CN220830329U - Flight power supply system - Google Patents
Flight power supply system Download PDFInfo
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- CN220830329U CN220830329U CN202322509583.8U CN202322509583U CN220830329U CN 220830329 U CN220830329 U CN 220830329U CN 202322509583 U CN202322509583 U CN 202322509583U CN 220830329 U CN220830329 U CN 220830329U
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000004891 communication Methods 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 241000282472 Canis lupus familiaris Species 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 238000012544 monitoring process Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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Abstract
The utility model relates to a flight power supply system for supplying power to an intelligent mobile device, comprising a power supply device, at least one flight relay device and a control device; the power supply device outputs an output power through a positioning cable drum; each flying relay device comprises a reelable cable, and each flying relay device is connected in series through each cable to transmit the output power of the power supply device; the control equipment receives a position signal of the intelligent mobile equipment and controls each flying relay equipment to fly to a relay position; the output power is output to the intelligent mobile device relative to the terminal flight relay device of the power supply device, and the power requirement of the intelligent mobile device during long-time or complex mobile operation is met by improving the mobility and dynamic wiring capability of a power supply system.
Description
Technical Field
A power supply system, in particular to a flight power supply system for transmitting power through a flight carrier.
Background
Many intelligent machines are developed to replace traditional manual operations, such as robots, robot dogs, etc., and along with the evolution and maturity of technology, the functions of the intelligent machines are more various, the body types are more exquisite, and the maneuverability is improved, so that the intelligent mechanical energy is perfectly applied to different environments and industries. In military, intelligent mechanical energy is used for investigation and monitoring; in the aspect of the public field, the intelligent mechanical energy is applied to logistics transmission, public facility inspection and police security, or goes deep into dangerous terrain and disaster areas to perform disaster investigation and rescue operation, and the intelligent mechanical energy replaces manpower to perform high-repeatability, high-labor or high-risk work, and reduces the manpower cost.
However, the intelligent machine is powered by an internal battery, the size of the battery is limited by the volume and weight limitation of the intelligent machine, the capacity of the battery is limited, when the intelligent machine executes high-power operation or needs long-time operation, the internal battery cannot meet the power requirement of the intelligent machine, and if the existing power supply equipment is directly connected with the intelligent machine for power supply, the power supply equipment is difficult to cooperate with the high mobility of the unmanned aerial vehicle due to the limited line length and difficult movement of the machine body, and even extra manpower is needed for assisting in winding and unwinding the line, so that the intelligent machine is more inconvenient to use in mountain areas and rugged environments.
Therefore, how to improve the mobility of the power supply device, so that the power supply device can support the power requirement of the intelligent machine in high power or long-time operation is one of the problems to be solved in the current urgent need.
Disclosure of utility model
In view of the above, the present utility model provides a flight power supply system for providing the maneuverability and convenience of the power supply system.
In order to achieve the above object, the present utility model provides a flight power supply system for supplying power to an intelligent mobile device, the flight power supply system comprising:
an electric power supply apparatus comprising:
a power converter for converting an input power into an output power;
A positioning cable drum, on which a cable is wound, the cable being connected to the power converter to transmit the output power;
At least one flying relay device, each flying relay device comprises a cable capable of being reeled, each flying relay device is connected in series between the power supply device and the intelligent mobile device through each cable so as to transmit the output power of the power supply device to the intelligent mobile device through each cable;
The control equipment is in communication connection with the power supply equipment, the at least one flight relay equipment and the intelligent mobile equipment, receives a position signal sent by the intelligent mobile equipment, and controls each flight relay equipment to fly to a relay position between the power supply equipment and the intelligent mobile equipment according to the position signal;
The flying relay device at the tail end relative to the power supply device is connected to the intelligent mobile device through a cable thereof so as to transmit the output power of the power supply device to the intelligent mobile device.
In the flight power supply system, when the intelligent mobile device moves, the control device can control the movement of each flight relay device according to the position signal sent by the intelligent mobile device so as to adjust the length of each cable and the position of each flight relay device. The utility model provides the dynamic wiring function which can meet the movement requirement of the intelligent mobile equipment through the mobility of each flight relay equipment and the control of the control equipment on each flight relay equipment and each cable, can stably supply power to the intelligent mobile equipment when the intelligent mobile equipment performs complex movement operation under the condition of not influencing the operation of the intelligent mobile equipment, and meets the power requirement of the intelligent mobile equipment when the intelligent mobile equipment performs high-power or long-time operation.
