determined by acquiring the output signal of the positioning device through the control device. The embodiment of the application provides unmanned aerial vehicle system has solved the technical problem that the operating personnel who exists can't obtain unmanned aerial vehicle body position when unmanned aerial vehicle crashes among the prior art, has reached and has improved operating personnel right unmanned aerial vehicle's controllability.)

1. An unmanned aerial vehicle system, comprising:

a drone (100);

a storage tank (200) provided in the drone (100);

the positioning device (300) is arranged in the accommodating groove (200);

the control device (400) is in communication connection with the positioning device (300) and is used for determining the position of the unmanned aerial vehicle (100) according to the information output by the positioning device (300);

and the alarm equipment (500) is arranged in the accommodating groove (200) and is electrically connected with the positioning device (300).

2. The drone system of claim 1, wherein the positioning device (300) comprises:

the positioning equipment (310) is arranged in the accommodating groove (200) and is in communication connection with the control device (400);

the mobile power supply (320) is arranged in the accommodating groove (200) and is electrically connected with the positioning equipment (310).

3. The drone system of claim 2, wherein the tank (200) includes:

the positioning accommodating groove (210) is connected with the unmanned aerial vehicle (100), and the positioning equipment (310) is arranged in the positioning accommodating groove (210);

the alarm containing groove (220) is connected with the positioning containing groove (210), and the alarm equipment (500) is arranged in the alarm containing groove (220).

4. The drone system of claim 3, wherein the tank (200) further includes:

and the cover plate (230) is arranged on the positioning containing groove (210) and the alarm containing groove (220) in a covering mode.

5. The drone system of claim 4, wherein the alert device (500) is an audible alert device.

6. The unmanned aerial vehicle system of claim 5, wherein the cover plate (230) defines a sound diffusing hole (231), and the sound diffusing hole (231) is located directly above the alarm receiving slot (220).

7. The unmanned aerial vehicle system of claim 4, wherein the cover plate (230) is perforated with heat dissipation holes (232).

8. The drone system of claim 3, wherein the height of the positioning receptacle (210) is greater than the height of the alert receptacle (220).

9. The drone system of claim 1, wherein the tank (200) includes two opposing first and second side surfaces; the drone system (10) further comprising:

the first fixing piece (600) is arranged on the first side surface and used for connecting the accommodating groove (200) and the unmanned aerial vehicle (100);

the second fixing piece (700) is arranged on the second side surface and used for connecting the accommodating groove (200) and the unmanned aerial vehicle (100).

10. The drone system of claim 9, wherein the tank (200) further includes:

a third side surface perpendicular to both the first side surface and the second side surface;

the drone system (10) further comprising:

the clamping piece (800) is arranged on the third side surface and used for connecting the accommodating groove (200) and the unmanned aerial vehicle (100).

Technical Field

The application relates to the technical field of aircrafts, in particular to an unmanned aerial vehicle system.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle controlled by radio remote control equipment and self-contained program control equipment, and the unmanned aerial vehicle can perform excellent functions of tracking, positioning, remote control, remote measurement, digital transmission and the like on remote control stations such as the ground, ships, mother aircraft and the like through radars and the like, so that the unmanned aerial vehicle is widely applied to aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like. Unmanned aerial vehicles have been used in military applications, and are also gradually and widely used in various civil industries as science and technology progresses. The operating personnel is basically from the wireless communication transmission of long-range radar etc. to unmanned aerial vehicle's state information, but the flying environment of unmanned aerial vehicle operation in-process is more complicated, consequently, the staff can't carry out unmanned aerial vehicle's state monitoring in real time. When unmanned aerial vehicle is in beyond visual range flight, during the condition such as bump, crash, operating personnel just can't obtain unmanned aerial vehicle's specific position.

Disclosure of Invention

Based on this, it is necessary to provide an unmanned aerial vehicle system to the problem that exists among the prior art when unmanned aerial vehicle is in beyond visual range flight, when the circumstances such as bump, crash, the operating personnel just can't obtain unmanned aerial vehicle's specific position.

An unmanned aerial vehicle system comprising:

an unmanned aerial vehicle;

the accommodating groove is formed in the unmanned aerial vehicle;

the positioning device is arranged in the accommodating groove;

the control device is in communication connection with the positioning device and used for determining the position of the unmanned aerial vehicle according to the information output by the positioning device;

and the alarm equipment is arranged in the accommodating groove and is electrically connected with the positioning device.

