CN218258784U - Unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligent hangar - Google Patents
Unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligent hangar Download PDFInfo
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- CN218258784U CN218258784U CN202222596590.1U CN202222596590U CN218258784U CN 218258784 U CN218258784 U CN 218258784U CN 202222596590 U CN202222596590 U CN 202222596590U CN 218258784 U CN218258784 U CN 218258784U
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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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Abstract
The utility model discloses an unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligence hangar. The unmanned aerial vehicle battery replacing equipment comprises a moving device, a battery clamping device and a cabin lock rotating device, wherein the moving device is used for adjusting the positions of the cabin lock rotating device and the battery clamping device; the other end of the connecting arm is provided with a first driving piece, and the fixing piece can be abutted against and separated from the second surface under the driving of the first driving piece, so that the battery is clamped and fixed between the fixing piece and the abutting piece. Through setting up foretell mobile device, storehouse lock rotary device and battery clamp and get the device, can realize the action of the automatic battery of changing of M300 unmanned aerial vehicle with the less spare part of quantity, the cost of manufacture is low, and the control degree of difficulty is low, and use cost is low.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle intelligence hangar technical field especially relates to an unmanned aerial vehicle battery replacement equipment.
Background
M300 unmanned aerial vehicle is a high performance unmanned aerial vehicle, is provided with many load platforms, through changing different loads, can carry out multiple operations such as aerial vision is patrolled and examined, aerial material concentration detects. However, due to the restriction of the battery capacity, the unmanned aerial vehicle needs to continuously return to the home and replace the battery after long-time inspection.
At present, in order to realize automatic battery replacement and save labor cost, an unmanned aerial vehicle intelligent hangar with an automatic battery replacement function has been developed. However, in the existing unmanned aerial vehicle intelligent hangar, the used unmanned aerial vehicle battery replacement equipment is designed for various unmanned aerial vehicles, and has the disadvantages of complex structure, high manufacturing cost and great control difficulty for compatibility; and the structure in M300 unmanned aerial vehicle battery storehouse also has certain particularity, is different from other unmanned aerial vehicles, and current unmanned aerial vehicle battery replacement equipment can not be used for conveniently changing M300 unmanned aerial vehicle's battery, and use cost is higher.
Based on above, need for an unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligence hangar urgently, have simple structure, can satisfy the demand that the battery was changed in the automation of M300 unmanned aerial vehicle with lower cost of manufacture and use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle battery replacement equipment has simple structure, can satisfy the demand that the battery was changed in the automation of M300 unmanned aerial vehicle with lower cost of manufacture and use cost.
To achieve the purpose, the utility model adopts the following technical proposal:
unmanned aerial vehicle battery replacement equipment for the automatic battery of changing M300 unmanned aerial vehicle includes:
the bin lock rotating device is used for locking and unlocking a battery bin of the M300 unmanned aerial vehicle;
a battery clamping device, comprising an abutting part, a connecting arm, a first driving part and a fixing part, wherein the abutting part is installed at one end of the connecting arm, the battery is provided with a first surface and a second surface, the first surface and the second surface are perpendicular to the sliding installation direction of the battery in the battery compartment, and the abutting part is used for abutting against the first surface; the other end of the connecting arm is provided with the first driving piece, the fixing piece is in transmission connection with the first driving piece, and the fixing piece can be abutted against and separated from the second surface under the driving of the first driving piece, so that the battery has a clamping state of being clamped and fixed between the fixing piece and the abutting piece and a free state of not being clamped and fixed;
and the moving device is used for moving and adjusting the positions of the bin lock rotating device and the battery clamping device.
Optionally, the first driving element is a steering engine, one end of the fixing element is mounted on a swing shaft of the steering engine, and the other end of the fixing element can be abutted against and separated from the second surface under the driving of the first driving element.
Optionally, the other end of the fixing member is provided with a guide surface.
Optionally, the bin lock rotating device includes a rotating buckle and a second driving element, the rotating buckle is connected to the second driving element in a transmission manner, the rotating buckle has a slot, the locking knob of the battery bin can be clamped in the slot, and the rotating buckle can drive the locking knob to rotate forward and backward under the driving of the second driving element.
Optionally, the width of the card slot gradually increases along a direction from the bottom of the card slot to the opening of the card slot.
