CN113879548A - Unmanned aerial vehicle capable of rapidly disassembling and assembling battery - Google Patents

Unmanned aerial vehicle capable of rapidly disassembling and assembling battery Download PDF

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Publication number
CN113879548A
CN113879548A CN202111297822.7A CN202111297822A CN113879548A CN 113879548 A CN113879548 A CN 113879548A CN 202111297822 A CN202111297822 A CN 202111297822A CN 113879548 A CN113879548 A CN 113879548A
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CN
China
Prior art keywords
hole
buckle
section
plate
battery
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Pending
Application number
CN202111297822.7A
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Chinese (zh)
Inventor
程启平
张凌威
李飞
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Huizhou Yifei Intelligent Technology Co ltd
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Huizhou Yifei Intelligent Technology Co ltd
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Publication date
Application filed by Huizhou Yifei Intelligent Technology Co ltd filed Critical Huizhou Yifei Intelligent Technology Co ltd
Publication of CN113879548A publication Critical patent/CN113879548A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/80Exchanging energy storage elements, e.g. removable batteries
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Battery Mounting, Suspending (AREA)

Abstract

The invention relates to an unmanned aerial vehicle capable of quickly disassembling and assembling a battery, which comprises a machine body and a battery, wherein the battery is arranged on a movable part, the movable part is arranged at the bottom of the machine body, the front end of the movable part protrudes out to form a clamping part, and two sides of the clamping part extend outwards to form side protrusions; the buckle structure is arranged at the bottom of the machine body and comprises a buckle body and two buckle plates, wherein the middle position of each buckle plate is provided with an installation hole and is installed on the buckle body through a torsion spring, and the two buckle plates are adjacently arranged and form a sliding channel; the end part of the buckle plate close to the buckle body is provided with a buckle part; after the movable piece slides into the buckle body along the sliding channel, the side protrusions and the buckle parts form interference, so that the movable piece is fixed on the buckle structure. The invention has the advantages of rapid and convenient installation and disassembly modes, less steps and improved efficiency.

Description

Unmanned aerial vehicle capable of rapidly disassembling and assembling battery
Technical Field
The invention relates to an unmanned aerial vehicle, in particular to an unmanned aerial vehicle with a battery capable of being rapidly disassembled and assembled.
Background
Among the current unmanned aerial vehicle, generally adopt the battery to provide the electric energy, rotate through the motor and drive the screw and rotate for unmanned aerial vehicle can be in the quick flight in the air. The battery of the existing unmanned aerial vehicle is generally bound to the body through a binding band, and when the battery needs to be replaced, the battery needs to be disassembled or assembled in a relatively complicated mode, so that the battery is replaced with low efficiency and long time.
Disclosure of Invention
Based on this, it is necessary to provide a but unmanned aerial vehicle of quick dismantlement installation battery to the problem that battery change inefficiency, camera do not have safeguard measure.
Unmanned aerial vehicle capable of rapidly disassembling and assembling battery comprises a body, a battery and
the battery is arranged on the movable piece, the movable piece is arranged at the bottom of the machine body, the front end of the movable piece protrudes to form a clamping part, and two sides of the clamping part extend outwards to form side protrusions;
the buckle structure is arranged at the bottom of the machine body and comprises a buckle body and two buckle plates, wherein the middle position of each buckle plate is provided with an installation hole and is installed on the buckle body through a torsion spring, and the two buckle plates are adjacently arranged and form a sliding channel;
the end part of the buckle plate close to the buckle body is provided with a buckle part;
after the movable piece slides into the buckle body along the sliding channel, the side protrusions and the buckle parts form interference, so that the movable piece is fixed on the buckle structure.
In one embodiment, when the movable member is fixed to the fastening structure, the fastening plate abuts against the side wall of the fastening portion.
In one embodiment, a rotating channel is arranged on the buckle body, and the buckle part rotates along the rotating channel.
In one embodiment, a handle portion is disposed on the latch plate at a position away from the latch body.
In one embodiment, the mobile part further comprises a support structure, wherein the support structure comprises an opening arranged on the mobile part and a support part fixed on the machine body;
one end of the supporting piece is fixed on the machine body, the other end of the supporting piece extends along the peripheral side to form a supporting plate, and a gap is formed between the machine body and the supporting plate;
the opening hole is provided with two sections, namely a first section hole and a second section hole, wherein the first section hole is communicated with the second section hole, the width of the first section hole is larger than that of the second section hole, and the width of the support plate is between the width of the first section hole and that of the second section hole;
when the movable piece is inserted into the buckle structure, the support piece moves from the first section of hole to the second section of hole relatively, and the movable piece is fixed on the second section of hole stably.
