CN222202935U - Battery and unmanned aerial vehicle - Google Patents

Battery and unmanned aerial vehicle Download PDF

Info

Publication number
CN222202935U
CN222202935U CN202421685489.6U CN202421685489U CN222202935U CN 222202935 U CN222202935 U CN 222202935U CN 202421685489 U CN202421685489 U CN 202421685489U CN 222202935 U CN222202935 U CN 222202935U
Authority
CN
China
Prior art keywords
battery
unmanned aerial
aerial vehicle
limiting
drone
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202421685489.6U
Other languages
Chinese (zh)
Inventor
刘利
包秀媛
杨睿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhongke Tancarbon Beijing Technology Co ltd
Original Assignee
Zhongke Tancarbon Beijing Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhongke Tancarbon Beijing Technology Co ltd filed Critical Zhongke Tancarbon Beijing Technology Co ltd
Priority to CN202421685489.6U priority Critical patent/CN222202935U/en
Application granted granted Critical
Publication of CN222202935U publication Critical patent/CN222202935U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Forklifts And Lifting Vehicles (AREA)

Abstract

The utility model provides a battery and an unmanned aerial vehicle, belongs to the technical field of unmanned aerial vehicles, and is used for solving the problems that in the prior art, the battery of the unmanned aerial vehicle is not detachable or the disassembling process is complex. Wherein the battery includes golden finger and limit structure, and the battery head end bottom is located to the golden finger, and limit structure includes first limit structure and second limit structure, and battery head end both sides are located to first limit structure, and first limit structure is the spacing hole of indent, and battery tail end both sides are located to second limit structure, and second limit structure is convex spacing. The unmanned aerial vehicle includes above battery, and unmanned aerial vehicle's body top is provided with the cavity, and the shape and the battery of cavity match, and the cavity has the electric connection end that matches with battery golden finger, and the cavity side has the recess that matches with the spacing of battery, and the cavity side still has the spacing post that can insert or extract the spacing hole of battery. The combination of battery and unmanned aerial vehicle has the characteristics of easy dismounting, convenient change.