Optionally, the moving device at least comprises an X-axis moving assembly, a Y-axis moving assembly and a Z-axis moving assembly.
Optionally, the moving device further includes an angle adjusting device, the angle adjusting device includes a fixing plate and a rotating plate, the fixing plate is fixedly mounted on one of the X-axis moving assembly, the Y-axis moving assembly and the Z-axis moving assembly, the rotating plate is angularly and rotatably connected to the fixing plate, and the bin lock rotating device and the battery clamping device are connected to the rotating plate.
Optionally, above-mentioned unmanned aerial vehicle battery replacement equipment still includes visual identification device, and above-mentioned visual identification device is used for discerning the position of above-mentioned battery and guides above-mentioned mobile device.
Optionally, the above-mentioned unmanned aerial vehicle battery replacing apparatus further includes a plurality of sensors, and the plurality of sensors are mounted on at least one of the above-mentioned bin lock rotating device, the above-mentioned battery clamping device, and the above-mentioned moving device.
The utility model provides an unmanned aerial vehicle battery replacement equipment's beneficial effect lies in: through setting up foretell mobile device, storehouse lock rotary device and battery clamp and getting the device, can realize the automatic action of changing the battery of M300 unmanned aerial vehicle with the less spare part of quantity, and the cost of manufacture is lower, and the control degree of difficulty is lower, can conveniently be used for changing M300 unmanned aerial vehicle's battery, and use cost is lower.
Another object of the utility model is to provide an unmanned aerial vehicle intelligence hangar can satisfy the demand that the battery was changed in the automation of M300 unmanned aerial vehicle with lower cost of manufacture and use.
To achieve the purpose, the utility model adopts the following technical proposal:
unmanned aerial vehicle intelligence hangar includes foretell unmanned aerial vehicle battery and changes equipment.
The utility model provides an unmanned aerial vehicle intelligence hangar's beneficial effect lies in: the unmanned aerial vehicle battery replacement equipment is adopted, and compared with the existing hangar applied to various unmanned aerial vehicles, the unmanned aerial vehicle battery replacement equipment is simple in structure, and can meet the requirement of automatically replacing batteries of M300 unmanned aerial vehicles with lower manufacturing cost and use cost.
Drawings
Fig. 1 is a perspective view of the unmanned aerial vehicle battery replacing apparatus provided by the present invention when clamping a battery;
fig. 2 is a perspective view of the unmanned aerial vehicle battery replacing device provided by the present invention when a battery is to be clamped;
FIG. 3 is an enlarged view of a portion of FIG. 2 at A;
FIG. 4 is an enlarged view of a portion of FIG. 2 at B;
fig. 5 is a perspective view of the battery of the unmanned aerial vehicle according to the present invention;
fig. 6 is a top view of the battery of the drone of the present invention;
fig. 7 is a top view of the unmanned aerial vehicle battery changer apparatus provided by the present invention gripping a battery;
FIG. 8 is an enlarged view of a portion of FIG. 7 at C;
fig. 9 is a front view of the battery replacing apparatus of the unmanned aerial vehicle provided by the present invention when a battery is to be clamped;
FIG. 10 is an enlarged view of a portion of FIG. 9 at D;
fig. 11 is a perspective view of a part of the Y-axis moving assembly and the angle adjusting device of the present invention;
fig. 12 is a bottom view of the partial Y-axis moving assembly and the angle adjustment apparatus of the present invention;
fig. 13 is a side view of the partial Y-axis moving assembly and the angle adjusting device of the present invention.
In the figure:
1. a battery; 101. a first surface; 102. a second surface; 11. locking the knob;
2. a battery clamping device; 21. a connecting arm; 22. a first driving member; 23. an abutting member; 24. a fixing member;
3. a mobile device; 31. an X-axis moving assembly; 32. a Z-axis moving assembly; 33. a Y-axis moving assembly;
4. a bin lock rotating device; 41. rotating the buckle; 42. a second driving member;
5. a visual recognition device;
6. an angle adjusting device; 61. a fixing plate; 62. a rotating plate; 63. a first thrust bearing; 64. a second thrust bearing; 65. a rotating shaft;
7. a sensor.
