Unmanned aerial vehicle mounting device

By designing the drone mounting device, the automatic fixing and separation of items straps using electric telescopic cylinders and magnetic suction connections is solved, and the problems of risk and inefficiency of manual connections in drone operations are improved, and operation safety and efficiency are improved.

CN222859724UActive Publication Date: 2025-05-13INNER MONGOLIA ELECTRONICS INFORMATION VOCATIONAL TECHN COLLEGE
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Patent Information

Application Number
CN202421787144.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-26
Publication Date
2025-05-13
Estimated Expiration
2034-07-26

AI Technical Summary

Technical Problem

When UAVs are used for mountain agricultural picking and transportation, personnel need to manually connect UAVs and cargo, resulting in dangerous and inefficient operations.

Method used

A drone mounting device is designed, including a first mounting rack, a second mounting rack and a lower mounting rack. The automatic fixing and separation operation of the item straps is achieved through the electric telescopic cylinder and magnetic suction connection, reducing manual intervention.

Benefits of technology

The device greatly reduces the risk of personnel operating under hovered drones, improves operating efficiency, reduces the take-off and landing time of the drone and the swaying during cargo movement, and reduces the operating pressure.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides an unmanned aerial vehicle mounting device which relates to the technical field of unmanned aerial vehicle accessories and comprises a first mounting frame, a second mounting frame and a lower fixing frame, the second mounting frame is arranged on the lower portion of the first mounting frame, the lower fixing frame is hinged to the lower end of the second mounting frame, upper limiting frames are hinged to the two sides of the top of the second mounting frame, and the upper limiting frames are hinged to the lower fixing frame. A side guide ring is fixed to the side face of the upper limiting frame, an outer balancing weight is fixed to the head end of the upper limiting frame, a lower connecting port is slidably formed in the middle of the second mounting frame, and second electric telescopic cylinders are fixed to the two sides of the lower portion of the second mounting frame. The lower connecting column is in butt joint and fixed with the second mounting frame along with descending of the unmanned aerial vehicle, manual butt joint of the lower connecting column and the second mounting frame by personnel is omitted, butt joint operation of the personnel under hovering of the unmanned aerial vehicle is omitted, and the problems that hooks need to be manually connected with cargo bandages by the personnel, the distance between the personnel and the unmanned aerial vehicle is short, and danger is large are solved.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle accessories, and in particular to a mounting device for an unmanned aerial vehicle. Background Art

[0002] With the development of drones, in some mountainous agricultural harvesting, drones are used to transport fruits from the mountain to the foot of the mountain. Drones can transport fruits in a straight line over the mountain more quickly, without the need to walk on rugged mountain roads, thus speeding up transportation efficiency and shortening transportation time.

[0003] The drone is connected to the cargo straps through hooks and other devices. The hooks need to be manually connected to the cargo straps by personnel. It is dangerous for personnel to operate a hovering drone. In particular, in order to reduce the swaying during movement, the distance between the drone and the hook will not be particularly long, resulting in a closer distance between personnel and the drone, further increasing the danger. Summary of the invention

[0004] The disclosed embodiments relate to a mounting device for a drone, in which the second mounting frame and the lower fixing frame perform fixing and separation operations of item straps, and the first mounting frame and the second mounting frame can be actively controlled to separate. After the second mounting frame performs item strap fixation, the lower connecting column is docked and fixed with the second mounting frame as the drone descends, eliminating the need for personnel to manually dock the lower connecting column with the second mounting frame, and eliminating the need for personnel to perform docking operations under a hovering drone, which is safer for personnel.

[0005] According to a first aspect of the present disclosure, a drone mounting device is provided, specifically comprising: a first mounting frame, a second mounting frame and a lower fixing frame, wherein the second mounting frame is arranged at the lower portion of the first mounting frame, the lower end of the second mounting frame is hingedly connected to the lower fixing frame, a lower connecting column is welded to the lower end of the first mounting frame, a first electric telescopic cylinder is fixed on both sides of the lower connecting column, a telescopic rod of the first electric telescopic cylinder is fixedly connected to a limit pin, an upper connecting port is fixed on the bottom of the lower connecting column, and upper magnetic blocks are fixed on both sides of the upper connecting port.

