A method for rapidly launching a swarm of micro-rotor drones
Through the constraint device and connection mechanism in the storage device, the rapid release of the micro-rotor drone group is realized, solving the problem of cumbersome release operation in the prior art, improving efficiency and increasing storage capacity.
Patent Information
- Application Number
- CN202210966040.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-08-12
- Publication Date
- 2025-09-02
- Estimated Expiration
- 2042-08-12
AI Technical Summary
In the prior art, the operation of unloading drones is complicated, especially the group consisting of multiple drones cannot complete all the reloading tasks in a short time, which is inefficient.
A method of rapid release of micro rotor drone is adopted, and the constraint device, base and connection mechanism in the storage device is used to unfold the base by rotating the wall panel, removing the constraints, and applying outward tension to achieve rapid flattening and release of micro rotor drone wings.
It has realized that all micro-rotor drone groups are released in a short time, with short operating time and high working efficiency, and the storage device stores more drones in a limited volume.
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Figure CN117622684B_ABST
Abstract
Description
Technical Field
[0001] The present invention belongs to the field of micro-UAVs, and in particular relates to a method for quickly launching a group of micro-rotor UAVs. Background Art
[0002] A drone, short for unmanned aerial vehicle, is an unmanned aerial vehicle controlled by a radio remote control device and its own programmable control unit. Compared to manned aircraft, it offers advantages such as small size, low cost, and ease of use. From a technical perspective, drones can be categorized as unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned multi-rotor aircraft, and unmanned paragliders. From an application perspective, they can be divided into military and civilian applications. In the military, drones are divided into reconnaissance aircraft and target drones. In civilian applications, drones can be used in aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, store inspections, disaster relief, film and television production, and creating romance.
[0003] Patent CN 210122122U discloses a multi-rotor drone storage box, comprising a housing and a shock-absorbing base. The shock-absorbing base includes multiple slots for detachable rotor arms and two slots for landing poles. This box improves storage space utilization, reduces overall volume, and facilitates drone transportation. However, its drawback is that launching the drones is cumbersome and inefficient, especially when operating a swarm of drones, making it difficult to launch all of them simultaneously. Summary of the Invention
[0004] The technical problem to be solved by the present invention is to provide a method for quickly releasing a swarm of micro-UAVs and a storage device thereof.
[0005] To achieve the above object, the present invention adopts the following technical solutions:
[0006] The present invention relates to a method for quickly launching a micro-rotor drone, which comprises the following steps:
[0007] 1) Place a storage device for storing a micro-rotor drone in a suitable location; the storage device includes a storage box, a restraint device, a base, and a connecting mechanism; the storage box has at least three wall panels rotatably connected to a bottom panel; the restraint device is used to restrain the wings of the micro-rotor drone; there are multiple bases for accommodating the micro-rotor drone; the connecting mechanism is used to connect two adjacent bases and can be converted between a retracted state and an expanded state as needed; the restraint device, base, and connecting mechanism are located inside the storage box;
[0008] 2) Lay the rotatable wall panel of the storage box flat;
[0009] 3) Remove the restraints on the wings of the micro-rotor drone and apply an outward pulling force to the base to unfold all connecting mechanisms and move all bases away;
[0010] 4) The wings of the micro-rotor drone gradually flatten when the constraints are removed and there is enough space;
[0011] 5) Use the remote control device to launch the micro-rotor drone with its wings flattened.
[0012] Preferably, before applying an outward pulling force to the base to deploy all the connecting mechanisms, the restraint device restraining the micro-rotor drone is first removed.
[0013] Preferably, the operation of applying an outward pulling force to the base to unfold all the connecting mechanisms is performed simultaneously with the removal of the constraints on the micro-rotor UAV by the restraint device.
[0014] Preferably, the restraint device and the base are an integrated structure; the base includes a placement slot, an installation slot and a storage slot; the placement slot is used to place the bottom end of the main body of the micro-rotor drone; the installation slot is used to place the connecting mechanism; the storage slot is a restraint device and is a non-through structure.
[0015] Preferably, the restraint device and the base are separate structures; the base includes a placement slot and an installation slot; the placement slot is used to place the bottom end of the main body of the micro-rotor drone; and the installation slot is used to place the connecting mechanism.
[0016] Further preferably, the connecting mechanism is a hinge, including three hinge axes and four hinge pieces; the mounting groove is composed of a communicating bottom plate groove and a side wall groove, and is located at the junction of the side plate and the bottom plate of the base; the hinges at both ends of the connecting mechanism are respectively located in the bottom plate grooves of the two adjacent bases.
[0017] Further preferably, the base is composed of multiple structural units, and the number of structural units is consistent with the number of wings of the micro-rotor drone; adjacent structural units are connected by means of a connecting device; the connecting device can realize the conversion between the retracted state and the expanded state as needed.