Detailed Description
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Wherein the terms "first position" and "second position" are two different positions.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may include, for example, a fixed connection or a detachable connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1 to 13 below to describe the utility model provides an unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligence hangar, this unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligence hangar are used for realizing the automatic battery 1 of changing M300 unmanned aerial vehicle, are provided with two batteries 1 in every M300 unmanned aerial vehicle, can change one alone, also can change two simultaneously, the utility model discloses in with changing two as the example introduce. It should be noted that the utility model provides an unmanned aerial vehicle battery replacement equipment and unmanned aerial vehicle intelligence hangar are based on M300 unmanned aerial vehicle's battery compartment structure and battery 1's mounting means and design, and relevant information such as M300 unmanned aerial vehicle's battery compartment structure and battery 1's mounting means all can follow the guan shang official network and obtain, consequently the utility model discloses in not redundant one give unnecessary.
Specifically, as shown in fig. 1 to 13, the unmanned aerial vehicle battery exchange apparatus includes a moving device 3, a battery gripping device 2, and a bin lock rotating device 4. In the present embodiment, the moving device 3 includes an X-axis moving assembly 31, a Y-axis moving assembly 33, and a Z-axis moving assembly 32, the X-axis moving assembly 31 is fixedly mounted on a sidewall of the machine base (not shown in the figure), the Z-axis moving assembly 32 is mounted on the X-axis moving assembly 31, and the Y-axis moving assembly 33 is mounted on the Z-axis moving assembly 32. The Y-axis moving assembly 33 is slidably mounted with the battery gripping device 2 and the bin lock rotating device 4, and the positions of the battery gripping device 2 and the bin lock rotating device 4 are adjusted by driving the X-axis moving assembly 31, the Y-axis moving assembly 33 and the Z-axis moving assembly 32. Of course, in some other embodiments, the connection sequence between the X-axis moving assembly 31, the Y-axis moving assembly 33, and the Z-axis moving assembly 32 may be changed according to actual needs, and in some more specific embodiments, an automatic device such as a mechanical arm may be further adopted to achieve the effects of moving the battery clamping device 2 and the bin lock rotating device 4, and the detailed structure of the moving device 3 is not specifically limited in the present invention. Optionally, in this embodiment, the X-axis moving assembly 31, the Y-axis moving assembly 33, and the Z-axis moving assembly 32 are assembled by using a module (or a lead screw) and a motor, and a drag chain is used to prevent a plurality of power lines and signal lines from being wound or pulled during the moving process to cause a safety hazard.
It should be particularly emphasized that, in the M300 drone, as shown in fig. 5 and 6, two batteries 1 are slidably mounted in a battery compartment, and the battery compartment has a rotating buckle 41, which can form a snap joint by rotating to lock the batteries 1 in the battery compartment, or rotate to avoid the position, so that the two batteries 1 are both in a state of being able to slidably take out the battery compartment (see the relevant structural description and the use instruction of the M300 drone). More specifically, the battery 1 has a first surface 101 and a second surface 102, the first surface 101 and the second surface 102 are perpendicular to the sliding installation direction of the battery 1 in the battery compartment, the second surface 102 and the side wall of the battery compartment are left with a protruding gap, and the first surface 101 can form a snap-fit relationship with the rotating buckle 41.
Referring to fig. 2 and 3, the battery clamping device 2 includes an abutting member 23, a connecting arm 21, a first driving member 22 and a fixing member 24, wherein the abutting member 23 is mounted at one end of the connecting arm 21, and the abutting member 23 is used for abutting against the first surface 101; the other end of the connecting arm 21 is provided with a first driving member 22, the fixing member 24 is connected to the first driving member 22 in a transmission manner, and the fixing member 24 can extend into and leave the extending gap under the driving of the first driving member 22, and further can abut against and separate from the second surface 102, so that the battery 1 has a clamped state in which the battery is clamped and fixed between the fixing member 24 and the abutting member 23, and a free state in which the battery is not clamped and fixed (the free state is only not clamped and fixed, and is not meant that the battery 1 can move freely).
