CN215707208U - Unmanned aerial vehicle trades electric installation and unmanned aerial vehicle basic station - Google Patents
Unmanned aerial vehicle trades electric installation and unmanned aerial vehicle basic station Download PDFInfo
- Publication number
- CN215707208U CN215707208U CN202121975844.XU CN202121975844U CN215707208U CN 215707208 U CN215707208 U CN 215707208U CN 202121975844 U CN202121975844 U CN 202121975844U CN 215707208 U CN215707208 U CN 215707208U
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- aerial vehicle
- unmanned aerial
- base
- battery
- guide seat
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides an unmanned aerial vehicle power exchanging device and an unmanned aerial vehicle base station, wherein the unmanned aerial vehicle power exchanging device comprises: the battery clamping device comprises a base, a three-axis moving module arranged on the base and a battery clamping module connected with the three-axis moving module; the battery clamp is got the module include with triaxial remove module swing joint's base, set up removal track on the base, two with removal track swing joint's splint and drive splint are followed removal track removal's second power component, two be formed with spacing space between the splint, splint orientation be provided with on the side of spacing space with the unblock button assorted unblock portion of unmanned aerial vehicle battery. Compared with the prior art, the unmanned aerial vehicle battery replacing device can conveniently replace the battery of the unmanned aerial vehicle, achieves unmanned operation and is high in operation efficiency.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle battery replacement device and an unmanned aerial vehicle base station.
Background
With the development of wireless communication technology, aerial remote sensing mapping technology, GPS navigation positioning technology and automatic control technology, the unmanned aerial vehicle develops rapidly and is widely applied to multiple fields such as infrastructure planning, line inspection, emergency response, topographic survey and the like. The unmanned aerial vehicle basic station is the platform that unmanned aerial vehicle takes off and land, and the accurate descending of unmanned aerial vehicle can store, charge the operation such as after the unmanned aerial vehicle basic station.
The existing unmanned aerial vehicle battery on the market at present is changed through the manual work, and is inefficient.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the defects in the prior art and provides an unmanned aerial vehicle battery replacement device and an unmanned aerial vehicle base station.
One embodiment of the present invention provides an unmanned aerial vehicle battery replacement device, including: the battery clamping device comprises a base, a three-axis moving module arranged on the base and a battery clamping module connected with the three-axis moving module;
the three-axis moving module comprises a first guide seat arranged on the base, a second guide seat movably connected with the first guide seat, a third guide seat connected with the second guide seat and a first power assembly, and guide tracks are arranged on the first guide seat, the second guide seat and the third guide seat;
the battery clamping module comprises a base movably connected with a guide rail of the third guide seat, a moving rail arranged on the base, two clamping plates movably connected with the moving rail and a second power assembly driving the clamping plates to move along the moving rail, a limiting space is formed between the two clamping plates, and an unlocking part matched with an unlocking button of the unmanned aerial vehicle battery is arranged on the side, facing the limiting space, of each clamping plate;
the power assembly drives the second guide seat to move along the guide rail of the first guide seat, drives the third guide seat to move along the guide rail of the second guide seat, and drives the base to move along the guide rail of the third guide seat.
Compared with the prior art, the unmanned aerial vehicle battery replacing device can conveniently replace the battery of the unmanned aerial vehicle, achieves unmanned operation and is high in operation efficiency.
Further, the unlocking part comprises a limiting groove arranged on the side face, facing the limiting space, of the clamping plate.
Further, the module is got to battery clamp still is in including setting up reference column on the base, the shape at reference column top matches with the recess phase-match on the unmanned aerial vehicle battery.
Furthermore, still be provided with flexible subassembly on the base, flexible end of flexible subassembly with the reference column is connected.
Furthermore, the battery clamping module further comprises a plurality of positioning blocks arranged on the base, and the positioning blocks are arranged on the side edges of the limiting space.
Furthermore, the battery clamping module further comprises a plurality of positioning blocks arranged on the base, and the positioning blocks and the positioning columns are respectively arranged on two opposite sides of the limiting space.
Further, still be provided with a plurality of constant head tanks on the base, the shape of constant head tank and the shape phase-match of fixed unmanned aerial vehicle's structure.
