A UAV cluster launching device

Abstract

The utility model discloses a drone cluster launch device, which belongs to the technical field of drone launch devices. It includes: a movable base, a rotating mechanism, a first lifting member, a second lifting member, and a launch tube; the movable base includes: a support frame, a walking part arranged in the support frame, and a counterweight part arranged on the top surface of the support frame; the rotating mechanism is arranged on the counterweight part; the rotating mechanism includes: the drive assembly, and a rotating member connected to the drive assembly by transmission; the first lifting member and the second lifting member are correspondingly arranged on the rotating member; the bottom surface of the launch tube is connected to the first lifting member and the second lifting member. The utility model realizes the all-round adjustment of the launch orientation of the drone cluster, which is no longer limited to a single direction; the drone cluster can quickly respond to the needs of various complex environments and changing tasks, and enhance flexibility and effectiveness.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicle launching devices, and in particular relates to a unmanned aerial vehicle cluster launching device. Background Art

[0002] With the rapid advancement of drone technology, the efficient deployment and rapid launch capabilities of drone swarms have become the key to improving application efficiency.

[0003] Traditional drone cluster launch devices often use hydraulic cylinder lifting technology to adjust the launch angle of drones, but this method can only achieve angle adjustment in a single direction and cannot change the direction or orientation of the launch in all directions; moreover, the entire device is bulky and inconvenient to carry and operate.

[0004] In drone application scenarios where frequent changes in launch positions or rapid responses are required, this design obviously cannot meet actual needs. Utility Model Content

[0005] Purpose of the utility model: In order to solve the above-mentioned problems, the utility model provides a UAV cluster launching device.

[0006] Technical solution: A UAV cluster launching device, comprising:

[0007] The movable base comprises: a support frame, a walking portion arranged in the support frame, and a counterweight portion arranged on the top surface of the support frame;

[0008] A rotating mechanism is arranged on the counterweight part; the rotating mechanism comprises: a driving assembly, and a rotating member connected to the driving assembly in a transmission manner;

[0009] A first lifting member and a second lifting member are correspondingly arranged on the rotating member;

[0010] The bottom surface of the launching tube is connected to the first lifting member and the second lifting member.

[0011] In a further embodiment, the rotating member includes a disc portion, and an expansion portion disposed at an edge of the disc portion and extending outward.

[0012] In a further embodiment, the first lifting member is disposed at a center position of the disc portion.

[0013] In a further embodiment, it also includes:

[0014] A connecting rod is arranged on the extension part; the connecting rod is connected to the second lifting member.

[0015] In a further embodiment, it also includes:

[0016] A first connecting block, provided at an output end of the first lifting member;

[0017] The second connecting block is arranged at the output end of the second lifting member.

[0018] In a further embodiment, the bottom of the launch tube is provided with a first snap-in groove and a second snap-in groove;

[0019] The first clamping slot is adapted to be connected to the first connecting block, and the second clamping slot is adapted to be connected to the second connecting block.

[0020] In a further embodiment, a pushing rod is provided on the support frame.

[0021] In a further embodiment, the first lifting member and the second lifting member are hydraulic cylinders.

[0022] In a further embodiment, the walking part is an electric walking wheel.

[0023] In a further embodiment, the counterweight portion is a counterweight block.

[0024] Beneficial effects:

[0025] (1) The utility model uses a driving assembly to drive the rotating member to rotate, thereby driving the first lifting member, the second lifting member and the launch tube to rotate, so as to adjust the launch direction of the UAV cluster; after the direction is adjusted, the first lifting member and the second lifting member are controlled to rise and fall based on demand to adjust the angle of the launch tube and the launch angle of the UAV cluster; the launch direction of the UAV cluster can be adjusted in all directions, no longer limited to a single direction; the UAV cluster can quickly respond to the needs of various complex environments and changing tasks, and enhance flexibility and effectiveness;

[0026] (2) The utility model is provided with a supporting frame, a walking part, and a counterweight part; the arrangement of the walking part enables the device to move freely in different terrains and environments, greatly enhancing the maneuverability and flexibility of the device; the counterweight part effectively balances the center of gravity of the device, further improving the stability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Figure 1 It is a structural schematic diagram of the utility model;

[0028] Figure 2 It is a partial structural schematic diagram of the utility model.

[0029] Figure 1 to Figure 2 The markings are as follows: support frame 1, walking part 2, counterweight part 3, driving assembly 4, rotating part 5, disc part 51, expansion part 52, first lifting part 6, second lifting part 7, launching tube 8, connecting rod 9, first connecting block 10, second connecting block 11, pushing rod 12. DETAILED DESCRIPTION

[0030] Example 1

[0031] like Figure 1 to Figure 2 As shown, this embodiment provides a UAV cluster launching device, including: a movable base, a rotating mechanism, a first lifting member 6, a second lifting member 7, and a launching tube 8.

