Portable six-rotor unmanned aerial vehicle

By optimizing the folding method of the drone's tripod, battery and arm, the problem of larger size after folding of existing drones is solved, achieving smaller folding size and higher portability.

CN119872962AActive Publication Date: 2025-04-25华启天成(深圳)智能科技有限公司
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Patent Information

Application Number
CN202510234974.4
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-02-28
Publication Date
2025-04-25
Estimated Expiration
2045-02-28

AI Technical Summary

Technical Problem

Existing drones are larger in size after folding, resulting in inconvenience in use and transfer.

Method used

By optimizing the footrest, battery placement and arm folding, a portable hexagonal drone is designed to achieve a smaller folding size.

Benefits of technology

The drone is minimized in folding size, reducing the inconvenience of use and transfer, and improving portability.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to a portable six-rotor unmanned aerial vehicle. The unmanned aerial vehicle comprises a machine frame, machine arms are installed on the machine frame in a foldable mode, the machine arms comprise the two first machine arms, the two second machine arms and the two third machine arms, the two first machine arms, the two second machine arms and the two third machine arms are symmetrically arranged on the two sides of the machine frame respectively, and when folded, the first machine arms, the second machine arms and the third machine arms are all folded to be parallel to the machine frame. Meanwhile, the second vehicle arm is located below the first vehicle arm and the third vehicle arm, in addition, a storage battery is detachably placed on the storage battery containing part, and meanwhile when the first vehicle arm, the second vehicle arm and the third vehicle arm are folded, the storage battery containing part is located below all the vehicle arms. The unmanned aerial vehicle is ingenious in structure, on one hand, the storage batteries are arranged on the two sides of the rack, the size of the unmanned aerial vehicle is reduced, on the other hand, all the vehicle arms are located on the two sides of the rack when folded, meanwhile, the second vehicle arm is located below the first vehicle arm and the third vehicle arm, the size after folding is further reduced, and convenience is brought to use.
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Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to a portable six-rotor unmanned aerial vehicle. Background Art

[0002] With the development of drone technology, it has been widely used because of its safety, speed and efficiency. Currently, drones can be seen in aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting and other fields, which have a significant promoting effect on improving work efficiency.

[0003] In the process of drone application, in order to facilitate the transfer and transportation of drones, the drones often need to be folded and collapsed. Therefore, the existing drones with many foldable arms, although they can achieve the folding of drones to a certain extent, bringing convenience to transfer and transportation, are still not fully utilized in terms of space, and there is a lot of room for improvement.

[0004] Therefore, the present invention proposes a portable six-rotor UAV, which obtains a model with unparalleled folding size through optimization and innovation of a tripod, a battery, and a folding method, thereby bringing convenience to practical applications. Summary of the invention

[0005] The purpose of the present invention is to provide a portable six-rotor drone to solve the problem that the existing drones are large in size after being folded, which brings inconvenience in use and transfer.

[0006] To achieve the above object, the present invention adopts the following technical solution: a portable six-rotor drone, comprising a frame, wherein the frame comprises a tail connection part, a nose connection part, a battery placement part and a battery connection part;

[0007] The frame is provided with arms which can be folded and mounted thereon, and the arms include a first arm, a second arm and a third arm; the first arm, the second arm and the third arm each have two arms and are symmetrically arranged on both sides of the frame;

[0008] The tail connection part is connected to the two second machine arms, and the nose connection part is connected to the two first machine arms and the two third machine arms respectively;

[0009] The battery placement parts and the battery connection parts are respectively provided with two and are symmetrically arranged on both sides of the frame, and the battery placement parts are respectively provided with batteries, and the batteries are detachably connected to the corresponding battery connection parts;

[0010] When the arms are folded, the first arm, the second arm and the third arm are arranged outward from the frame axis, the second arm is located below the first arm and the third arm; the first arm, the second arm and the third arm are all located above the battery placement portion;

[0011] When the machine arm is unfolded, it is fixedly connected to the frame through the first locking mechanism; when the machine arm is folded, it is fixedly connected to the frame through the second locking mechanism.

[0012] Furthermore, a tripod is detachably mounted below the frame.

[0013] Furthermore, the tripod comprises a connecting portion and a supporting portion, the connecting portion is detachably fixedly connected to the frame, and the supporting portion is foldably hinged to the connecting portion.

