Multifunctional flying platform based on unmanned aerial vehicle

Abstract

The utility model discloses a multifunctional flying platform based on an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle corollary equipment, which comprises a plurality of module cabins stacked up and down, and an isolation component positioned between two adjacent module cabins and used for fixing the two module cabins, the top supporting plate is arranged on the upper side of the stacked module cabins, and the bottom supporting plates are arranged on the upper side and the lower side of the stacked module cabins. The platform has multiple flight states, synchronous and distributed adjustment can be carried out according to flight requirements, in addition, the unmanned aerial vehicle platform can take off and land in a stacked state and can also be detached into a plurality of single modules to achieve landing and take-off of an unmanned aerial vehicle, and the landing platforms in the second nest and the first nest can also be rotated to the opposite directions, so that the unmanned aerial vehicle can take off and land. Or the unmanned aerial vehicle moves upwards synchronously, so that the unmanned aerial vehicle is in a stored state and an exposed state at the flying platform.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane supporting equipment technical field, especially in based on the multifunctional flight platform of unmanned plane. BACKGROUND

[0002] The unmanned plane flight platform (it is a kind of flight vehicle that can be autonomously or remotely controlled flight, is widely used in multiple fields, such as agricultural monitoring, environmental detection, disaster rescue, military reconnaissance, aerial photography, logistics distribution etc. The flight platform of unmanned plane can be designed with different structures and performance characteristics according to task demand.

[0003] The unmanned plane flight platform is integrally designed with nest, the existing unmanned plane platform is designed separately, and a unmanned plane is loaded in separate nest, when using, the nest is unfolded into flight platform, and the plane take-off platform is formed, and the mode has the following defects, first, it is inconvenient to carry, and each numbered unmanned plane needs to be repeatedly counted when being recycled and used, second, it occupies large space, third, it needs to be opened by artificial and used, and operation is inconvenient. UTILITY MODEL CONTENT

[0004] The utility model aims at providing multifunctional flight platform based on unmanned plane, solves the problem in the background art.

[0005] To realize the above-mentioned purpose, the utility model provides the following technical scheme: multifunctional flight platform based on unmanned plane, including multiple module cabins arranged in up-down stacking, isolation assembly between adjacent two module cabins and fixed two module cabins, top supporting plate arranged on the upper side of stacked module cabin, and bottom supporting plate arranged on the upper and lower sides of stacked module cabin.

[0006] Among them, the module cabin includes rotating mechanism, first nest and second nest arranged on the outer surface of the rotating mechanism, the first nest and the second nest are both provided with reversible landing platform, and the centering clamping device is arranged on the landing platform.

[0007] Further, the rotating mechanism includes bidirectional fixed sleeve shaft, the upper and lower ends of the bidirectional fixed sleeve shaft are both fixed with first rotating bearing sleeve and second rotating bearing sleeve through bearing sleeve, the first rotating bearing sleeve and the second rotating bearing sleeve are both fixedly connected with driving device, and the driving device is used to rotate the first rotating bearing sleeve and the second rotating bearing sleeve.

[0008] Further, the two driving devices comprise motor mounting seats arranged in rotation in the first rotating receiving sleeve or the second rotating receiving sleeve, the motor mounting seats are fixedly connected with servo motors, output ends of the servo motors are fixedly connected with receiving rotating plates, and the two receiving rotating plates are fixedly connected with inner walls of the second rotating receiving sleeve and the first rotating receiving sleeve respectively.

[0009] Further, the isolation assembly comprises an isolation plate, outer side walls of the isolation plate are fixedly connected with connecting pieces, and upper and lower sides of the connecting pieces are fixedly connected with butt joint shafts.

[0010] Further, the motor mounting seat is provided with a butt joint hole in an outer side, and the butt joint shafts are matched with the butt joint hole.

[0011] Further, the first nest and the second nest are both provided with open centering mechanisms with open mouths facing outward, and the open centering mechanisms have a state of gradually converging from an annular self-opening direction to the inside.

[0012] Further, the landing platform comprises a landing platform, the landing platform is located in a small-cavity cavity of the open centering mechanism, and one side of the landing platform is fixedly connected with a rotating mechanism.