[0032] The movable base includes: a support frame 1, multiple groups of walking parts 2, and a counterweight part 3. A push rod 12 is provided on the support frame 1. The walking parts 2 are arranged in an array inside the support frame 1. The walking parts 2 are electric walking wheels, which are driven by a motor to rotate and walk. The counterweight part 3 is fixed on the top surface of the support frame 1. The counterweight part 3 is a counterweight block; the counterweight block is used to adjust the center of gravity position of the device to ensure the balance and stability of the device.

[0033] The rotating mechanism includes: a driving assembly 4 disposed on the top surface of the counterweight, and a rotating member 5 connected to the driving assembly 4. The driving assembly 4 uses a servo motor, a transmission gear, a transmission shaft, etc. to drive the rotating member 5 to rotate. The rotating member 5 includes a disc portion 51 and an extension portion 52 disposed on the edge of the disc portion 51 and extending outward.

[0034] The first lifting member 6 and the second lifting member 7 are hydraulic cylinders. The first lifting member 6 is installed at the center of the disc portion 51. The second lifting member 7 is connected to the extension portion 52. A connecting rod 9 is provided between the second lifting member 7 and the extension portion 52. The connecting rod 9 is fixed to the extension portion 52. In this embodiment, the second lifting member 7 is provided in two groups. The first lifting member 6 and the second lifting member 7 together provide a more uniform and stable support for the launch tube 8, effectively reducing the shaking and tilting during the launch process, thereby ensuring the accuracy and safety of the launch.

[0035] The bottom surface of the launch tube 8 is connected to the first lifting member 6 and the second lifting member 7. The launch tube 8 is provided with a plurality of cavities for accommodating the UAV. In this example, compressed air is used as a power source for catapult-type launching of the UAV, which is a prior art and will not be described in detail here.

[0036] In a further embodiment, the output end of the first lifting member 6 is installed with a first connection block 10, and the output end of the second lifting member 7 is installed with a second connection block 11. The first lifting member 6 and the first connection block 10, and the second lifting member 7 and the second connection block 11 can be connected by threaded connection or pin shaft.

[0037] The bottom of the launch tube 8 is provided with a first snap-in groove and a second snap-in groove. The first snap-in groove is adapted to be connected with the first connection block 10, and the second snap-in groove is adapted to be connected with the second connection block 11. The above structure can realize the rapid disassembly and assembly between the launch tube 8 and the first lifting member 6 and the second lifting member 7, thereby improving the working efficiency.

[0038] Here’s how it works:

[0039] When launching a cluster of drones, at any orientation, the first lifting member 6 and the second lifting member 7 are lifted and lowered to drive the launching tube 8 to adjust the angle, so as to adjust the launching angle of the drone cluster; the driving assembly 4 drives the rotating member 5 to rotate, and the rotating member 5 drives the first lifting member 6, the second lifting member 7 and the launching tube 8 to adjust the orientation, thereby realizing the adjustment of the launching orientation of the drone cluster.

Claims

1. A drone cluster launching device, characterized in that: include: The movable base comprises: a support frame, a walking portion arranged in the support frame, and a counterweight portion arranged on the top surface of the support frame; A rotating mechanism is arranged on the counterweight part; the rotating mechanism comprises: a driving assembly, and a rotating member connected to the driving assembly in a transmission manner; A first lifting member and a second lifting member are correspondingly arranged on the rotating member; The bottom surface of the launching tube is connected to the first lifting member and the second lifting member.

2. A UAV cluster launching device as claimed in claim 1, characterized in that: The rotating member comprises a disc portion and an expansion portion which is arranged at the edge of the disc portion and extends outward.

3. A UAV cluster launching device as claimed in claim 2, characterized in that: The first lifting member is arranged at the center of the disc portion.

4. The UAV cluster launching device according to claim 2, characterized in that: Also includes: A connecting rod is arranged on the extension part; the connecting rod is connected to the second lifting member.

5. The UAV cluster launching device according to claim 1, characterized in that: Also includes: A first connecting block, provided at an output end of the first lifting member; The second connecting block is arranged at the output end of the second lifting member.

6. The UAV cluster launching device according to claim 5, characterized in that: The bottom of the launch tube is provided with a first clamping groove and a second clamping groove; The first clamping slot is adapted to be connected to the first connecting block, and the second clamping slot is adapted to be connected to the second connecting block.

7. The UAV cluster launching device according to claim 1, characterized in that: A pushing rod is arranged on the supporting frame.

8. The UAV cluster launching device according to claim 1, characterized in that: The first lifting member and the second lifting member are hydraulic cylinders.

9. The UAV cluster launching device according to claim 1, characterized in that: The walking part is an electric walking wheel.

10. The UAV cluster launching device according to claim 1, characterized in that: The counterweight part is a counterweight block.

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