[0006] In at least some embodiments, upper limit frames are hinged on both sides of the top of the second mounting frame, side guide rings are fixed to the sides of the upper limit frame, an external counterweight is fixed to the head end of the upper limit frame, a lower connecting port is slidably provided in the middle of the second mounting frame, lower magnetic blocks are fixed on both sides of the lower connecting port, second electric telescopic cylinders are fixed on both sides of the lower part of the second mounting frame, and the telescopic rod of the second electric telescopic cylinder is fixed to the lower guide block.

[0007] In at least some embodiments, both sides of the lower connecting column are axially sliding with limit pins, and the side guide ring is extended to the lower part of the head end of the upper limit frame. After the first mounting frame and the second mounting frame are separated, the external counterweight block presses down the upper limit frame and rotates it outward, and the side guide ring tilts upward. The lower connecting column moves down to dock with the top groove of the second mounting frame, and the side guide ring is pressed down synchronously. The lower magnetic block and the upper magnetic block are adsorbed with opposite magnetic poles, the upper connecting port and the lower connecting port are vertically docked and electrically connected, and the lower connecting port is electrically connected to the second electric telescopic cylinder.

[0008] In at least some embodiments, the two ends of the lower connecting column are fitted with the upper grooves of the second mounting frame, and when the limit pin and the side hole of the upper limit frame are slidably inserted, the upper limit frame is fitted on the upper part of the lower connecting column, and the upper limit frame is rotated and pressed down on the top of the lower connecting column. The first electric telescopic cylinder is extended to push the limit pin and the upper limit frame to slide, and the position of the upper limit frame is fixed. The upper limit frame is fixed on the upper part of the lower connecting column, and the lower connecting column and the second mounting frame are fixed.

[0009] In at least some embodiments, a first clamping block is slidably disposed at the front end of the lower fixing frame, a supporting spring is fixed to the rear end of the first clamping block, and the rear end of the supporting spring is fixedly connected to the lower fixing frame.

[0010] In at least some embodiments, the bottom plane of the first end of the first clamping block is engaged with the lower part of the second mounting frame, the upper inclined surface of the first clamping block is slidably fitted with the lower guide block, and after the first clamping block is engaged with the second mounting frame, the lower fixing frame and the lower part of the second mounting frame are closed and maintained in a ring shape.

[0011] In at least some embodiments, when the lower guide block moves downward and the upper inclined surface of the first clamping block is pressed downward, the first clamping block moves away from the second mounting frame, the limit latch moves and separates from the upper limit frame, and the upper limit frame rotates upward.

[0012] The utility model provides a UAV mounting device, which has the following beneficial effects:

[0013] The item straps are fixed and separated between the second mounting rack and the lower fixing rack, and the first mounting rack and the second mounting rack can be actively controlled to separate. After the second mounting rack is fixed with the item straps, the lower connecting column is docked and fixed with the second mounting rack as the UAV descends, eliminating the need for personnel to manually dock the lower connecting column with the second mounting rack, and eliminating the need for personnel to perform docking operations under a hovering UAV, which is safer for personnel.

[0014] The upper connection port and the lower connection port are magnetically attracted by the lower magnetic block and the upper magnetic block to ensure a snug connection. At the same time, the upper connection port and the lower connection port are smoothly separated as the first mounting frame and the second mounting frame are separated, avoiding obstruction of the separation of the first mounting frame and the second mounting frame. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the technical solution of the embodiment of the utility model, the drawings of the embodiment will be briefly introduced below.

[0016] The drawings described below only relate to some embodiments of the present invention, but are not intended to limit the present invention.

