Vertical take-off and landing hangar for unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle vertical take-off and landing hangar which comprises a hangar body, an electric push rod and a lifting plate are arranged in an inner cavity of the hangar body, a parking apron is arranged on the top of the lifting plate, and baffles are arranged on the front face and the back face of the parking apron. Four fixing blocks and two L-shaped cover plates are arranged at the top of the lifting plate, an electric push rod is matched with the lifting plate to lift the parking apron out of the hangar body, in the process, under the action of the unfolding mechanism, the fixing blocks and a rotating shaft, the two L-shaped cover plates serving as the top cover plates of the hangar body are slowly unfolded, and an unmanned aerial vehicle lands on the parking apron. And the baffle is matched in the descending and retracting process of the parking apron through reverse operation, the L-shaped cover plate slowly rotates by 90 degrees to be closed to cover the top to seal the hangar, and the problem that an existing unmanned aerial vehicle vertical take-off and landing hangar is difficult to take off, land and collect the unmanned aerial vehicle rapidly is solved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a vertical take-off and landing hangar for unmanned aerial vehicles. Background Art

[0002] Unmanned aircraft, also known as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices. There is no cockpit on the aircraft, but it is equipped with autopilots, program control devices and other equipment. Personnel on the ground, on ships or at the remote control station of the mother aircraft use radar and other equipment to track, locate, remotely control, telemeter and transmit digital data to it.

[0003] The patent with publication number CN 218662398 U discloses a drone electric energy supply landing hangar, which includes a landing hangar fixedly connected to one side of the equipment box, door panels movably connected to the top and sides of the landing hangar, a helipad arranged on one side of the interior of the landing hangar, and locators fixedly connected to the four corners of the helipad. The bottom of the drone of the device has a charging interface. After the drone is parked, the charging interface matches the charging slot at the helipad, and is controlled and debugged in combination with a control panel. The control panel is used to control internal electrical functions and is suitable for use in drone electric energy supply landing hangars. However, when taking off and landing a drone, the device needs to open the door panel first, and then use a lifter and a lifting rod to move the helipad out of the landing hangar before the drone can be landed on the helipad. Then, the above process is reversed to complete the collection of the drone. The process is cumbersome and complicated. Therefore, a drone vertical take-off and landing hangar is proposed to solve the problem that the existing drone vertical take-off and landing hangar is difficult to collect drones for rapid take-off and landing. Utility Model Content

[0004] 1. Technical issues to be solved

[0005] In view of the deficiencies in the prior art, the utility model provides a vertical take-off and landing hangar for unmanned aerial vehicles, which solves the technical problem that the existing vertical take-off and landing hangar for unmanned aerial vehicles is difficult to collect for rapid take-off and landing of unmanned aerial vehicles.

[0006] (II) Technical solution

[0007] In order to achieve the above objectives, the present invention is implemented through the following technical solutions:

[0008] A hangar for vertical take-off and landing of unmanned aerial vehicles comprises a hangar body, an inner cavity of the hangar body is provided with an electric push rod and a lifting plate, a helipad is provided on the top of the lifting plate, baffles are provided on the front and back of the helipad, four fixing blocks and two L-shaped cover plates are provided on the top of the lifting plate, the L-shaped cover plates are provided between two groups of the fixing blocks by means of a rotating shaft, a launching mechanism is provided on one side of the L-shaped cover plates on the back, and a maintenance mechanism is provided on one side of the hangar body;

[0009] The bottom and top of the electric push rod are fixedly connected to the bottom of the inner cavity of the hangar body and the bottom of the lifting plate respectively, and the baffle is fixedly connected to the top of the lifting plate.

[0010] The launching mechanism is composed of a moving groove, a pressing plate, a compression groove, a sliding column and a spring;

[0011] Wherein, the movable groove is opened on one side of the L-shaped cover plate, and the pressing plate is arranged in the inner cavity of the movable groove.

[0012] Preferably: a compression groove is provided at the bottom of the pressure plate, and the upper part of the sliding column and the spring are both provided with an inner cavity of the compression groove;

[0013] The bottom of the sliding column is fixedly connected to the bottom of the inner cavity of the moving groove, and the two ends of the spring are fixedly connected to the inner cavity of the compression groove and the bottom of the inner cavity of the moving groove respectively.