Description

Battery and unmanned aerial vehicle
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a battery and an unmanned aerial vehicle.
Background
Along with the rapid development of unmanned aerial vehicle technology, unmanned aerial vehicle is more and more widely applied in each field, especially in tasks such as field data acquisition, environmental monitoring, resource investigation, unmanned aerial vehicle has played irreplaceable effect by virtue of its high-efficient, nimble characteristic. However, unmanned aerial vehicles often face power limiting challenges in performing these tasks. Because the existing unmanned aerial vehicle battery adopts the complicated design of the undetachable connection or the detaching process, the unmanned aerial vehicle can not be quickly and effectively replaced when the electric quantity is exhausted, and the operation time and the efficiency of the unmanned aerial vehicle are greatly limited.
In particular, existing unmanned aerial vehicle battery designs typically tightly secure the battery to the unmanned aerial vehicle body to form a non-detachable connection. Although the design improves the structural compactness and stability of the unmanned aerial vehicle, great inconvenience is brought to the battery replacement. Once the unmanned aerial vehicle is exhausted, specialized tools are required for disassembly and replacement, which is time consuming and labor intensive, as well as increasing maintenance costs.
Therefore, existing unmanned aerial vehicle battery designs fail to meet the needs of automated battery replacement. This limitation is particularly acute in situations where large-scale cluster measurements and the like require a large number of unmanned aerial vehicles to work in concert. Frequent manual replacement of the battery not only reduces the working efficiency, but also increases the safety risk.
Disclosure of utility model
In view of the above-mentioned drawbacks of the prior art, an object of the present utility model is to provide a battery and an unmanned aerial vehicle, which are used for solving the problems of the prior art that the battery of the unmanned aerial vehicle is not detachable or the disassembly process is complex.
To achieve the above and other related objects, the present utility model provides a battery and a unmanned aerial vehicle.
The battery comprises a golden finger and a limiting structure, wherein the golden finger is arranged at the bottom of the battery head end, the limiting structure comprises a first limiting structure and a second limiting structure, the first limiting structure is arranged at two sides of the battery head end, the first limiting structure is a concave limiting hole, the second limiting structure is arranged at two sides of the battery tail end, and the second limiting structure is a convex limiting strip.
Optionally, a concave cavity is formed in the top of the tail end of the battery, and a grabbing shaft is arranged in the concave cavity.
The unmanned aerial vehicle comprises the battery, wherein the top of the unmanned aerial vehicle body is provided with a concave cavity, the shape of the concave cavity is matched with that of the battery, the concave cavity is provided with an electric connection end matched with a golden finger of the battery, the side surface of the concave cavity is provided with a groove matched with a limit battery strip, and the side surface of the concave cavity is also provided with a limit column capable of being inserted into or pulled out of a limit battery hole.
Optionally, the limit post is controlled by a telescopic mechanism disposed within the unmanned aerial vehicle body.
Optionally, the spacing post side direction runs through the unmanned aerial vehicle body, through screw-thread fit between spacing post and the unmanned aerial vehicle body.
Optionally, the portion of the spacing post that exceeds the unmanned aerial vehicle body is smooth cylindrical, and the tip has key indent cross-section.
Optionally, a portion of the spacing post beyond the unmanned aerial vehicle body is a key-shaped cross section.
Optionally, battery and unmanned aerial vehicle's side contact department, spacing hole and spacing post are provided with two sets of mutually, and are located same level.
Optionally, a protruding guide table is arranged between the two limiting columns on the side of the unmanned aerial vehicle, and the width of the guide table is gradually reduced from high to low.
Optionally, an environment detection device is mounted on the bottom of the unmanned aerial vehicle.
As described above, the battery and the unmanned aerial vehicle provided by the utility model have at least the following beneficial effects:
The unmanned aerial vehicle battery is convenient and quick to detach, and the connection mode of the unmanned aerial vehicle battery and the machine body is greatly simplified by adopting the novel design, so that the battery detachment process becomes extremely convenient and quick, the battery replacement can be completed quickly, complicated manual operation is not needed, and the operation efficiency is greatly improved. This also makes this battery and unmanned aerial vehicle's combination can be applicable to the scene of automatic change battery, and the complexity of corollary equipment is also lower.
Drawings
Fig. 1 shows a schematic view of a battery according to the present utility model.
Fig. 2 shows a schematic view of the back of the unmanned aerial vehicle according to the present utility model.
Fig. 3 is an enlarged view of a portion of fig. 2 at a in accordance with the present utility model.
Fig. 4 shows an overall schematic of the unmanned aerial vehicle of the present utility model.
Fig. 5 is an enlarged view of a portion of fig. 4 at B in accordance with the present utility model.
Fig. 6 shows a schematic bottom view of the unmanned aerial vehicle of the present utility model.
Fig. 7 is a schematic view showing a parking state of the present utility model.