[0017] In the attached picture:

[0018] Figure 1 A schematic diagram showing the overall structure of the present application;

[0019] Figure 2 A schematic diagram showing a second mounting frame structure of the present application is shown;

[0020] Figure 3 A schematic structural diagram of a cross section of the lower fixing frame of the present application is shown;

[0021] Figure 4 A schematic structural diagram of the lower fixing frame of the present application is shown;

[0022] Figure 5 A schematic structural diagram of the upper limit frame of the present application is shown;

[0023] Figure 6 A schematic diagram showing the structure of the split state of the present application;

[0024] Reference numerals list

[0025] 1. First mounting frame; 101. First electric telescopic cylinder; 102. Limiting bolt; 103. Upper connection port; 104. Upper magnetic block; 105. Lower connection column;

[0026] 2. Second mounting frame; 201. Upper limit frame; 202. Side guide ring; 203. External counterweight; 204. Lower connection port; 205. Lower magnetic block; 206. Second electric telescopic cylinder; 207. Lower guide block;

[0027] 3. Lower fixing frame; 301. First clamping block; 302. Support spring. DETAILED DESCRIPTION

[0028] In order to make the purpose, technical solution and advantages of the embodiment of the utility model clearer, the technical solution of the embodiment of the utility model will be clearly and completely described below in conjunction with the drawings of the embodiment of the utility model. Obviously, the described embodiment is a part of the embodiment of the utility model, not all of the embodiments. Based on the described embodiment of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0029] Example 1: Please refer to Figures 1 to 6 :

[0030] The utility model proposes a drone mounting device, comprising: a first mounting frame 1, a second mounting frame 2 and a lower fixing frame 3, wherein a lower connecting column 105 is welded at the lower end of the first mounting frame 1, a first electric telescopic cylinder 101 is fixed on both sides of the lower connecting column 105, a telescopic rod of the first electric telescopic cylinder 101 is fixedly connected to a limit pin 102, an upper connecting port 103 is fixed at the bottom of the lower connecting column 105, upper magnetic blocks 104 are fixed on both sides of the upper connecting port 103, a second mounting frame 2 is arranged at the lower part of the first mounting frame 1, and a first electric telescopic cylinder 101 is fixedly connected to a telescopic rod of the first electric telescopic cylinder 101, and an upper magnetic block 104 is fixed on both sides of the upper connecting port 103. The upper limit frames 201 are hinged on both sides of the top of the second mounting frame 2, and the side guide rings 202 are fixed on the sides of the upper limit frames 201. The head end of the upper limit frames 201 is fixed with an external counterweight block 203. A lower connecting port 204 is slidably provided in the middle of the second mounting frame 2, and lower magnetic blocks 205 are fixed on both sides of the lower connecting port 204. Second electric telescopic cylinders 206 are fixed on both sides of the lower part of the second mounting frame 2, and the telescopic rod of the second electric telescopic cylinder 206 is fixed to the lower guide block 207. Both sides of the lower connecting column 105 are axially sliding with limited insertion. Pin 102, the side guide ring 202 is extended to the lower part of the head end of the upper limit frame 201. After the first mounting frame 1 and the second mounting frame 2 are separated, the outer counterweight block 203 presses the upper limit frame 201 downward to rotate outward, and the side guide ring 202 tilts upward. The lower connecting column 105 moves downward to dock with the top groove of the second mounting frame 2. The side guide ring 202 is pressed downward synchronously. The lower magnetic block 205 and the upper magnetic block 104 are adsorbed by opposite magnetic poles. The upper connection port 103 and the lower connection port 204 are vertically docked and electrically connected. The lower connection port 204 and the second The electric telescopic cylinder 206 is electrically connected, and the lower end of the second mounting frame 2 is hinged with a lower fixed frame 3, and a first clamping block 301 is slidably arranged at the front end of the lower fixed frame 3, and a supporting spring 302 is fixed to the rear end of the first clamping block 301, and the rear end of the supporting spring 302 is fixedly connected to the lower fixed frame 3, and the bottom plane of the front end of the first clamping block 301 is engaged with the lower part of the second mounting frame 2, and the upper inclined surface of the first clamping block 301 is slidably fitted with the lower guide block 207. After the first clamping block 301 is engaged with the second mounting frame 2, the lower fixed frame 3 and the lower part of the second mounting frame 2 are closed and maintained in a ring shape.

