Logistics unmanned aerial vehicle with separated cargo hold

Abstract

The utility model discloses a logistics unmanned aerial vehicle with a separated cargo hold, which comprises a main body component, a plurality of supporting components, a plurality of supporting components and a plurality of supporting components, wherein the main body component comprises an unmanned aerial vehicle and a cargo hold; the hoisting component comprises a groove, a supporting frame, a tensioning spring and a limiting plate; the shielding part comprises a baffle plate; the unmanned aerial vehicle is arranged above the cargo hold, the grooves are symmetrically formed in the top face of the cargo hold, the supporting frames are symmetrically and fixedly connected to the bottom of the unmanned aerial vehicle, and the baffles are symmetrically and fixedly connected to the side walls of the two sides of the grooves. The problems that when an existing unmanned aerial vehicle transports goods, a cargo hold containing the goods must be hoisted, if the bottom of the cargo hold makes contact with the ground, the unmanned aerial vehicle cannot fly forwards, meanwhile, due to the fact that the unmanned aerial vehicle deflates the cargo hold through manual work or a telescopic sling, the cargo hold needs to be placed manually, and the cargo hold cannot fly forwards are solved. And therefore, the problem that the unmanned aerial vehicle is inconvenient to use due to the increased labor force of workers is solved.

Description

Technical Field

[0001] The utility model relates to the technical field of logistics unmanned aerial vehicles, in particular to a logistics unmanned aerial vehicle with a detachable cargo hold. Background Art

[0002] The logistics drone is controlled by remote control, so that the drone can move the goods that need to be transported and carry out transportation work. The transportation gravity of this type of drone can reach ten kilograms, which can provide convenience for the transportation of goods.

[0003] However, it still has the following disadvantages in actual use:

[0004] When existing drones are transporting goods, the cargo hold containing the goods must be lifted. If the bottom of the cargo hold touches the ground, the drone cannot fly forward. At the same time, since the drone uses manual or telescopic slings to deflat the cargo hold, it is necessary to manually position the cargo hold, which increases manual labor and makes the use of drones inconvenient. Utility Model Content

[0005] The purpose of the utility model is to provide a logistics drone with a detachable cargo hold to solve the problem raised in the above-mentioned background technology that, when existing drones are transporting goods, the cargo hold containing the goods must be lifted. If the bottom of the cargo hold touches the ground, the drone cannot fly forward. At the same time, since the drone deflates the cargo hold manually or with a telescopic sling, it is necessary to manually position the cargo hold, which increases the manual labor and makes the use of the drone inconvenient.

[0006] In order to solve the above technical problems, the utility model is realized by the following technical solutions:

[0007] The utility model is a logistics drone with a detachable cargo hold, comprising:

[0008] The main body components include the drone and the cargo hold;

[0009] A hoisting component, the hoisting component comprising a groove, a support frame, a tension spring and a limit plate;

[0010] A shielding component, wherein the shielding component comprises a baffle;

[0011] The UAV is arranged above the cargo hold, the groove is symmetrically arranged inside the top surface of the cargo hold, the support frame is symmetrically fixedly connected to the bottom of the UAV, the baffle is symmetrically fixedly connected to the side walls on both sides of the groove, and the top surface of the baffle is level with the top surface of the cargo hold, the limit plates are respectively arranged inside the groove and below the baffle, the right ends of the limit plates are hinged to the right side wall of the groove, the tensioning spring is symmetrically arranged inside the groove, the top of the tensioning spring is fixedly connected to the right bottom surface of the limit plate, and the bottom of the tensioning spring is fixedly connected to the right side wall of the groove, and the distance between the two baffles is less than the length of the limit plate.

[0012] Furthermore, the hoisting component also includes a through hole and a limiting rod;

[0013] The through hole is arranged inside the support frame, the limiting rod is fixedly connected to the side wall of the support frame and is arranged on the left side of the through hole, and the limiting rod and the side wall of the limiting plate are fitted to each other.

[0014] Furthermore, the hoisting component also includes a connecting groove;

[0015] The connecting groove is arranged on the bottom surface of the limiting plate, and the connecting groove is a semicircular groove.

[0016] Further, it includes a moving part, and the moving part includes a universal wheel;

[0017] The universal wheels are symmetrically fixedly installed on both sides of the bottom surface of the cargo hold.

[0018] Furthermore, the length of the limiting rod is smaller than the thickness of the limiting plate.

[0019] Furthermore, the connecting parts of the support frame are all round tubes, and the width of the groove is greater than the width of the support frame.

