Unmanned aerial vehicle hangar
By setting interceptor boards, placement boards and limit boards in the storage compartment of the drone hangar, the problem of drone landing position deviation is solved, and the stability and position accuracy of the drone during storage is achieved.
Patent Information
- Application Number
- CN202421348937.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-13
- Publication Date
- 2025-03-21
- Estimated Expiration
- 2034-06-13
AI Technical Summary
Due to the influence of wind or man-made control, the drone may not land completely within the specified range when landing, resulting in a deviation in the landing position of the rack, which may easily cause collisions on the drone's wings during storage.
A drone hangar was designed. By setting interceptor plates, placement plates and limit plates in the storage compartment, the movement of the interceptor plates and the rotation of the placement plates are used to adjust and limit the frame position to ensure the stable position of the drone during storage.
It effectively prevents bumps in the drone wings during storage, improves the stability of the drone during storage, and ensures the accurate position of the rack when landing.
Smart Images

Figure CN222646307U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle hangar. Background Art
[0002] A drone hangar refers to a facility specifically used for the storage and maintenance of drones. A drone hangar typically includes the following features and equipment: Storage area: An area used to store drones, usually with a specially designed hangar to ensure that drones can be safely stored and protected. Charging equipment: A drone hangar is usually equipped with charging equipment for charging the drone's batteries. The charging equipment needs to meet the specifications and requirements of the drone's batteries to ensure that the charging process is safe and reliable. Maintenance equipment: A drone hangar may also be equipped with maintenance equipment, such as tool boxes, repair tables, etc., for daily maintenance and servicing of drones. Safety facilities: A drone hangar needs to meet safety standards and may include facilities such as surveillance cameras and anti-theft systems to ensure the safety of drones and equipment.
[0003] After searching, the Chinese patent publication number CN220721436U discloses a drone hangar, including a warehouse body, with two inner covers and two outer covers arranged on the top of the warehouse body, the two inner covers are located between the two outer covers, and horizontal sliding components are installed on both sides of the upper part of the warehouse body, which drive the outer cover to move horizontally through the horizontal sliding components, and the adjacent outer covers and inner covers are connected by a flipping component. The horizontal movement of the outer cover can drive the horizontal movement of the inner cover, and the inner cover can be flipped and lifted on the outer cover by the flipping component.
[0004] In the above scheme, when the drone falls, due to the influence of wind or human control, the drone will not fall completely within the specified range, and the landing position of the rack will deviate, which will easily cause bumps on the wings of the drone when the drone is stored. Utility Model Content
[0005] The purpose of the utility model is to solve the problem in the prior art that due to the influence of wind or human control, the drone will not fall completely within the specified range, and the landing position of the rack will deviate, which will easily cause bumps on the wings of the drone when the drone is stored, and a drone hangar is proposed.
[0006] In order to achieve the above purpose, the utility model adopts the following technical solutions:
[0007] A drone hangar comprises a storage bin, wherein a support plate is slidably connected to the storage bin, an interception plate is slidably connected to the surface of the support plate, a placement plate is rotatably arranged in the middle of the support plate, a limit plate is connected to the axial position of the support plate, an end of the placement plate extends to the top of the limit plate, and the placement plate can be in the same horizontal plane as the support plate, and when the interception plate moves toward the placement plate, the limit plate is pressed by the end of the placement plate.
[0008] In order to facilitate limiting the sliding direction of the intercepting plate, preferably, a sliding groove is opened on the support plate, the intercepting plate is slidably connected to the sliding groove, the placement plate is rotatably connected in the sliding groove through a connecting seat, and a contact block is fixedly connected to the intercepting plate, and the contact block can cooperate with the connecting seat.
[0009] In order to facilitate sliding of the intercepting plate, further, a guide cylinder is fixedly connected to the bottom of the support plate, a guide rod is slidably connected to the guide cylinder, and the guide rod is fixedly connected to the intercepting plate.
[0010] In order to facilitate the pushing of the guide rod on the guide cylinder, further, a boosting cylinder is fixedly connected in the storage bin, a boosting rod is slidably connected to the boosting cylinder, one end of the boosting rod is fixedly connected to a support plate, and a piston is provided at the other end of the boosting rod, the piston is fitted with the inner wall of the boosting cylinder, and the boosting cylinder is communicated with the guide cylinder.
[0011] In order to facilitate the movement of the support plate, preferably, a reciprocating screw is rotatably connected in the storage bin, a movable block is threadedly connected to the reciprocating screw, and the movable block fits against the inner wall of the storage bin, and the support plate is fixedly connected to the movable block.
