Unmanned aerial vehicle hangar

Abstract

The utility model provides an unmanned aerial vehicle hangar which comprises a cabin body, at least one cabin door, at least one first transmission rod and at least one second transmission rod. A cabin opening is formed in the top of the cabin body. The first transmission rod corresponds to the cabin door, the first end of the first transmission rod is rotationally connected to the cabin body around a first pivot axis, and the second end of the first transmission rod is rotationally connected to the cabin door around a second pivot axis. The second transmission rod corresponds to the cabin door, the first end of the second transmission rod is rotationally connected to the cabin body around a third pivot axis, and the second end of the second transmission rod is rotationally connected to the cabin door around a fourth pivot axis. Wherein the first pivot axis, the second pivot axis, the third pivot axis and the fourth pivot axis are arranged in parallel, so that the cabin door can be movably connected to the cabin body between a closed position and an open position. According to the unmanned aerial vehicle hangar, the overlarge space inside and outside the cabin cannot be occupied, and the influence on take-off and landing of an unmanned aerial vehicle is reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of unmanned aerial vehicle hangar more specifically relates to a kind of unmanned aerial vehicle hangar. BACKGROUND

[0002] In recent years, many manufacturers in China Different types of unmanned aerial vehicle airport combine industry scene, build integrated solution with artificial intelligence as core, take "unattended + full-automatic operation" operation mode, realize unattended, autonomous charging, remote monitoring, unmanned data processing, full autonomous flight operation, safety, reliability, professional performance requirements reach industry application scene requirements.

[0003] But the current market product is mainly small unmanned aerial vehicle hangar, hangar's hatch opening mechanism volume is larger, after hatch is opened, it will encroach on the vertical and horizontal space of hangar, not only will affect the take-off and landing of unmanned aerial vehicle, also occupy the space where hangar is, so that the environmental range of hangar applicable is limited. UTILITY MODEL CONTENT

[0004] A series of simplified concepts are introduced in the utility model content part, which will be described in detail in the specific embodiment part. The utility model content part of the utility model does not mean to try to limit the key features and necessary technical features of the claimed technical solution, and does not mean to try to determine the protection scope of the claimed technical solution.

[0005] To at least partially solve the above problems, the utility model provides an unmanned aerial vehicle hangar, which comprises:

[0006] A cabin body, the top of the cabin body is provided with a hatch;

[0007] At least one hatch for opening and closing the hatch;

[0008] At least one first transmission rod, the first transmission rod is arranged corresponding to the hatch, the first end of the first transmission rod is rotatably connected to the cabin body around the first pivot axis, and the second end of the first transmission rod is rotatably connected to the hatch around the second pivot axis; and

[0009] At least one second transmission rod, the second transmission rod is arranged corresponding to the hatch, the first end of the second transmission rod is rotatably connected to the cabin body around the third pivot axis, and the second end of the second transmission rod is rotatably connected to the hatch around the fourth pivot axis;

[0010] Wherein, the first pivot axis, the second pivot axis, the third pivot axis and the fourth pivot axis are arranged in parallel with each other, so that the hatch can be movably connected to the cabin body between the closed position and the open position.

[0011] The unmanned aerial vehicle hangar according to the utility model, through the transmission of the first transmission rod and the second transmission rod, the cabin door can be arranged on the side of the hatch when being moved to the open position and will not protrude from the top of the cabin body in a large range, so that the vertical and horizontal space of the hangar will not be occupied after the cabin door is opened, the take-off and landing of the unmanned aerial vehicle are prevented from being affected by the cabin door, the space occupied by the unmanned aerial vehicle hangar is reduced, and the environmental range applicable to the unmanned aerial vehicle hangar is expanded.

[0012] Optionally, when the cabin door is in the open position, a line connecting the first pivot axis and the second pivot axis intersects a line connecting the third pivot axis and the fourth pivot axis in a projection of the unmanned aerial vehicle hangar along an extension direction of the first pivot axis.

[0013] Optionally, the first transmission rod and the second transmission rod are configured as bent rods, so that when the cabin door is in the open position, the first transmission rod and the second transmission rod span the side wall of the cabin body.