Further, an accommodating cavity is arranged in the base;
the moving track comprises a sliding chute arranged on the base and two through grooves arranged in the sliding chute, and the through grooves are communicated with the accommodating cavity;
the second power assembly comprises a screw rod arranged in the containing cavity and a motor in transmission connection with the screw rod, the clamping plate is in sliding connection with the sliding groove and penetrates through the through groove to extend into the containing cavity, and the clamping plate is in transmission connection with the screw rod.
Further, the triaxial removes the module still including set up on the base and with first tow chain mechanism that the second guide holder is connected, set up on the second guide holder and with second tow chain mechanism that the third guide holder is connected and set up on the third guide holder and with the third tow chain mechanism that the base is connected.
Another embodiment of the present invention provides an unmanned aerial vehicle base station, including: base station housing, setting are in shut down platform and battery compartment in the base station housing and as above-mentioned an unmanned aerial vehicle trades electric installation, the base sets up in the base station housing, the triaxial removes module drive the battery clamp is got the module and is in shut down the platform with remove between the battery compartment.
In order that the utility model may be more clearly understood, specific embodiments thereof will be described hereinafter with reference to the accompanying drawings.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle battery swapping device according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a battery clamping module according to an embodiment of the utility model;
fig. 3 is a cross-sectional view of a battery clamping module according to an embodiment of the utility model;
fig. 4 is a partial structural view of the bottom of the drone battery of one embodiment of the present invention.
Description of reference numerals:
10. a base; 21. a first guide seat; 22. a second guide seat; 23. a third guide seat; 241. a first linear motor; 242. a second linear motor; 243. a third linear motor; 25. a first drag chain mechanism; 26. a second tow chain mechanism; 27. a third drag chain mechanism; 30. a battery clamping module; 31. a base; 311. a positioning column; 312. a telescoping assembly; 313. positioning blocks; 314. positioning a groove; 315. an accommodating cavity; 32. a moving track; 321. a chute; 322. a through groove; 33. a splint; 331. an unlocking portion; 34. a second power assembly; 341. a screw; 342. a motor; 40. an unmanned aerial vehicle battery; 41. an unlocking key; 42. and (4) a groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Please refer to fig. 1, which is a schematic structural diagram of an unmanned aerial vehicle battery swapping device according to an embodiment of the present invention, the unmanned aerial vehicle battery swapping device includes: unmanned aerial vehicle trades electric installation includes: the battery clamping device comprises a base 10, a triaxial moving module arranged on the base 10 and a battery clamping module 30 connected with the triaxial moving module.
The triaxial removes the module including setting up first guide holder 21 on the base 10, with first guide holder 21 swing joint's second guide holder 22, with third guide holder 23 and the first power component that second guide holder 22 is connected, first guide holder 21 the second guide holder 22 with all be provided with the direction track on the third guide holder 23. Referring to fig. 2, 3 and 4, fig. 2 is a schematic structural diagram of a battery clamping module according to an embodiment of the present invention, fig. 3 is a cross-sectional view of the battery clamping module according to an embodiment of the present invention, fig. 4 is a schematic partial structural diagram of a bottom of an unmanned aerial vehicle battery according to an embodiment of the present invention, the battery clamping module 30 includes a base 31 movably connected to a guide rail of the third guide seat 23, a moving rail 32 disposed on the base 31, two clamping plates 33 movably connected to the moving rail 32, and a second power assembly 34 driving the clamping plates 33 to move along the moving rail 32, a limiting space is formed between the two clamping plates 33, and an unlocking portion 331 matched with an unlocking button 41 of the unmanned aerial vehicle battery 40 is disposed on a side of the clamping plates 33 facing the limiting space; the power assembly drives the second guide seat 22 to move along the guide rail of the first guide seat 21, drives the third guide seat 23 to move along the guide rail of the second guide seat 22, and drives the base 31 to move along the guide rail of the third guide seat 23. Trade the electric installation during operation at unmanned aerial vehicle, remove the accurate battery department that removes unmanned aerial vehicle of module drive base 31 through the triaxial, then second power component 34 drive splint 33 is close to each other, the unblock portion 331 on the splint 33 supports the unblock button 41 of pressing unmanned aerial vehicle battery 40, make unmanned aerial vehicle battery 40 be in the unblock state, then triaxial removes module drive base 31 and leaves unmanned aerial vehicle, thereby take off unmanned aerial vehicle battery 40, the process of putting into unmanned aerial vehicle with the battery compartment is the same with above-mentioned principle, no longer describe herein. In the present embodiment, the unmanned aerial vehicle battery 40 is connected to the unmanned aerial vehicle through a buckle, an unlocking button 41 connected to the buckle is disposed on the surface of the unmanned aerial vehicle battery 40, and the unmanned aerial vehicle battery 40 can be unlocked by pressing the unlocking button 41 through the unlocking portion 331, so that the unmanned aerial vehicle battery 40 can be removed. Under unmanned aerial vehicle's the circumstances that the platform that stops can rotate, set up the angle according to unmanned aerial vehicle trades electric installation, can follow other angle clamps and get unmanned aerial vehicle battery 40, can not restrict the angle of stopping the platform, for example stop and fall down to put after the platform rotates, unmanned aerial vehicle is falling to fix on stopping the platform this moment, and unmanned aerial vehicle trades electric installation and sets up in stopping the platform below, can follow the unmanned aerial vehicle and take out the battery.