[0013] Further, the centering clamping device comprises a centering clamp, one side of the centering clamp is fixedly connected with a telescopic mechanism, the telescopic mechanism is fixed with a rotating end of the rotating mechanism, and a free end of the telescopic mechanism is fixedly connected with one side of the centering clamp.

[0014] Further, the diameter of the top supporting plate is the same as the diameter of the second nest and the first nest, and the top supporting plate and the bottom supporting plate are both provided with connecting pieces.

[0015] Further, the two servo motors are arranged in opposite directions, and gaps are reserved on opposite sides of the first rotating receiving sleeve and the second rotating receiving sleeve.

[0016] Technical effects and advantages of the utility model:

[0017] 1. When the unmanned aerial vehicle is recycled, the open centering mechanism can guide the precisely descending unmanned aerial vehicle, so that the unmanned aerial vehicle lands on the central position, i.e. falls on the landing platform, and the unmanned aerial vehicle is clamped to the middle position by the centering clamps on both sides, so that the stability of the aircraft in clamping is ensured, the shaking during carrying is reduced, and the safety of the unmanned aerial vehicle is ensured.

[0018] 2. In specific use, the landing platform can rotate by 180 degrees, since the first nest and the second nest are integrated in the storage state, so that the two unmanned aerial vehicles can be rotated to the close state, when rotating out, the two landing platforms can shield the unmanned aerial vehicles, when taking off, the first nest and the second nest are staggered, and then the landing platform rotates the unmanned aerial vehicles to the upward state, thereby improving the safety and privacy of the unmanned aerial vehicles.

[0019] 3. The platform has multiple flight states, can be adjusted synchronously and distributed according to flight needs, and can take off and land in a stacked state, can be split into multiple single modules to realize unmanned aerial vehicle landing and taking off, and can rotate the landing platforms in the second nest and the first nest to opposite directions or synchronously upward, so that the unmanned aerial vehicles are in a storage state and an exposed state on the flight platform. BRIEF DESCRIPTION OF DRAWINGS

[0020] Figure 1 It is a stacked storage state perspective view of the utility model;

[0021] Figure 2 It is a first state schematic view of the utility model;

[0022] Figure 3 It is a second state schematic view of the utility model;

[0023] Figure 4 It is a sectional view of the rotating mechanism in the stacked state of the utility model;

[0024] Figure 5 It is a schematic view of the first nest of the utility model;

[0025] Figure 6 It is a partial sectional view of the first nest of the utility model.

[0026] In the drawing:

[0027] 1, bottom supporting plate; 2, top supporting plate; 3, isolation plate; 4, first nest; 5, second nest; 6, connecting piece; 7, first rotating receiving sleeve; 8, open centering mechanism; 9, landing platform; 10, second rotating receiving sleeve; 11, bidirectional fixed sleeve shaft; 12, servo motor; 13, receiving rotating plate; 14, butt joint shaft; 15, butt joint hole; 16, centering clamp; 17, telescopic mechanism; 18, rotating mechanism. DETAILED DESCRIPTION

[0028] Clearly and completely describe the technical scheme in the embodiments of the utility model with reference to the drawings in the embodiments of the utility model, obviously, the described embodiment is only a part of the embodiment of the utility model, and is not all the embodiment. Based on the embodiment in the utility model, all other embodiments obtained by the ordinary skill in the art without creative labor belong to the scope of the utility model protection.

[0029] Referring to Figures 1 to 6 The multi-functional flight platform based on unmanned aerial vehicle shown in the figure comprises a plurality of module cabins arranged in a stack, as shown in Figure 1 By stacking the plurality of module cabins, the plurality of unmanned aerial vehicles can be stacked in sequence according to the number, which effectively manages the plurality of unmanned aerial vehicles and occupies less space, facilitating the carrying and management of the operator.

[0030] The isolation assembly is located between the adjacent two module cabins and fixes the two module cabins, and the isolation assembly comprises an isolation plate 3, the outer side wall of the isolation plate 3 is fixedly connected with a connecting piece 6, the upper and lower sides of the connecting piece 6 are fixedly connected with a butt joint shaft 14, and the outer side of the motor mounting seat is provided with a butt joint hole 15, and the butt joint shaft 14 is matched with the butt joint hole 15.