With continued reference to fig. 4 and 8, the bin lock rotator 4 is mounted to the Y-axis moving assembly 33 for locking and unlocking the battery bin of the M300 drone. In this embodiment, as shown in fig. 10, the bin lock rotating device 4 includes a rotating buckle 41 and a second driving element 42, the rotating buckle 41 is connected to the second driving element 42 in a transmission manner, the rotating buckle 41 has a slot, the locking knob 11 of the battery bin can be clamped in the slot, and the rotating buckle 41 can drive the locking knob 11 to rotate in forward and reverse directions (the forward and reverse rotation angles are 360 ° in total) under the driving of the second driving element 42. Of course, in some other embodiments, other structures capable of driving the locking knob 11 to rotate in the forward direction and the reverse direction, such as a crank structure, etc., may also be adopted, and these are also within the scope of the present invention.
In use, for example, after the unmanned aerial vehicle to replace the battery 1 (hereinafter referred to as an old battery) reaches a preset position, the battery clamping device 2 and the bin lock rotating device 4 are moved by the moving device 3, so that the bin lock rotating device 4 is inserted into the locking knob 11 of the battery bin, and the abutting piece 23 of the battery clamping device 2 abuts against the first surface 101. Then, the bin lock rotating device 4 is driven to rotate the locking knob 11 in the forward direction to unlock the battery bin, and at the same time, the fixing member 24 is driven by the first driving member 22 to extend into the extending gap to abut against the second surface 102, so as to clamp and fix the old battery between the fixing member 24 and the abutting member 23. Finally, the moving device 3 drives the old battery, the battery clamping device 2 and the bin lock rotating device 4 to move reversely along the sliding installation direction of the battery 1, so that the old battery is slidingly drawn out of the battery bin, and the taking-out procedure of the old battery is completed.
After the old battery is taken out, the old battery is placed in the old battery placing position by the moving device 3, and after the old battery is placed, the position of the battery clamping device 2 is moved again, and the battery 1 to be mounted (hereinafter, simply referred to as a new battery) is clamped and fixed between the fixing member 24 and the abutting member 23 by the clamping and fixing action of the fixing member 24 and the abutting member 23. After the clamping and fixing are completed, the new battery, the battery clamping device 2 and the bin lock rotating device 4 are moved by the moving device 3 again and move along the sliding installation direction of the battery 1, so that the new battery is slidably installed in the battery bin, then the locking knob 11 is rotated reversely to lock the new battery in the battery bin, and meanwhile, the fixing piece 24 is also separated from the extending gap under the driving of the first driving piece 22. Finally, the battery clamping device 2 and the bin lock rotating device 4 are moved to the position where the takeoff of the unmanned aerial vehicle is not affected through the moving device 3.
Through setting up foretell mobile device 3, storehouse lock rotary device 4 and battery clamp and get device 2, can realize the automatic action of changing battery 1 of M300 unmanned aerial vehicle with the less spare part of quantity, and the cost of manufacture is lower, and the control degree of difficulty is lower, can be used for changing M300 unmanned aerial vehicle's battery 1 conveniently, and use cost is lower.
Optionally, in this embodiment, the first driving element 22 is a steering engine, the fixing element 24 is rectangular, one end of the fixing element 24 is mounted on a swing shaft of the steering engine, and the other end of the fixing element 24 can swing into the above-mentioned extending gap and then abut against the second surface 102 of the battery 1, or swing away from the second surface 102 of the battery 1 and separate from the above-mentioned extending gap under the driving of the steering engine. Illustratively, in this embodiment, the mount 24 is capable of 90 ° oscillation. It should be noted that, in the present invention, the swinging direction may be the swinging of the fixing member 24 along the swinging axis parallel to the second surface 102, or the swinging of the fixing member 24 along the swinging axis perpendicular to the second surface 102 as shown in fig. 3.
Alternatively, in some embodiments, the first driving element 22 may also be a linear motor, and the fixing element 24 is driven to slide along a direction parallel to the second surface 102, so that the fixing element 24 can slide and abut against the second surface 102, or slide and disengage from the second surface 102. It is understood that, in the present invention, the movement mode or the movement direction of the fixing member 24 is not particularly limited as long as the battery 1 can enter the extending gap, be clamped and fixed between the abutting member 23 and the fixing member 24, and be separated from the second surface 102, so that the battery 1 can be separated from the clamped and fixed state.
Further, as shown in fig. 3, the other end of the fixing member 24 is provided with a guide surface. The guiding surface may be an inclined plane (e.g., a flat chamfer) or a curved surface (e.g., a rounded chamfer), and when the fixing member 24 abuts against the second surface 102, the guiding surface guides the fixing member 24 to slide along the second surface 102, so as to prevent the fixing member 24 from directly abutting against the side surface of the battery 1, and causing the fixing member 24 and the first driving member 22 to be jammed.