[0018] Further preferably, the restraining device is a block, and a vertical groove is opened on its outer wall; the base also includes a storage groove; the storage groove is a through structure, and the block is placed in the storage groove in a rotatable manner; the installation groove is a vertical groove, which is connected with the vertical groove of the block; the connecting mechanism is a hinge structure, which is composed of two groups of chains, each group of chains is composed of multiple chains connected in series, and the two adjacent chains are rotatably connected at the ends; the corresponding chains of the two groups of chains are rotatably connected at non-end positions; the ends of one group of chains of the connecting mechanism are rotatably placed in the vertical groove of the block, and the ends of the other group of chains are rotatably placed in the installation groove.
[0019] Preferably, the storage device further comprises four traction ropes, which are respectively located between the four wall panels and the base of the storage box; the traction ropes are connected to all the blocks located at the outermost sides.
[0020] The present invention provides a method for rapidly launching a swarm of micro-rotor drones. Using a storage device, a swarm of micro-rotor drones with wings in a retracted state can be quickly launched, offering advantages such as short operation time and high efficiency. The dedicated storage device, when storing the micro-rotor drones, uses a restraining device to constrain the retracted wings, preventing them from unfolding within the storage box, thereby effectively reducing storage volume and allowing more micro-rotor drones to be stored within the box's limited volume. When launching the micro-rotor drones, a connecting mechanism separates the bases, allowing the drones to be quickly separated and the wings of the unconstrained micro-rotor drones to unfold smoothly for launch. BRIEF DESCRIPTION OF THE DRAWINGS
[0021] Figure 1 It shows a schematic diagram of the structure of the storage device of the first embodiment when it is folded;
[0022] Figure 2 It shows a schematic structural diagram of the storage device of the first embodiment when it is unfolded;
[0023] Figure 3 It shows the schematic diagram of the storage plate structure of the first embodiment;
[0024] Figure 4 It shows a schematic diagram of the base structure of the first embodiment;
[0025] Figure 5 It shows a schematic diagram of the base structure of the second embodiment;
[0026] Figure 6 It shows a schematic diagram of the base structure of the third embodiment;
[0027] Figure 7 It shows a schematic diagram of the combined structure of the base, the stopper and the connecting mechanism of the fifth embodiment;
[0028] Figure 8 The diagram shows the connection between the traction rope and the block in the fifth embodiment.
[0029] Among them, 1-micro rotor drone, 2-storage box, 3-constraint plate, 31-constraint hole, 4-base, 41-placement slot, 42-installation slot, 43-storage slot, 44-connecting device, 5-connecting mechanism, 6-stop block, 7-traction rope. DETAILED DESCRIPTION
[0030] The present invention will be further described in detail below with reference to the embodiments and the accompanying drawings, but they are not intended to limit the technical solutions of the present invention.
[0031] Example 1
[0032] The micro-rotor drone 1 of this embodiment has a cylindrical main body with four circumferentially evenly distributed wings, which are rotatably connected to the main body at the wing roots.
[0033] The storage device for a micro-rotor drone group includes a storage box 2, a constraint plate 3, a base 4 and a connecting mechanism 5. Figure 1 and 2 shown.
[0034] The storage box 2 is composed of a box cover and a box body, wherein the rear wall of the box body is fixedly connected to the bottom plate, and the left, right and front wall plates are rotatably connected to the bottom plate by hinges. When the box is folded, the left and right wall plates are respectively connected to the front and rear wall plates with buckles.
[0035] The constraint plate 3 is a flat plate structure with 5 rows and 10 columns in the middle, totaling 50 constraint holes 31. The constraint hole 31 is a circular through hole in the middle, and four circumferentially evenly distributed square grooves are opened outward from its outer circumference. The structural dimensions of the grooves match the wing shape of the micro-rotor drone 1. Figure 3 shown.
[0036] The base 4 is a square structure with a mounting groove 41 on the top. The inner diameter of the circular structure is consistent with the outer diameter of the main body of the micro-rotor drone 1. The four side panels and the bottom panel are respectively provided with mounting grooves 42, which are composed of interconnected bottom panel grooves and side wall grooves. Figure 4 shown.
[0037] The connecting structure 5 is a hinge, which includes three hinge shafts and four hinge pieces.
[0038] The storage device for a swarm of micro-rotor drones of this embodiment includes 50 bases 4, which are placed in a storage box 2. Among them, in a row of bases 4 that are in contact with the rear wall of the storage box 2, the base 4 near the middle position is fixedly connected to the rear wall of the storage box 2; two adjacent bases 4 are connected by a connecting mechanism 5. When connected, the hinges at both ends of the connecting mechanism 5 are respectively fixed in the bottom plate grooves of two adjacent mounting grooves 42.