[0014] Optionally, the cabin door in the open position protrudes upward from the top surface of the cabin body by a distance less than or equal to one-fifth of the size of the cabin door in the open position along the height direction of the cabin body.

[0015] Optionally, when the cabin door is in the open position, the first transmission rod is in a first position, and when the cabin door is in the closed position, the first transmission rod is in a second position, and an angle between the first position and the second position is greater than or equal to 120 degrees; and / or

[0016] When the cabin door is in the open position, the second transmission rod is in a third position, and when the cabin door is in the closed position, the second transmission rod is in a fourth position, and an angle between the third position and the fourth position is greater than or equal to 120 degrees.

[0017] Optionally, the unmanned aerial vehicle hangar further comprises a rotary driving member, the rotary driving member is arranged correspondingly to the first transmission rod, and is used for driving the corresponding first transmission rod to rotate around the first pivot axis.

[0018] Optionally, a first end of the first transmission rod is provided with a first rotating shaft, an axis of the first rotating shaft is the first pivot axis, and the rotary driving member is used for driving the first rotating shaft to rotate.

[0019] Optionally, the UAV hangar further comprises a speed reducer, the rotating driving member is connected to the speed reducer, and the speed reducer is connected to the first rotating shaft.

[0020] Optionally, the rotating driving member is arranged above the centerline of the cabin body in the height direction of the cabin body.

[0021] Optionally, the UAV hangar comprises two cabin doors, and the two cabin doors are arranged in a direction perpendicular to the first pivot axis, so that the two cabin doors can be located on two sides of the hatch in the open position respectively.

[0022] Optionally, when the two cabin doors are in the closed position, the two cabin doors are in sealing contact with each other, and the cabin doors are in sealing contact with the hatch.

[0023] Optionally, one of the two cabin doors is provided with a first sealing strip, and the first sealing strip is used for abutting against the bottom of the other cabin door when the two cabin doors are in the closed position; and / or

[0024] At least one of the two cabin doors is provided with a second sealing strip arranged on the top of the cabin door in the closed position, and the second sealing strip is used for abutting against the other cabin door when the two cabin doors are in the closed position.

[0025] Optionally, the periphery of the hatch is provided with a third sealing strip for abutting against the lower surface of the cabin door in the closed position.

[0026] Optionally, the top surface of the cabin door in the closed position is higher at the end close to the other cabin door than at the end away from the other cabin door; and / or

[0027] During the process that the cabin door is moved from the closed position to the open position, the top surface of the cabin door in the closed position is deflected towards the outside of the hatch.

[0028] Optionally, each cabin door is connected with two first transmission rods, and the two first transmission rods are arranged at intervals in the extension direction of the first pivot axis; and / or

[0029] Each cabin door is connected with two second transmission rods, and the two second transmission rods are arranged at intervals in the extension direction of the third pivot axis.

[0030] Optionally, the cabin door is provided with a heating device for heating and melting snow on the cabin door. BRIEF DESCRIPTION OF DRAWINGS

[0031] The following drawings for the embodiments of the present application are used herein as a part of the present application for understanding the present application. The drawings show the embodiments of the present application and their descriptions, which are used to explain the principles of the present application. In the drawings,

[0032] Figure 1 is a perspective view of a UAV hangar of a preferred embodiment of the present application, and the hatch is in a closed position;

[0033] Figure 2 is a cross-sectional view taken along Figure 1 the center line A-A;

[0034] Figure 3 is a position view of the hatch in the Figure 2 from the closed position to the open position;

[0035] Figure 4 is a view of the hatch in the Figure 2 in the open position;

[0036] Figure 5 is a connection view between the hatch in the closed position, the first transmission rod and the second transmission rod;

[0037] Figure 6 is a cross-sectional view taken along Figure 5 the center line B-B;

[0038] Figure 7 is a view of the hatch in the Figure 6 in the open position;

[0039] Figure 8 is a structure view of the sealed connection between the hatches;

[0040] Figure 9 is a structure view of the sealed connection between the hatch and the bent edge; and

[0041] Figure 10 is a perspective view of a UAV hangar of another preferred embodiment of the present application, and the hatch is in the open position.