Since some of the clips of the drone battery 40 protrude from the surface of the drone battery 40, in order to make the drone battery 40 clamped more stably, in some alternative embodiments, the two sides of the clamping plates 33 facing each other are provided with limiting grooves matched with the clips of the drone battery 40, and the clips of the drone battery 40 are pressed into the drone battery 40 by the inner walls of the limiting grooves to realize unlocking, and meanwhile, the clips of the drone battery 40 are limited in the limiting grooves, so that the drone battery 40 is more stably limited between the clamping plates 33. Of course, the structure of the unlocking portion 331 is not limited to this, and those skilled in the art can also select other suitable unlocking keys 41 according to the teachings of the present invention, and is not limited to the form of the limiting groove shown in the drawings.
Some unmanned aerial vehicle battery 40's bottom equipotential is provided with recess 42, and in order to improve the precision of getting to press from both sides and get unmanned aerial vehicle battery 40, in some optional embodiments, the battery presss from both sides module 30 still including setting up reference column 311 on base 31, the shape at reference column 311 top matches with recess 42 on unmanned aerial vehicle battery 40, and after base 31 was close to the unmanned aerial vehicle, reference column 311 stretched into in the recess 42 on unmanned aerial vehicle battery 40, realizes the location.
In order to improve the positioning stability, in some alternative embodiments, a telescopic assembly 312 is further disposed on the base 31, and a telescopic end of the telescopic assembly 312 is connected to the positioning column 311. The telescopic assembly 312 may employ an air cylinder, an electric cylinder, or the like.
In some optional embodiments, the battery clamping module 30 further includes a plurality of positioning blocks 313 disposed on the base 31, and the positioning blocks 313 are disposed at the sides of the limiting space. When being provided with reference column 311 on base 31, locating piece 313 with reference column 311 can arrange respectively spacing space's relative both sides are close to unmanned aerial vehicle back at base 31, fix a position the side of unmanned aerial vehicle's battery in advance through locating piece 313, and flexible subassembly 312 drives reference column 311 afterwards and stretches into in unmanned aerial vehicle battery 40's the recess 42, realizes further location, then drives splint 33 and cliies unmanned aerial vehicle battery 40 again.
Be provided with fixed unmanned aerial vehicle's structure on some platforms that stop, for example some arm lock, thereby the arm lock cliies unmanned aerial vehicle and avoids unmanned aerial vehicle to remove, in some optional embodiments, still be provided with a plurality of constant head tanks 314 on the base 31, the shape of constant head tank 314 and the shape phase-match of fixed unmanned aerial vehicle's structure, after base 31 is close to unmanned aerial vehicle, fixed unmanned aerial vehicle's structure stretches into in the constant head tank 314 to realize the location of base 31, thereby improve the accuracy that the module 30 was got to the battery clamp.