In one embodiment, the first section of hole is a round hole, and the second section of hole is a square hole.
In one embodiment, the aperture of the round hole is larger than the width of the square hole.
In one embodiment, the support plate is a circular structure or a plate-like structure.
In one embodiment, the camera further comprises a camera head and a mounting assembly for mounting the camera head, wherein the mounting assembly comprises a first fixing piece and a protection plate, the protection plate is fixed on the machine body, and the first fixing piece is located between the protection plate and the camera head; the first fixing piece is provided with a first arc-shaped hole and a second arc-shaped hole, a first through hole is formed in the first fixing piece corresponding to the first arc-shaped hole, and a second through hole is formed in the first fixing piece corresponding to the second arc-shaped hole; adopt a screw to pass first through-hole from first arc hole and fix to on the camera, adopt another screw to pass the second through-hole from second arc hole and fix to on the camera, the interval between two screws is unchangeable.
In one embodiment, the propeller structure further comprises a plurality of propellers, and a protective cover is arranged on the periphery of each propeller.
The battery can be quickly installed or disassembled to play a role in quickly replacing the battery, the battery is installed on the moving part, the moving part can be fixed on the buckle structure only by aligning the first section of the hole with the support part to push upwards and then push laterally, the moving part is matched with the support and stabilization effect of the support part, the moving part can be stably installed on the machine body, the whole installation and disassembly mode is quick and convenient, the steps are few, and the efficiency is improved.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an overall exploded view of the present invention;
FIG. 3 is a schematic structural view of the movable member of the present invention;
FIG. 4 is a schematic structural view of the snap structure of the present invention;
FIG. 5 is a schematic view of the movable member and snap structure of the present invention prior to assembly
FIG. 6 is a schematic view of the movable member and the snap structure of the present invention after assembly;
FIG. 7 is a schematic view of the structure of the support member of the present invention;
FIG. 8 is another exploded view of the present invention in its entirety;
fig. 9 is an exploded view of the mounting assembly and camera head of the present invention.
Reference numerals: the camera module comprises a body 10, a battery 11, a camera 12, a mounting assembly 130, a first fixing member 131, a protection plate 132, a first arc-shaped hole 133, a second arc-shaped hole 134, a first through hole 135, a second through hole 136, a second fixing member 137, a third fixing member 138, a propeller 14, a protective cover 15, a movable member 20, a clamping portion 21, a side protrusion 22, an opening 24, a clamping structure 30, a clamping body 31, a sliding channel 311, a rotating channel 312, a clamping plate 32, a clamping portion 321, a mounting hole 322, a handle portion 323, a support member 40, a support plate 41, a first section hole 241 and a second section hole 242.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses.
Techniques and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail, but are intended to be considered a part of the specification where appropriate.
In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.
The invention relates to an unmanned aerial vehicle, in particular to an unmanned aerial vehicle capable of rapidly disassembling and assembling a battery, and avoiding troubles of battery assembly and disassembly.
Referring to fig. 1 and 2, the unmanned aerial vehicle comprises a body 10 and a battery 11, wherein the battery 11 needs to be installed on the body 10 so as to supply power to the whole unmanned aerial vehicle.
Referring to fig. 3-6, the battery module includes a movable member 20 and a latch structure 30, wherein the battery 11 is mounted on the latch structure 30, the movable member 20 is mounted at the bottom of the body 10, and the battery 11 is mounted on the body 10 by the cooperation of the movable member 20 and the latch structure 30.
Specifically, the battery 11 is installed on a movable member, the movable member 20 is disposed at the bottom of the body 10, a front end of the movable member 20 protrudes to form a clamping portion 21, and two sides of the clamping portion 21 extend outward to form side protrusions 22.
The buckle structure 30 is arranged at the bottom of the machine body 10 and comprises a buckle body 31 and two buckle plate pieces 32, the two buckle plate pieces 32 are adjacently arranged and form a sliding channel 311, and the middle position of each buckle plate piece is provided with an installation hole 322 and is installed on the buckle body through a torsion spring;
the snap plate comprises a snap part 321, and the side protrusion 22 and the snap part 321 form interference;
the movable element 20 slides into the buckle body 31 along the sliding channel 311, and is fixed on the buckle structure 30 by the interference of the side protrusion 22 and the buckle part 321.