[0042] Reference Signs List

[0043] 100: hangar 110: cabin body

[0044] 111: hatch 112: bent edge

[0045] 113: first bent edge 114: second bent edge

[0046] 115: third bent edge 116: third sealing strip

[0047] 140: parking apron 120: hatch

[0048] 121: heat preservation cavity 122: first transmission rod

[0049] 123: second transmission rod 124: first connecting part

[0050] 125: second connecting part 126: third connecting part

[0051] 127: fourth connecting part 128: rotary driving member

[0052] 129: speed reducer 130: first rotating seat

[0053] 131: second rotating seat 132: first sealing strip

[0054] 133: second sealing strip 134: connecting piece

[0055] 135: first rotating shaft 136: third rotating shaft

[0056] 137: second rotating shaft 138: fourth rotating shaft

[0057] AX1: first pivot axis AX2: second pivot axis

[0058] AX3: third pivot axis AX4: fourth pivot axis

[0059] D1: height direction D2: length direction

[0060] D3: width direction 140: parking apron DETAILED DESCRIPTION

[0061] In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present application. It will be apparent, however, to one skilled in the art that the present application can be practiced without one or more of these specific details. In other instances, well-known features have not been described in detail so as not to unnecessarily obscure the present application.

[0062] In this document, the ordinal numbers such as "first" and "second" cited in the present application are merely identifiers but do not have any other meaning, for example, specific order, etc. Moreover, for example, the term "first component" itself does not imply the existence of "second component", and the term "second component" itself does not imply the existence of "first component".

[0063] In this document, "upper", "lower", "front", "back", "left", "right", etc. are merely used to indicate relative positional relationship between relevant parts, but do not limit the absolute position of these relevant parts.

[0064] In this document, "approximately," "about," and the like are understood to encompass amounts that would be considered by those of ordinary skill in the art to be equivalent in context to the recited characteristic values.

[0065] Unless otherwise indicated, numerical ranges herein are inclusive of the recited two endpoints and include any sub-ranges falling within the indicated ranges.

[0066] Figures 1 to 9 An unmanned aerial vehicle hangar 100 is shown, which comprises a cabin body 110, at least one cabin door 120, at least one first transmission rod 122, and at least one second transmission rod 123. The top of the cabin body 110 is provided with a hatch 111. The cabin door 120 is used to open and close the hatch 111.

[0067] The first transmission rod 122 is arranged corresponding to the cabin door 120, and the first end of the first transmission rod 122 is rotatably connected to the cabin body 110 about a first pivot axis AX1, and the second end of the first transmission rod 122 is rotatably connected to the cabin door 120 about a second pivot axis AX2. The second transmission rod 123 is arranged corresponding to the cabin door 120, and the first end of the second transmission rod 123 is rotatably connected to the cabin body 110 about a third pivot axis AX3, and the second end of the second transmission rod 123 is rotatably connected to the cabin door 120 about a fourth pivot axis AX4.

[0068] The first pivot axis AX1, the second pivot axis AX2, the third pivot axis AX3, and the fourth pivot axis AX4 are all arranged parallel to each other, so that the cabin door 120 can be movably connected to the cabin body 110 between the closed position and the open position.

[0069] According to the unmanned aerial vehicle hangar 100 of the utility model, through the transmission of the first transmission rod 122 and the second transmission rod 123, the cabin door 120 can be arranged on the side of the hatch 111 when moving to the open position and will not protrude greatly from the top of the cabin body 110, so that the vertical and horizontal space of the hangar 100 will not be occupied after the cabin door 120 is opened, preventing the cabin door 120 from affecting the take-off and landing of the unmanned aerial vehicle, and also reducing the occupation of the space by the unmanned aerial vehicle hangar 100, expanding the environmental range applicable to the unmanned aerial vehicle hangar 100. In addition, the first transmission rod 122 and the second transmission rod 123 are used to transmit the cabin door 120, which will not occupy too much cabin space, reducing the influence on the take-off and landing of the unmanned aerial vehicle.