[0031] In the embodiment of the present disclosure, the two ends of the lower connecting column 105 are fitted with the upper grooves of the second mounting frame 2. When the limit pin 102 and the side hole of the upper limit frame 201 are slidably inserted, the upper limit frame 201 is fitted on the upper part of the lower connecting column 105, and the upper limit frame 201 is rotated and pressed down on the top of the lower connecting column 105. The first electric telescopic cylinder 101 is extended to push the limit pin 102 and the upper limit frame 201 to slide, and the position of the upper limit frame 201 is fixed. The upper limit frame 201 is fixed to the upper part of the lower connecting column 105, and the lower connecting column 105 and the second mounting frame 2 are fixed.

[0032] In the disclosed embodiment, when the lower guide block 207 moves downward and the upper inclined surface of the first clamping block 301 is pressed downward, the first clamping block 301 moves away from the second mounting rack 2, the limit latch 102 moves and separates from the upper limit rack 201, the upper limit rack 201 rotates upward, and the second mounting rack 2 naturally falls to the ground.

[0033] Embodiment 2, based on embodiment 1, the upper limit frame 201 is not set, the first electric telescopic cylinder 101 pushes the limit pin 102 to move and directly connect and fix with the slot of the second mounting frame 2, the second mounting frame 2 and the first mounting frame 1 are provided with laser for guidance and positioning, so that the automatic guidance of the UAV completes the fixing operation of the second mounting frame 2 and the first mounting frame 1, eliminating the situation of manual alignment of the personnel, thereby improving work efficiency.

[0034] The working principle of this embodiment is as follows: the first mounting frame 1 is fixedly connected to the drone by bolts, the second mounting frame 2 and the lower fixing frame 3 are fixed and separated by the item straps, the first electric telescopic cylinder 101, the upper connection port 103 and the control end line connector of the drone are connected, the first mounting frame 1 and the second mounting frame 2 and the lower fixing frame 3 and the mounted goods move with the drone, after the drone and the goods move into place, the drone lands and the goods come into contact with the ground, the second electric telescopic cylinder 206 is extended, the second electric telescopic cylinder 206 pushes the lower guide block 207 to move downward, the lower guide block 207 and the first electric telescopic cylinder 101 are connected ... and the lower guide block 207 and the first electric telescopic cylinder 101 are connected. The upper inclined surface of the card block 301 contacts, and the lower guide block 207 presses down the upper inclined surface of the first card block 301 to guide the first card block 301 to move outward and compress the support spring 302, the first card block 301 and the second mounting frame 2 move and separate, the lower fixing frame 3 moves downward away from the second mounting frame 2, and the strap between the lower fixing frame 3 and the second mounting frame 2 falls downward along with the opening of the lower fixing frame 3 and the second mounting frame 2, so that the cargo strap is separated, the first mounting frame 1 and the second mounting frame 2 are connected through the UAV remote control, the first mounting frame 1 and the second mounting frame 2 are separated by active control, and then the UAV returns to the initial position;

[0035] The first electric telescopic cylinder 101 is shortened, and the first electric telescopic cylinder 101 and the limit pin 102 move synchronously. The limit pin 102 moves and separates from the upper limit frame 201, and the upper limit frame 201 rotates upward, and the second mounting frame 2 naturally falls to the ground. The personnel again fix the second mounting frame 2 and the lower fixing frame 3 with straps. After the first mounting frame 1 and the second mounting frame 2 are separated, the external counterweight 203 presses the upper limit frame 201 downward to rotate outward, and the side guide ring 202 tilts upward. The lower connecting column 105 moves downward to dock with the top groove of the second mounting frame 2, and the side guide ring 202 moves downward synchronously. The side guide ring 202 moves downward and drives the upper limit frame 201 to rotate at the same time. The upper limit frame 201 rotates and presses down on the top of the lower connecting column 105. The first electric telescopic cylinder 101 extends to push the limit latch 102 and the upper limit frame 201 to slide, and the position of the upper limit frame 201 is fixed. The upper limit frame 201 is fixed to the upper part of the lower connecting column 105, and the lower connecting column 105 is fixed to the second mounting frame 2. The lower connecting column 105 is docked and fixed with the second mounting frame 2 as the drone descends, eliminating the need for personnel to manually dock the lower connecting column 105 with the second mounting frame 2, eliminating the need for personnel to dock under the hovering drone, making personnel safer, eliminating the time for waiting for the drone to land, reducing the take-off and landing time of the drone, shortening the mounting time, further shortening the distance between the drone and the lower mounted cargo, reducing the swaying and sliding of the drone cargo during movement, and reducing the unmanned operation pressure;