It is understood that the movable member 20 is embodied as a plate-like structure, and the battery 11 can be fixed to the movable member 20. At the front end of the moving element 20, that is, at the position matching with the buckle structure 30, there are two side protrusions 22 formed by extending the two sides of the buckle portion 21 outwards, and two side protrusions 22 are provided and respectively provided at the two sides of the buckle portion 21, and can be integrally provided with the buckle portion 21, and the buckle portion 21 can be inserted into the buckle structure 30, so as to fix the moving element 20 on the buckle structure 30.
The buckle structure 30 includes a buckle body 31 and two buckle plates 32, wherein a mounting hole 322 is disposed in the middle of the buckle plate 32, the buckle plate 32 is movably disposed on the buckle body 31 through a torsion spring, the buckle plate 32 is rotatable, a buckling portion 321 is disposed at an end of the buckle plate 32, and the buckling portion 321 is close to the buckle body 31. Meanwhile, two catch plates 32 are adjacently disposed, thereby forming a slide passage 311. Since the two buckling plates 32 are provided, the distance between the two buckling parts 321 can be movably adjusted by the torsion spring. Therefore, when the movable element 20 slides along the sliding channel 311, the side protrusion 22 can open the distance between the two fastening portions 321, so as to slide into the fastening body 31, and due to the arrangement of the torsion spring, the fastening plate 32 will be reset and reset to abut against the fastening portion 21, and at this time, the side protrusion 22 and the fastening portion 321 form interference, so as to fix the movable element 20 on the fastening structure 30.
When the battery needs to be installed, the battery only needs to be fixed to the movable member 20, and the movable member 20 slides along the sliding channel 311, so that the battery can slide into the buckle body 31 and then be fixed on the buckle structure 30. The specific fixing principle is as follows: the side protrusion 22 expands the distance between the two fastening parts 321 to smoothly slide into the fastening body 31, and due to the torsion spring, the fastening plate 32 is reset to abut against the fastening part 21, and at this time, the side protrusion 22 interferes with the fastening part 321, so that the movable member 20 can be fixed on the fastening structure 30.
When the battery needs to be disassembled, the movable member 20 can be disassembled from the snap structure 30 only by holding the handle portion 323 and increasing the distance between the two snap portions 321.
The whole disassembly and assembly structure is simple, batteries are efficiently replaced, the replacement of the batteries is quickly realized, and the battery replacement time is saved.
In the present embodiment, when the movable element 20 is fixed to the fastening structure 30, the fastening plate 32 abuts against the sidewall of the fastening portion 21.
The torsion spring has a certain elasticity, and after the side protrusion 22 expands the two buckling parts 321, the torsion spring will return to the original position, and the buckling plate 32 will abut against the side wall of the buckling part 21, so as to enhance the interference effect between the side protrusion 22 and the buckling part 321. In addition, the sliding channel 311 is a trapezoid structure, and the shape of the clamping portion 21 is consistent with that of the sliding channel 311. It can be understood that the whole sliding channel 311 is a trapezoidal structure, when the moving part 20 is fixed on the buckle structure 30, the shape of the clamping portion 21 is consistent with that of the sliding channel 311, the length of the side wall of the clamping portion 21 abutted against the buckle plate 32 is increased, the buckle structure 30 is not easy to shake, and the stability of the moving part 20 when being fixed with the buckle structure 30 is improved.
In this embodiment, the buckle body is provided with a rotating channel 312, and the buckling portion 321 rotates along the rotating channel 312.
After the side protrusions 22 open the two locking parts 321, the locking parts 321 rotate around the mounting hole 322, and in order to avoid interference when the locking parts 321 rotate, a rotation channel 312 is disposed on a rotation path of the locking parts 321, so that the locking parts 321 can rotate smoothly, and the assembly and disassembly of the movable element 20 and the locking structure 30 are completed.
In the present embodiment, the catch plate 32 is provided with a handle portion 323 at a position away from the catch body 31. The position of the mounting hole 322 of the latch plate 32 is used as a fulcrum, the latch portion 321 is disposed at one end close to the latch body 31, and the handle portions 323 are disposed at the other end away from the latch body 31, so that when the battery needs to be detached, only two handle portions 323 need to be pulled, and the movable member 20 can be detached from the latch structure 30.