[0070] Figure 1 The overall structure of the unmanned aerial vehicle hangar 100 according to the utility model is shown, Figures 2 to 4 The process of moving the cabin door 120 from the closed position to the open position relative to the cabin body 110 is shown. Figures 5 to 7The connection structure between the hatch 120 and the first transmission rod 122 and the second transmission rod 123 is shown. Figure 8 The sealing structure between hatches 120 is shown, while Figure 9 The sealing structure between the hatch 120 and the hull 110 is shown.

[0071] The opening method of the hatch 111 of the unmanned aerial vehicle hangar 100 according to this embodiment is exemplified by two opposing hatches 120. (Refer to...) Figure 1 The drone hangar 100 includes two hatches 120, which are arranged along a direction perpendicular to the first pivot axis AX1 (the width direction D3 of the cabin 110), combined with Figure 4 As shown, this allows the two hatches 120 to be positioned on either side of the hatch 111 when in the open position, preventing the open hatches 120 from obstructing the drone entering or exiting the hatch 111.

[0072] Reference Figure 4 Optionally, each hatch 120 is connected to two first transmission rods 122, which are spaced apart along the extension direction of the first pivot axis AX1 (i.e., the length direction D2 of the cabin 110). Each hatch 120 is also connected to two second transmission rods 123, which are spaced apart along the extension direction of the third pivot axis AX3. The arrangement of the first transmission rods 122 and the second transmission rods 123 makes the opening and closing process of the hatch 120 more stable and improves the wind resistance of the hatch 120.

[0073] Optionally, combined Figure 8 and Figure 9 As shown, when the two hatches 120 are in the closed position, the two hatches 120 are in sealed contact with each other, and the hatches 120 are in sealed contact with the hatch opening 111, so that the hatches 120 and the cabin 110 are fully sealed, which can prevent rainwater from entering the cabin 110 and ensure the normal operation of the equipment inside the cabin 110.

[0074] Optionally, the cabin 110 is provided with a bent edge 112 that seals against the hatch 120. The bent edge 112 surrounds the hatch 111, and the surface of the bent edge 112 that mates with the hatch 120 protrudes above the hatch 111 along the height direction D1. This prevents rainwater accumulated on the top of the cabin 110 from entering the cabin 110 through the hatch 111, thereby improving the waterproof performance of the UAV hangar 100.

[0075] Furthermore, the bent edge 112 includes a first bent edge 113, a second bent edge 114, and a third bent edge 115. The first bent edge 113 is perpendicular to the height direction D1 of the cabin 110 and is connected to the inner wall of the hatch 111. The third bent edge 115 is arranged above the hatch 111 along the height direction D1 to fit into the hatch 120, and is perpendicular to the height direction D1 of the cabin 110. The second bent edge 114 connects the first bent edge 113 and the second bent edge 115, and is arranged inside the first bent edge 113 and the third bent edge 115. The bent edge 112 effectively prevents rainwater from the top of the cabin 110 from entering the hatch 111, improving the waterproof performance of the UAV hangar 100.

[0076] Optionally, refer to Figure 2 and Figure 6 Along the vertical direction D1, the top surface of the hatch 120 in the closed position, near the middle of the hatch 111, is higher than the outer side of the top surface of the hatch 120 near the hatch 111. This creates an arched structure between the two hatches 120, allowing rainwater to drain quickly from the top of the closed hatch 120 and preventing snow accumulation on the hatch 120, further enhancing the waterproof performance of the UAV hangar 100. Furthermore, combined with... Figure 3 As shown, during the process of the hatch 120 moving from the closed position to the open position, the top surface of the hatch 120 (when the hatch 120 is in the closed position) is always deflected towards the outside of the hatch 111, thereby preventing snow and rainwater from falling into the cabin 110.

