Airplane hangar

Abstract

This utility model discloses an aircraft landing bay, including a parking bay, a lifting platform, a lifting drive mechanism, a ring wall, and a rotation drive mechanism. The ring wall is located at the center of the parking bay. The rotation drive mechanism drives the ring wall to rotate relative to the parking bay. The side walls of the ring wall have entrances and exits. A passageway is provided in the central area of ​​the top of the parking bay, corresponding to the hollow part of the ring wall. Multiple compartments are arranged circumferentially within the parking bay, and these compartments surround the outer perimeter of the ring wall. The lifting platform is horizontally positioned within the ring wall, and the lifting drive mechanism drives the lifting platform to move up and down in the height direction. This utility model can improve site utilization and save costs.

Description

Technical Field

[0001] This utility model relates to the field of takeoff and landing technology, and in particular to an aircraft takeoff and landing cabin. Background Technology

[0002] Existing eVTOL landing pads, in sparsely populated areas, resemble traditional helicopter landing pads, with some design concepts still adhering to the standards of the helicopter era. The extensive and redundant space planning, lacking significant improvements, means that if the urban commuting market requires large-scale eVTOL traffic and distributed landing pads across various urban areas, the limited space on high-rise rooftops and the small footprint of aircraft wings make precise management and parking difficult. This results in the landing pads not being used to their full potential, failing to save rental costs for landing pad operators. Utility Model Content

[0003] The purpose of this invention is to provide an aircraft take-off and landing cabin that can improve site utilization and save costs.

[0004] To solve the above-mentioned technical problems, this utility model provides the following technical solution:

[0005] An aircraft landing bay includes a parking bay, a lifting platform, a lifting drive mechanism, a ring wall, and a rotation drive mechanism. The ring wall is located at the center of the parking bay. The rotation drive mechanism drives the ring wall to rotate relative to the parking bay. The side walls of the ring wall have entrances and exits. The central area of ​​the top of the parking bay, corresponding to the hollow part of the ring wall, has a passageway. The parking bay has multiple compartments arranged circumferentially, and the multiple compartments surround the outer perimeter of the ring wall. The lifting platform is horizontally located inside the ring wall, and the lifting drive mechanism drives the lifting platform to move up and down in the height direction.

[0006] Preferably, the aircraft landing bay further includes a rotating platform and a rotating drive mechanism. The rotating platform is located on the upper part of the lifting platform, and the rotating drive mechanism is located on the lifting platform and is used to drive the rotating platform to rotate relative to the lifting platform.

[0007] Preferably, the lower end of the annular wall is pressed against the bottom wall inside the parking compartment, and the annular wall is rotatably connected to the bottom wall inside the parking compartment. The upper end of the annular wall is supported by the top wall inside the parking compartment, and the annular wall is rotatably connected to the top wall inside the parking compartment.

[0008] Preferably, the aircraft compartment is equipped with multiple firewalls, which divide the aircraft compartment into multiple compartments.

[0009] Preferably, the firewall includes a load-bearing wall and a movable wall, the movable wall and the load-bearing wall being arranged sequentially along the radial direction of the annular wall and away from the annular wall, the movable wall being movable along the radial direction of the annular wall to allow communication or closure between two adjacent compartments.

[0010] Preferably, the entrance and exit of the annular wall are provided with sliding doors, which are used to open or close the entrance and exit.

[0011] Preferably, at least one of the multiple cabins is a waiting cabin, and the remaining cabins are parking cabins.

[0012] Preferably, the outer periphery of the parking cabin is provided with multiple glass walls, and the multiple glass walls correspond one-to-one with the multiple cabins.

[0013] Preferably, the outer perimeter of the top of the parking cabin is provided with a fall protection net.

[0014] Preferably, the parking bay is hexagonal in shape, and six compartments are arranged circumferentially inside the parking bay.