Referring to fig. 5-7, the present embodiment further includes a support structure, which includes an opening 24 disposed on the movable member 20 and a support member 40 fixed to the body 10; the opening 24 is provided with two sections, namely a first section hole 241 and a second section hole 242, wherein the width of the first section hole 241 is greater than the width of the second section hole 242, one end of the support member 40 is fixed on the fuselage 10, the other end extends along the peripheral side to form a support plate 41, and a gap is formed between the fuselage 10 and the support plate 41; the width of the supporting plate 41 is between the width of the first section hole 241 and the width of the second section hole 242; when the movable member 20 is inserted into the snap structure 30, the support member 40 moves relatively from the first section of the hole 241 to the second section of the hole 242, and the movable member 20 is fixed on the second section of the hole 242.
After the movable member 20 is assembled with the fastening structure 30, the movable member 20 has only one fixing point, so as to better fix the movable member 20 on the machine body 10 stably, and further includes a supporting structure, the supporting structure can be disposed on the other side opposite to the fastening structure 30, and can also be disposed on the two sides or the tail of the movable member 20, when the movable member 20 is installed on the machine body 10, there can be at least two fixing points, preferably three fixing points, so that the movable member 20 is installed more stably.
Wherein, be fixed with support piece 40 on fuselage 10, support piece 40's one end is fixed on fuselage 10, and the other end that keeps away from fuselage 10 extends along week side and forms backup pad 41 to, form the space between fuselage 10 and the backup pad 41, this space forms a fixed position, blocks the moving part 20 between fuselage 10 and backup pad 41, can install moving part 20 on fuselage 10.
The opening 24 is formed in the movable member 20, and the opening 24 includes two sections, which are a first section hole 241 and a second section hole 242, and the first section hole 241 and the second section hole 242 are communicated with each other. The widths of the first segment hole 241, the second segment hole 242, and the support plate 41 are set as: the width of the first segment hole 241 is greater than that of the second segment hole 242, and the width of the support plate 41 is between the width of the first segment hole 241 and the width of the second segment hole 242, so that, in that the support 40 is already fixed to the body 10 before the mobile element 20 is mounted, the mobile element 20, when assembled, the width of the first sectional hole 241 is larger, and the movable member 20 can pass through the first sectional hole 241, at this time, the movable member 20 is equivalent to between the machine body 10 and the supporting plate 41, after the movable member 20 is pushed, the supporting member 40 moves relatively from the first section of the hole 241 to the second section of the hole 242, and at this time, the supporting plate 41 is located below the second section of the hole 242, since the width of the supporting plate 41 is greater than the width of the second section of hole 242, the supporting plate 41 can support the movable member 20, and the movable member 20 and the snap structure 30 are arranged in a snap fit manner, the movable member 20 is more stably fixed on the body 10. Meanwhile, the thickness of the movable member 20 may be equal to or slightly smaller than the gap between the body 10 and the support plate 41, so that a certain interference may be formed, and the movable member 20 may be clamped between the body 10 and the support member 40, so that the movable member 20 may also be fixed on the support member 40.
In addition, the opening 24 may be provided in two, i.e., the support structure may be provided in two, to better secure the moveable member 20 and the snap structure 30 together.
When it is desired to install the battery, the moveable member 20 is pushed up through the first section of aperture 241 and then pushed laterally, such that the moveable member 20 is secured to the second section of aperture 242. When the battery needs to be disassembled, the operation is reversed.
Therefore, the movable member 20 is further secured to the body 10 and is easily disassembled by the engagement of the movable member 20 and the snap structure 30 and the assembly of the support member 40 to the movable member 20.
In one embodiment, the first section of hole 241 is a circular hole, the second section of hole 242 is a square hole, the circular hole is communicated with the square hole, and the diameter of the circular hole is larger than the width of the square hole. The aperture of the circular hole is larger than the width of the square hole, so that the movable member 20 can smoothly pass through the circular hole and push the square hole.