[0014] Preferably: the inspection mechanism is composed of an inspection port, an inspection plate, a second rotating shaft, a limiting slide groove and a limiting slider;

[0015] The inspection port is opened through one side of the hangar body, and the inspection plate is arranged in the inner cavity of the inspection port by means of a second rotating shaft.

[0016] Preferably: a limit slide groove is provided on the top of the lifting plate and one side of the inspection plate and is interconnected, and a limit slide block is provided in the inner cavity of the limit slide groove;

[0017] Wherein, the limit sliding block is fixedly connected to the bottom of the apron.

[0018] Preferably: grooves are provided on both sides of the hangar body, and a storage box is provided in the inner cavity of the groove;

[0019] A handle is provided on one side of the storage box, a slide groove is provided on the inner wall of the groove, a slider is provided in the inner cavity of the slide groove, and the slider is fixedly connected to the storage box.

[0020] (III) Beneficial effects

[0021] 1. Use the electric push rod in conjunction with the lifting plate to lift the apron out of the hangar body. During the process, under the action of the unfolding mechanism, fixed block and rotating shaft, the two L-shaped covers serving as the top cover of the hangar body slowly unfold to land the drone on the apron. In the reverse operation, the apron is lowered and retracted, and the L-shaped cover slowly rotates 90 degrees to close and cover the top to seal the hangar, solving the problem that the existing drone vertical take-off and landing hangar is difficult to quickly take off and land drones.

[0022] 2. When the UAV is on the apron inside the hangar body, the inspection plate inside the inspection port can be rotated ninety degrees under the action of the second rotating shaft, and then the apron can be pulled out of the hangar body and placed on the inspection plate under the action of the limiting slider in the limiting slide slot. At this time, the battery of the UAV can be replaced or maintenance work can be carried out. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] The above description is only an overview of the technical solution of the utility model. In order to more clearly understand the technical means of the utility model and implement it according to the contents of the specification, the following is a detailed description of the preferred embodiments of the utility model in conjunction with the accompanying drawings.

[0024] Figure 1 This is the structural diagram of the utility model;

[0025] Figure 2 This is a cross-sectional view of the structure of the utility model;

[0026] Figure 3 The utility model structure Figure 1 Enlarged view of point A in the middle;

[0027] Figure 4 This is a cross-sectional view of the structure of the utility model;

[0028] Figure 5 This is a structural diagram of the utility model.

[0029] Legend: 1. Hangar body; 2. Electric push rod; 3. Lifting plate; 4. Apron; 5. Baffle; 6. Fixed block; 7. L-shaped cover; 8. Rotating shaft; 9. Opening mechanism; 91. Moving groove; 92. Pressure plate; 93. Compression groove; 94. Slide column; 95. Spring; 10. Maintenance mechanism; 101. Maintenance port; 102. Maintenance plate; 103. Second rotating shaft; 104. Limiting slide groove; 105. Limiting slider; 11. Groove; 12. Storage box; 13. Slide groove; 14. Slider. DETAILED DESCRIPTION

[0030] The embodiment of the present application provides a hangar for vertical take-off and landing of unmanned aerial vehicles, which effectively solves the problem that it is difficult for existing hangars for vertical take-off and landing of unmanned aerial vehicles to quickly take off and land. The apron is lifted out of the hangar body by an electric push rod in cooperation with a lifting plate. During the process, under the action of an unfolding mechanism, a fixed block and a rotating shaft, two L-shaped covers serving as the top cover of the hangar body are slowly unfolded to land the unmanned aerial vehicle on the apron. The apron is lowered and retracted in reverse operation to cooperate with the baffle, and the L-shaped cover slowly rotates ninety degrees to close and cover the top to seal the hangar.