[0020] Compared with the prior art, the advantages of the present invention are:

[0021] According to the utility model, when transporting the cargo hold, the drone is controlled to move the support frame to the top of the groove, so that the support frame squeezes the limit plate, and the left end of the limit plate moves downward until the support frame enters the interior of the groove. Under the action of the tensioning spring, the limit plate can be reset, and when the drone is lifted, the support frame will enter the interior of the connecting groove, and the limit plate can be shielded by the baffle. After placing the cargo hold, the drone is moved downward to move the limit rod to the bottom of the limit plate, and then the drone is moved to the position so that the limit plate is in the through hole position. When the drone is moved upward, the cargo hold can be conveniently placed stably, and the drone can move to a new position.

[0022] Based on the above beneficial effects, through the cooperation between the support frame and the limit plate, the support frame can be easily entered into the interior of the limit plate, and through the cooperation between the limit plate and the baffle, the cargo hold can be easily lifted. When lowering the cargo hold, the limit plate is moved to the through hole, so that the drone can be easily separated from the cargo hold, and when the cargo hold is on land, the universal wheels set at the lower end can be used to conveniently use the drone to drive the cargo hold to move, which can reduce the time of lifting the drone and protect it. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings required for describing the embodiments are briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0024] Figure 1 It is the main figure of the utility model;

[0025] Figure 2 This is a side view of the UAV of the utility model;

[0026] Figure 3 This is a schematic diagram of the cargo hold structure of the utility model;

[0027] Figure 4 For the utility model Figure 3 Schematic diagram of the structure of part A.

[0028] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0029] 11. Drone; 12. Cargo hold;

[0030] 21. Universal wheel;

[0031] 31. groove; 32. support frame; 33. through hole; 34. limit rod; 35. tension spring; 36. limit plate; 37. connection groove;

[0032] 41. Baffle. DETAILED DESCRIPTION

[0033] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are described in detail below with reference to the accompanying drawings.

[0034] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific implementation methods disclosed below.

[0035] In order to make the purpose, technical solution and advantages of the present invention more clear, the implementation mode of the present invention will be further described in detail below with reference to the accompanying drawings.

[0036] See also Figure 1-4 As shown, this embodiment is a logistics drone with a detachable cargo hold, comprising:

[0037] Main body components, including a drone 11 and a cargo hold 12;

[0038] The cargo hold 12 can carry cargo, and the cargo hold 12 can be lifted by the drone 11 to facilitate transportation of the cargo hold 12;

[0039] The hoisting component includes a groove 31, a support frame 32, a tension spring 35 and a limit plate 36;

[0040] A shielding component, the shielding component includes a baffle 41;

[0041] The drone 11 is arranged above the cargo hold 12, the groove 31 is symmetrically arranged inside the top surface of the cargo hold 12, the support frame 32 is symmetrically fixedly connected to the bottom of the drone 11, the baffle 41 is symmetrically fixedly connected to the side walls of the groove 31, and the top surface of the baffle 41 is level with the top surface of the cargo hold 12, the limit plates 36 are respectively arranged inside the groove 31, and are arranged below the baffle 41, the right ends of the limit plates 36 are hinged to the right side wall of the groove 31, the tension spring 35 is symmetrically arranged inside the groove 31, the top of the tension spring 35 is fixedly connected to the right bottom surface of the limit plate 36, and the bottom of the tension spring 35 is fixedly connected to the right side wall of the groove 31, and the distance between the two baffles 41 is less than the length of the limit plate 36;

[0042] When transporting the cargo hold, the support frame 32 of the drone 11 is moved to the top of the groove 31, so that the support frame 32 presses the limit plate 36, and the left end of the limit plate 36 moves downward until the support frame 32 enters the inside of the groove 31. Through the cooperation with the tension spring 35, the support frame 32 can enter the inside of the groove 31, so that the limit plate 36 is reset;

[0043] It includes moving parts, and the moving parts include universal wheels 21;

[0044] The universal wheels 21 are symmetrically fixedly mounted on both sides of the bottom surface of the cargo hold 12;

[0045] It is convenient to move the cargo hold 12 on the ground by the drone 11;

[0046] Working principle: When the cargo hold 12 is lifted and transported by the drone 11, the drone 11 is controlled to move the drone 11 to the top of the cargo hold 12, and the support frame 32 is moved to the top of the groove 31, so that the support frame 32 squeezes the limit plate 36, and the left end of the limit plate 36 moves downward until the support frame 32 enters the inside of the groove 31. Under the action of the tensioning spring 35, the limit plate 36 can be reset. When the drone 11 is lifted, the support frame 32 is against the bottom of the limit plate 36. At the same time, under the action of the baffle, the limit plate 36 can be prevented from being squeezed out by the support frame 32. When the cargo hold 12 moves on land, the universal wheel 21 set at the lower end can conveniently use the drone 11 to drive the cargo hold to move, which can reduce the lifting time of the drone 11 and protect the drone 11.