In one embodiment, the first section of hole 241 is perpendicular to the second section of hole 242, and the first section of hole 241 and the second section of hole 242 are square holes. First section hole 241 also can be the quad slit, and when adopting the quad slit, first section hole 241 can be perpendicular second section hole 242, is the T style of calligraphy structure in other words, and then the width in first section hole square hole is greater than the width in second section hole square hole, and moving part 20 can pass first section hole quad slit smoothly to promote the position in second section hole square hole. The widths of the two sections are both widths perpendicular to the extending direction of the second section of the square hole.
In addition, the support plate 41 has a circular structure or a plate-like structure. The support plate 41 may be an irregular structure, and only needs to have a width greater than the width of the second section of hole 242, so as to support the movable member 20. The support member 40 is provided with a screw thread to be screwed to the body 10.
In this embodiment, referring to fig. 8 and 9, the present invention includes a main body 10 and a camera 12, and the camera 12 may be disposed on the main body 10, and preferably, may be disposed at a front position of the main body 10 to avoid being blocked by the main body 10 during image capturing.
In one embodiment, the camera module further comprises a mounting assembly 130, wherein the mounting assembly 130 comprises a first fixing member 131 and a protection plate 132, the protection plate 132 is fixed on the main body 10, and the first fixing member 131 is located between the protection plate 132 and the camera 12.
The mounting assembly 130 is a structure for fixing the camera 12, and includes a first fixing member 131 and a protection plate 132, wherein the first fixing member 131 is located between the camera 12 and the protection plate 132, and the protection plate 132 is fixed to the body 10, and in order to fix the camera 12, screws may be used to pass through the first fixing member 131 from the protection plate 132 and extend to the camera 12 for fixing. The screw can set up to two, three, four or more, aims at can passing protection shield 132 and first mounting 131 and fix, and protection shield 132 can carry out the function protection to the camera, and protection shield 132 can be dull and stereotyped structure, reduces the impaired risk of camera.
In this embodiment, the protective plate 132 is provided with a first arc-shaped hole 133 and a second arc-shaped hole 134, the first fixing member 131 is provided with a first through hole 135 corresponding to the first arc-shaped hole 133, and a second through hole 136 corresponding to the second arc-shaped hole 134; one screw is used to fasten the camera head 12 from the first arcuate hole 133 through the first through hole 135 and the other screw is used to fasten the camera head 12 from the second arcuate hole 134 through the second through hole 136.
For better fixing the protection board, first mounting and camera mutually, be provided with first arc hole 133 and second arc hole 134 on protection board 132, be provided with first through-hole 135 corresponding first arc hole 133 on first mounting 131, be provided with second through-hole 136 corresponding second arc hole 134, can pass first arc hole 133 and first through-hole 135 through the screw correspondence, second arc hole 134 and second through-hole 136 are fixed, be equivalent to and be provided with two fixed points in one side position of camera 12, thereby can fix firmly.
Meanwhile, the design of the first arc-shaped hole 133 and the second arc-shaped hole 134 is adopted, the screws can move along the first arc-shaped hole 133 or the second arc-shaped hole 134, the distance between the two screws is constant all the time, and the design can enable the camera angle adjusting function to be achieved. For example, referring to fig. 9, two end portions of the first arc-shaped hole 133 are set as d1 and d2, two end portions of the second arc-shaped hole 134 are set as d3 and d4, and a distance between d1 and d3 is equal to a distance between d2 and d4, so that the arc-shaped holes are adopted in a design that a distance between one screw at the position of the first arc-shaped hole 133 and the other screw at the position of the second arc-shaped hole 134 is constant and equal to a distance between d1 and d3 or a distance between d2 and d4, so that the camera can be fixed, the camera angle can be adjusted, and aerial photographs with different angles can be taken conveniently.
In one embodiment, the mounting assemblies 130 are provided in two sets, one on each side of the camera head 12. Two sets of installation component 130 set up in the both sides of camera 12, can play fixed action, angle regulation effect and guard action.
Preferably, the first arc-shaped hole 133 is disposed at a position of a sidewall of the protection plate 132. The first arc-shaped holes 133 are disposed on the side wall of the protection plate 132, and may be disposed vertically, or disposed obliquely, that is, the positions of d1 and d2 are not at the same height, so that the angle of the camera 12 may be adjusted by adjusting the height of the first arc-shaped holes 133 through screws.
Preferably, the second arc-shaped hole 134 is disposed at a top position of the protection plate 132. The second arc-shaped hole 134 can be used as an adaptive design for adjusting the height of the screw in the first arc-shaped hole 133, so that each set of the mounting assemblies 130 has at least two fixed positions, and the fixation is firmer.
