Airport cabin door and airport

Through the asymmetric door body design and inner barrier along the water guide groove structure, the problem of limited installation location of the drone airport detection component is solved, and better detection effect and structural waterproofing performance are achieved.

CN223279360UActive Publication Date: 2025-08-29FOSHAN HENENG THINGS SOFTWARE DEV CO LTD +1
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Patent Information

Application Number
CN202422155534.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-03
Publication Date
2025-08-29
Estimated Expiration
2034-09-03

AI Technical Summary

Technical Problem

The installation location of the inspection components of existing drone airports is limited, resulting in poor inspection results or inability to achieve.

Method used

The asymmetric left door body and right door body design is adopted. The left door body is higher than the right door body. The position of the installation detection component is located on the upper part of the left door body, and is located inside the cabin after the hatch door is closed. The inner barrier and barrier water guide groove design is used to avoid rainwater seepage, increase the installation height of the detection component and avoid obstruction of the right door body.

Benefits of technology

The installation height and detection effect of the detection components are improved, the interference of the right door body on detection in the open state is reduced, the structural strength is enhanced and the rainwater seepage is effectively prevented.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an airport cabin door and an airport, and belongs to the technical field of unmanned aerial vehicles, the airport cabin door comprises a left door body and a right door body, the left door body and the right door body are oppositely arranged and adopt an overturning opening and closing mode, after the left door body and the right door body are overturned and opened through a driving mechanism, the overall height of the left door body is higher than that of the right door body, and the overall height of the right door body is lower than that of the left door body. The upper portion of the left door body is provided with a mounting position used for mounting the detection assembly, the detection assembly can be directly mounted on the mounting position or mounted on the mounting position through a mounting support, the arrangement height of the mounting position is effectively increased by adopting the asymmetric door bodies, namely the large door and the small door, and therefore the mounting height of the detection assembly is effectively increased; the detection assembly can obtain a better detection effect compared with an unmanned aerial vehicle, and meanwhile, when the surrounding environment is detected through the detection assembly, the right door body can be effectively prevented from interfering with or shielding detection of the detection assembly by lifting the installation height of the detection assembly and reducing the height of the right door body in the open state.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), in particular to an airport cabin door and an airport. Background Art

[0002] For unmanned drone airports, it is necessary to rely on the airport's own detection components to determine the status of the drone or airport, so as to ensure the normal operation of the drone and the airport.

[0003] However, at existing airports, due to the limitations of their own structures, the installation locations of detection components for detecting the status of drones or the surrounding environment of the airport are relatively restricted, resulting in the inability of the detection components to perform detection or poor detection effects. Utility Model Content

[0004] In order to overcome the defects of the prior art, the utility model provides an airport cabin door and an airport.

[0005] The technical solution adopted by the utility model to solve its technical problems is: an airport cabin door, comprising a left door body and a right door body, after the left door body and the right door body are flipped open by a driving mechanism, the left door body is higher than the right door body, and an installation position for installing a detection component is provided on the upper part of the left door body, and the detection component can be directly installed in the installation position or installed on the installation position through a mounting bracket.

[0006] Preferably, the installation position is located inside the left door body, that is, after the airport hatch is closed, the detection component is located inside the airport cabin body.

[0007] Preferably, when the airport door is flipped open, the horizontal position of the installation position is higher than the right door body.

[0008] Preferably, the left door body and the right door body are L-shaped, and are provided with side baffles on both sides. When the left door body and the right door body are in a closed state, they can form a closed baffle cover.

[0009] Preferably, the front end of the left door body is provided with an inner guard edge, and the inner guard edge extends to the side baffles on both sides of the left door body. In the closed state, the right door body is buckled and covered on the inner guard edge.

[0010] Preferably, a water guide groove is provided on the inner edge in the extension direction. In the closed state, the front end of the right door body is opposite to the water guide groove.

[0011] An airport comprises an airport bottom cabin and the above-mentioned airport cabin door, wherein the left door body and the right door body are respectively arranged on the left and right sides of the airport bottom cabin.

[0012] Preferably, after the left door body and the right door body are flipped open, the horizontal position of the installation position is higher than the airport bottom cabin.

[0013] Preferably, the installation position is located on the inner side of the inner baffle, and the front and rear sides of the airport bottom cabin are provided with protrusions, and the protrusions are provided with ventilation windows or external interfaces. In the closed state, the side baffles of the left door body and the right door body are respectively buckled and covered on the upper outer edge of the protrusion, and the upper outer edge of the protrusion forms a guide surface.