[0077] Optionally, the hatch 120 is equipped with a heating device to heat and melt snow and ice on the hatch 120, thereby ensuring the safety and normal operation of the UAV hangar 100. Optionally, the heating device can be a heating plate attached to the inner side of the top surface of the hatch 120, or it can be a heating rod or other heating device. It is understood that any heating device capable of heating the hatch 120 should be within the protection scope of this utility model. Furthermore, the heating device is preferably installed inside the hatch 120 to facilitate protection of the heating device.

[0078] Optionally, the hatch 120 can adopt a hollow structure formed by connecting inner and outer panels, so that the hatch 120 forms an insulation cavity 121. The insulation cavity 121 can be filled with thermal insulation material, thereby improving the thermal insulation performance of the UAV hangar 100 and reducing the impact of the external temperature environment on the equipment inside the UAV hangar 100.

[0079] Reference Figure 8One of the two hatches 120 is equipped with a first sealing strip 132. When both hatches 120 are in the closed position, the first sealing strip 132 abuts against the bottom of the other hatch 120, forming a seal between the two hatches 120 to prevent rainwater from entering the hatch 111 through the gap between the hatches 120. Furthermore, the hatch 120 equipped with the first sealing strip 132 (e.g., Figure 8 The right-hand hatch 120 is near another hatch 120 (e.g., the hatch on the right side of the middle). Figure 8 The left hatch 120 is equipped with a connector 134. The connector 134 has an L-shaped cross-section perpendicular to the length direction D2 of the hull 110. The first sealing strip 132 can be fitted onto the connector 134 and abut against the bottom of the other hatch 120. The connector 134 further reduces rainwater penetration into the hatch 111 and improves the sealing between the hatches 120.

[0080] Optionally, one of the two hatches 120 (e.g. Figure 8 The left-hand hatch 120 is equipped with a second sealing strip 133. The second sealing strip 133 is located on top of the hatch 120 when it is in the closed position. When both hatches 120 are in the closed position, the second sealing strip 133 is used to abut against the other hatch 120 (e.g., Figure 8 The hatch 120 on the right side is used to form another sealing structure between the two hatches 120, preventing rainwater from entering the hatch 111 through the gap between the hatches 120. Furthermore, both hatches 120 can also be equipped with a second sealing strip 133. When both hatches 120 are in the closed position, the second sealing strips 133 of the two hatches 120 abut together, further improving the sealing performance between the hatches 120.

[0081] Optionally, refer to Figure 9 A third sealing strip 116 is provided around the hatch 111. The third sealing strip 116 is located on the third fold 115 of the bent edge 112. When the hatch 120 is in the closed position, the third sealing strip 116 abuts against the lower surface of the hatch 120 in the closed position, thereby further improving the sealing between the hatch 120 and the cabin 110.

[0082] Reference Figure 4 Optionally, the UAV hangar 100 also includes a rotary drive component 128, which is correspondingly arranged with the first transmission rod 122 and is used to drive the corresponding first transmission rod 122 to rotate around the first pivot axis AX1, thereby driving the hatch 120. In addition, the rotary drive component 128 can be a servo motor, which occupies less space in the cabin 110 compared with linear drive elements (such as electric push rods), thereby reducing the impact on UAV take-off and landing.

[0083] Furthermore, the first end of the first transmission rod 122 is provided with a first rotating shaft 135, the axis of the first rotating shaft 135 is the first pivot axis AX1, and the rotation drive component 128 is used to drive the first rotating shaft 135 to rotate, thereby ultimately driving the hatch 120 to move between the closed position and the open position.

[0084] Optionally, the UAV hangar 100 also includes a reducer 129. The output end of the rotary drive component 128 is connected to the input end of the reducer 129, and the output end of the reducer 129 is connected to the first rotating shaft 135, thereby achieving a deceleration drive for the hatch 120. This facilitates the control of the opening sequence, angle, and speed of the hatch 120 through system programming. The reducer 129 can also be a worm gear reducer mechanism. The worm is connected to the rotary drive component 128, and the worm wheel is connected to the first rotating shaft 135, with the worm meshing with the worm wheel. When the rotary drive component 128 is activated, the worm drives the worm wheel to rotate, thereby driving the first transmission rod 122 to rotate. Furthermore, due to the self-locking nature of the worm gear reducer mechanism, the wind resistance of the hatch 120 can be improved.