Alternatively, in this embodiment, as shown in fig. 10, the width of the slot of the rotating buckle 41 gradually increases in a direction from the bottom of the slot to the opening of the slot, forming a bell mouth shape. Similar with foretell guide face is, when the locking button of unmanned aerial vehicle battery compartment was pegged graft to the draw-in groove in, the shape of horn mouth can play the guide effect, can guide locking button to peg graft to the draw-in groove in, prevents the opening part of locking button butt at the draw-in groove, and then leads to unable locking button locking or unblock battery compartment of driving through rotatory buckle 41.
Further, unmanned aerial vehicle battery replacement equipment still includes angle adjusting device 6. As shown in fig. 11 to 13, the angle adjusting device 6 includes a fixed plate 61 and a rotating plate 62, the fixed plate 61 is fixedly mounted on the Y-axis moving assembly 33, the rotating plate 62 is angularly and rotatably connected to the fixed plate 61, and the bin lock rotating device 4 and the battery gripping device 2 are connected to the rotating plate 62. When unmanned aerial vehicle landing angle is skew, when the slip direction that leads to cell 1's slidable mounting direction and Y axle removal subassembly 33 to go up storehouse lock rotary device 4 and battery clamp to get device 2 deviates mutually, can finely tune storehouse lock rotary device 4 and battery clamp through angle adjusting device 6 and get the slip direction of device 2 for even unmanned aerial vehicle landing angle is skew, unmanned aerial vehicle battery replacement equipment still can normally work in order to change battery 1.
Of course, in some other embodiments, the fixing plate 61 can also be installed on the X-axis moving assembly 31 or the Z-axis moving assembly 32, as long as the angular adjustment of the bin lock rotating device 4 and the battery clamping device 2 can be realized, which all fall within the scope of the present invention.
Alternatively, as shown in fig. 13, in the present embodiment, a first thrust bearing 63 is mounted on the fixed plate 61, a second thrust bearing 64 is mounted on the rotating plate 62, and the first thrust bearing 63 and the second thrust bearing 64 are mounted on both ends of a rotating shaft 65, so that the rotating plate 62 and the fixed plate 61 can swing relative to each other about the rotating shaft 65.
Further, still be connected with the spring between fixed plate 61 and the rotor plate 62, can make the sliding direction that device 2 was got to storehouse lock rotary device 4 and battery clamp have the trend that tends to certain angle of presetting, and then make things convenient for the unmanned aerial vehicle descending angle of calculation and make things convenient for the unmanned aerial vehicle battery to change equipment butt joint, reduce the use cost of unmanned aerial vehicle battery change equipment, improve the change efficiency of unmanned aerial vehicle battery change equipment.
Optionally, as shown in fig. 9 and 10, in this embodiment, the battery replacing apparatus for the unmanned aerial vehicle further includes a visual recognition device 5, where the visual recognition device 5 includes a camera, and can recognize the position of the battery 1, and has a real-time observation capability, so that the whole process of replacing the battery 1 is visualized and visualized, and the fine deviation of the positions of the batteries 1 on both sides can be seen very clearly, thereby preventing the normal clamping of the battery 1 on one side, and preventing the battery 1 on the other side from being in a loose and easily-dropped clamping state, so as to ensure the normal replacement of the battery 1.
Optionally, as shown in fig. 7, in the utility model, the battery replacing device for unmanned aerial vehicle further includes a plurality of sensors 7, and the sensors 7 are installed in the above-mentioned X-axis moving assembly 31, Y-axis moving assembly 33 and Z-axis moving assembly 32 for sensing the moving position of each direction moving assembly. Of course, similar sensors 7 can be installed in the magazine lock rotating unit 4 and the battery clamping unit 2 to sense whether the lock button is normally rotated and whether the battery 1 is normally clamped and fixed.
The utility model also provides an unmanned aerial vehicle intelligence hangar, including foretell unmanned aerial vehicle battery change equipment, compare in the current hangar of being applied to multiple unmanned aerial vehicle, simple structure can satisfy the automatic demand of changing battery 1 of M300 unmanned aerial vehicle with lower cost of manufacture and use.