In one embodiment, the positioning device comprises:

the positioning equipment is arranged in the accommodating groove and is in communication connection with the control device;

and the mobile power supply is arranged in the accommodating groove and is electrically connected with the positioning equipment.

In one embodiment, the receiving groove includes:

the positioning accommodating groove is connected with the unmanned aerial vehicle, and the positioning equipment is arranged in the positioning accommodating groove;

and the alarm accommodating groove is connected with the positioning accommodating groove, and the alarm equipment is arranged in the alarm accommodating groove.

In one embodiment, the accommodating groove further includes:

and the cover plate is covered on the positioning accommodating groove and the alarm accommodating groove.

In one embodiment, the alarm device is an audible alarm device.

In one embodiment, the cover plate is provided with a sound amplifying hole, and the sound amplifying hole is positioned right above the alarm accommodating groove.

In one embodiment, the cover plate is provided with heat dissipation holes.

In one embodiment, the height of the positioning accommodating groove is greater than the height of the alarm accommodating groove.

In one embodiment, the accommodating groove comprises two opposite first side surfaces and second side surfaces; the unmanned aerial vehicle system further comprises:

the first fixing piece is arranged on the first side surface and used for connecting the accommodating groove and the unmanned aerial vehicle;

the second fixing piece is arranged on the second side surface and used for being connected with the accommodating groove and the unmanned aerial vehicle.

In one embodiment, the accommodating groove further includes:

a third side surface perpendicular to both the first side surface and the second side surface;

the unmanned aerial vehicle system further comprises:

the clamping piece is arranged on the third side surface and used for being connected with the accommodating groove and the unmanned aerial vehicle.

The embodiment of the application provides an unmanned aerial vehicle system, include: the unmanned aerial vehicle, the storage tank, positioner and controlling means. This application embodiment the unmanned aerial vehicle system through with positioner set up in with unmanned aerial vehicle links to each other in the storage tank, positioner with unmanned aerial vehicle mutual independence works as unmanned aerial vehicle is destroyed and during unable normal work, positioner can also continue normal work. The specific position of the unmanned aerial vehicle can be determined by acquiring the output signal of the positioning device through the control device. The embodiment of the application provides unmanned aerial vehicle system has solved the technical problem that the operating personnel who exists can't obtain unmanned aerial vehicle body position when unmanned aerial vehicle crashes among the prior art, has reached and has improved operating personnel right unmanned aerial vehicle's controllability.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments or the conventional technologies of the present application, the drawings used in the descriptions of the embodiments or the conventional technologies will be briefly introduced below, it is obvious that the drawings in the following descriptions are only some embodiments of the present application, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle system provided in an embodiment of the present application;

fig. 2 is a schematic structural diagram of a positioning apparatus of an unmanned aerial vehicle system according to an embodiment of the present application;

fig. 3 is a schematic partial structure diagram of an unmanned aerial vehicle system according to an embodiment of the present application;

fig. 4 is a schematic partial structure diagram of an unmanned aerial vehicle system according to an embodiment of the present application;

fig. 5 is a schematic partial structure diagram of an unmanned aerial vehicle system according to an embodiment of the present application;

fig. 6 is a schematic view of a partial structure of an unmanned aerial vehicle system provided in an embodiment of the present application.

Description of reference numerals:

10. an unmanned aerial vehicle system;

100. an unmanned aerial vehicle;

200. a containing groove;

210. positioning the accommodating groove;

220. an alarm accommodating groove;

230. a cover plate;

231. a sound expansion hole;

232. heat dissipation holes;

300. a positioning device;

310. positioning equipment;

320. a mobile power supply;

400. a control device;

500. an alarm device;

600. a first fixing member;

700. a second fixing member;

800. the fastener.

Detailed Description

In order to make the purpose, technical solution and advantages of the present application more clearly understood, the unmanned aerial vehicle system of the present application is further described in detail through the embodiments and with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.

The numbering of the components as such, e.g., "first", "second", etc., is used herein only to distinguish the objects as described, and does not have any sequential or technical meaning. The term "connected" and "coupled" when used in this application, unless otherwise indicated, includes both direct and indirect connections (couplings). In the description of the present application, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present application and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be considered as limiting the present application.

In this application, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may be directly contacting the first and second features or indirectly contacting the first and second features through intervening media. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.

The embodiment of the present application provides an unmanned aerial vehicle system 10, which can be applied to any environment for aerial work, such as tracking, positioning, remote control, telemetry, digital transmission, and the like in the ground, sea, air, and other environments.