[0085] Optionally, refer to Figures 5 to 7 The UAV hangar 100 also includes a first rotating seat 130 and a second rotating seat 131. The first rotating seat 130 is disposed inside the cabin and can be mounted to the inner wall of the cabin body 110. A first transmission rod 122 is rotatably connected to the first rotating seat 130 via a first rotating shaft 135, and the first end of the second transmission rod 123 is provided with a second rotating shaft 137 and is rotatably connected to the first rotating seat 130 via the second rotating shaft 137. The axis of the second rotating shaft 137 is a third pivot axis AX3. Correspondingly, the second rotating seat 131 is disposed at the door 120, and the second end of the first transmission shaft is provided with a third rotating shaft 136. The axis of the third rotating shaft 136 is a second pivot axis AX2, and the first transmission rod 122 is rotatably connected to the second rotating seat 131 via the third rotating shaft 136. The second end of the second transmission shaft is provided with a fourth rotating shaft 138. The axis of the fourth rotating shaft 138 is a fourth pivot axis AX4, and the second transmission rod 123 is rotatably connected to the second rotating seat 131 via the fourth rotating shaft 138. By setting the first rotating seat 130 and the second rotating seat 131, the ends of the first transmission rod 122 and the second transmission rod 123 are integrated together, which makes installation convenient and transmission stable.

[0086] Optionally, along the height direction D1 of the cabin 110, the rotary drive component 128 is arranged above the centerline of the cabin 110 (the center position of the dimensions of the cabin 110 along the height direction D1), which can further reduce the space occupied by the rotary drive component 128 in the cabin 110 and facilitate the arrangement of equipment in the cabin 110.

[0087] Specifically, let's look at the structure of the first transmission rod 122 and the second transmission rod 123.

[0088] Reference Figure 5 The first transmission rod 122 includes a first connecting portion 124 and a second connecting portion 125. The first connecting portion 124 is connected to the interior of the cabin 110 (specifically, the first rotating seat 130), and the second connecting portion 125 is connected to the hatch 120. The first connecting portion 124 and the second connecting portion 125 are arranged at an included angle. The second transmission rod 123 includes a third connecting portion 126 and a fourth connecting portion 127. The third connecting portion 126 is connected to the interior of the cabin 110 (specifically, the first rotating seat 130), and the fourth connecting portion 127 is connected to the hatch 120. The third connecting portion 126 and the fourth connecting portion 127 are arranged at an included angle. The first connecting portion 124 and the second connecting portion 125 are connected by an arc-shaped transition. Figure 4 As shown, the first transmission rod 122 can avoid the wall of the cabin 110 and the edge of the hatch 111 when the hatch 120 is in the open position. Similarly, the third connecting part 126 and the fourth connecting part 127 are connected by an arc-shaped transition, so that the second transmission rod 123 can avoid the wall of the cabin 110 and the edge of the hatch 111 when the hatch 120 is in the open position. In other words, the first transmission rod 122 and the second transmission rod 123 are constructed as bent rods, so that when the hatch 120 is in the open position, the first transmission rod 122 and the second transmission rod 123 cross the side wall of the cabin 110.

[0089] Optionally, the first connecting part 124 and the second connecting part 125 may be arranged at a zigzag angle, and the third connecting part 126 and the fourth connecting part 127 may also be arranged at a zigzag angle, which can also avoid the walls of the cabin 110 and the edge of the hatch 111.

[0090] Reference Figure 4 The distance by which the hatch 120 in the open position protrudes upward from the top surface of the cabin 110 is less than or equal to one-fifth of the dimension of the hatch 120 in the height direction D1 in the open position. This ensures that the hatch 120 in the open position does not protrude too much from the top surface of the cabin 110, thereby further reducing the adverse effects of the hatch 120 in the open position on the take-off and landing of the UAV.