[0031] The isolation assembly can splice the adjacent two module cabins, is used for maintaining the stability between the two module cabins, and can be used as a limiting piece when the two module cabins are rotated out, so as to ensure the stability of the rotation of the module cabin, and in addition, as a clamping mechanism for splicing, the safety of the stacked module cabin is improved.

[0032] Specifically, the butt joint shaft 14 on the connecting piece 6 is inserted into the butt joint hole 15 arranged on the module cabin.

[0033] A top supporting plate 2 arranged on the upper side of the stacked module cabin, and a bottom supporting plate 1 arranged on the upper and lower sides of the stacked module cabin.

[0034] The module cabin comprises a rotating mechanism, a first nest 4 and a second nest 5 arranged on the outer surface of the rotating mechanism, a reversible landing platform arranged in the first nest 4 and the second nest 5, and a centering clamping device arranged on the landing platform.

[0035] The rotating mechanism comprises a bidirectional fixed sleeve shaft 11, the upper and lower ends of the bidirectional fixed sleeve shaft 11 are fixedly sleeved with a first rotating bearing sleeve 7 and a second rotating bearing sleeve 10 through a bearing sleeve respectively, the first rotating bearing sleeve 7 and the second rotating bearing sleeve 10 are fixedly connected with a driving device, and the driving device is used for rotating the first rotating bearing sleeve 7 and the second rotating bearing sleeve 10.

[0036] The two drive devices include motor mounting bases rotatably disposed within the first rotating receiving sleeve 7 or the second rotating receiving sleeve 10. A servo motor 12 is fixedly connected to the motor mounting base. A receiving rotating plate 13 is fixedly connected to the output end of the servo motor 12. The two receiving rotating plates 13 are respectively fixedly connected to the inner walls of the second rotating receiving sleeve 10 and the first rotating receiving sleeve 7.

[0037] The rotating mechanism consists of a bidirectional fixed sleeve shaft 11, a first rotating receiving sleeve 7, and a second rotating receiving sleeve 10, which can realize independent or synchronous control of the two rotating components.

[0038] When moving synchronously, the first nest 4 and the second nest 5 rotate out synchronously, as follows: Figure 2 As shown, when they are out of sync, the first nest 4 and the second nest 5 rotate out respectively, as... Figure 3 As shown.

[0039] The bidirectional fixed shaft 11 serves as the central axis, providing fixed support for the first rotating bearing sleeve 7 and the second rotating bearing sleeve 10. This allows the first rotating bearing sleeve 7 and the second rotating bearing sleeve 10 to rotate at their respective positions on the bidirectional fixed shaft 11 under the drive of the servo motor 12, ensuring that the first machine nest 4 and the second machine nest 5 can be stored in a stacked state or unfolded into a platform state.

[0040] The purpose of this setup is to allow multiple drones to take off and land simultaneously, and to collect drones in a synchronized manner.

[0041] Both the first nest 4 and the second nest 5 are equipped with an open-ended centering mechanism 8 with its opening facing outward. The open-ended centering mechanism 8 has a ring-shaped structure that gradually narrows inward from the opening direction.

[0042] The landing platform includes a landing platform 9, which is located inside the small oral cavity of the open centering mechanism 8. A rotating mechanism 18 is fixedly connected to one side of the landing platform 9.

[0043] The centering clamping device includes a centering clamp 16, a telescopic mechanism 17 is fixedly connected to one side of the centering clamp 16, the telescopic mechanism 17 is fixed to the rotating end of the rotating mechanism 18, and the free end of the telescopic mechanism 17 is fixedly connected to one side of the centering clamp 16.

[0044] When recovering the drone, the open centering mechanism 8 can guide the drone to land accurately, so that the drone lands in the center position, that is, on the landing platform 9, and the centering clamps 16 on both sides clamp the drone to the center position, thus ensuring the stability of the aircraft in the clamping, reducing shaking during transportation, and ensuring the safety of the drone.

[0045] In specific use, the landing platform 9 can rotate by 180 degrees, since the first nest 4 and the second nest 5 are integrated in the storage state, so that the two unmanned aerial vehicles can be rotated to the close state, when rotating out, the two landing platforms 9 can shield the unmanned aerial vehicles, when taking off, the first nest 4 and the second nest 5 are staggered, then the landing platform 9 rotates the unmanned aerial vehicles to the upward state, thereby the safety and privacy of the unmanned aerial vehicles can be improved.