[0014] Furthermore, a fastener is provided on the connecting part, and the fastener includes a fixing piece, which is fixedly connected to the connecting part, and a first fastener is fixedly connected to the fixing piece, one end of the first fastener is hinged to one end of the second fastener, and the other end of the first fastener is locked and matched with the other end of the second fastener.

[0015] Furthermore, a shell is detachably mounted on the frame, and a tail docking portion and a nose docking portion are arranged on the shell, the tail docking portion cooperates with the tail connecting portion, and the nose docking portion cooperates with the nose connecting portion; battery matching portions are arranged on both sides of the shell, the battery matching portions cooperate with the battery when the arm is unfolded, and cooperate with the arm when the arm is folded.

[0016] Furthermore, a parachute mounting part is arranged on the frame below the shell, and the parachute mounting part includes a round umbrella mounting part and a square umbrella mounting part; a parachute matching part is correspondingly arranged on the shell, and the parachute matching part includes a round umbrella matching part and a square umbrella matching part, the round umbrella matching part matches with the round umbrella mounting part, and the square umbrella matching part matches with the square umbrella mounting part; the parachute matching part is made of ABS plastic material and is adaptively cut according to the type of parachute installed.

[0017] Furthermore, a connecting piece is fixedly connected to the end of the machine arm, and the connecting piece is hinged to the frame; the first locking mechanism cooperates with the machine arm, and the second locking mechanism cooperates with the connecting piece.

[0018] Furthermore, the first locking mechanism includes a ring buckle, the ring buckle is hinged to the frame, a slot is provided on the ring buckle, a first clamp is provided on the frame, the first clamp is hinged to the frame, and the first clamp cooperates with the slot.

[0019] Furthermore, the second locking mechanism includes an installation portion, which is hinged to the second clamp, a clamping spring is arranged between the second clamp and the frame, a clamp head is arranged below the second clamp, and a clamp head matching portion is arranged on the connecting member, which matches with the clamp head.

[0020] Beneficial effects of the present invention:

[0021] 1. The present invention is equipped with a foldable tripod, and the tripod is detachably connected to the frame, so that it can be installed during use and can be disassembled, folded and folded after use, which greatly reduces the space occupied by the tripod and reduces the volume after folding;

[0022] 2. The present invention places the batteries on both sides of the frame, installs them when in use, and removes them when not in use. The volume of the machine body is not increased during the process, and the volume after folding is effectively reduced;

[0023] 3. The arms of the present invention are foldable, and during the process, the arms are folded on both sides of the frame respectively. On the one hand, the second arm is located below the first and third arms after folding, which reduces space occupancy. On the other hand, the first, second and third arms are all located above the battery placement portion, which greatly reduces the volume after folding. This makes the drone of the present invention have an unparalleled size after folding, which brings convenience to use. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 This is a schematic diagram of the overall structure of the present invention in an unfolded state;

[0025] Figure 2 It is a schematic diagram of the shell structure of the present invention;

[0026] Figure 3 It is a schematic diagram of the frame structure of the present invention;

[0027] Figure 4 It is a schematic diagram of the tripod installation structure of the present invention;

[0028] Figure 5 It is a schematic diagram of the tripod structure of the present invention;

[0029] Figure 6 The present invention Figure 5 A partial enlarged schematic diagram of part A;

[0030] Figure 7 The present invention Figure 5 A partial enlarged schematic diagram of part B;

[0031] Figure 8 It is a schematic diagram of the second machine arm and the frame installation structure of the present invention;

[0032] Fig. 9It is a schematic diagram of the structure when the machine arm of the present invention is connected to the connecting piece;

[0033] Fig.10 It is a schematic diagram of the locking mechanism structure of the present invention;

[0034] Fig.11 It is a schematic diagram of the installation structure of the first and third machine arms and the frame of the present invention;

[0035] Fig.12 The present invention Fig.11 A partial enlarged schematic diagram of part C in the middle;

[0036] Fig.13 It is a schematic diagram of the folded state of the present invention.