Referring to fig. 1, an embodiment of the present application provides an unmanned aerial vehicle system 10, including: the unmanned aerial vehicle 100, storage tank 200, positioner 300, controlling means 400 and alarm device 500.

The unmanned aerial vehicle 100 is used for performing aerial operations, such as functions of monitoring, tracking, remote measuring and the like in the air, the unmanned aerial vehicle 100 can comprise an unmanned aerial vehicle body, wings and the like, and the unmanned aerial vehicle 100 can comprise a positioning system, an image acquisition device, a radar transmitting system, a power supply and the like. Unmanned aerial vehicle 100 can be fixed wing unmanned aerial vehicle, rotor unmanned aerial vehicle, unmanned airship, umbrella wing unmanned aerial vehicle, flapping wing unmanned aerial vehicle etc. this embodiment is right unmanned aerial vehicle 100 does not do any restriction, only need satisfy can realize carrying out the function of ordinary aerial operation.

The accommodating groove 200 is disposed in the unmanned aerial vehicle 100 for providing an accommodating space. The containing groove 200 may be fixed on the drone 100, or may be embedded in the drone 100. The receiving groove 200 may be closed, open, or semi-closed, and the receiving groove 200 may be made of any material, for example: plastic, rubber, metal, wood, etc., and the receiving groove 200 may be square, circular, oval, or any other shape. The embodiment does not limit the receiving groove 200, and only needs to satisfy the function of providing the receiving space.

Positioner 300 set up in the storage tank 200, positioner 300 is used for right unmanned aerial vehicle 100 advances line location, positioner 300 works in real time when unmanned aerial vehicle 100 breaks down, positioner 300 still can continue unmanned aerial vehicle 100's concrete position is tracked and is fixed a position. It should be noted that, in this embodiment, the positioning device 300 and the positioning system of the drone 100 are independent of each other, the positioning device 300 may include a GPS positioning system, an ultrasonic positioning system, a power supply, and the like, and the positioning device 300 may independently perform the daily positioning work on the drone 100. This embodiment is right positioner 300 does not do any restriction, only need can realize with unmanned aerial vehicle mutual independence, and can be right unmanned aerial vehicle 100 carries out the function of fixing a position can.

The control device 400 is in communication connection with the positioning device 300, and is configured to determine a specific position of the drone 100 according to the information output by the positioning device 300. The control device 400 is separated from the drone 100, and the control device 400 may be disposed on a control platform, etc. for controlling the positioning device 300. The control device 400 may be only in communication connection with the positioning device 300 for controlling the positioning device 300. The control device 400 can also simultaneously communicate with the unmanned aerial vehicle 100 and the positioning device 300, the unmanned aerial vehicle 100 and the positioning device 300 are mutually independent, the control device 400 can simultaneously control the unmanned aerial vehicle 100 and the positioning device 300, so as to improve the high integration and the cost reduction of the unmanned aerial vehicle system 10. The communication connection may be a wireless connection, such as a bluetooth connection, a remote control connection, a 5G network connection, or the like, or a wired connection, such as a USB data connection, or the like. The control device 400 may be a server, a processor, a PLC chip, a mobile phone, etc., and the control device 400 is not limited in this embodiment, and only needs to satisfy the function of controlling the positioning device 300.

The alarm device 500 is disposed in the accommodating groove 200, electrically connected to the positioning device 300, and configured to send an alarm signal to remind an operator of the location of the unmanned aerial vehicle 100. The warning device 500 may operate continuously for a long time, sending a warning signal all the time to alert an operator of the location of the drone 100. The alarm device 500 may also be in communication with the control device 400, and the control device 400 controls the alarm device 500 to operate for a certain period, for example, 15 minutes, 30 minutes, one hour, etc. The alarm device 500 may be an audible alarm, a light alarm, or a combination audible and visual alarm. This embodiment does not make any restriction to alarm device 500, only need to satisfy can send alarm signal to remind operating personnel the function of unmanned aerial vehicle 100 position can.

The embodiment of the application provides the operating principle of unmanned aerial vehicle system 10 is as follows:

in the unmanned aerial vehicle system 10 of the present application the unmanned aerial vehicle 100 can not continue to work normally if a fault occurs, such as collision or crash, so as to lose contact with the console on the ground. The positioning device 300 and the alarm device 500 are disposed in the accommodating groove 200, and are independent of each other of the unmanned aerial vehicle 100. The positioning device 300 is in communication connection with the control device 400, the output information of the positioning device 300 is transmitted to the control device 400 in real time, and the control device 400 can determine the specific position of the drone 100 according to the output information of the positioning device 300. Meanwhile, the alarm device 500 sends out an alarm signal, and simultaneously reminds an operator or related personnel of the specific position of the unmanned aerial vehicle 100. Therefore, even when the drone 100 fails and cannot work normally, the operator can determine the specific position of the drone 100 through the positioning device 300 and the alarm device 500.