[0091] Reference Figure 10The drone hangar 100 according to this utility model may further include a landing pad 140 for parking drones. The landing pad 140 is raised and lowered within the cabin 110 using a lifting mechanism. When all the doors 120 are in the open position, the lifting mechanism drives the landing pad 140 to its highest position, allowing the drone to rise outside the hatch 111 for easier take-off and landing. Preferably, the top surface of the landing pad 140 at its highest position is higher than the open doors 120, thereby preventing the drone from moving laterally during take-off and contacting the doors 120, and preventing the doors 120 from interfering with the drone's take-off and landing.

[0092] Optionally, refer to Figures 2 to 4 When the hatch 120 is in the open position, the first transmission rod 122 is in the first position. When the hatch 120 is in the closed position, the first transmission rod 122 is in the second position. The angle between the first position and the second position is greater than or equal to 120 degrees.

[0093] When the hatch 120 is in the open position, the second drive rod 123 is in the third position. When the hatch 120 is in the closed position, the second drive rod 123 is in the fourth position. The angle between the third and fourth positions is greater than or equal to 120 degrees.

[0094] With the above configuration, the first transmission rod 122 and the second transmission rod 123 have a large rotation angle, which allows the hatch 120 to be fully extended to both sides of the cabin 110.

[0095] Optionally, refer to Figure 6 When the hatch 120 is in the closed position, in the projection of the UAV hangar 100 along the extension direction of the first pivot axis AX1 (the length direction D2 of the cabin 110), the line connecting the first pivot axis AX1 and the second pivot axis AX2 (as shown in the image) Figure 6 The dashed line segment in the diagram is parallel to the line connecting the third pivot axis AX3 and the fourth pivot axis AX4 (e.g., ...). Figure 6 The dashed line segment in the diagram is used to make the projections of the first transmission rod 122 and the second transmission rod 123 along the extension direction of the first pivot axis AX1 (the length direction D2 of the cabin 110) overlap as much as possible, so as not to occupy too much space inside the cabin 110.

[0096] Optionally, refer to Figure 7 When the hatch 120 is in the open position, in the projection of the UAV hangar 100 along the extension direction of the first pivot axis AX1, the line connecting the first pivot axis AX1 and the second pivot axis AX2 (as shown in the image) Figure 7 The dashed line segment in the diagram intersects the line connecting the third pivot axis AX3 and the fourth pivot axis AX4 (as shown in the diagram). Figure 7The dashed line segment in the diagram allows the side wall of the hatch 120 near the hull 110 when it is in the open position to be adjusted to a position parallel to the height direction D1 of the hull 110, further saving the space occupied by the hatch 120 on the outer side of the hull 110. Furthermore, the hatch 120 is connected by a first transmission rod 122 and a second transmission rod 123, resulting in a stable structure that prevents the hatch 120 from shaking and bumping against the outer side wall of the hull 110 when it is in the open position.

[0097] Unless otherwise defined, the technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art. The terminology used herein is for descriptive purposes only and is not intended to limit the scope of the invention. Terms such as “set” appearing herein can refer to either a component being directly attached to another component or a component being attached to another component via an intermediary. A feature described in one embodiment may be applied, alone or in combination with other features, to another embodiment, unless that feature is not applicable in that other embodiment or is otherwise stated.

[0098] This utility model has been described through the above embodiments. However, it should be understood that the above embodiments are for illustrative purposes only and are not intended to limit this utility model to the described embodiments. Those skilled in the art will understand that many more variations and modifications can be made based on the teachings of this utility model, and all such variations and modifications fall within the scope of protection claimed by this utility model.

Claims

1. A hangar for unmanned aerial vehicles (UAVs), characterized in that, The drone hangar includes: The cabin has a hatch on its top; At least one hatch for opening and closing the hatch; At least one first transmission rod, the first transmission rod being correspondingly disposed to the hatch, a first end of the first transmission rod being rotatably connected to the cabin body about a first pivot axis, and a second end of the first transmission rod being rotatably connected to the hatch about a second pivot axis; and At least one second transmission rod is provided, the second transmission rod is correspondingly provided with the hatch, the first end of the second transmission rod is rotatably connected to the cabin body about a third pivot axis, and the second end of the second transmission rod is rotatably connected to the hatch about a fourth pivot axis; The first pivot axis, the second pivot axis, the third pivot axis, and the fourth pivot axis are all arranged parallel to each other, so that the hatch can be movably connected to the cabin body between a closed position and an open position.