[0037] The names corresponding to the marks in the figure are:

[0038] 1. Frame; 11. Tail connection; 12. Nose connection; 13. Parachute mounting; 131. Round parachute mounting; 132. Square parachute mounting; 14. Battery placement; 15. Battery connection; 2. Shell; 21. Tail docking; 22. Nose docking; 23. Parachute matching; 231. Round parachute matching; 232. Square parachute matching; 24. Battery matching; 3. Tripod; 31. Connecting; 32. Support; 33. Fastener; 331. Fixing; 332. The first fastener; 333, the second fastener; 34, the hinge; 341, the first hinged part; 342, the second hinged part; 343, the slide groove; 344, the locking member; 4, the battery; 5, the arm; 51, the first arm; 52, the second arm; 53, the third arm; 6, the propeller; 7, the first locking mechanism; 71, the buckle; 711, the slot; 72, the first clamp; 8, the second locking mechanism; 81, the mounting part; 82, the second clamp; 821, the clamp head; 83, the retaining spring; 9, the connecting member; 91, the clamp head mating part. DETAILED DESCRIPTION

[0039] The technical solution of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0040] like Figure 1-3 As shown in FIG. 13 , in this embodiment, the drone of the present invention includes a frame 1, a tail connection portion 11 is arranged at the end of the frame 1, a nose connection portion 12 is arranged at the front end of the frame 1, a shell 2 is fixedly installed through the tail connection portion 11 and the nose connection portion 12, the shell 2 includes a tail docking portion 21 and a nose docking portion 22, the tail docking portion 21 is detachably fixedly connected to the tail connection portion 11, and the nose docking portion 22 is detachably fixedly connected to the nose connection portion 12.

[0041] Battery placement parts 14 are provided on both sides of the frame 1, and batteries 4 are placed through the battery placement parts 14. The battery placement parts 14 are located on both sides of the shell 2, and battery matching parts 24 are respectively provided on both sides of the shell 2; battery connecting parts 15 are also provided on both sides of the frame 1, and the battery connecting parts 15 match with the battery 4.

[0042] The machine arm 5 is foldably connected to the machine frame 1 through the tail connecting part 11 and the nose connecting part 12, and the machine arm 5 is connected to the propeller 6, wherein the machine arm 5 includes six machines arms, three of which are arranged on each side of the frame 1 and are arranged symmetrically, the tail connecting part 11 is connected to two mutually symmetrical second machines arms 52, the nose connecting part 12 is respectively connected to two mutually symmetrical first machines arms 51 and two mutually symmetrical third machines arms 53, and the first machines arms 51 and the third machines arms 53 are respectively provided on both sides of the frame 1; when the machine arms 5 are folded, the arms 5 are respectively folded on both sides of the frame 1 and are located above the battery placement part 14.

[0043] like Figure 8-12 As shown, in another embodiment of the present invention, the front end of each arm 5 is fastened to the connecting member 9, the connecting member 9 is respectively hinged to the tail connecting part 11 and the nose connecting part 12, and a first locking mechanism 7 is provided on the tail connecting part 11 and the nose connecting part 12. The first locking mechanism 7 is used to fix the arm 5 to the frame 1 when the arm 5 is unfolded, wherein the first locking mechanism 7 includes a buckle 71, the buckle 71 is respectively hinged to the tail connecting part 11 and the nose connecting part 12, a card slot 711 is provided on the buckle 71, and a first clamping member 72 is correspondingly hingedly installed on the tail connecting part 11 and the nose connecting part 12, and the first clamping member 72 is connected to the card slot 711. 11 is matched; a second locking mechanism 8 is also provided on the tail connection part 11 and the nose connection part 12, and the second locking mechanism 8 is used to fix the arm 5 to the frame 1 when the arm 5 is folded and retracted, wherein the second locking mechanism 8 includes a mounting portion 81, and the mounting portion 81 is fixedly connected to the tail connection part 11 and the nose connection part 12 respectively, and a second clamping member 82 is hinged through the mounting portion 81, and a retaining spring 83 is respectively provided between the second clamping member 82 and the tail connection part 11 and the nose connection part 12, and a clamping head 821 is provided at the lower end of the second clamping member 82, and a clamping head matching portion 91 is provided above the connecting member 9, and the clamping head matching portion 91 matches with the clamping head 921.

[0044] like Figure 4-7 As shown, in another embodiment of the present invention, a tripod 3 is detachably installed below the frame 1 .