[0012] In order to facilitate supporting the end of the placement plate, preferably, a spring is fixedly connected to the axial position of the support plate, and the limit plate is fixedly connected to the connecting end of the spring.
[0013] Compared with the prior art, the utility model provides a drone hangar with the following features:
[0014] Beneficial effects:
[0015] 1. The drone hangar moves the interception plate to push the position of the rack, so that the drone can be pushed to a specified range, and the position of the rack that deviates when landing can be adjusted to prevent the drone's wings from being bumped when being stored;
[0016] 2. The drone hangar forms an inverted cone-shaped placement plate by rotating, and can also limit the drone rack so that the placement plate is in an inclined state, thereby improving the stability of the drone when it is stored and preventing it from shaking during movement.
[0017] The parts not involved in the device are the same as the existing technology or can be implemented by using the existing technology. The utility model can use the interception plate to push the position of the rack, so that it can push the position of the drone to a specified range, adjust the position of the rack that deviates when landing, and prevent the wings of the drone from being bumped when being stored. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 This is a structural schematic diagram of a UAV hangar storage compartment proposed by the utility model;
[0019] Figure 2 This is a schematic diagram of a first-person perspective of a UAV hangar support plate proposed by the utility model;
[0020] Figure 3 This is a schematic diagram of a second viewing angle of a UAV hangar support plate proposed by the utility model;
[0021] Figure 4 This is a structural schematic diagram of a cross-section of a UAV hangar support plate proposed by the utility model.
[0022] In the figure: 1. Storage bin; 101. Reciprocating screw rod; 102. Movable block; 2. Support plate; 201. Slide groove; 3. Intercepting plate; 301. Contact block; 4. Guide cylinder; 401. Guide rod; 5. Boosting cylinder; 501. Boosting rod; 6. Placement plate; 601. Connecting seat; 7. Limiting plate. DETAILED DESCRIPTION
[0023] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.
[0024] In the description of the present invention, it should be understood that the terms "upper", "lower", "front", "back", "left", "right", "top", "bottom", "inside", "outside", etc., indicating directions or positional relationships, are based on the directions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore should not be understood as a limitation on the present invention.
[0025] Example:
[0026] Reference Figure 1-Figure 4A drone hangar comprises a storage bin 1, a side wall of the storage bin 1 is provided with a bay opening, so that the drone can enter the storage bin 1 from the bay opening, and a rotatable reciprocating screw 101 is installed in the storage bin 1, a movable block 102 is threadedly connected to the reciprocating screw 101, and the movable block 102 is in contact with the inner wall of the storage bin 1, and then a support plate 2 is fixedly connected to the movable block 102, and the support plate 2 can extend to the outside of the storage bin 1 through the bay opening, and a driving machine or motor is also provided in the storage bin 1 to drive the reciprocating screw 101 to rotate. During the rotation of the reciprocating screw 101, the movable block 102 will move on the reciprocating screw 101, and at this time, the support plate 2 will be driven to move, so that it can move from the bay opening position of the storage bin 1 to the outside.
[0027] In addition, a slide groove 201 is provided on the surface of the support plate 2, and an interception plate 3 is slidably connected to the slide groove 201. The interception plate 3 is arc-shaped and can be arranged in six groups. When the six groups of interception plates 3 are close to each other, a circular range can be formed. A rotatable placement plate 6 is also provided within the circular range, and a connecting seat 601 is provided at one end of the placement plate 6. The connecting seat 601 is rotatably connected to the slide groove 201 through a rotating shaft, and a limiting plate 7 is connected to the axial position of the support plate 2 through a spring, and the top of the limiting plate 7 can be against the other end of the placement plate 6, which is used to support the placement plate 6 so that it is in the same horizontal plane as the support plate 2, and the elastic force of the spring in the device can support the placement plate 6 so that the surfaces of the placement plate 6 and the support plate 2 are parallel to each other. When the UAV lands, the frame of the UAV can contact the surface of the placement plate 6, and during this process, the spring can continue to support the placement plate 6 so that the surfaces of the placement plate 6 and the support plate 2 are parallel to each other.
[0028] Please refer to Figure 3 As shown in the figure, a guide cylinder 4 is fixedly connected to the bottom of the support plate 2, and a guide rod 401 is slidably connected to the guide cylinder 4, and then the extended end of the guide rod 401 is fixedly connected to the intercepting plate 3, and a piston is also provided on the guide rod 401, and the piston is in contact with the inner wall of the guide cylinder 4. When the guide rod 401 needs to move, gas can be transported into the guide cylinder 4, thereby pushing the guide rod 401.