Fig. 8 is an enlarged view of a portion of fig. 7 at C in accordance with the present utility model.
The environment detection device comprises a golden finger 20, a limiting hole 21, a limiting strip 22, a grabbing shaft 23, an electric connection end 10, a groove 11, a limiting column 202, a key-shaped section 203, a guide table 204 and an environment detection device 5.
Detailed Description
Further advantages and effects of the present utility model will become apparent to those skilled in the art from the disclosure of the present utility model, which is described by the following specific examples.
Please refer to fig. 1 to 8. It should be understood that the structures, proportions, sizes, etc. shown in the drawings are for illustration purposes only and should not be construed as limiting the utility model to the extent that it can be practiced, since modifications, changes in the proportions, or adjustments of the sizes, which are otherwise, used in the practice of the utility model, are included in the spirit and scope of the utility model which is otherwise, without departing from the spirit or scope thereof. Also, the terms such as "upper," "lower," "left," "right," "middle," and "a" and the like recited in the present specification are merely for descriptive purposes and are not intended to limit the scope of the utility model, but are intended to provide relative positional changes or modifications without materially altering the technical context in which the utility model may be practiced.
The following examples are given by way of illustration only. Various embodiments may be combined and are not limited to only what is presented in the following single embodiment.
Referring to fig. 1, the embodiment of a battery provided by the present utility model includes a gold finger 20 and a limiting structure, wherein the gold finger 20 is disposed at the bottom of the battery head end, the limiting structure includes a first limiting structure and a second limiting structure, the first limiting structure is disposed at two sides of the battery head end, the first limiting structure is a concave limiting hole 21, the second limiting structure is disposed at two sides of the battery tail end, and the second limiting structure is a convex limiting strip 22.
The golden finger 20 is used for realizing the electric connection with the unmanned aerial vehicle or the charger, and consists of a plurality of conductive contact pieces, and the surface of the golden finger can be plated with gold to realize oxidation resistance and improve conductivity, so that the battery replacement process is not easy to wear, and the stability of power supply and signal transmission is ensured. After the limit bar 22 is matched with a groove on the unmanned aerial vehicle, the battery can only slide along the limit bar 22, so that the unmanned aerial vehicle body is pulled out of the battery, or the battery is pushed into the unmanned aerial vehicle body, the angle of the battery in the unmanned aerial vehicle is unique in the mode, and therefore the connection mode of the golden finger 20 of the battery to the electrode joint of the unmanned aerial vehicle or the charger can be carried out according to the expected angle, and the effect that the battery can only be plugged in and pulled out from a single direction is achieved. Once the battery is inserted into the unmanned aerial vehicle, the limiting structure in the unmanned aerial vehicle body is inserted into the limiting hole 21, and then the battery can be thoroughly fixed on the unmanned aerial vehicle body. When the battery needs to be taken out, the limiting structure in the unmanned aerial vehicle body is withdrawn from the limiting hole 21 of the battery, and then the battery can be pulled out, but only along the direction of the limiting strip 22, so that the golden finger is prevented from being damaged in the unexpected pulling-out direction. The scheme of the embodiment has the characteristics of reliable limit, simple disassembly and unique battery disassembly and assembly angles, and the stability of the battery structure and electrical connection is obviously improved.
Further, a concave cavity is arranged at the top of the tail end of the battery, and a grabbing shaft 23 is arranged in the concave cavity. The grabbing shaft 23 is used for conveniently grabbing and clamping the battery by the battery replacement machine, and automatic battery replacement is conveniently achieved. The gripping shaft 23 may be made of metal that can be attracted by a magnet, and the clamping mechanism may use a magnetic attraction manner to simplify the structure of the clamping jaw. The snatch axle 23 sets up at the tail end, conveniently pulls out the battery from the unmanned aerial vehicle, perhaps pushes the battery into the unmanned aerial vehicle body.
Referring to fig. 2, an embodiment of an unmanned aerial vehicle is matched with the battery, a concave cavity is arranged at the top of the unmanned aerial vehicle body, the shape of the concave cavity is matched with the battery, an electric connection end 10 matched with a battery golden finger 20 is arranged in the concave cavity, a groove 11 matched with a battery limit bar 22 is arranged on the side surface of the concave cavity, and a limit post 202 capable of being inserted into or pulled out of a battery limit hole 21 is arranged on the side surface of the concave cavity.
During the implementation, battery and unmanned aerial vehicle contact position, especially the top of golden finger can also set up the sealing strip, after the battery pushes into the unmanned aerial vehicle body, compress tightly the sealing strip voluntarily to prevent when unmanned aerial vehicle is in aerial operation, the aqueous vapor accumulation gets into golden finger department. The combination of the unmanned aerial vehicle and the battery has the characteristics of reliable battery fixation and convenient disassembly and assembly, and is particularly suitable for the scene of automatic battery replacement.