[0031] Example

[0032] The technical solution in the embodiment of the present application effectively solves the technical problem that the existing UAV vertical take-off and landing hangar is difficult to collect UAVs for rapid take-off and landing. The overall idea is as follows:

[0033] In view of the problems existing in the prior art, the utility model provides a hangar for vertical take-off and landing of unmanned aerial vehicles, including a hangar body 1, an inner cavity of the hangar body 1 is provided with an electric push rod 2 and a lifting plate 3, a helipad 4 is provided on the top of the lifting plate 3, baffles 5 are provided on the front and back of the helipad 4, four fixed blocks 6 and two L-shaped cover plates 7 are provided on the top of the lifting plate 3, the L-shaped cover plate 7 is arranged between the two groups of fixed blocks 6 by a rotating shaft 8, a launching mechanism 9 is provided on one side of the back L-shaped cover plate 7, and a side of the hangar body 1 is provided with a lifting mechanism 9. A maintenance mechanism 10 is provided, and the electric push rod 2 cooperates with the lifting plate 3 to lift the apron 4 out of the hangar body 1. During the process, under the action of the unfolding mechanism, the fixing block 6 and the rotating shaft 8, the two L-shaped cover plates 7 serving as the top cover plates of the hangar body 1 are slowly unfolded to land the UAV on the apron 4. During the reverse operation of the apron 4 descending and retracting, the baffle plate 5 is cooperated, and the L-shaped cover plate 7 slowly rotates 90 degrees to close and cover the top to seal the hangar, which solves the problem that the existing UAV vertical take-off and landing hangar is difficult to collect UAVs for rapid take-off and landing;

[0034] The bottom and top of the electric push rod 2 are fixedly connected to the bottom of the inner cavity of the hangar body 1 and the bottom of the lifting plate 3 respectively, and the baffle 5 is fixedly connected to the top of the lifting plate 3.

[0035] The unfolding mechanism 9 is composed of a moving groove 91, a pressure plate 92, a compression groove 93, a sliding column 94 and a spring 95; wherein the moving groove 91 is opened on one side of the L-shaped cover plate 7, and the pressure plate 92 is arranged in the inner cavity of the moving groove 91; a compression groove 93 is opened at the bottom of the pressure plate 92, and the upper half of the sliding column 94 and the spring 95 are both provided with the inner cavity of the compression groove 93; wherein the bottom of the sliding column 94 is fixedly connected to the bottom of the inner cavity of the moving groove 91, and the two ends of the spring 95 are respectively fixedly connected to the inner cavity of the compression groove 93 and the bottom of the inner cavity of the moving groove 91. When the UAV is put into the hangar body 1, the spring 95 in the compression groove 93 in the unfolding mechanism 9 is in a compressed state, the apron is raised, and the L-shaped cover plate 7 has an outward rotational force under the action of the rotating shaft 8 and the pressure plate 92 on the sliding column 94 in the moving groove 91, so that the two L-shaped cover plates 7 can be smoothly unfolded to both sides, ensuring that the UAV on the apron 4 can take off smoothly.

[0036] The inspection mechanism 10 is composed of an inspection port 101, an inspection plate 102, a second rotating shaft 103, a limiting slide 104 and a limiting slider 105; wherein, the inspection port 101 is opened through one side of the hangar body 1, and the inspection plate 102 is arranged in the inner cavity of the inspection port 101 by using the second rotating shaft 103; the top of the lifting plate 3 and one side of the inspection plate 102 are both provided with a limiting slide 104 and are interconnected, and the inner cavity of the limiting slide 104 is provided with a limiting slider 105; wherein, the limiting slider 105 is fixedly connected to the bottom of the apron 4. When the UAV is located on the apron 4 in the hangar body 1, the inspection plate 102 in the inspection port 101 can be rotated ninety degrees under the action of the second rotating shaft 103, and then the apron 4 can be pulled out of the hangar body 1 and placed on the inspection plate 102 under the action of the limiting slider 105 in the limiting slide 104, and then the battery of the UAV can be replaced or inspection work can be carried out.

[0037] Grooves 11 are provided through both sides of the hangar body 1, and a storage box 12 is provided in the inner cavity of the groove 11; a pull handle is provided on one side of the storage box 12, a slide groove 13 is provided on the inner wall of the groove 11, and a slider 14 is provided in the inner cavity of the slide groove 13, and the slider 14 is fixedly connected to the storage box 12. The storage groove 12 is pulled out of the groove 11 by using the pull handle and the slider 14 in the slide groove 13, and the drone maintenance tools or batteries are placed in the storage groove 12 for storage, which improves the functionality of this drone vertical take-off and landing hangar and facilitates subsequent drone maintenance.