[0045] In this embodiment, the tripod 3 includes a connecting portion 31, which is detachably fixedly connected to the lower part of the frame 1, and a supporting portion 32 is hingedly installed at the lower part of the connecting portion 31, and the supporting portion 32 is foldably hinged to the connecting portion 31; wherein a fastener 33 is provided on the connecting portion 31, and the tripod 3 is detachably fixedly connected to the frame 1 through the fastener 33, and the fastener 33 includes a fixing member 331, and the fixing member 331 is fixedly connected to the connecting portion 31, and a first fastener 332 is fixedly connected to the fixing member 331, and one end of the first fastener 332 is hinged to one end of the second fastener 333, The other end of the second fastener 333 is fastened to the other end of the second fastener 333 by bolts; the connecting part 31 is hinged to the supporting part 32 through a hinge 34, wherein the hinge 34 includes a first hinge part 341 and a second hinge part 342, the first hinge part 341 is fixedly connected to the supporting part 32, the second hinge part 342 is fixedly connected to the connecting part 31, a slide groove 343 is provided on the second hinge part 342, and locking parts 344 are respectively hinged on both sides of the first hinge part 341, and a bolt is connected through the locking part 344, and the bolt passes through the slide groove 343 and cooperates with the slide groove 343.

[0046] like Figure 2-3 As shown, in another embodiment of the present invention, a parachute mounting portion 13 is further provided on the frame 1, wherein the parachute mounting portion 13 includes a circular parachute mounting portion 131 and a square parachute mounting portion 132, and a parachute matching portion 23 is correspondingly provided on the outer shell 2, including a circular parachute matching portion 231 and a square parachute matching portion 232, the circular parachute mounting portion 131 is used to install a cylindrical parachute, and the circular parachute matching portion 231 matches the cylindrical parachute in space; the square parachute mounting portion 132 is used to place and install a rectangular parachute, and the square parachute matching portion 232 matches the rectangular parachute in space, and only one of the cylindrical parachute and the rectangular parachute can be configured at the same time.

[0047] The principle of the present invention is:

[0048] When the present invention is in use, the tripod 3 is unfolded and then fixedly installed under the frame 1 through the fastener 33. After use, the tripod 3 can be disassembled, thereby facilitating the reduction of the size of the folded drone of the present invention. At the same time, the tripod 3 is also foldable. When the tripod 3 is not in use, it can be folded and placed in a backpack, which also helps to reduce the size of the folded drone of the present invention.

[0049] When the present invention is used, the arm 5 needs to be unfolded, and the drone of the present invention can be folded as shown in the attached figure. Fig.13 As shown, the first arm 51 is as shown Figure 1As shown on the outside, it is folded counterclockwise at the innermost side, the second arm 52 is folded clockwise in the middle, and the third arm 53 is folded counterclockwise at the outermost side. At this time, the second clamp 82 in the second locking mechanism 8 is pressed down or lifted, so the clamp head 821 will be lifted. When the clamp head 821 is separated from the clamp head matching part 91, the arms can be unfolded in sequence. At this time, the battery 4 can be installed for use. After use, the battery 4 is removed and the arm 5 and the propeller 6 are folded. It should be noted that in the present invention, the structural design of the second locking mechanism 8 at each position is slightly different. It is adapted to the outer shell 2 and is convenient for use in actual operation. Although there are some differences in structure, the principle is the same. It is not difficult for technicians in the field of this invention to understand, so it will not be explained separately.

[0050] During the use of the drone of the present invention, different types of parachutes can be adapted, such as cylindrical and rectangular types, but only one type can be configured at a time. The parachute matching part 23 on the shell 2 is ABS plastic. When the parachute is equipped, this part is adaptively cut according to the type of the parachute to facilitate the ejection of the parachute.

[0051] In an application example of the present invention, the empty weight is 23kg, the wheelbase is 2200mm; the layout is 6-axis and 6-propeller, the standard load is 50kg; the empty-load endurance is 70min, and the 50kg endurance is 25min; it can withstand wind level 6, the operating temperature is -20 to 60℃; the maximum flight speed is 20m / s, and the maximum operating altitude is 5000m.

[0052] In this example, the drone of the present invention is 1140 mm long, 860 mm wide and 350 mm high after being folded, and has an extremely small storage size. At the same time, the tripod 3 is 820 mm long, 630 mm wide and 115 mm high after being folded, and the tripod 3 is 430 mm high before being folded, which effectively reduces the size of the tripod 3 and also facilitates storage, bringing convenience to use.

[0053] The present invention is not limited to the above-mentioned optimal implementation mode. Anyone can derive other various forms of products under the inspiration of the present invention. However, no matter what changes are made in the shape or structure, all technical solutions that are the same or similar to those of the present application fall within the protection scope of the present invention.