In this embodiment, the aircraft further comprises a plurality of propellers 14 all arranged on the aircraft body 10, and a protective cover 15 is arranged on the periphery of each propeller 14. The protective cover 15 can protect the propeller 14 from directly colliding with the propeller 14 when the propeller 14 collides with foreign objects in a shuttling manner, thereby reducing damage to the propeller 14.
In this embodiment, the mounting assembly 130 further includes a second fixing member 137 and a plurality of third fixing members 138, one end of each of the third fixing members 138 is fixed on the second fixing member 137 by a screw, and the other end of each of the third fixing members 138 is fixed on the protection plate 132 by a screw.
In order to better fix the camera 12 on the body 10, a second fixing member 137 and a plurality of third fixing members 138 are provided, and the third fixing members 138 are of a flat plate structure, are mainly fixed on the body 10, and can be fixed by screws, so as to be convenient to detach and replace. Meanwhile, the third fixing member 138 may be provided in several numbers, and it is provided with two fixing holes, wherein one fixing hole is fixed to the second fixing member 137 by a screw, and the other fixing hole is fixed to the protection plate 132 by a screw, so that the camera 12 can be well fixed to the body 10. In addition, the third fixing members 138 may be three, four or five, and preferably four, and are disposed around the second fixing member 137.
In this embodiment, the propeller device further includes a plurality of propellers 14, and a protective cover 15 is disposed on an outer periphery of each propeller 14. The protective cover 15 can protect the propeller 14 from directly colliding with the propeller 14 when the propeller 14 collides with foreign objects in a shuttling manner, thereby reducing damage to the propeller 14.
The battery can be quickly installed or disassembled to play a role in quickly replacing the battery, the battery is installed on the moving part, the moving part can be fixed on the buckle structure only by aligning the first section of the hole with the support part to push upwards and then push laterally, the moving part is matched with the support and stabilization effect of the support part, the moving part can be stably installed on the machine body, the whole installation and disassembly mode is quick and convenient, the steps are few, and the efficiency is improved.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.

Claims (10)

1. An unmanned aerial vehicle capable of rapidly disassembling and assembling a battery comprises a body (10) and a battery (11), and is characterized by further comprising
The battery is arranged on the movable piece, the movable piece is arranged at the bottom of the machine body, the front end of the movable piece protrudes to form a clamping part (21), and two sides of the clamping part extend outwards to form side protrusions (22);
the buckle structure (30) is arranged at the bottom of the machine body and comprises a buckle body (31) and two buckle plate pieces (32), wherein the middle position of each buckle plate piece is provided with a mounting hole (322) and is mounted on the buckle body through a torsion spring, and the two buckle plate pieces are adjacently arranged and form a sliding channel (311);
a clamping part (321) is arranged at the end part of the clamping plate close to the clamping body;
after the movable piece slides into the buckle body along the sliding channel, the side protrusions and the buckle parts form interference, so that the movable piece is fixed on the buckle structure.
2. The unmanned aerial vehicle capable of being rapidly disassembled and assembled with a battery as claimed in claim 1, wherein when the movable member is fixed on the buckle structure, the buckle plate abuts against the side wall of the clamping portion.
3. The unmanned aerial vehicle capable of rapidly dismounting and mounting a battery according to claim 1, wherein a rotating channel (312) is arranged on the buckle body, and the buckle part rotates along the rotating channel.
4. The unmanned aerial vehicle capable of quickly and detachably mounting a battery as claimed in claim 1, wherein a handle portion (323) is provided on a position of the buckle plate away from the buckle body.
5. The battery quick disconnect unmanned aerial vehicle of claim 1, further comprising a support structure including an aperture (24) disposed on the moving member and a support member (40) secured to the fuselage;
one end of the supporting piece is fixed on the machine body, the other end of the supporting piece extends along the peripheral side to form a supporting plate (41), and a gap is formed between the machine body and the supporting plate;
the opening hole is provided with two sections, namely a first section hole (241) and a second section hole (242), wherein the first section hole is communicated with the second section hole, the width of the first section hole is larger than that of the second section hole, and the width of the support plate is between the width of the first section hole and that of the second section hole;
when the movable piece is inserted into the buckle structure, the support piece moves from the first section of hole to the second section of hole relatively, and the movable piece is fixed on the second section of hole stably.