[0046] The diameter of the top supporting plate 2 is the same as that of the second nest 5 and the first nest 4, the top supporting plate 2 and the bottom supporting plate 1 are provided with the connecting pieces 6, and the overall appearance is improved.

[0047] The two servo motors 12 are oppositely arranged, and the first rotating receiving sleeve 7 and the second rotating receiving sleeve 10 are provided with gaps on opposite sides, so that the first rotating receiving sleeve 7 and the second rotating receiving sleeve 10 can be conveniently rotated, and the friction is reduced.

[0048] Finally, it should be noted that: the above only for the preferred embodiments of the present application, and not for limiting the present application, although the present application has been described in detail with reference to the foregoing embodiments, for those skilled in the art, it still can modify the technical solutions recorded in the foregoing embodiments, or make equivalent replacement for part of the technical features, any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application, should be included in the protection scope of the present application.

Claims

1. A multi-functional flying platform based on a drone, characterized in that, The module cabin includes a rotating mechanism, and a first nest (4) and a second nest (5) are arranged on the outer surface of the rotating mechanism, and a reversible landing platform is arranged in the first nest (4) and the second nest (5), and a centering clamping device is arranged on the landing platform. The rotating mechanism includes a bidirectional fixing sleeve shaft (11), the upper and lower ends of the bidirectional fixing sleeve shaft (11) are respectively fixedly sleeved with a first rotating receiving sleeve (7) and a second rotating receiving sleeve (10) through a bearing sleeve, and a driving device is fixedly connected in the first rotating receiving sleeve (7) and the second rotating receiving sleeve (10), and the driving device is used to rotate the first rotating receiving sleeve (7) and the second rotating receiving sleeve (10).

2. The multi-functional drone-based flying platform of claim 1, wherein, Two driving devices include a motor mounting seat rotatably arranged in the first rotating receiving sleeve (7) or the second rotating receiving sleeve (10), a servo motor (12) is fixedly connected on the motor mounting seat, an accommodating rotating plate (13) is fixedly connected to the output end of the servo motor (12), and the two accommodating rotating plates (13) are fixedly connected with the inner walls of the second rotating receiving sleeve (10) and the first rotating receiving sleeve (7) respectively.

3. The multi-functional drone-based flying platform of claim 2, wherein, The isolation component includes an isolation plate (3), and the outer side wall of the isolation plate (3) is fixedly connected with a connecting piece (6), and the upper and lower sides of the connecting piece (6) are fixedly connected with a butt joint shaft (14).

4. The multi-functional drone-based flying platform of claim 3, wherein, The outer side of the motor mounting seat is provided with a butt joint hole (15), and the butt joint shaft (14) is matched with the butt joint hole (15).

5. The multi-functional drone-based flying platform of claim 3, wherein, The first nest (4) and the second nest (5) are provided with an open centering mechanism (8) with an open mouth facing outward, and the open centering mechanism (8) has a state of gradually converging inward from the annular self-opening direction.

6. The multi-functional drone-based flying platform of claim 1, wherein, The landing platform includes a landing platform (9), and the landing platform (9) is located in the inner cavity of the open centering mechanism (8), and one side of the landing platform (9) is fixedly connected with a rotating mechanism (18).

7. The multi-functional drone-based flying platform of claim 6, wherein, The centering clamp (16) is fixedly connected with a telescopic mechanism (17) on one side, the telescopic mechanism (17) is fixed with the rotating end of the rotating mechanism (18), and the free end of the telescopic mechanism (17) is fixedly connected with one side of the centering clamp (16).

8. The multi-functional drone-based flying platform of claim 7, wherein, The diameter of the top supporting plate (2) is the same as the diameter of the second nest (5) and the first nest (4), and the top supporting plate (2) and the bottom supporting plate (1) are provided with connecting pieces (6).

9. The multi-functional drone-based flying platform of claim 8, wherein, Two servo motors (12) are arranged in opposite directions, and a gap is reserved on the opposite side of the first rotating receiving sleeve (7) and the second rotating receiving sleeve (10).

10. The multi-functional drone-based flying platform of claim 9, wherein, ​

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