Claims

1. A portable six-rotor drone, characterized by: The machine frame (1) comprises a machine tail connection part (11), a machine head connection part (12), a battery placement part (14) and a battery connection part (15); The frame (1) is provided with an arm (5) which can be folded and mounted thereon, and the arm (5) comprises a first arm (51), a second arm (52) and a third arm (53); the first arm (51), the second arm (52) and the third arm (53) are provided in pairs and are symmetrically arranged on two sides of the frame (1); The tail connection part (11) is connected to the two second machine arms (52), and the nose connection part (12) is respectively connected to the two first machine arms (51) and the two third machine arms (53); The battery placement parts (14) and the battery connection parts (15) are provided with two each and are symmetrically arranged on both sides of the frame (1); the battery placement parts (14) are respectively provided with batteries, and the batteries are detachably connected to the corresponding battery connection parts (15); When the arms (5) are folded, the first arm (51), the second arm (52) and the third arm (53) are arranged outward from the axis of the frame (1), the second arm (52) is located below the first arm (51) and the third arm (53); the first arm (51), the second arm (52) and the third arm (53) are all located above the battery placement portion (14); When the machine arm (5) is unfolded, it is fixedly connected to the frame (1) via a first locking mechanism (7); when the machine arm (5) is folded, it is fixedly connected to the frame (1) via a second locking mechanism (8).

2. A portable six-rotor drone according to claim 1, characterized in that: A tripod (3) is detachably mounted below the frame (1).

3. A portable six-rotor drone according to claim 2, characterized in that: The tripod (3) comprises a connecting portion (31) and a supporting portion (32); the connecting portion (31) is detachably fixedly connected to the frame (1); and the supporting portion (32) is foldably hinged to the connecting portion (31).

4. The portable six-rotor drone according to claim 3, characterized in that: The connecting portion (31) is provided with a fastener (33), the fastener (33) includes a fixing member (331), the fixing member (331) is fixedly connected to the connecting portion (31), a first fastener (332) is fixedly connected to the fixing member (331), one end of the first fastener (332) is hinged to one end of the second fastener (333), and the other end of the first fastener (332) is locked with the other end of the second fastener (333).

5. The portable six-rotor drone according to claim 1, characterized in that: The frame (1) is detachably mounted with a housing (2), and a tail docking portion (21) and a nose docking portion (22) are arranged on the housing (2). The tail docking portion (21) cooperates with the tail connecting portion (11), and the nose docking portion (22) cooperates with the nose connecting portion (12). Battery matching portions (24) are arranged on both sides of the housing (2), and the battery matching portions (24) cooperate with the battery (4) when the arm (5) is unfolded, and cooperate with the arm (5) when the arm (5) is folded.

6. The portable six-rotor drone according to claim 5, characterized in that: A parachute mounting portion (13) is arranged on the frame (1) below the shell (2), and the parachute mounting portion (13) includes a circular umbrella mounting portion (131) and a square umbrella mounting portion (132); a parachute matching portion (23) is correspondingly arranged on the shell (2), and the parachute matching portion (23) includes a circular umbrella matching portion (231) and a square umbrella matching portion (232), the circular umbrella matching portion (231) matches with the circular umbrella mounting portion (131), and the square umbrella matching portion (232) matches with the square umbrella mounting portion (132); the parachute matching portion (23) is made of ABS plastic material and is adaptively cut according to the type of parachute installed.

7. The portable six-rotor drone according to claim 1, characterized in that: The end of the machine arm (5) is fixedly connected with a connecting piece (9), and the connecting piece (9) is hinged to the frame (1); the first locking mechanism (7) cooperates with the machine arm (5), and the second locking mechanism (8) cooperates with the connecting piece (9).

8. The portable six-rotor drone according to claim 7, characterized in that: The first locking mechanism (7) comprises a buckle (71), the buckle (71) is hinged to the frame (1), a slot (711) is provided on the buckle (71), a first clamping member (72) is provided on the frame (1), the first clamping member (72) is hinged to the frame (1), and the first clamping member (72) matches the slot (711).

9. The portable six-rotor drone according to claim 7, characterized in that: The second locking mechanism (8) comprises a mounting portion (81), the mounting portion (81) is hinged to the second clamping member (82), a clamping spring (83) is arranged between the second clamping member (82) and the frame (1), a clamping head (821) is arranged below the second clamping member (82), and a clamping head matching portion (91) is arranged on the connecting member (9), and the clamping head matching portion (91) matches with the clamping head (821).

Citation Information

Patent Citations

  • Multi-rotor helicopter folding system

    CN107054637A

  • Systems and methods related to transformable unmanned aerial vehicles

    US20200062373A1