[0029] In order to facilitate the pushing of the guide rod 401, a booster cylinder 5 is fixedly connected in the storage bin 1, and a booster rod 501 is slidably connected to the booster cylinder 5. One end of the booster rod 501 is fixedly connected to the support plate 2, and a piston is provided at the other end of the booster rod 501. The piston fits against the inner wall of the booster cylinder 5, and the cavity on the outside of the piston close to the booster rod 501 is connected to the guide cylinder 4, while the cavity on the outside of the piston away from the booster rod 501 is connected to the outside air.
[0030] When the support plate 2 moves from the inside of the storage bin 1 to the outside, at this time, the boost rod 501 will transport the air from the boost cylinder 5 to the guide cylinder 4. At this time, the guide rod 401 drives the interception plate 3 to move on the slide groove 201, so that the interception plate 3 moves in the opposite direction away from the placement plate 6. Then, a landing command can be issued to the drone. At this time, the expanded interception plate 3 will form a ring pattern on the support plate 2, and then the frame part of the drone can fall onto the placement plate 6. When the frame of the drone deviates from the placement plate 6, it means that the frame of the drone lands on the side close to the interception plate 3, and the placement plate 6 will remain parallel to the plane of the support plate 2 under the limiting action of the limiting plate 7. At this time, the drive motor or motor is started to drive the reciprocating screw 101 to rotate, so that the support plate 2 enters the storage bin 1.
[0031] During this process, the gas in the guide cylinder 4 will return to the booster cylinder 5, and then the intercepting plate 3 will move in the slide groove 201, so that it moves toward the placement plate 6. The intercepting plate 3 is also fixedly connected to the contact block 301, and the contact block 301 can cooperate with the connecting seat 601. During the movement, the contact block 301 will contact the outer wall of the connecting seat 601, and then push the connecting seat 601, so that it can drive the placement plate 6 to rotate, and at the same time press the limit plate 7, so that the placement plate 6 is in the shape of an inverted cone. During this process, the intercepting plate 3 will push the position of the frame, so that it can push the position of the drone within the specified range, adjust the position of the deviation generated when the frame lands, and prevent the wings of the drone from being bumped during storage. The placement plate 6 that forms an inverted cone shape by rotation can also limit the frame of the drone, so that the placement plate 6 is in a tilted state, thereby improving the stability of the drone during storage and preventing shaking during movement.
[0032] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.
Claims
1. A drone hangar, comprising a storage compartment (1), characterized in that: The storage bin (1) is slidably connected to a support plate (2), and an interception plate (3) is slidably connected to the surface of the support plate (2). A placement plate (6) is rotatably arranged in the middle of the support plate (2), and a limiting plate (7) is connected to the axial position of the support plate (2). The end of the placement plate (6) extends to the top of the limiting plate (7), and the placement plate (6) can be in the same horizontal plane as the support plate (2). When the interception plate (3) moves toward the placement plate (6), the limiting plate (7) is pressed by the end of the placement plate (6).
2. The drone hangar according to claim 1, characterized in that: The support plate (2) is provided with a slide groove (201), the intercepting plate (3) is slidably connected to the slide groove (201), the placement plate (6) is rotatably connected in the slide groove (201) via a connecting seat (601), and the intercepting plate (3) is fixedly connected with a contact block (301), and the contact block (301) can cooperate with the connecting seat (601).
3. The drone hangar according to claim 2, characterized in that: The bottom of the support plate (2) is fixedly connected to a guide cylinder (4), the guide cylinder (4) is slidably connected to a guide rod (401), and the guide rod (401) is fixedly connected to the intercepting plate (3).
4. The drone hangar according to claim 3, characterized in that: A boost cylinder (5) is fixedly connected inside the storage bin (1), a boost rod (501) is slidably connected to the boost cylinder (5), one end of the boost rod (501) is fixedly connected to the support plate (2), and a piston is provided at the other end of the boost rod (501), the piston is in contact with the inner wall of the boost cylinder (5), and the boost cylinder (5) is connected to the guide cylinder (4).
5. The drone hangar according to claim 1, characterized in that: A reciprocating screw rod (101) is rotatably connected inside the storage bin (1), a movable block (102) is threadedly connected to the reciprocating screw rod (101), and the movable block (102) is in contact with the inner wall of the storage bin (1), and the support plate (2) is fixedly connected to the movable block (102).
6. The drone hangar according to claim 1, characterized in that: The support plate (2) is fixedly connected to a spring at the axial center position, and the limit plate (7) is fixedly connected to the connection end of the spring.
Citation Information
Patent Citations
Unmanned aerial vehicle hangar
CN220721436U
Cited By
Novel modularized light-weight unmanned aerial vehicle hangar cabin
CN224029272U