The present embodiment provides an unmanned aerial vehicle system 10, including: the unmanned aerial vehicle 100, the accommodating groove 200, the positioning device 300 and the control device 400. This embodiment the unmanned aerial vehicle system 10 through with positioner 300 set up in with unmanned aerial vehicle 100 links to each other in the storage tank 200, positioner 300 with unmanned aerial vehicle 100 is mutually independent, works as unmanned aerial vehicle 100 is destroyed and when unable normal work, positioner 300 can also continue normal work. The specific position of the drone 100 can be determined by the control device 400 obtaining the output signal of the positioning device 300. The unmanned aerial vehicle system 10 that this embodiment provided has solved the technical problem that the operating personnel who exists can't obtain unmanned aerial vehicle body position when unmanned aerial vehicle crashes among the prior art, has reached and has improved operating personnel to unmanned aerial vehicle 100's controllability.

Referring to fig. 2, in one embodiment, the positioning apparatus 300 includes: a pointing device 310 and a mobile power source 320.

The positioning device 310 is disposed in the accommodating groove 200, and is in communication connection with the control apparatus 400, so as to determine the position of the drone 100. The positioning device 310 may be a bluetooth positioner that has low power consumption and high positioning accuracy. The positioning device 310 may also be a wireless locator, and the wireless locator is based on the existing WLAN network, and the WLAN network is widely deployed, mature in product, free of additional devices, and low in cost. The positioning device 310 may also employ an RSSI locator, which may provide greater accuracy. The positioning device 310 is not limited in this embodiment, and only needs to satisfy the function of determining the position of the drone 100.

The mobile power source 320 is disposed in the containing groove 200, electrically connected to the positioning device 310, and configured to supply power to the positioning device 310. In this embodiment, the mobile power source 320 is independent from the drone 100, that is, the mobile power source 320 is only used for providing power to the positioning device 310, but not for providing power to the drone 100. Portable power source 320 set up in the storage tank 200, storage tank 200 is right portable power source 320 plays to place the effect that holds, can be fixed in the storage tank 200, also can inlay and locate in the storage tank 200, portable power source 320 does positioning device 310 provides the power, and simultaneously with unmanned aerial vehicle 100 is mutually independent, thereby guarantees positioning device 310 can be the normal work of long-time continuation. The mobile power source 320 may be a polymer lithium battery, a rechargeable nickel-chromium battery or a nickel-hydrogen battery, etc., and the embodiment is not limited, and only needs to satisfy the requirement that the positioning device 300 can be independent and can supply power.

Referring to fig. 3, in an embodiment, the accommodating groove 200 includes: a positioning receiving groove 210 and an alarm receiving groove 220.

In this embodiment, the accommodating groove 200 is divided into two portions, namely, the positioning accommodating groove 210 and the alarm accommodating groove 220, so as to form two relatively independent accommodating spaces for storing the positioning device 310 and the alarm device 500, respectively.

The positioning accommodating groove 210 is connected to the unmanned aerial vehicle 100, and the positioning device 310 is disposed in the positioning accommodating groove 210. The positioning receiving groove 210 may be square, trapezoidal, circular, or any other shape, and the positioning receiving groove 210 may also be specifically selected or designed according to the shape of the positioning device 310, and this embodiment is not limited, and only needs to implement the function of independently receiving the positioning device 310.

The alarm receiving groove 220 is connected to the positioning receiving groove 210, and the alarm device 500 is disposed in the alarm receiving groove 220. The height of the alarm receiving groove 220 may be smaller than the height of the positioning receiving groove 210, so as to better match the structural features of the positioning device 310 and the alarm device 500, thereby saving space. The alarm receiving groove 220 may be square, trapezoidal, circular or any other shape, and the alarm receiving groove 220 may also be specifically selected or designed according to the shape of the alarm device 500, and this embodiment is not limited, and only needs to be able to realize the function of independently receiving the alarm receiving groove 220.

Referring to fig. 4, in an embodiment, the accommodating groove 200 further includes: a cover plate 230.