Drawings
Fig. 1: the utility model relates to a three-dimensional appearance diagram of a flight power supply system.
Fig. 2: another perspective view of the present utility model flying power supply system.
Fig. 3: the utility model relates to a block schematic diagram of a power supply path of a flight power supply system.
Fig. 4: the utility model relates to a stereoscopic appearance diagram of a flight relay device.
Detailed Description
Referring to fig. 1 to 3, the flight power supply system 1 of the present utility model supplies power to an intelligent mobile device 2, where the flight power supply system 1 includes a power supply device 10, at least one flight relay device 20 and a control device 30, and it should be noted that, in fig. 1 to 3, the at least one flight relay device 20 is taken as an example of two flight relay devices 20, but the number of the at least one flight relay devices 20 may be one or more, not limited to this embodiment, where the intelligent mobile device 2 may be a mobile intelligent electronic device such as a robot, a robot dog, a unmanned aerial vehicle, a robot car, etc., and the intelligent mobile device 2 may be provided with a positioning unit, and the positioning unit may send a position signal through a global positioning system (Global Positioning System, GPS) or radio wave positioning.
The power supply apparatus 10 includes a power converter 11 and a positioning cable drum 12, the power converter 11 includes a power output port 111, the power converter 11 converts an input power provided by a utility power or a solar panel into an output power, and the output power is output through the power output port 111; the positioning cable drum 12 of the power converter 11 includes a power receiving port 121, and a cable 122 is wound around the positioning cable drum 12, the power receiving port 121 is connected to the power output port 111 of the power converter 11 through a line to receive the output power from the power converter 11, one end of the cable 122 is a fixed end, the other end is a movable end, the fixed end is connected to the power receiving port 121 of the positioning cable drum 12, the movable end is wound or unwound by rotation of the positioning cable drum 12, the positioning cable drum 12 receives the output power from the power receiving port 121 through the fixed end of the cable 122, and outputs the output power through the movable end of the cable 122, wherein when the positioning cable drum 12 of the power supply apparatus 10 receives the output power, a part of the output power is used for supplying power to the positioning cable drum 12 to maintain the operation of the positioning cable drum 12, and the positioning cable drum 12 outputs the remaining output power to the rear end.
Referring further to fig. 4, the at least one flight relay device 20 is connected between the power supply device 10 and the smart mobile device 2, each flight relay device 20 includes a drone 21 and an on-board cable reel 22, the drone 21 includes a plurality of motors and a plurality of rotors 211, the plurality of rotors 211 are driven by the plurality of motors to rotate, and the plurality of rotors 211 provide the flight relay device 20 with flight movement capability; the on-board cable drum 22 is disposed on the unmanned aerial vehicle 21 and includes a power receiving port 221, and a cable 222 is wound on the corresponding on-board cable drum 22, and one end of the cable 222 is a fixed end, and the other end is a movable end, and the fixed end is connected to the power receiving port 221 of the corresponding on-board cable drum 22, and the movable end is wound or unwound by the rotation of the on-board cable drum 22, wherein the power receiving port 221 of each flying relay device 20 is connected to the movable end of the cable 122 of the closest positioning cable drum 12 or the movable end of the cable drum 22 of the closest last flying relay device 20 to receive the output power, that is, the movable end of the cable 22 in each flying relay device 20 is connected to the power receiving port 221 of the on-board cable drum 22 of the closest next flying relay device 20, and the nearest flying relay device 20 outputs the output power to the smart mobile device 2 through the movable end of the cable 222.
When the at least one flying relay device 20 is a flying relay device 20, the flying relay device 20 is connected to the movable end of the cable 122 of the positioning cable drum 12 in the power supply device 10 through the power receiving port 121 to receive the output power outputted from the positioning cable drum 12 in the power supply device 10.
Similarly, when the at least one flying relay device 20 is two flying relay devices 20, the two flying relay devices 20 are connected in series between the power supply device 10 and the smart mobile device 2 through the respective cables 222, the first flying relay device 20 is connected to the active end of the cable 122 of the positioning cable drum 12 in the power supply device 10 through the corresponding power receiving port 121, the second flying relay device 20 is also connected to the active end of the cable 222 of the on-board cable drum 22 in the first flying relay device 20 through the corresponding power receiving port 221, and the active end of the cable 222 of the on-board cable drum 22 in the second flying relay device 20 is connected to the smart mobile device 2, and so on.