[0039] When using the storage device of this embodiment to store a group of micro-rotor drones, the storage box 2 is retracted, with adjacent bases 4 in close contact. The two hinges in the middle of the connecting structure 5 are bent upward and stored in the sidewall grooves of two adjacent mounting slots 42. Each base 4 has a micro-rotor drone 1 placed in its placement slot 41, with its wings rotated downward and stowed. The restraining plate 3 is located within the storage box 2, above the base 4. Its restraining holes 31 fit over the micro-rotor drone 1 with its wings retracted, preventing the wings from unfolding within the storage box 2.
[0040] When flying a swarm of micro-rotor drones, first, open the lid of the storage box 2, loosen the connecting buckles of the side panels of the box, and flatten and unfold the front, left and right side panels; then remove the constraint plate 3 from the top, apply outward pulling force to the base 4 from the front, left and right directions, and the hinges of the connecting mechanism 5 gradually flatten as the base 4 moves, and the wings of the micro-rotor drone 1 also gradually flatten. Under the control of the remote control, the wings rotate, and the micro-rotor drone 1 flies out of the storage box 2.
[0041] The micro-rotor UAV group stored by the storage device of this embodiment can realize the takeoff of any number of micro-rotor UAVs under the control of the remote controller as needed.
[0042] Example 2
[0043] The difference from Example 1 is that:
[0044] The storage device for a micro-rotor drone swarm of this embodiment includes a storage box 2 , a base 4 and a connecting mechanism 5 .
[0045] The base 4 has a placement slot 41 with four circumferentially evenly distributed square receiving slots 43. Figure 5 shown.
[0046] When using the storage device of this embodiment to store a group of micro-rotor drones, first fold up the wings of the micro-rotor drone 1 and insert it into the placement groove 41 of the base 4. The wings fall into the storage groove 43 and are constrained by it.
[0047] When using the storage device of this embodiment to release a group of micro-rotor drones, first, according to the number of drones to be released, the corresponding micro-rotor drone 1 is pulled upward from the placement slot 41 by a certain distance until the wings are free from the constraints of the storage slot 43 and are in an unfolded state; then the micro-rotor drone 1 is released to maintain its vertical state in the storage box 2; finally, under the control of the remote control, the wings rotate and the micro-rotor drone 1 flies out of the storage box 2.
[0048] Example 3
[0049] The difference from Example 2 is that:
[0050] The base 4 of this embodiment is composed of four identical structural units, and a connecting device 44 is provided at the connection between two adjacent structural units. The connecting device 44 is a hinge. Figure 6 shown.
[0051] When a group of micro-rotor drones is launched using the storage device of this embodiment, when an outward pulling force is applied to the base 4, the four structural units constituting the base 4 move away from each other, driving the hinge to extend, and the wings of the micro-rotor drone 1 break free from the constraints of the storage slot 43 and gradually flatten.
[0052] The storage device of this embodiment eliminates the need to manually release the wing restraints when launching the micro-rotor drone 1, thereby further shortening the launch time and improving the launch efficiency. In addition, as the structural units of the base 4 move away from each other, the friction force during the launch of the micro-rotor drone can be reduced.
[0053] Example 4
[0054] The difference from Example 3 is that:
[0055] The connecting device 44 is a spring.
[0056] In the storage device of this embodiment, after the wings of the micro-rotor drone 1 are flattened and the tension is removed, the four structural units of the base 4 are rebounded by the springs and restored to the assembled state, thereby shortening the reassembly time of the storage device.
[0057] Example 5
[0058] The difference from Example 1 is that:
[0059] The storage device for a micro-rotor drone swarm of this embodiment includes a storage box 2 , a base 4 , a connecting mechanism 5 , a stopper 6 and a traction rope 7 .
[0060] The storage box 2, the box cover and the rear wall plate and the four wall plates and the bottom plate are all rotatably connected by hinges. A sealing strip is set at the wall plate joint to ensure the sealing of the storage box 2.
[0061] The base 4 has a placement slot 41 with four circumferentially evenly distributed through receiving slots 43, and a vertical mounting slot 42 in the middle of the side wall. Figure 6 shown.
[0062] The connecting mechanism 5 is a hinge structure, which is composed of two sets of symmetrically arranged chains. Each set of chains is connected by two square bars at the ends in a rotatable manner, and the corresponding square bars of the two sets of chains are connected in a rotatable manner in the middle position. Figure 7 shown.
[0063] The stopper 6 is a square block with a vertical groove on its outer wall, and its structural dimensions match the vertical mounting groove 42.