It is obvious that the above embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement or improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
Claims (10)
1. Unmanned aerial vehicle battery replacement equipment for automatic change M300 unmanned aerial vehicle's battery (1), its characterized in that includes:
the bin lock rotating device (4) is used for locking and unlocking a battery bin of the M300 unmanned aerial vehicle;
the battery clamping device (2) comprises an abutting part (23), a connecting arm (21), a first driving part (22) and a fixing part (24), wherein the abutting part (23) is installed at one end of the connecting arm (21), the battery (1) is provided with a first surface (101) and a second surface (102), the first surface (101) and the second surface (102) are perpendicular to the sliding installation direction of the battery (1) in the battery compartment, and the abutting part (23) is used for abutting against the first surface (101); the other end of the connecting arm (21) is provided with the first driving piece (22), the fixing piece (24) is in transmission connection with the first driving piece (22), the fixing piece (24) can be abutted against and separated from the second surface (102) under the driving of the first driving piece (22), so that the battery (1) has a clamped state of being clamped and fixed between the fixing piece (24) and the abutting piece (23) and a free state of not being clamped and fixed;
the battery clamping device comprises a moving device (3), wherein the bin lock rotating device (4) and the battery clamping device (2) are installed on the moving device (3), and the moving device (3) is used for moving and adjusting the positions of the bin lock rotating device (4) and the battery clamping device (2).
2. The unmanned aerial vehicle battery replacement device of claim 1, wherein the first driving member (22) is a steering engine, one end of the fixing member (24) is mounted on a swinging shaft of the steering engine, and the other end of the fixing member can be abutted against and separated from the second surface (102) under the driving of the first driving member (22).
3. The unmanned aerial vehicle battery exchange apparatus of claim 2, wherein the other end of the mount (24) is provided with a guide surface.
4. The unmanned aerial vehicle battery exchange apparatus of claim 1, wherein the bin lock rotating device (4) comprises a rotating buckle (41) and a second driving member (42), the rotating buckle (41) is in transmission connection with the second driving member (42), the rotating buckle (41) is provided with a clamping groove, a locking knob (11) of the battery bin can be clamped in the clamping groove, and the rotating buckle (41) can drive the locking knob (11) to rotate forward and backward under the driving of the second driving member (42).
5. The drone battery exchange device of claim 4, wherein the width of the card slot increases progressively in a direction from the card slot bottom to the card slot opening.
6. The unmanned aerial vehicle battery exchange apparatus of claim 1, wherein the moving device (3) comprises at least an X-axis moving assembly (31), a Y-axis moving assembly (33), and a Z-axis moving assembly (32).
7. The UAV battery exchange apparatus according to claim 6, wherein the moving device (3) further comprises an angle adjusting device (6), the angle adjusting device (6) comprises a fixing plate (61) and a rotating plate (62), the fixing plate (61) is fixedly installed on one of the X-axis moving assembly (31), the Y-axis moving assembly (33) and the Z-axis moving assembly (32), the rotating plate (62) is angularly and rotatably connected to the fixing plate (61), and the cabin lock rotating device (4) and the battery clamping device (2) are connected to the rotating plate (62).
8. Unmanned aerial vehicle battery exchange apparatus of claim 1, further comprising visual recognition means (5), the visual recognition means (5) being for recognizing the position of the battery (1) and guiding the moving means (3).
9. The UAV battery exchange apparatus according to claim 1, further comprising a plurality of sensors (7), wherein the plurality of sensors (7) are mounted to at least one of the bin lock rotating device (4), the battery clamping device (2) and the moving device (3).
10. Unmanned aerial vehicle intelligent hangar, characterized in that, includes unmanned aerial vehicle battery change equipment of any one of claims 1-9.
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN117103236A (en) * | 2023-10-19 | 2023-11-24 | 北京云圣智能科技有限责任公司 | Cylindrical coordinate robot and aircraft hangar |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN117103236A (en) * | 2023-10-19 | 2023-11-24 | 北京云圣智能科技有限责任公司 | Cylindrical coordinate robot and aircraft hangar |
CN117103236B (en) * | 2023-10-19 | 2024-01-23 | 北京云圣智能科技有限责任公司 | Cylindrical coordinate robot and aircraft hangar |
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