Each of the flying relay devices 20 further comprises a power converter 23, the power converter 23 is connected between the power receiving port 221 and the unmanned aerial vehicle 21, the power converter 23 converts a portion of the output power received by the power receiving port 221 into an operating power and transmits the operating power to the unmanned aerial vehicle 21, so as to supply power to the unmanned aerial vehicle 21 and maintain the operation of the unmanned aerial vehicle 21, and the corresponding on-board cable drum 22 outputs the remaining output power to the next flying relay device 20 or the intelligent mobile device 2.
Preferably, the blades of the plurality of rotors 211 face the top of the unmanned aerial vehicle 21, and the on-board cable drum 22 is disposed at the bottom of the unmanned aerial vehicle 21, so that the cable 222 of the on-board cable drum 22 is spaced apart from the plurality of rotors 211, and the cable 222 is prevented from winding around the plurality of rotors 211 to affect the operation of the unmanned aerial vehicle 21.
The control device 30 is disposed on the power supply device 10 and is communicatively connected to the power supply device 10, the at least one flight relay device 20, and the smart mobile device 2. When the smart mobile device 2 moves, the control device 30 receives a position signal transmitted by the positioning unit of the smart mobile device 2, calculates a required cable length and a flight distance of each unmanned aerial vehicle 21 according to the position signal by the control device 30, outputs a cable control signal to the positioning cable tray 12 and each onboard cable tray 22 according to the cable length, and outputs a flight control signal to each unmanned aerial vehicle 21 according to the flight distance, controls the positioning cable tray 12 of the power supply device 10 and each onboard cable tray 22 of the at least one onboard cable tray 22 to rotate according to the flight distance, thereby increasing or decreasing the active end lengths of the cable 122 of the positioning cable tray 12 and the cable 222 of each onboard cable tray 22, and controls the operation of each unmanned aerial vehicle 21 of the at least one flight relay device 20 according to the cable length, controls the flight movement of each flight relay device 20 to a position between the power supply device 10 and the smart mobile device 2 according to the flight distance, and dynamically changes the position signal of the smart mobile device 2, wherein the flight distance and the horizontal wiring distance include the horizontal wiring distance and the horizontal wiring distance of each cable 222.
By simultaneously controlling the cable length of the positioning cable drum 12, each on-board cable drum 22 and the moving position of each flying relay device 20 by the control device 30, the horizontal distance between each flying relay device 20 is prevented from being smaller than the cable lengths of the positioning cable drum 12 and each on-board cable drum 22, so that each cable 122,222 drops down to hook up sundries on the ground; the horizontal distance between the flying relay devices 20 is larger than the cable lengths of the positioning cable drum 12 and the on-board cable drum 22, so that the flying relay devices 20 are pulled mutually, and the stability and the line safety of the flying relay devices 20 are prevented from being affected; and preventing the vertical distance difference between the flying relay devices 20 from being too large, resulting in the respective cables 122,222 being caught in the plurality of rotors 211 of the flying relay devices 20.
The control device 30 is electrically connected to the power converter 11 of the power supply device 10, and a portion of the output power is converted into an operating power by the power converter 11 and then transmitted to the control device 30, so as to supply power to the control device 30 and maintain the operation of the control device 30; the control device 30 may be an arithmetic processing device such as a controller or a microcomputer.
As shown in fig. 2, when the intelligent mobile device 2 needs to move according to different operation requirements, the control device 30 of the present utility model can calculate the cable length required by each cable 122,222 and the flight distance required by each unmanned aerial vehicle 21 in real time according to the position signal sent by the intelligent mobile device 2, each unmanned aerial vehicle 21 can adjust the height and position of the unmanned aerial vehicle 21 according to the received flight control signal, and the present utility model enables the flight power supply system 1 to dynamically route each cable 122,222 of each unmanned aerial vehicle 21 through the high mobility of each unmanned aerial vehicle 21 and the real-time control of the control device 30, so as to not only improve the convenience and mobility of the flight power supply system 1 during the routing, but also to perform complex intelligent mobile operation in cooperation with the intelligent mobile device 2 without additional manpower assistance without affecting the operation of the intelligent mobile device 2, and to meet the power requirements of the intelligent mobile device 2 during high power or long-time operation.
The present utility model is not limited to the above-mentioned embodiments, but is capable of modification and variation in all embodiments without departing from the spirit and scope of the present utility model.