[0064] The storage device for a micro-rotor drone swarm of this embodiment includes 25 bases 4 placed in a storage box 2, wherein the base 4 at the center is fixedly connected to the bottom plate of the storage box 2. A block 6 is placed in the through storage groove 43 of the base 4, and the two are rotatably connected, wherein the vertical groove of the block 6 is connected to the vertical mounting groove 42. Four traction ropes 7 are respectively located between the four wall panels of the storage box 2 and the base 4; the traction ropes 7 are connected to all the block 6 located on the outermost side by means of elastic pull ropes, such as Figure 8 shown.
[0065] When the storage box 2 is in the retracted state, adjacent bases 4 are in close contact; the two chains of the connecting structure 5 are in a tightened state, stored in the vertical mounting slots 42 and vertical slots of the adjacent bases 4 and the stopper 6. Each micro-rotor drone 1 placed in the base 4 has its wings restrained by the stopper 6 and in a retracted downward position.
[0066] To launch a swarm of micro-rotor drones, first open the lid of storage box 2, loosen the latches connecting the side panels, and flatten the front, left, and right side panels. Then, pull base 4 outward from the front, left, and right. The hinges of connecting mechanism 5 gradually flatten as base 4 moves. Driven by connecting mechanism 5, stoppers 6 rotate outward. Unconstrained by the constraints, the wings of micro-rotor drones 1 automatically rotate upward, gradually flattening. Under the control of the remote control, the wings rotate, and micro-rotor drones 1 fly out of storage box 2.
Claims
1. A method for rapidly launching a group of micro-rotor drones, characterized in that: Here are the steps: 1) placing a storage device for storing a micro-rotor drone (1) in a suitable position; the storage device comprises a storage box (2), a restraining device, a base (4) and a connecting mechanism (5); at least three wall panels of the storage box (2) are rotatably connected to the bottom plate; the restraining device is used to restrain the wings of the micro-rotor drone (1); there are multiple bases (4) for placing the micro-rotor drone (1); the connecting mechanism (5) is used to connect two adjacent bases (4), and can realize the conversion between the contracted state and the expanded state as required, thereby driving the two adjacent bases (4) to approach or separate; the restraining device, the base (4) and the connecting mechanism (5) are all located inside the storage box (2); the restraining device and the base (4) are split structures; the base (4) comprises a placement groove (41) and an installation groove (42); the placement groove (41) is used to place the bottom end of the main body of the micro-rotor drone (1); the installation groove (42) is used to place the connecting mechanism (5); the base (4) consists of multiple The structure is composed of structural units, the number of which is consistent with the number of wings of the micro-rotor drone (1); adjacent structural units are connected by means of a connecting device (44); the connecting device (44) can realize the conversion between the retracted state and the expanded state as needed; the restraining device is a stopper (6), the outer wall of which is provided with a vertical groove; the base (4) also includes a receiving groove (43); the receiving groove (43) is a through structure, and the stopper (6) is rotatably placed in the receiving groove (43); the mounting groove (42) is a vertical groove, which is connected to the vertical groove of the stopper (6); the connecting mechanism (5) is a hinge structure, consisting of two groups of chains, each group of chains consisting of a plurality of chains connected in series, and the two adjacent chains are connected in a rotatable manner at the ends; the corresponding chains of the two groups of chains are connected in a rotatable manner at non-end positions; the ends of one group of chains of the connecting mechanism (5) are rotatably placed in the vertical groove of the stopper (6), and the ends of the other group of chains are rotatably placed in the mounting groove (42); 2) Lay the rotatable wall panel of the storage box (2) flat; 3) removing the restraint device from the wings of the micro-rotor drone (1), and applying an outward pulling force to the base (4) so that all the connecting mechanisms (5) are unfolded and all the bases (4) are separated from each other; 4) The wings of the micro-rotor drone (1) gradually flatten out when the constraints are removed and there is enough space; 5) Use the remote control device to launch the desired micro-rotor drone (1) with its wings flattened.
2. The method for rapidly launching a swarm of micro-rotor drones according to claim 1, characterized in that: Before applying an outward pulling force to the base (4) to deploy all the connecting mechanisms (5), the restraint device restraining the micro-rotor drone (1) is first removed.
3. The method for rapidly launching a swarm of micro-rotor drones according to claim 1, characterized in that: The operation of applying an outward pulling force to the base (4) to unfold all the connecting mechanisms (5) is performed simultaneously with the removal of the restraint of the micro-rotor drone (1) by the restraint device.
4. The method for rapidly launching a swarm of micro-rotor drones according to claim 1, characterized in that: The storage device further comprises four traction ropes (7) respectively located between the four wall panels and the base (4) of the storage box (2); the traction ropes (7) are connected to all the outermost blocks (6).
Citation Information
Patent Citations
Multi-rotor unmanned aerial vehicle storage box
CN210122122U
Storage device for miniature rotor unmanned aerial vehicle group
CN218705571U