Further, the stopper post 202 is controlled by a telescopic mechanism provided in the unmanned aerial vehicle body. When the battery is required to be replaced, the limiting column 202 is retracted from the limiting hole 21 of the battery, and the battery can be pulled out along the limiting strip 22 at the moment, so that the unlocking process is simpler and the operation is convenient. When the full-power battery is installed, the telescopic mechanism controls the limit post 202 to extend out, so that the full-power battery is inserted into the limit hole 21 of the battery to fix the battery.
As an alternative, the spacing post 202 laterally penetrates the unmanned aerial vehicle body, and the spacing post 202 is in threaded engagement with the unmanned aerial vehicle body. The limiting column 202 is located at the outer end portion of the unmanned aerial vehicle body through screwing, and the limiting column 202 can move along the axis of the unmanned aerial vehicle body, so that the battery can be locked or unlocked through inserting or extracting the battery into the limiting hole 21. In this way, the locked or unlocked state can be manually controlled, and when the unmanned aerial vehicle has no electricity or no unmanned aerial vehicle controller (remote controller), the battery can be manually unlocked or locked by a simple tool for battery replacement.
In this embodiment, the portion of the spacing post 202 beyond the unmanned aerial vehicle body is smooth and cylindrical, and the end portion has a key-shaped concave section. The smooth cylindrical shape makes the post 202 difficult to manually screw, while the keyed concave cross-section requires a specially matched screwdriver to screw, which ensures that the battery can be removed only when a special tool is needed or is present.
In this embodiment, the portion of the spacing post 202 beyond the unmanned aerial vehicle body is a key-shaped cross section 203. The scheme can also screw the limit post 202 to realize the loosening or fixing of the battery on the premise of no special tool, and has great convenience in certain scenes.
In this embodiment, referring to fig. 3-8, two sets of limiting holes 21 and limiting posts 202 are disposed adjacent to each other at the contact position between the battery and the unmanned aerial vehicle, and are located at the same level, and are located at two sides of the unmanned aerial vehicle and the battery, respectively.
This unmanned aerial vehicle and battery's collocation is applicable to unmanned aerial vehicle and changes the scene of battery automatically, and the lower part is for shutting down the platform in fig. 7, and unmanned aerial vehicle is stopped at the platform in-process of shutting down, is fixed a position by shutting down the platform to unmanned aerial vehicle to the machinery that conveniently trades the battery is taken or is installed the battery. The stopping platform is provided with a notch structure corresponding to the limiting columns 202, as shown in fig. 8, after the unmanned aerial vehicle is stopped, the limiting columns 202 on two sides of the unmanned aerial vehicle enter the notch 202A of the stopping platform, a sleeve part 361 with an opening on the upper side is originally arranged in the notch, the sleeve part 361 is connected with a rotating power source through a shaft rod, and the sleeve part 361 and the rotating power source are both arranged on the stopping platform.
When the unmanned aerial vehicle stops into the parking platform, the spacing posts 202 on two sides of the unmanned aerial vehicle just enter the external member 361, and when the external member 361 rotates, the spacing posts 202 can be driven to rotate, so that the spacing posts 202 are inserted into the spacing holes 21 of the battery or pulled out from the battery, and the battery is locked or loosened. If the unmanned aerial vehicle needs to be fixed on the shutdown platform, the opening at the original upper part when the sleeve member 361 stops rotating is not upward any more, namely the sleeve member 361 covers the limit posts 202 on two sides of the unmanned aerial vehicle, so that the unmanned aerial vehicle is fixedly connected with the shutdown platform.
In this embodiment, referring to fig. 7 and 8, a protruding guide table 204 is disposed between two limiting posts 202 on the side of the unmanned aerial vehicle, and the width of the guide table 204 gradually decreases from high to low. The structure 204A matched with the unmanned aerial vehicle is arranged on the stopping platform, and the function of the guiding table 204 and the structure 204A matched with the guiding table is utilized in the unmanned aerial vehicle stopping process, so that the unmanned aerial vehicle stopping process can be automatically positioned and centered, the accurate position after stopping is ensured, and the subsequent battery replacement process is facilitated.
As shown in fig. 6, the unmanned aerial vehicle is loaded with an environment detection device 5 at the bottom. The number, the model and the like of the environment detection devices 5 can be changed and set according to the requirements during actual detection, so that the environment detection device is suitable for various environment detection scenes.
In summary, the utility model effectively overcomes various disadvantages in the prior art, can produce beneficial technical effects, and has remarkable progress.
The above embodiments are merely illustrative of the principles of the present utility model and its effectiveness, and are not intended to limit the utility model. Modifications and variations may be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the utility model. Accordingly, it is intended that all equivalent modifications and variations of the utility model be covered by the claims, which are within the ordinary skill of the art, be within the spirit and scope of the present disclosure.