Claims (12)
1. A flying power supply system for supplying power to an intelligent mobile device, the intelligent mobile device emitting a position signal, the flying power supply system comprising:
an electric power supply apparatus comprising:
a power converter for converting an input power into an output power;
A positioning cable drum, on which a cable is wound, the cable being connected to the power converter to transmit the output power;
At least one flying relay device, each flying relay device comprises a cable capable of being reeled, each flying relay device is connected in series between the power supply device and the intelligent mobile device through each cable, so as to transmit the output power of the power supply device to the intelligent mobile device through each cable;
the control equipment is in communication connection with the power supply equipment, the at least one flight relay equipment and the intelligent mobile equipment, and outputs a flight control signal for controlling each flight relay equipment to move to a relay position between the power supply equipment and the intelligent mobile equipment according to the position signal;
The flying relay device at the tail end relative to the power supply device is connected to the intelligent mobile device through a cable thereof so as to transmit the output power of the power supply device to the intelligent mobile device.
2. The flying power supply system according to claim 1, wherein each flying relay device comprises:
A drone having a plurality of rotors;
The on-board cable drum is arranged on the unmanned aerial vehicle, the cable is wound on the on-board cable drum, and the output power output by the power supply equipment is transmitted by the cable.
3. The flying power supply system according to claim 2 wherein the control device outputs a cable control signal for controlling the rotation of the positioning cable drum and each of the on-board cable drums according to a cable length to pay in and pay out each of the cables of the positioning cable drum and each of the on-board cable drums.
4. The flight power supply system of claim 2, wherein the control device outputs the flight control signal for controlling each of the unmanned aerial vehicles to fly to move to the relay position.
5. The flying power supply system according to claim 2, wherein the at least one flying relay device comprises a plurality of flying relay devices connected in series between the power supply device and the smart mobile device by respective cables.
6. The flying power supply system according to claim 1 wherein the power converter of the power supply device includes a power output port, the positioning cable drum includes a power receiving port, the power receiving port of the positioning cable drum is connected to the power output port of the power converter to receive the output power from the power converter.
7. The flying power supply system according to claim 2, wherein in the positioning cable drum, one end of the cable is a fixed end, and the other end is a movable end, the fixed end is connected to a power output port of the power converter, and the movable end is wound or unwound by rotation of the positioning cable drum;
Each on-board cable reel comprises a power receiving port, the on-board cable reel receives the output power from the power receiving port, one end of each cable is a fixed end, the other end of each cable is a movable end, the fixed end is connected with the power receiving port of each on-board cable reel, and the movable end is rolled or unrolled by the rotation of each on-board cable reel.
8. The flying power supply system according to claim 7 wherein the at least one flying relay device is a flying relay device, the power receiving port of the flying relay device is connected to the active end of the cable in the power supply device to receive the output power outputted by the power supply device, and the active end of the cable of the flying relay device is connected to the smart mobile device to supply power to the smart mobile device.
9. The flying power supply system according to claim 7, wherein the at least one flying relay device comprises a plurality of flying relay devices connected in series between the power supply device and the smart mobile device by respective cables;
The power receiving port of the first one of the flying relay devices nearest to the power supply device is connected to the movable end of the cable of the power supply device to receive the output power outputted by the power supply device;
And the power receiving port of each of the flying relay devices except the first flying relay device is connected with the movable end of the cable of the previous flying relay device to receive the output power output by the previous flying relay device.
10. The flying power supply system according to claim 7 wherein each flying relay device further comprises a power converter connected between the power receiving port and the unmanned aerial vehicle, the power converter converting a portion of the output power received by the power receiving port into an operating power for transmission to the unmanned aerial vehicle.
11. The flying power supply system according to claim 1, wherein the control device is electrically connected to the power converter of the power supply device, and a part of the output power is converted into an operating power by the power converter and then transmitted to the control device.
12. The flying power supply system according to claim 2, wherein in each flying relay device, the blades of the plurality of rotors face the top of the unmanned aerial vehicle, and the onboard cable drum is disposed at the bottom of the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322509583.8U CN220830329U (en) | 2023-09-15 | 2023-09-15 | Flight power supply system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322509583.8U CN220830329U (en) | 2023-09-15 | 2023-09-15 | Flight power supply system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220830329U true CN220830329U (en) | 2024-04-23 |
Family
ID=90726873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322509583.8U Active CN220830329U (en) | 2023-09-15 | 2023-09-15 | Flight power supply system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220830329U (en) |
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2023
- 2023-09-15 CN CN202322509583.8U patent/CN220830329U/en active Active
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