The cover plate 230 covers the positioning receiving groove 210 and the alarm receiving groove 220, and the cover plate 230 is used for sealing the positioning receiving groove 210 and the alarm receiving groove 220 to form the receiving groove 200 in a fully-enclosed structure. The accommodating groove 200 of the totally enclosed structure can protect the positioning device 310 and the alarm device 500 from being stably placed in the accommodating groove 200, and the situation that an accident occurs due to the flying-out in an accident situation is avoided. The cover plate 230 covers the positioning receiving groove 210 and the alarm receiving groove 220, and the cover plate may be fixedly connected or may be connected in any manner such as scarf joint, threaded connection, or snap connection. The cover plate 230 may be matched with the positioning receiving groove 210 and the alarm receiving groove 220 to fit the positioning receiving groove 210 and the alarm receiving groove 220. The area of the cover plate 230 may also be slightly larger or smaller than the total area of the positioning receiving groove 210 and the alarm receiving groove 220, and only the positioning receiving groove 210 and the alarm receiving groove 220 are required to form the receiving groove 200 in a fully enclosed structure. The cover plate 230 may be made of any material, such as hard material: plastic, metal, alloy, wood, etc., or soft materials: rubber, and the like. In this embodiment, the cover plate 230 is not specifically limited, and only needs to be capable of covering the positioning receiving groove 210 and the alarm receiving groove 220 to seal the positioning receiving groove 210 and the alarm receiving groove 220.

In one embodiment, the cover plate 230 defines a sound diffusing hole 231 and a heat dissipating hole 232.

The cover plate 230 is provided with a sound diffusing hole 231, and the sound diffusing hole 231 is located right above the alarm accommodating groove 220. When the alarm device 500 is an acoustic alarm device, such as a buzzer, etc., sound waves emitted from the acoustic alarm device may be transmitted along the sound expansion hole 231 to improve the alarm performance of the acoustic alarm device. The sound diffusing holes 231 may be a plurality of holes, and are uniformly formed at positions of the cover plate 230 close to the alarm receiving groove 220. The sound diffusing hole 231 of the present embodiment is not limited in any way, and only needs to satisfy the function of providing a sound wave transmission space for the acoustic alarm apparatus 500.

The heat dissipation holes 232 may be spaced apart from each other on the cover plate 230, and the heat dissipation holes 232 are distributed right above the positioning receiving groove 210 and the alarm receiving groove 220 for heat dissipation. The positioning device 310 and the alarm device 500 generate heat during working, long-time heat accumulation inevitably affects the working performance of the positioning device 310 and the alarm device 500, and the heat dissipation holes 232 can effectively improve the mobility of the positioning containing groove 210 and the alarm containing groove 220 with the outside air, so that the heat dissipation performance of the positioning device 310 and the alarm device 500 is improved. The heat dissipation holes 232 may be circular, square or any other shape, and the heat dissipation holes 232 are not limited in this embodiment, and only the function of heat dissipation needs to be satisfied.

Referring to fig. 5 and 6 together, in one embodiment, the drone system 10 further includes: a first fixing member 600, a second fixing member 700, and a clip member 800.

The receiving groove 200 includes two opposite first and second side surfaces, and further includes a third side surface perpendicular to both the first and second side surfaces. The first fixing member 600 is disposed on the first side surface, and is configured to connect the accommodating groove 200 and the drone 100. The second fixing member 700 is disposed on the second side surface, and is configured to connect the accommodating groove 200 and the drone 100. The first fixing member 600 and the second fixing member 700 may be any one or any combination of bolts, sheath nails, etc., and the first fixing member 600 and the second fixing member 700 may be made of any rigid material, for example: plastics, alloys, polymeric materials, and the like. The second mounting 700 with first mounting 600 can be the same, also can be different, and this embodiment is right first mounting 600 with second mounting 700 does not do any restriction, only need satisfy can realize with storage tank 200 is fixed in function on the unmanned aerial vehicle 100 can.

The clip 800 is disposed on the third side surface, and is configured to connect the accommodating groove 200 and the drone 100. The fastener 800 can be a common concave fastener, and also can be a spring fastener, the fastener 800 can be made of metal materials, and also can be made of plastics or other high polymer materials, and this embodiment is right the fastener 800 does not have any limitation, and only needs to satisfy and can realize that the storage tank 200 is clamped and arranged in the function of the unmanned aerial vehicle 100.

The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.

The above-mentioned embodiments only express several embodiments of the present application, and the description thereof is more specific and detailed, but not construed as limiting the claims. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.