[0038] Working principle: When using this UAV vertical take-off and landing hangar, the electric push rod 2 can be used to cooperate with the lifting plate 3 to lift the apron 4 out of the hangar body 1. During the rising process, under the action of the unfolding mechanism, the fixed block 6 and the rotating shaft 8, the two L-shaped cover plates 7 serving as the top cover of the hangar body 1 are slowly unfolded and opened, so that the UAV can be landed on the apron 4. After parking, the apron 4 is operated in reverse. During the descent process, the baffle 5 is cooperated, and the L-shaped cover plate 7 slowly rotates ninety degrees to close and cover the top to seal the hangar, which solves the problem that the existing UAV vertical take-off and landing hangar is difficult to collect UAVs for rapid take-off and landing.

[0039] Finally, it should be noted that: Obviously, the above embodiments are only examples for clearly explaining the present invention, and are not intended to limit the implementation methods. For ordinary technicians in the relevant field, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to list all the implementation methods here. The obvious changes or modifications derived from this are still within the scope of protection of the present invention.

Claims

1. A hangar for vertical take-off and landing of unmanned aerial vehicles, comprising a hangar body (1), characterized in that: The inner cavity of the hangar body (1) is provided with an electric push rod (2) and a lifting plate (3), a parking apron (4) is provided on the top of the lifting plate (3), baffles (5) are provided on the front and back of the parking apron (4), four fixing blocks (6) and two L-shaped cover plates (7) are provided on the top of the lifting plate (3), the L-shaped cover plate (7) is arranged between two groups of the fixing blocks (6) by means of a rotating shaft (8), an opening mechanism (9) is provided on one side of the L-shaped cover plate (7) on the back, and a maintenance mechanism (10) is provided on one side of the hangar body (1); The bottom and top of the electric push rod (2) are respectively fixedly connected to the bottom of the inner cavity of the hangar body (1) and the bottom of the lifting plate (3), and the baffle (5) is fixedly connected to the top of the lifting plate (3).

2. The UAV vertical take-off and landing hangar according to claim 1, characterized in that: The unfolding mechanism (9) is composed of a moving groove (91), a pressing plate (92), a compression groove (93), a sliding column (94) and a spring (95); The movable groove (91) is provided on one side of the L-shaped cover plate (7), and the pressing plate (92) is arranged in the inner cavity of the movable groove (91).

3. The UAV vertical take-off and landing hangar according to claim 2, characterized in that: The bottom of the pressure plate (92) is provided with a compression groove (93), and the upper part of the sliding column (94) and the spring (95) are both provided with an inner cavity of the compression groove (93); The bottom of the sliding column (94) is fixedly connected to the bottom of the inner cavity of the movable groove (91), and the two ends of the spring (95) are respectively fixedly connected to the inner cavity of the compression groove (93) and the bottom of the inner cavity of the movable groove (91).

4. The UAV vertical take-off and landing hangar according to claim 1, characterized in that: The inspection mechanism (10) is composed of an inspection port (101), an inspection plate (102), a second rotating shaft (103), a limiting sliding groove (104) and a limiting sliding block (105); The inspection opening (101) is opened through one side of the hangar body (1), and the inspection panel (102) is arranged in the inner cavity of the inspection opening (101) by means of a second rotating shaft (103).

5. The UAV vertical take-off and landing hangar according to claim 1, characterized in that: The top of the lifting plate (3) and one side of the inspection plate (102) are both provided with a limit slide groove (104) and are interconnected, and the inner cavity of the limit slide groove (104) is provided with a limit slider (105); Wherein, the limiting sliding block (105) is fixedly connected to the bottom of the apron (4).

6. The UAV vertical take-off and landing hangar according to claim 1, characterized in that: Grooves (11) are provided on both sides of the hangar body (1), and a storage box (12) is provided in the inner cavity of the groove (11); A handle is provided on one side of the storage box (12), a slide groove (13) is provided on the inner wall of the groove (11), a slider (14) is provided in the inner cavity of the slide groove (13), and the slider (14) is fixedly connected to the storage box (12).

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