To improve the stability of the clamping plate 33 in clamping the battery 40 of the drone, in some alternative embodiments, a housing cavity 315 is provided in the base 31; the moving track 32 comprises a sliding slot 321 arranged on the base 31 and two through slots 322 arranged in the sliding slot 321, and the through slots 322 are communicated with the accommodating cavity 315; the second power assembly 34 includes a screw 341 disposed in the accommodating cavity 315 and a motor 342 in transmission connection with the screw 341, the clamping plate 33 is in sliding connection with the sliding groove 321, penetrates through the through groove 322, extends into the accommodating cavity 315, and is in transmission connection with the screw 341, and after the motor 342 drives the screw 341 to rotate, the two clamping plates 33 move along the through groove 322 and the sliding groove 321 relatively or reversely. Of course, the structures of the moving track 32 and the second power assembly 34 are not limited thereto, and those skilled in the art may select other suitable structures according to the teachings of the present invention, for example, the power assembly may be a screw rod driving assembly, a rotating motor 342 translation driving assembly, a belt translation assembly, an air cylinder translation driving assembly or a linear motor translation driving assembly, wherein the working principle of the screw rod driving assembly, the rotating motor 342 translation driving assembly, the belt translation driving assembly, the air cylinder translation driving assembly or the linear motor translation driving assembly is the same as that discussed above, and is not described in detail herein, and the moving track 32 may be designed by matching the structure of the second power assembly 34.
In order to facilitate the power connection of the electric equipment on the second guide seat 22, the electric equipment on the third guide seat 23 and the electric equipment on the base 31, and avoid the cable confusion, in some optional embodiments, the three-axis mobile module further includes a first drag chain mechanism 25 disposed on the base 10 and connected to the first support arm, a second drag chain mechanism 26 disposed on the first support arm and connected to the second support arm, and a third drag chain mechanism 27 disposed on the second support arm and connected to the base 31.
In this embodiment, the first power assembly includes a first linear motor 241 disposed on the base 10, a second linear motor 242 disposed on the first support arm, and a third linear motor 243 disposed on the second support arm, the first linear motor 241 is in transmission connection with the first support arm to drive the first support arm to move along the first guide rail, the second linear motor 242 is in transmission connection with the second support arm to drive the second support arm to move along the second guide rail, and the third linear motor 243 is in transmission connection with the base 31 to drive the base 31 to move along the third guide rail. Of course, the structures of the guide rail and the first power assembly are not limited thereto, and those skilled in the art may select other suitable structures according to the teachings of the present invention, for example, the first power assembly may adopt a screw rod driving assembly, a rotating motor 342 translation driving assembly, a belt translation assembly or a cylinder translation driving assembly, wherein the working principle of the screw rod driving assembly, the rotating motor 342 translation driving assembly, the belt translation assembly or the cylinder translation driving assembly is the same as that discussed above, and will not be described in detail herein. In addition, the guide rail may be designed to match the structure of the first power assembly and the guide seat, such as a sliding groove 321, a guide rod or a convex rail. In addition, the first guide holder 21 may be provided integrally with the base 10.
In order to improve the stability of the first support arm, in some alternative embodiments, two first guide seats 21 are provided on the base 10, and two ends of the second guide seat 22 are respectively connected to the first guide seats 21.
Above-mentioned unmanned aerial vehicle trade electric installation and can use on the unmanned aerial vehicle basic station, this unmanned aerial vehicle basic station includes: base station housing, setting are in shut down platform and battery compartment in the base station housing and as aforesaid unmanned aerial vehicle trade electric installation, base 10 sets up in the base station housing, base 10 can with the integrative setting of base station housing, perhaps, base 10 is formed by the partial structure of base station housing, the drive of triaxial removal module the module 30 is got to the battery clamp shut down the platform with remove between the battery compartment.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides an unmanned aerial vehicle trades electric installation which characterized in that includes: the battery clamping device comprises a base, a three-axis moving module arranged on the base and a battery clamping module connected with the three-axis moving module;
the three-axis moving module comprises a first guide seat arranged on the base, a second guide seat movably connected with the first guide seat, a third guide seat connected with the second guide seat and a first power assembly, and guide tracks are arranged on the first guide seat, the second guide seat and the third guide seat;
the battery clamping module comprises a base movably connected with a guide rail of the third guide seat, a moving rail arranged on the base, two clamping plates movably connected with the moving rail and a second power assembly driving the clamping plates to move along the moving rail, a limiting space is formed between the two clamping plates, and an unlocking part matched with an unlocking button of the unmanned aerial vehicle battery is arranged on the side, facing the limiting space, of each clamping plate;
the power assembly drives the second guide seat to move along the guide rail of the first guide seat, drives the third guide seat to move along the guide rail of the second guide seat, and drives the base to move along the guide rail of the third guide seat.