[0014] Preferably, the detection component includes but is not limited to a camera, an infrared camera, a thermal imaging camera, an ultrasonic sensor, and a non-contact temperature sensor.

[0015] The beneficial effect of the present invention is that by adopting an asymmetric door body, that is, a large and small door, the setting height of the installation position is effectively raised, thereby effectively raising the installation height of the detection component, so that the detection component can achieve better detection effect relative to the drone. At the same time, when the detection component detects the surrounding environment, by raising the installation height of the detection component and lowering the height of the right door body in the open state, it can effectively avoid the right door body interfering with or blocking the detection of the detection component. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a three-dimensional diagram of the left door body and the right door body of an embodiment of the present utility model;

[0017] Figure 2 for Figure 1 A magnified schematic diagram of point A in the middle;

[0018] Figure 3 The three-dimensional airport in the embodiment of the utility model Figure 1 (Airport door open state);

[0019] Figure 4 The three-dimensional airport in the embodiment of the utility model Figure 2 (Airport door closed state);

[0020] Figure 5 This is a partial cross-sectional schematic diagram of the closed state of the left door body and the right door body in an embodiment of the present invention (the arrow in the figure indicates the direction of rainwater infiltration).

[0021] In the figure, 10, left door body; 11, installation position; 12, inner guard edge; 13, guard edge water guide groove; 20, right door body; 31, side baffle; 40, detection component; 50, airport bottom cabin; 51, outer protrusion; 52, guide surface; 53, ventilation window; 54, external interface. DETAILED DESCRIPTION

[0022] The following further describes specific embodiments of the present invention in conjunction with the accompanying drawings. It should be noted that the descriptions of these embodiments are intended to aid understanding of the present invention and do not constitute limitations on the present invention. Furthermore, the technical features involved in the various embodiments of the present invention described below may be combined with one another as long as they do not conflict with one another.

[0023] As attached Figure 1 、 2 As shown in Figure 5, the utility model provides an airport cabin door, including a left door body 10 and a right door body 20. The left door body 10 and the right door body 20 are arranged opposite to each other and adopt a flipping opening and closing method. After the left door body 10 and the right door body 20 are flipped and opened by the driving mechanism, the overall height of the left door body 10 is higher than that of the right door body 20. A mounting position 11 for mounting a detection component 40 is provided on the upper part of the left door body 10. The detection component 40 can be directly mounted on the mounting position 11 or mounted on the mounting position 11 through a mounting bracket.

[0024] Specifically, by adopting an asymmetric door body, that is, a large and small door, the setting height of the installation position 11 is effectively raised, thereby effectively raising the installation height of the detection component 40, so that the detection component 40 can achieve better detection effect relative to the drone. At the same time, when detecting the surrounding environment through the detection component 40, by raising the installation height of the detection component 40 and lowering the height of the right door body 20 in the open state, it can effectively avoid the right door body 20 interfering with or blocking the detection of the detection component 40.

[0025] Furthermore, in order to prevent the detection component 40 from being exposed to bad weather, the installation position 11 is located on the inner side of the left door body 10, that is, after the airport hatch is closed, the detection component 40 is located inside the airport cabin.

[0026] Furthermore, when the airport door is flipped open, the horizontal position of the installation position 11 is higher than the right door body 20, that is, when it is open, the horizontal setting height of the detection component 40 is higher than the right door body 20, thereby more effectively avoiding the right door body 20 blocking the detection component 40 in the open state, thereby interfering with the detection of the airport's external environment.

[0027] Furthermore, the left door body 10 and the right door body 20 are L-shaped, and side baffles 31 are provided on both sides. When the left door body 10 and the right door body 20 are in a closed state, they can form a closed baffle. By providing the side baffles 31, the overall structural strength of the left door body 10 and the right door body 20 is improved, that is, the overall structural strength of the baffle is improved.

[0028] Furthermore, an inner guard edge 12 is provided at the front end of the left door body 10, and the inner guard edge 12 extends to the side baffles 31 on both sides of the left door body 10. In the closed state, the right door body 20 is snapped on and covers the inner guard edge 12, thereby forming a relative seal. On rainy days, rainwater that penetrates into the door gap is discharged to both sides through the inner guard edge 12 to prevent rainwater from penetrating into the interior. At the same time, compared with the conventional sealing method using sealing strips, it can effectively avoid water seepage caused by aging of the sealing strips.

[0029] Furthermore, in order to improve the diversion effect of the inner guard edge 12 on rainwater, a guard edge water guide groove 13 is provided on the inner guard edge 12 in the extension direction. In the closed state, the front end of the right door body 20 is opposite to the guard edge water guide groove 13. After the rainwater seeps in through the door gap, it can directly fall into the guard edge water guide groove 13 and then be quickly discharged from both sides.