2. The drone hangar according to claim 1, characterized in that, When the hatch is in the open position, in the projection of the UAV hangar along the extension direction of the first pivot axis, the line connecting the first pivot axis and the second pivot axis intersects the line connecting the third pivot axis and the fourth pivot axis.

3. The drone hangar according to claim 1, characterized in that, The first and second transmission rods are constructed as bent rods such that when the hatch is in the open position, the first and second transmission rods cross the side wall of the cabin.

4. The drone hangar according to claim 3, characterized in that, The distance by which the hatch in the open position protrudes upward from the top surface of the cabin is less than or equal to one-fifth of the dimension of the hatch in the open position along the height direction of the cabin.

5. The drone hangar according to claim 1, characterized in that, When the hatch is in the open position, the first transmission rod is in a first position; when the hatch is in the closed position, the first transmission rod is in a second position, and the angle between the first position and the second position is greater than or equal to 120 degrees; and / or When the hatch is in the open position, the second transmission rod is in the third position; when the hatch is in the closed position, the second transmission rod is in the fourth position; the angle between the third position and the fourth position is greater than or equal to 120 degrees.

6. The unmanned aerial vehicle hangar according to any one of claims 1 to 5, characterized in that, The drone hangar also includes a rotation drive component, which is correspondingly arranged with the first transmission rod and is used to drive the corresponding first transmission rod to rotate around the first pivot axis.

7. The unmanned aerial vehicle hangar according to claim 6, characterized in that, The first end of the first transmission rod is provided with a first rotating shaft, the axis of the first rotating shaft is the first pivot axis, and the rotation drive component is used to drive the first rotating shaft to rotate.

8. The drone hangar according to claim 7, characterized in that, The drone hangar also includes a speed reducer, the rotary drive component is connected to the speed reducer, and the speed reducer is connected to the first rotating shaft.

9. The unmanned aerial vehicle hangar according to claim 7, characterized in that, Along the height direction of the cabin, the rotation drive component is arranged above the centerline of the cabin.

10. The unmanned aerial vehicle hangar according to claim 1, characterized in that, The drone hangar includes two hatches arranged in a direction perpendicular to the first pivot axis, such that the two hatches can be located on opposite sides of the hatch opening when in the open position.

11. The unmanned aerial vehicle hangar according to claim 10, characterized in that, When the two hatches are in the closed position, the two hatches are in sealed contact with each other, and the hatches are in sealed contact with the hatch openings.

12. The unmanned aerial vehicle hangar according to claim 11, characterized in that, One of the two hatches is provided with a first sealing strip, which, when both hatches are in the closed position, abuts against the bottom of the other hatch; and / or At least one of the two hatches is provided with a second sealing strip, which is disposed on the top of the hatch when it is in the closed position, and the second sealing strip is used to abut against the other of the two hatches when both hatches are in the closed position.

13. The unmanned aerial vehicle hangar according to claim 11, characterized in that, A third sealing strip is provided around the hatch, and the third sealing strip is used to abut against the lower surface of the hatch located in the closed position.

14. The unmanned aerial vehicle hangar according to claim 10, characterized in that, The top surface of the hatch in the closed position is higher at the end near the other hatch than at the end away from the other hatch; and / or During the process of the hatch moving from the closed position to the open position, the top surface of the hatch in the closed position deflects toward the outside of the hatch opening.

15. The unmanned aerial vehicle hangar according to claim 10, characterized in that, Each of the hatches is connected to two of the first drive rods, the two first drive rods being spaced apart along the extension direction of the first pivot axis; and / or Each of the hatches is connected to two second drive rods, which are spaced apart along the extension direction of the third pivot axis.

16. The unmanned aerial vehicle hangar according to claim 1, characterized in that, The hatch is equipped with a heating device for heating and melting the snow on the hatch.

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