6. The unmanned aerial vehicle capable of being rapidly disassembled and assembled with batteries as claimed in claim 5, wherein the first section of hole is a round hole, and the second section of hole is a square hole.
7. The unmanned aerial vehicle capable of being rapidly disassembled and assembled with batteries as claimed in claim 6, wherein the diameter of the round hole is larger than the width of the square hole.
8. The unmanned aerial vehicle capable of being rapidly disassembled and assembled with batteries as claimed in claim 5, wherein the supporting plate is of a circular structure or a plate-shaped structure.
9. The unmanned aerial vehicle capable of quickly dismounting and mounting a battery according to claim 1, further comprising a camera (12) and a mounting assembly (130) for mounting the camera, wherein the mounting assembly comprises a first fixing piece (131) and a protection plate (132), the protection plate is fixed on the machine body, and the first fixing piece is positioned between the protection plate and the camera; a first arc-shaped hole (133) and a second arc-shaped hole (134) are formed in the protective plate, a first through hole (135) is formed in the first fixing piece corresponding to the first arc-shaped hole, and a second through hole (136) is formed in the first fixing piece corresponding to the second arc-shaped hole; adopt a screw to pass first through-hole from first arc hole and fix to on the camera, adopt another screw to pass the second through-hole from second arc hole and fix to on the camera, the interval between two screws is unchangeable.
10. The unmanned aerial vehicle capable of quickly dismounting and mounting a battery according to claim 1, further comprising a plurality of propellers (14), wherein a protective cover (15) is arranged on the periphery of each propeller.
CN202111297822.7A 2021-09-15 2021-11-04 Unmanned aerial vehicle capable of rapidly disassembling and assembling battery Pending CN113879548A (en)

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CN202122232641 2021-09-15
CN2021222326418 2021-09-15

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CN103311469A (en) * 2012-03-12 2013-09-18 海洋王照明科技股份有限公司 Opening-closing device of battery box
KR20170100775A (en) * 2016-02-26 2017-09-05 송기준 Virtual reality shooting camera gimbal with drones
CN206629354U (en) * 2017-03-31 2017-11-10 北京三五二环保科技有限公司 A kind of novel remote controller
CN109792091A (en) * 2017-04-20 2019-05-21 深圳市大疆创新科技有限公司 Battery fastening structure and electronic device
WO2019134170A1 (en) * 2018-01-08 2019-07-11 深圳市道通智能航空技术有限公司 Pan-tilt, photography assembly, unmanned aerial vehicle, damping member, and mounting seat
CN209739367U (en) * 2019-04-27 2019-12-06 杭州威宏能源科技有限公司 high-energy unmanned aerial vehicle power supply
CN110785034A (en) * 2019-10-11 2020-02-11 杭州海兴电力科技股份有限公司 Self-locking structure based on sliding groove guide rail
CN210126642U (en) * 2019-03-19 2020-03-06 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and battery
CN212358808U (en) * 2020-08-19 2021-01-15 安徽山水空间装饰有限责任公司 Integrated ceiling mounting structure

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103311469A (en) * 2012-03-12 2013-09-18 海洋王照明科技股份有限公司 Opening-closing device of battery box
KR20170100775A (en) * 2016-02-26 2017-09-05 송기준 Virtual reality shooting camera gimbal with drones
CN206629354U (en) * 2017-03-31 2017-11-10 北京三五二环保科技有限公司 A kind of novel remote controller
CN109792091A (en) * 2017-04-20 2019-05-21 深圳市大疆创新科技有限公司 Battery fastening structure and electronic device
WO2019134170A1 (en) * 2018-01-08 2019-07-11 深圳市道通智能航空技术有限公司 Pan-tilt, photography assembly, unmanned aerial vehicle, damping member, and mounting seat
CN210126642U (en) * 2019-03-19 2020-03-06 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and battery
CN209739367U (en) * 2019-04-27 2019-12-06 杭州威宏能源科技有限公司 high-energy unmanned aerial vehicle power supply
CN110785034A (en) * 2019-10-11 2020-02-11 杭州海兴电力科技股份有限公司 Self-locking structure based on sliding groove guide rail
CN212358808U (en) * 2020-08-19 2021-01-15 安徽山水空间装饰有限责任公司 Integrated ceiling mounting structure

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