[0015] Compared with the prior art, the beneficial effects of this embodiment of the aircraft takeoff and landing cabin are as follows:

[0016] In this invention, before the aircraft lands back into the parking bay, the top surface of the lifting platform is flush with the top surface of the parking bay, allowing the aircraft to land on the lifting platform. Then, the lifting drive mechanism drives the lifting platform to descend, allowing the aircraft to enter the parking bay. The aircraft can then enter the cabin through the entrance / exit of the annular wall. Simultaneously, the rotation drive mechanism can drive the annular wall to rotate, aligning the entrance / exit of the annular wall with one of the cabins, facilitating parking the aircraft in any of the cabins. Since the parking bay has multiple cabins arranged circumferentially, it is convenient to park multiple aircraft, ensuring a regular and compact parking arrangement, facilitating management, fully utilizing the space, and saving on subsequent management costs. When the aircraft needs to take off, it can enter the lifting platform through the entrance / exit of the annular wall, and then the lifting drive mechanism can drive the lifting platform to rise until it is flush with the top surface of the parking bay, allowing the aircraft to take off. Attached Figure Description

[0017] Figure 1 This is a perspective view of one embodiment of the present utility model;

[0018] Figure 2 This is another perspective view of an embodiment of the present utility model;

[0019] Figure 3 This is a perspective view of one embodiment of the present utility model;

[0020] Figure 4 This is another perspective view of an embodiment of the present utility model;

[0021] Figure 5 This is a schematic diagram of the ring wall, lifting platform and rotating platform according to an embodiment of the present utility model;

[0022] Figure 6 This is a schematic diagram of the first application of the parking bay according to an embodiment of the present utility model;

[0023] Figure 7 This is a schematic diagram illustrating a second application of the parking bay according to an embodiment of the present utility model;

[0024] Figure 8 This is a schematic diagram of the third application of the parking bay according to an embodiment of this utility model;

[0025] Figure 9 This is a schematic diagram of the fourth application of the parking bay in this utility model embodiment.

[0026] In the diagram, 1 is the aircraft bay; 11 is the passageway; 12 is the compartment; 13 is the firewall; 131 is the load-bearing wall; 132 is the movable wall; 14 is the glass wall; and 15 is the fall protection net.

[0027] 2. Lifting platform; 3. Lifting drive mechanism; 4. Circular wall; 41. Entrance / exit; 42. Side sliding door; 5. Rotating platform; 6. Elevator; 7. Bearing wheel assembly. Detailed Implementation

[0028] The specific embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are used to illustrate this utility model, but are not intended to limit its scope.

[0029] In the description of this utility model, it should be understood that the term "comprising" as used in this specification means the presence of the stated features, integers, steps, operations, parts, and / or components, but does not exclude the presence or addition of one or more other features, integers, steps, operations, parts, components, and / or groups thereof. It should be understood that when we say a part is "connected" to another part, it can be directly connected to the other part, or there may be intermediate parts. The term "and / or" as used herein includes all or any unit and all combinations of one or more associated listed items.

[0030] like Figures 1 to 9As shown, this utility model relates to an aircraft takeoff and landing cabin, including a parking cabin 1, a lifting platform 2, a lifting drive mechanism 3, a ring wall 4, and a rotation drive mechanism. The ring wall 4 is located at the center of the parking cabin 1. The rotation drive mechanism is used to drive the ring wall 4 to rotate relative to the parking cabin 1. The side wall of the ring wall 4 has an entrance / exit 41. The central area of ​​the top of the parking cabin 1 and the hollow part of the ring wall 4 have a passage opening 11. The parking cabin 1 has a plurality of compartments 12 arranged circumferentially, and the plurality of compartments 12 surround the outer periphery of the ring wall 4. The lifting platform 2 is horizontally arranged inside the ring wall 4. The lifting drive mechanism 3 is used to drive the lifting platform 2 to move up and down in the height direction.