[0030] As attached Figure 3-5 As shown, an airport includes an airport bottom cabin 50 and the above-mentioned airport cabin door. A landing platform is provided on the airport bottom cabin 50, and the drone can land on the landing platform. The left door body 10 and the right door body 20 are respectively arranged on the left and right sides of the airport bottom cabin 50, and are connected to the airport bottom cabin 50 through a flipping mechanism. The flipping mechanism is driven by a driving mechanism, which can drive the left door body 10 and the right door body 20 to flip open or close.

[0031] Furthermore, after the left door body 10 and the right door body 20 are flipped open, the horizontal position of the installation position 11 is higher than the airport bottom cabin 50. Similarly, by adopting an asymmetric door body, the setting height of the installation position 11 is effectively raised, avoiding the airport bottom cabin 50 being too high and affecting the detection of the detection component 40.

[0032] Furthermore, the installation position 11 is located on the inner side of the inner baffle 12, and the front and rear sides of the airport bottom cabin 50 are provided with an outer protrusion 51, and the outer protrusion 51 is provided with a ventilation window 53 or an external interface 54. In the closed state, the side baffles 31 of the left door body 10 and the right door body 20 are respectively buckled and covered on the upper outer edge of the outer protrusion 51, and the upper outer edge of the outer protrusion 51 forms a guide surface 52. The guide surface 52 can form a guide gap relative to the left door body 10 and the right door body 20. Rainwater can quickly flow down along both sides of the outer protrusion 51 through the guidance of the guide surface 52 and the guide gap, thereby reducing the probability of rainwater seeping in from the ventilation window 53 or the external interface 54.

[0033] Furthermore, the detection component 40 includes but is not limited to one or more of a camera, an infrared camera, a thermal imaging camera, an ultrasonic sensor, and a non-contact temperature sensor. In this example, the detection component 40 is a camera.

[0034] The embodiments of the present invention are described in detail above with reference to the accompanying drawings, but the present invention is not limited to the described embodiments. It is apparent to those skilled in the art that various changes, modifications, substitutions, and variations to these embodiments may be made without departing from the principles and spirit of the present invention, and these changes and modifications still fall within the scope of protection of the present invention.

Claims

1. An airport door, characterized in that: The invention comprises a left door body (10) and a right door body (20); after the left door body (10) and the right door body (20) are flipped and opened, the left door body (10) is higher than the right door body (20); and an installation position (11) for installing a detection component (40) is provided on the upper part of the left door body (10).

2. The airport door according to claim 1, characterized in that: The installation position (11) is located on the inner side of the left door body (10).

3. The airport door according to claim 1, characterized in that: In the flip-open state, the horizontal position of the mounting position (11) is higher than the right door body (20).

4. The airport door according to claim 1, characterized in that: The left door body (10) and the right door body (20) are L-shaped, and are provided with side baffles (31) on both sides.

5. The airport door according to claim 4, characterized in that: The front end of the left door body (10) is provided with an inner retaining edge (12), and the inner retaining edge (12) extends to the side retaining plates (31) on both sides of the left door body (10). In the closed state, the right door body (20) is buckled and covered on the inner retaining edge (12).

6. The airport door according to claim 5, characterized in that: A water guide groove (13) is provided on the inner edge (12) in the extension direction. In the closed state, the front end of the right door body (20) faces the water guide groove (13).

7. An airport, characterized in that: It comprises an airport bottom cabin (50) and the airport cabin door according to any one of claims 1 to 6, wherein the left door body (10) and the right door body (20) are respectively arranged on the left and right sides of the airport bottom cabin (50).

8. The airport according to claim 7, characterized in that After the left door body (10) and the right door body (20) are flipped open, the horizontal position of the installation position (11) is higher than the airport bottom cabin (50).

9. The airport according to claim 7, characterized in that The mounting position (11) is located on the inner side of the inner baffle (12), and the front and rear sides of the airport bottom cabin (50) are both provided with outer protrusions (51), and the outer protrusions (51) are provided with ventilation windows (53) or external interfaces (54). In the closed state, the side baffles (31) of the left door body (10) and the right door body (20) are respectively buckled and covered on the upper outer edges of the outer protrusions (51), and the upper outer edges of the outer protrusions (51) form a guide surface (52).

10. The airport according to claim 7, characterized in that The detection component (40) includes but is not limited to a camera, an infrared camera, a thermal imaging camera, an ultrasonic sensor, and a non-contact temperature sensor.