2. The unmanned aerial vehicle trades electric installation of claim 1, its characterized in that: the unlocking part comprises a limiting groove arranged on the side face, facing the limiting space, of the clamping plate.
3. The unmanned aerial vehicle trades electric installation of claim 1, its characterized in that: the battery clamping module is characterized by further comprising a positioning column arranged on the base, and the shape of the top of the positioning column is matched with the groove in the battery of the unmanned aerial vehicle.
4. The unmanned aerial vehicle trades electric installation of claim 3, its characterized in that: the base is further provided with a telescopic assembly, and the telescopic end of the telescopic assembly is connected with the positioning column.
5. The unmanned aerial vehicle trades electric installation of claim 1, its characterized in that: the battery clamping module further comprises a plurality of positioning blocks arranged on the base, and the positioning blocks are arranged on the side edges of the limiting space.
6. The unmanned aerial vehicle trades electric installation of claim 4, its characterized in that: the battery clamping module further comprises a plurality of positioning blocks arranged on the base, and the positioning blocks and the positioning columns are respectively arranged on two opposite sides of the limiting space.
7. The unmanned aerial vehicle trades electric installation of claim 1, its characterized in that: still be provided with a plurality of constant head tanks on the base, the shape of constant head tank and the shape phase-match of fixed unmanned aerial vehicle's structure.
8. An unmanned aerial vehicle trades electric installation of any one of claims 1 to 7, its characterized in that: an accommodating cavity is formed in the base;
the moving track comprises a sliding chute arranged on the base and two through grooves arranged in the sliding chute, and the through grooves are communicated with the accommodating cavity;
the second power assembly comprises a screw rod arranged in the containing cavity and a motor in transmission connection with the screw rod, the clamping plate is in sliding connection with the sliding groove and penetrates through the through groove to extend into the containing cavity, and the clamping plate is in transmission connection with the screw rod.
9. An unmanned aerial vehicle trades electric installation of any one of claims 1 to 7, its characterized in that: the three-axis moving module further comprises a first drag chain mechanism, a second drag chain mechanism and a third drag chain mechanism, wherein the first drag chain mechanism is arranged on the base and connected with the second guide seat, the second drag chain mechanism is arranged on the second guide seat and connected with the third guide seat, and the third drag chain mechanism is arranged on the third guide seat and connected with the base.
10. An unmanned aerial vehicle basic station, its characterized in that includes: the unmanned aerial vehicle trades electric installation of base station housing, setting up shut down platform and battery compartment in the base station housing and any one of claims 1 to 9, the base sets up in the base station housing, triaxial removes the module drive the battery presss from both sides and gets the module and move between shut down platform with the battery compartment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121975844.XU CN215707208U (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle trades electric installation and unmanned aerial vehicle basic station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121975844.XU CN215707208U (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle trades electric installation and unmanned aerial vehicle basic station |
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| Publication Number | Publication Date |
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| CN215707208U true CN215707208U (en) | 2022-02-01 |
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| CN202121975844.XU Active CN215707208U (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle trades electric installation and unmanned aerial vehicle basic station |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115071993A (en) * | 2022-08-01 | 2022-09-20 | 江苏阳铭互联智能系统有限公司 | Clamping device of automatic battery replacement base station of unmanned aerial vehicle |
-
2021
- 2021-08-20 CN CN202121975844.XU patent/CN215707208U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115071993A (en) * | 2022-08-01 | 2022-09-20 | 江苏阳铭互联智能系统有限公司 | Clamping device of automatic battery replacement base station of unmanned aerial vehicle |
| CN115071993B (en) * | 2022-08-01 | 2023-08-01 | 江苏阳铭互联智能系统有限公司 | Clamping device of unmanned aerial vehicle automatic power conversion base station |
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