[0036] The upper connection port 103 and the lower connection port 204 are magnetically attracted to each other by the lower magnetic block 205 and the upper magnetic block 104 to ensure a snug connection. The upper connection port 103 and the lower connection port 204 ensure a snug fit for electric contact. At the same time, the magnetic attraction of the upper connection port 103 and the lower connection port 204 facilitates smooth separation as the first mounting rack 1 and the second mounting rack 2 are separated, thereby avoiding obstruction in the separation of the first mounting rack 1 and the second mounting rack 2.

[0037] In this article, there are a few points to note:

[0038] 1. The drawings of the embodiments of the present disclosure only involve structures related to the embodiments of the present disclosure, and other structures may refer to general designs.

[0039] 2. In the absence of conflict, the embodiments of the present disclosure and the features therein may be combined with each other to obtain new embodiments.

[0040] The above are only specific embodiments of the present disclosure, but the protection scope of the present disclosure is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present disclosure, which should be included in the protection scope of the present disclosure. Therefore, the protection scope of the present disclosure should be based on the protection scope of the claims.

Claims

1. A UAV mounting device, comprising: A first mounting frame (1), a second mounting frame (2) and a lower fixing frame (3); characterized in that the second mounting frame (2) is provided at the lower part of the first mounting frame (1), the lower end of the second mounting frame (2) is hingedly connected to the lower fixing frame (3), upper limit frames (201) are hingedly connected to both sides of the top of the second mounting frame (2), a side guide ring (202) is fixed to the side of the upper limit frame (201), an external counterweight (203) is fixed to the head end of the upper limit frame (201), a lower connecting port (204) is slidably provided in the middle of the second mounting frame (2), lower magnetic blocks (205) are fixed to both sides of the lower connecting port (204), a second electric telescopic cylinder (206) is fixed to both sides of the lower part of the second mounting frame (2), and the telescopic rod and the lower guide block (207) of the second electric telescopic cylinder (206) are fixed.

2. The drone mounting device according to claim 1, characterized in that: A lower connecting column (105) is welded to the lower end of the first mounting frame (1), a first electric telescopic cylinder (101) is fixed to both sides of the lower connecting column (105), a telescopic rod of the first electric telescopic cylinder (101) is fixedly connected to a limit latch (102), an upper connecting port (103) is fixed to the bottom of the lower connecting column (105), and upper magnetic blocks (104) are fixed to both sides of the upper connecting port (103).

3. The UAV mounting device according to claim 2, characterized in that: Both sides of the lower connecting column (105) are provided with axially sliding limit pins (102), the side guide ring (202) is extended to the lower part of the head end of the upper limit frame (201), the lower magnetic block (205) and the upper magnetic block (104) are attracted by opposite magnetic poles, the upper connecting port (103) and the lower connecting port (204) are vertically docked and electrically connected, and the lower connecting port (204) is electrically connected to the second electric telescopic cylinder (206).

4. The UAV mounting device according to claim 3, characterized in that: The two ends of the lower connecting column (105) fit in the upper grooves of the second mounting frame (2), and when the limit pin (102) and the side holes of the upper limit frame (201) are slidably inserted, the upper limit frame (201) fits in the upper part of the lower connecting column (105).

5. The UAV mounting device according to claim 1, characterized in that: A first clamping block (301) is slidably disposed at the front end of the lower fixing frame (3), a supporting spring (302) is fixed to the rear end of the first clamping block (301), and the rear end of the supporting spring (302) is fixedly connected to the lower fixing frame (3).

6. The UAV mounting device according to claim 5, characterized in that: The bottom plane of the first end of the first clamping block (301) is clamped with the lower part of the second mounting frame (2), and the upper inclined surface of the first clamping block (301) is slidably fitted with the lower guide block (207).

7. The UAV mounting device according to claim 6, characterized in that: When the lower guide block (207) moves downward and the upper inclined surface of the first clamping block (301) is pressed downward, the first clamping block (301) moves away from the second mounting frame (2).