[0047] See also Figure 1-4 As shown, this embodiment is based on the above embodiment 1, and the hanging component further includes a through hole 33 and a limiting rod 34;

[0048] The through hole 33 is arranged inside the support frame 32, the limiting rod 34 is fixedly connected to the side wall of the support frame 32 and arranged on the left side of the through hole 33, and the limiting rod 34 and the side wall of the limiting plate 36 are in contact with each other. When the cargo hold 12 is lifted, the limiting rod 34 can conveniently press the limiting plate 36 to prevent the cargo hold 12 from falling;

[0049] The lifting component also includes a connection slot 37;

[0050] The connecting groove 37 is arranged on the bottom surface of the limiting plate 36, and the connecting groove 37 is a semicircular groove;

[0051] When the drone 11 is raised, the support frame 32 can be connected to the inside of the connection groove 37;

[0052] The length of the limiting rod 34 is smaller than the thickness of the limiting plate 36;

[0053] Not only can the position of the limit plate 36 be blocked, but also the limit rod 34 can be moved to the inside of the groove 31 when the drone 11 is moved out;

[0054] The connecting parts of the support frame 32 are all round tubes, and the width of the groove 31 is greater than the width of the support frame 32;

[0055] The support frame 32 can be easily inserted into the groove 31 and can be easily matched with the connecting groove 37;

[0056] Working principle: When the drone 11 is being raised, the support frame 32 of the drone 11 can enter into the connecting groove 37, and the position of the support frame 32 can be limited to prevent the cargo hold 12 from shaking during transportation. When lowering the cargo hold 12, the cargo hold 12 is in contact with the ground, the drone 1 moves downward, the limit rod 34 enters into the groove 31, the drone 11 moves, and the limit plate 36 moves to the through hole 33, which can easily separate the drone 11 from the cargo hold.

[0057] In the description of the present invention, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "set", "install", "connect", and "connect" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0058] Finally, it should be noted that the above description is only a preferred embodiment of the utility model and is not intended to limit the utility model. Although the utility model is described in detail with reference to the above embodiments, those skilled in the art can still modify the technical solutions recorded in the above embodiments or replace some of the technical features therein by equivalents. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.

Claims

1. A logistics drone with a detachable cargo hold, characterized in that: include: A main body component, the main body component comprising a drone (11) and a cargo hold (12); A hoisting component, the hoisting component comprising a groove (31), a support frame (32), a tensioning spring (35) and a limiting plate (36); A shielding component, the shielding component comprising a baffle (41); The drone (11) is arranged above the cargo hold (12), the groove (31) is symmetrically arranged inside the top surface of the cargo hold (12), the support frame (32) is symmetrically fixedly connected to the bottom of the drone (11), the baffle (41) is symmetrically fixedly connected to the side walls on both sides of the groove (31), and the top surface of the baffle (41) is level with the top surface of the cargo hold (12), the limit plates (36) are respectively arranged inside the groove (31) and below the baffle (41), the right ends of the limit plates (36) are hinged to the right side wall of the groove (31), the tension spring (35) is symmetrically arranged inside the groove (31), the top of the tension spring (35) is fixedly connected to the right bottom surface of the limit plate (36), and the bottom of the tension spring (35) is fixedly connected to the right side wall of the groove (31), and the distance between the two baffles (41) is less than the length of the limit plate (36).

2. A logistics drone with a detachable cargo hold according to claim 1, characterized in that: The hanging component also includes a through hole (33) and a limiting rod (34); The through hole (33) is arranged inside the support frame (32), the limiting rod (34) is fixedly connected to the side wall of the support frame (32) and is arranged on the left side of the through hole (33), and the limiting rod (34) and the side wall of the limiting plate (36) are in contact with each other.

3. The logistics drone with a detachable cargo hold according to claim 1, characterized in that: The hanging component also includes a connecting groove (37); The connecting groove (37) is arranged on the bottom surface of the limiting plate (36), and the connecting groove (37) is a semicircular groove.

4. The logistics drone with a detachable cargo hold according to claim 1, characterized in that: It comprises a moving part, wherein the moving part comprises a universal wheel (21); The universal wheels (21) are symmetrically fixedly mounted on both sides of the bottom surface of the cargo hold (12).

5. The logistics drone with a detachable cargo hold according to claim 2, characterized in that: The length of the limiting rod (34) is smaller than the thickness of the limiting plate (36).

6. The logistics drone with a detachable cargo hold according to claim 1, characterized in that: The connecting parts of the support frame (32) are all round tubes, and the width of the groove (31) is greater than the width of the support frame (32).

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