Claims (10)

1.一种电池,其特征在于,包括金手指(20)和限位结构,所述金手指(20)设于电池头端底部,所述限位结构包括第一限位结构和第二限位结构,所述第一限位结构设于所述电池头端两侧,所述第一限位结构为内凹的限位孔(21),所述第二限位结构设于所述电池尾端两侧,所述第二限位结构为凸出的限位条(22)。1. A battery, characterized in that it comprises a gold finger (20) and a limiting structure, wherein the gold finger (20) is arranged at the bottom of the battery head end, and the limiting structure comprises a first limiting structure and a second limiting structure, wherein the first limiting structure is arranged at both sides of the battery head end, and the first limiting structure is a concave limiting hole (21), and the second limiting structure is arranged at both sides of the battery tail end, and the second limiting structure is a protruding limiting strip (22). 2.如权利要求1所述的一种电池,其特征在于,所述电池尾端顶部设有一凹腔,所述凹腔中设有一根抓取轴(23)。2. A battery as claimed in claim 1, characterized in that a cavity is provided at the top of the rear end of the battery, and a grabbing shaft (23) is provided in the cavity. 3.一种无人机,其特征在于,包括如权利要求1或2所述的电池,所述无人机的本体顶部设置有凹腔,所述凹腔的形状与所述电池匹配,所述凹腔有与所述电池金手指(20)匹配的电连接端(10),所述凹腔侧面有与所述电池限位条(22)匹配的凹槽(11),所述凹腔侧面还有能够插入或拔出所述电池限位孔(21)的限位柱(202)。3. A drone, characterized in that it comprises a battery as claimed in claim 1 or 2, a concave cavity is arranged on the top of the drone body, the shape of the concave cavity matches the battery, the concave cavity has an electrical connection end (10) matching the battery gold finger (20), the side of the concave cavity has a groove (11) matching the battery limit strip (22), and the side of the concave cavity also has a limit column (202) capable of being inserted into or removed from the battery limit hole (21). 4.如权利要求3所述的无人机,其特征在于,所述限位柱(202)由设置于无人机本体内的伸缩机构控制。4. The drone according to claim 3, characterized in that the limiting column (202) is controlled by a telescopic mechanism arranged in the drone body. 5.如权利要求3所述的无人机,其特征在于,所述限位柱(202)侧向贯穿所述无人机本体,所述限位柱(202)与无人机本体之间通过螺纹配合。5. The drone according to claim 3, characterized in that the limiting column (202) laterally penetrates the drone body, and the limiting column (202) and the drone body are engaged with each other through threads. 6.如权利要求5所述的无人机,其特征在于,所述限位柱(202)超出所述无人机本体的部分为光滑的圆柱形,端部有键形内凹截面。6. The drone according to claim 5, characterized in that the portion of the limiting column (202) that exceeds the drone body is smooth cylindrical, and the end portion has a key-shaped concave cross-section. 7.如权利要求5所述的无人机,其特征在于,所述限位柱(202)超出所述无人机本体的部分为键形截面(203)。7. The drone according to claim 5, characterized in that the portion of the limiting column (202) that extends beyond the drone body is a key-shaped cross-section (203). 8.如权利要求3所述的无人机,其特征在于,所述电池和无人机的侧面接触处,所述限位孔(21)和限位柱(202)相临设置有两组,且位于同一水平高度。8. The drone according to claim 3, characterized in that, at the contact point between the battery and the side of the drone, two groups of the limiting holes (21) and the limiting columns (202) are arranged adjacent to each other and are located at the same level. 9.如权利要求8所述的无人机,其特征在于,所述无人机侧面,两个所述限位柱(202)中间设有一个凸出的导向台(204),所述导向台(204)的宽度由高到低逐渐减小。9. The drone according to claim 8, characterized in that a protruding guide platform (204) is provided between the two limiting pillars (202) on the side of the drone, and the width of the guide platform (204) gradually decreases from high to low. 10.如权利要求3-9任一项所述的无人机,其特征在于,所述无人机底部挂载有环境探测装置(5)。10. The drone according to any one of claims 3 to 9, characterized in that an environment detection device (5) is mounted on the bottom of the drone.
CN202421685489.6U 2024-07-17 2024-07-17 Battery and unmanned aerial vehicle Active CN222202935U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202421685489.6U CN222202935U (en) 2024-07-17 2024-07-17 Battery and unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202421685489.6U CN222202935U (en) 2024-07-17 2024-07-17 Battery and unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN222202935U true CN222202935U (en) 2024-12-20

Family

ID=93870750

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202421685489.6U Active CN222202935U (en) 2024-07-17 2024-07-17 Battery and unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN222202935U (en)

Similar Documents

Publication Publication Date Title
EP4190495B1 (en) Apparatus for automatically disassembling power battery module
CN211219492U (en) Pin pulling device
CN118578330B (en) Quick assembly disassembly structure of cotter pin
CN222202935U (en) Battery and unmanned aerial vehicle
CN103567960B (en) Pin pulling device
CN217345260U (en) Positioning tool for assembling output shaft and flange
CN210732340U (en) Broken bolt taking-out device
CN211249850U (en) Unmanned aerial vehicle wheel split pin extractor
CN214754646U (en) Equipment for plugging and pulling line plug
CN204216248U (en) The universal bus grounding device of switch cubicle
CN222726604U (en) Eccentric bolt dismantling tool
CN108582666A (en) A kind of injection mold lock module
CN201895298U (en) Device for disassembling and assembling electric spindle clamping jaw
CN202534928U (en) Needle withdrawing device for connector thrusting needle
CN201249433Y (en) Universal pin removal
CN209273308U (en) An energy-saving disc wrench device for the rotor of the coupling of the air compressor
CN219054195U (en) Frock is dismantled to hollow round pin axle
CN223428025U (en) A quick-connect insulated operating rod
CN207683037U (en) Pressure head quick replacement device
CN220560114U (en) Straightening wheel puller
CN220755156U (en) Accurate split equipment PCB board tool
CN211029777U (en) Labor-saving wrench
CN222877437U (en) Wire rope inserts rope device
CN221447683U (en) Quick connecting device for electric engineering line
CN206690006U (en) A kind of gear maintenance frock

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant