CN211107997U - Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit - Google Patents
Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit Download PDFInfo
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- CN211107997U CN211107997U CN201922046341.3U CN201922046341U CN211107997U CN 211107997 U CN211107997 U CN 211107997U CN 201922046341 U CN201922046341 U CN 201922046341U CN 211107997 U CN211107997 U CN 211107997U
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- 238000004891 communication Methods 0.000 claims abstract description 12
- 239000000696 magnetic material Substances 0.000 claims abstract description 4
- 239000000725 suspension Substances 0.000 claims description 18
- 238000013016 damping Methods 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 4
- 238000007906 compression Methods 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- 239000003344 environmental pollutant Substances 0.000 description 1
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Abstract
The camera is arranged right below the unmanned aerial vehicle; the bottom of the unmanned aerial vehicle is provided with an undercarriage, and the tail end of the undercarriage is provided with a guide block; the guide block is made of conductive magnetic materials; a guide seat is arranged on the upper side of the surface of the unmanned vehicle; the position of the guide seat corresponds to that of the undercarriage, the guide seat is provided with an inner cavity with an opening at the top, and the bottom of the inner cavity of the guide seat is provided with an electromagnet; when the unmanned aerial vehicle is parked on the unmanned vehicle, the storage battery charges an electric board on the unmanned aerial vehicle; the unmanned aerial vehicle is provided with a first central controller and a first wireless communication module, and a driving motor of the unmanned aerial vehicle is connected with the first central controller; the unmanned vehicle is provided with a second central controller and a second wireless communication module, and a driving device of the unmanned vehicle is connected with the second central controller; unmanned aerial vehicle and unmanned vehicle keep real-time communication, and unmanned aerial vehicle flies to unmanned vehicle through GPS navigation. The invention can solve the problem of mobile charging of the multi-rotor unmanned aerial vehicle.
Description
Technical Field
The utility model relates to a many rotor unmanned aerial vehicle remove power supply unit.
Background
Along with the development of many rotor unmanned aerial vehicle technique, many rotor unmanned aerial vehicle have used in each field, for example rescue, electric power are patrolled and examined, the oil gas pipeline is patrolled and examined, security protection is patrolled and examined etc. because oil moves unmanned aerial vehicle bulky, the noise is big, the control degree of difficulty is big and discharge gaseous pollutants, so the overwhelming majority rotor unmanned aerial vehicle is electronic at present. But because battery capacity is limited, and electric unmanned aerial vehicle power consumption is great, electric unmanned aerial vehicle's duration is general very poor, hardly realizes carrying out long time task.
Disclosure of Invention
The utility model discloses overcome the poor problem of current unmanned aerial vehicle duration, provide an automatic many rotor unmanned aerial vehicle mobile power supply unit of navigation.
The utility model discloses a arrange many loads in relevant region and at the unmanned car that has the large capacity battery, be provided with corresponding charge interface on the unmanned car and charge for unmanned aerial vehicle to this duration that increases unmanned aerial vehicle.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
automatic unmanned aerial vehicle of navigation removes power supply unit, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle 1 and an unmanned aerial vehicle 2;
the unmanned aerial vehicle 1 is provided with a camera 101, an undercarriage 102 and a guide block 103, and the camera 101 is arranged right below the unmanned aerial vehicle; the bottom of the unmanned aerial vehicle 1 is provided with a plurality of undercarriage 102, and the tail end of the undercarriage 102 is provided with a guide block 103; the guide block 103 is made of conductive magnetic material.
The unmanned vehicle 2 comprises a vehicle surface 201, a guide seat 202 and two sets of driving devices 21, wherein the driving devices 21 are respectively arranged at the front end and the rear end of the vehicle surface 201 to form a four-wheel drive system; a guide seat 202 is arranged on the upper side of the vehicle surface 201; the position of the guide seat 202 corresponds to the position of the landing gear 102 when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, the guide seat 202 is provided with an inner cavity with an opening at the top, the bottom of the inner cavity of the guide seat 202 is provided with an electromagnet 203, the inner cavity and the guide block 103 are conical bodies with large top and small bottom, the guide block 103 is accommodated in the inner cavity when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, and the electromagnet 203 is contacted with the guide block 103;
the unmanned vehicle 2 is provided with a storage battery which is electrically connected with the electromagnet 203; an electric board on the unmanned aerial vehicle 1 is electrically connected with the guide block 103; when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, the storage battery charges an electric board on the unmanned aerial vehicle 1;
the unmanned aerial vehicle 1 is provided with a first central controller and a first wireless communication module, and the control end of a driving motor of a propeller of the unmanned aerial vehicle 1 is connected with the first central controller; the unmanned vehicle 2 is provided with a second central controller and a second wireless communication module, and the control end of the driving device 21 of the unmanned vehicle 2 is connected with the second central controller;
unmanned aerial vehicle 1 and unmanned vehicle 2 keep real-time communication, Global Positioning System (GPS) through the machine of carrying acquires respective position, unmanned aerial vehicle 1 calculates the relative distance with unmanned vehicle 2 at the moment of carrying out the task, and whether aassessment self electric quantity satisfies the flight and descends on unmanned vehicle 2, when unmanned aerial vehicle 1's electric quantity just in time satisfies or is greater than unmanned aerial vehicle 1 and arrives and descend to the required electric quantity on unmanned vehicle 2, unmanned vehicle 2 sends self longitude and latitude information for unmanned aerial vehicle 1, unmanned aerial vehicle 1 flies to support unmanned vehicle 2 through the GPS navigation.
Preferably, there are four of said guide seats 202, symmetrically distributed along the longitudinal and transversal axes of the deck 201. Preferably, the drone 1 is a quad-rotor drone.
Preferably, the driving device 21 is divided into a left driving unit 21a and a right driving unit 21b, wherein the left driving unit 21a includes wheels 211, a driving mounting bracket 212, a suspension upper plate 213, a damping compression spring 214, a suspension lower plate 215, a U-shaped screw 216, a bearing box 217, a driving motor 218, a driving belt 219, a driven pulley 2110, an axle 2111, a driving pulley 2112 and a connecting column 2113; the wheel 211 is fixedly connected with one end of an axle 2111, the axle 2111 is inserted into the bearing box 217, the other end of the axle 2111 extends out of the bearing box and is provided with a driven pulley 2110, the driving motor 218 is arranged on a bracket at the rear side of the bearing box 217, the driving pulley 2112 is fixedly connected with the axle end of the driving motor 218, and the driving belt 219 is arranged on the driving pulley 2112 and the driven pulley 2110 to form a belt transmission system; the driving mounting frame 212 is mounted on a suspension upper plate 213, two damping compression springs 214 are mounted between the suspension upper plate 213 and a suspension lower plate 215, and the suspension lower plate 215 is mounted on the left side of a bearing box 217 through two U-shaped screws 216; the left driving unit 21a and the right driving unit 21b have the same shape and number of parts, are distributed in a left-right mirror image, and have connecting columns 2113 connected with each other;
the utility model has the advantages that:
unmanned vehicles through rational distribution form unmanned aerial vehicle's charging network, and unmanned aerial vehicle and fill to connect reliably between the electric pile, and control cost is low, low in cost, maintain simply, and unmanned aerial vehicle's the work of independently charging of completion that can be fine has expanded unmanned aerial vehicle's duration.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of the adsorption charging device of the present invention;
fig. 3 is a schematic view of a driving device of the unmanned vehicle according to the present invention.
The reference numbers in the figures illustrate: 1. an unmanned aerial vehicle; 101. a camera; 102. a landing gear; 103. a guide block; 2, unmanned vehicles; 201. turning a surface; 202. a guide seat; 203. an electromagnet; 21. a drive device; 21a. a left drive unit; 21b. a right drive unit; 211. a wheel; 212. a drive mounting; 213. hanging the upper plate; 214. a damping pressure spring; 215. suspending the lower plate; a U-shaped screw; 217. a bearing housing; 218. a drive motor; 219. a drive belt; 2110. a driven pulley; 2111. an axle; 2112. a driving pulley; 2113, connecting column;
Detailed Description
The present invention will be further explained with reference to the accompanying drawings:
the unmanned aerial vehicle mobile power supply device with automatic navigation comprises an unmanned aerial vehicle 1 and an unmanned vehicle 2;
the unmanned aerial vehicle 1 is provided with a camera 101, an undercarriage 102 and a guide block 103, and the camera 101 is arranged right below the unmanned aerial vehicle; the bottom of the unmanned aerial vehicle 1 is provided with a plurality of undercarriage 102, and the tail end of the undercarriage 102 is provided with a guide block 103; the guide block 103 is made of conductive magnetic material.
The unmanned vehicle 2 comprises a vehicle surface 201, a guide seat 202 and two sets of driving devices 21, wherein the driving devices 21 are respectively arranged at the front end and the rear end of the vehicle surface 201 to form a four-wheel drive system; a guide seat 202 is arranged on the upper side of the vehicle surface 201; the position of the guide seat 202 corresponds to the position of the landing gear 102 when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, the guide seat 202 is provided with an inner cavity with an opening at the top, the bottom of the inner cavity of the guide seat 202 is provided with an electromagnet 203, the inner cavity and the guide block 103 are conical bodies with large top and small bottom, the guide block 103 is accommodated in the inner cavity when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, and the electromagnet 203 is contacted with the guide block 103;
the unmanned vehicle 2 is provided with a storage battery which is electrically connected with the electromagnet 203; an electric board on the unmanned aerial vehicle 1 is electrically connected with the guide block 103; when the unmanned aerial vehicle 1 is parked on the unmanned vehicle 2, the storage battery charges an electric board on the unmanned aerial vehicle 1;
the unmanned aerial vehicle 1 is provided with a first central controller and a first wireless communication module, and the control end of a driving motor of a propeller of the unmanned aerial vehicle 1 is connected with the first central controller; the unmanned vehicle 2 is provided with a second central controller and a second wireless communication module, and the control end of the driving device 21 of the unmanned vehicle 2 is connected with the second central controller.
Unmanned aerial vehicle 1 and unmanned vehicle 2 keep real-time communication, Global Positioning System (GPS) through the machine of carrying acquires respective position, unmanned aerial vehicle 1 calculates the relative distance with unmanned vehicle 2 at the moment of carrying out the task, and whether aassessment self electric quantity satisfies the flight and descends on unmanned vehicle 2, when unmanned aerial vehicle 1's electric quantity just in time satisfies or is greater than unmanned aerial vehicle 1 and arrives and descend to the required electric quantity on unmanned vehicle 2, unmanned vehicle 2 sends self longitude and latitude information for unmanned aerial vehicle 1, unmanned aerial vehicle 1 flies to support unmanned vehicle 2 through the GPS navigation.
The guide seats 202 are four in number and are symmetrically distributed along the longitudinal axis and the transverse axis of the vehicle surface 201. Unmanned aerial vehicle 1 adopts four rotor unmanned aerial vehicles on the market.
The driving device 21 is divided into a left driving unit 21a and a right driving unit 21b, wherein the left driving unit 21a comprises wheels 211, a driving mounting frame 212, a suspension upper plate 213, a damping pressure spring 214, a suspension lower plate 215, a U-shaped screw 216, a bearing box 217, a driving motor 218, a driving belt 219, a driven pulley 2110, an axle 2111, a driving pulley 2112 and a connecting column 2113; the wheel 211 is fixedly connected with one end of an axle 2111, the axle 2111 is inserted into the bearing box 217, the other end of the axle 2111 extends out of the bearing box and is provided with a driven pulley 2110, the driving motor 218 is arranged on a bracket at the rear side of the bearing box 217, the driving pulley 2112 is fixedly connected with the axle end of the driving motor 218, and the driving belt 219 is arranged on the driving pulley 2112 and the driven pulley 2110 to form a belt transmission system; the driving mounting frame 212 is mounted on a suspension upper plate 213, two damping compression springs 214 are mounted between the suspension upper plate 213 and a suspension lower plate 215, and the suspension lower plate 215 is mounted on the left side of a bearing box 217 through two U-shaped screws 216; the left driving unit 21a and the right driving unit 21b have the same shape and number of parts, and are distributed in a left-right mirror image, and the connection posts 2113 of the left driving unit and the right driving unit are connected with each other.
A plurality of unmanned vehicles with large-capacity storage batteries are arranged in related regions, and corresponding charging interfaces are arranged on the unmanned vehicles to charge the unmanned vehicles, so that the cruising ability of the unmanned vehicles is improved.
Unmanned aerial vehicle's operating personnel can manipulate unmanned aerial vehicle to fly to nearer unmanned vehicle to when unmanned aerial vehicle is close unmanned vehicle according to the image manipulation unmanned aerial vehicle descending that unmanned aerial vehicle returned, obtain charging on unmanned vehicle.
The embodiments described in this specification are merely illustrative of implementations of the inventive concepts, and the scope of the invention should not be considered limited to the specific forms set forth in the embodiments, but rather the scope of the invention is intended to include equivalent technical means as would be understood by those skilled in the art from the inventive concepts.
Claims (3)
1. Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit, its characterized in that: comprises an unmanned aerial vehicle (1) and an unmanned vehicle (2);
a camera (101) and an undercarriage (102) are arranged on the unmanned aerial vehicle (1), and the camera (101) is installed right below the unmanned aerial vehicle (1); the bottom of the unmanned aerial vehicle (1) is provided with a plurality of landing gears (102), and the tail ends of the landing gears (102) are provided with guide blocks (103); the guide block (103) is made of conductive magnetic materials;
the unmanned vehicle (2) comprises a vehicle surface (201), guide seats (202) and driving devices (21), wherein two sets of driving devices (21) are respectively arranged at the front end and the rear end of the vehicle surface (201) to form a four-wheel drive system; a guide seat (202) is arranged on the upper side of the vehicle surface (201); the position of the guide seat (202) corresponds to the position of the landing gear (102) when the unmanned aerial vehicle (1) is parked on the unmanned vehicle (2), the guide seat (202) is provided with an inner cavity with an opening at the top, an electromagnet (203) is installed at the bottom of the inner cavity of the guide seat (202), the inner cavity and the guide block (103) are conical bodies with large top and small bottom, the guide block (103) is accommodated in the inner cavity when the unmanned aerial vehicle (1) is parked on the unmanned vehicle (2), and the electromagnet (203) is in contact with the guide block (103);
the unmanned vehicle (2) is provided with a storage battery which is electrically connected with the electromagnet (203); an electric board on the unmanned aerial vehicle (1) is electrically connected with the guide block (103); when the unmanned aerial vehicle (1) is parked on the unmanned vehicle (2), the storage battery charges an electric board on the unmanned aerial vehicle (1);
the unmanned aerial vehicle (1) is provided with a first central controller and a first wireless communication module, and the control end of a driving motor of a propeller of the unmanned aerial vehicle (1) is connected with the first central controller; the unmanned vehicle (2) is provided with a second central controller and a second wireless communication module, and the control end of a driving device (21) of the unmanned vehicle (2) is connected with the second central controller;
unmanned aerial vehicle (1) and unmanned vehicle (2) keep real-time communication, Global Positioning System (GPS) through the machine of carrying acquires respective position, unmanned aerial vehicle (1) calculates the relative distance with unmanned vehicle (2) at the time of carrying out the task, and whether aassessment self electric quantity satisfies the flight and descends on unmanned vehicle (2), when the electric quantity of unmanned aerial vehicle (1) just in time satisfies or is greater than unmanned aerial vehicle (1) and reachs and descend to the required electric quantity on unmanned vehicle (2), unmanned vehicle (2) send self longitude and latitude information for unmanned aerial vehicle (1), unmanned aerial vehicle (1) flies to unmanned vehicle (2) through GPS navigation.
2. The self-navigating, multi-rotor drone mobile power supply of claim 1, characterized by: the guide seats (202) are four and are symmetrically distributed along the longitudinal axis and the transverse axis of the vehicle surface (201).
3. The self-navigating, multi-rotor drone mobile power supply of claim 1, characterized by: the driving device (21) is divided into a left driving unit (21a) and a right driving unit (21b), wherein the left driving unit (21a) comprises wheels (211), a driving installation frame (212), a suspension upper plate (213), a damping pressure spring (214), a suspension lower plate (215), a U-shaped screw (216), a bearing box (217), a driving motor (218), a driving belt (219), a driven pulley (2110), an axle (2111), a driving pulley (2112) and a connecting column (2113); the wheel (211) is fixedly connected to one end of an axle (2111), the axle (2111) is inserted into the bearing box (217), the other end of the axle (2111) extends out of the bearing box and is provided with a driven pulley (2110), the driving motor (218) is arranged on a support at the rear side of the bearing box (217), the driving pulley (2112) is fixedly connected to the shaft end of the driving motor (218), and the driving belt (219) is arranged on the driving pulley (2112) and the driven pulley (2110) to form a belt transmission system; the driving mounting frame (212) is mounted on a suspension upper plate (213), two damping compression springs (214) are mounted between the suspension upper plate (213) and a suspension lower plate (215), and the suspension lower plate (215) is mounted on the left side of a bearing box (217) through two U-shaped screws (216); the left driving unit (21a) and the right driving unit (21b) are identical in shape and number of parts, are distributed in a left-right mirror image mode, and are connected through connecting columns (2113).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922046341.3U CN211107997U (en) | 2019-11-22 | 2019-11-22 | Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201922046341.3U CN211107997U (en) | 2019-11-22 | 2019-11-22 | Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit |
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| CN211107997U true CN211107997U (en) | 2020-07-28 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110745239A (en) * | 2019-11-22 | 2020-02-04 | 浙江工业大学 | Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110745239A (en) * | 2019-11-22 | 2020-02-04 | 浙江工业大学 | Automatic many rotor unmanned aerial vehicle of navigation remove power supply unit |
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