[0031] In this invention, before the aircraft lands back into the parking bay 1, the top surface of the lifting platform 2 is flush with the top surface of the parking bay 1, allowing the aircraft to land on the lifting platform 2. Then, the lifting drive mechanism 3 drives the lifting platform 2 to descend, allowing the aircraft to enter the parking bay 1. The aircraft can then enter the compartment 12 through the entrance / exit 41 of the annular wall 4. Simultaneously, the rotation drive mechanism drives the annular wall 4 to rotate, aligning the entrance / exit 41 of the annular wall 4 with one of the compartments 12. The aircraft can be parked in any of the cabins 12. Since there are multiple cabins 12 arranged circumferentially in the parking cabin 1, it is convenient to park multiple aircraft. The parking positions of multiple aircraft are regular and compact, which is convenient for management, makes full use of the space, and saves later management costs. When the aircraft needs to take off, the aircraft can enter the lifting platform 2 through the entrance 41 of the ring wall 4. Then the lifting drive mechanism 3 can drive the lifting platform 2 to rise to be flush with the top surface of the parking cabin 1 so that the aircraft can take off.

[0032] It should be noted that the lifting drive mechanism 3 is a conventional lifting drive mechanism 3 on the market. The lifting drive mechanism 3 is a screw jack or a rigid chain jack.

[0033] In this embodiment, the aircraft takeoff and landing cabin further includes a rotating platform 5 and a rotating drive mechanism. The rotating platform 5 is located on the upper part of the lifting platform 2. The rotating platform 5 and the lifting platform 2 are rotatably connected by a bearing wheel set 7. Two rings of bearing wheel sets 7 are provided between the rotating platform 5 and the lifting platform 2. The rotating drive mechanism is located on the lifting platform 2 and is used to drive the rotating platform 5 to rotate relative to the lifting platform 2.

[0034] That is, when the aircraft lands on the rotating platform 5, the rotating drive mechanism drives the rotating platform 5 to rotate, so that the aircraft can face the entrance 41 of the annular wall 4, so that the aircraft can be parked in the cabin 12.

[0035] It should be noted that the rotary drive mechanism is also a conventional rotary drive mechanism on the market. The rotary platform 5 is rotatably connected to the lifting platform 2. The rotary drive mechanism can be a rotary drive mechanism composed of a motor and gears to drive the rotary platform 5 to rotate.

[0036] In this embodiment, the lower end of the annular wall 4 is pressed against the bottom wall inside the parking compartment 1, and the annular wall 4 is rotatably connected to the bottom wall inside the parking compartment 1. The upper end of the annular wall 4 is supported by the top wall inside the parking compartment 1, and the annular wall 4 is rotatably connected to the top wall inside the parking compartment 1.

[0037] Specifically, the lower end of the annular wall 4 is rotatably connected to the bottom wall of the parking compartment 1 via a bearing wheel set 7, and the upper end of the annular wall 4 is rotatably connected to the top wall of the parking compartment 1 via a bearing wheel set 7. Thus, while the annular wall 4 can rotate relative to the parking compartment 1, it can also support the parking compartment 1, ensuring the stability of the parking compartment 1.

[0038] In this embodiment, the parking bay 1 is provided with multiple firewalls 13, which divide the parking bay 1 into multiple compartments 12, thereby providing fire protection between adjacent compartments 12.

[0039] In this embodiment, the firewall 13 includes a load-bearing wall 131 and a movable wall 132. The movable wall 132 and the load-bearing wall 131 are arranged sequentially along the radial direction of the annular wall 4 and away from the annular wall 4. The movable wall 132 can move radially along the annular wall 4 to allow two adjacent compartments 12 to be connected or closed.

[0040] Specifically, a guide groove is provided in the load-bearing wall 131, and one end of the movable wall 132 enters the guide groove and can move along the guide groove so that the two adjacent compartments 12 can be connected or closed.

[0041] It should also be noted that when an aircraft enters the parking compartment 1 from inside the annular wall 4, or when an aircraft enters the annular wall 4 from inside the parking compartment 1, the width of the parking compartment 1 near the annular wall 4 can be increased by opening the movable wall 132 to facilitate the passage of the aircraft.

[0042] In this embodiment, a sliding door 42 is provided at the entrance / exit 41 of the annular wall 4, and the sliding door 42 is used to open or close the entrance / exit 41.

[0043] That is, by setting the side sliding door 42, the entrance / exit 41 can be opened or closed for easy use.

[0044] In this embodiment, at least one of the multiple cabins 12 is a waiting cabin, and the remaining cabins 12 are parking cabins, thereby facilitating users to board and disembark in the parking cabins 1.

[0045] In this embodiment, the outer periphery of the parking cabin 1 is provided with a plurality of glass walls 14, and the plurality of glass walls 14 correspond one-to-one with the plurality of cabins 12, so that the situation inside and outside the parking cabin 1 can be viewed through the glass walls 14, thereby improving practicality.

[0046] In this embodiment, a fall protection net 15 is provided on the outer periphery of the top of the parking cabin 1 to improve safety.

[0047] In this embodiment, the parking bay 1 is hexagonal in shape, and six compartments 12 are arranged circumferentially inside the parking bay 1. Thus, when multiple parking bays 1 are provided, multiple parking bays 1 can be easily spliced ​​together, which can also save space.

[0048] In this embodiment, an elevator 6 is provided in the waiting room of the aircraft carrier 1. Specifically, when the aircraft carrier 1 is located on the roof of a building, passengers can reach the waiting room of the aircraft carrier 1 via the elevator 6. It should be noted that when the aircraft carrier 1 is located on the ground, there is no need to provide an elevator 6.

[0049] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and substitutions can be made without departing from the technical principles of the present utility model, and these improvements and substitutions should also be considered within the protection scope of the present utility model.

Claims

1. An aircraft takeoff and landing cabin, characterized in that, The system includes a parking cabin, a lifting platform, a lifting drive mechanism, a ring wall, and a rotation drive mechanism. The ring wall is located at the center of the parking cabin. The rotation drive mechanism drives the ring wall to rotate relative to the parking cabin. The side walls of the ring wall have entrances and exits. The central area of ​​the top of the parking cabin, corresponding to the hollow part of the ring wall, has a passageway. The parking cabin has multiple compartments arranged circumferentially, and these compartments surround the outer perimeter of the ring wall. The lifting platform is horizontally located inside the ring wall, and the lifting drive mechanism drives the lifting platform to move up and down in the height direction.

2. The aircraft takeoff and landing cabin according to claim 1, characterized in that, It also includes a rotating platform and a rotating drive mechanism. The rotating platform is located on the upper part of the lifting platform, and the rotating drive mechanism is located on the lifting platform and is used to drive the rotating platform to rotate relative to the lifting platform.

3. The aircraft takeoff and landing cabin according to claim 1, characterized in that, The lower end of the annular wall is pressed against the bottom wall inside the parking compartment, and the annular wall is rotatably connected to the bottom wall inside the parking compartment. The upper end of the annular wall is supported by the top wall inside the parking compartment, and the annular wall is rotatably connected to the top wall inside the parking compartment.

4. The aircraft landing bay according to claim 1, characterized in that, The aircraft carrier bay is equipped with multiple firewalls, which divide the aircraft carrier bay into multiple compartments.

5. The aircraft landing bay according to claim 4, characterized in that, The firewall includes a load-bearing wall and a movable wall, which are arranged sequentially along the radial direction of the annular wall and away from the annular wall. The movable wall can move radially along the annular wall to allow communication or closure between two adjacent compartments.

6. The aircraft takeoff and landing cabin according to claim 1, characterized in that, The entrance and exit of the ring wall are equipped with sliding doors, which are used to open or close the entrance and exit.

7. The aircraft landing bay according to claim 1, characterized in that, At least one of the multiple cabins is a waiting cabin, and the remaining cabins are parking cabins.

8. The aircraft takeoff and landing cabin according to claim 1, characterized in that, The outer periphery of the parking cabin is provided with multiple glass walls, and each of the multiple glass walls corresponds to one of the multiple cabins.

9. The aircraft landing bay according to claim 1, characterized in that, The outer perimeter of the top of the parking cabin is equipped with a fall protection net.

10. The aircraft takeoff and landing cabin according to claim 1, characterized in that, The parking bay is hexagonal in shape, and six compartments are arranged circumferentially inside the parking bay.

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