Vehicle-mounted vertical take-off and landing aircraft parking apron

Abstract

The utility model discloses a vehicle-mounted vertical take-off and landing aircraft parking apron which comprises a foldable platform, a generator, a platform hinge, a charging gun and a parking apron body, the edge of the outer side of the parking apron body is movably connected with the foldable platform through the platform hinge, and a hydraulic supporting mechanism is further arranged between the foldable platform and the edge of the parking apron body. A generator is arranged below the parking apron, the generator is electrically connected with an arranged charging pile, and a charging gun is arranged on the charging pile; the vehicle-mounted vertical take-off and landing aircraft parking apron has the vehicle-mounted moving effect, meanwhile, a power source or a generator for charging an aircraft is arranged, the position of the take-off and landing platform is not limited any more, high flexibility, applicability and functionality are achieved, the foldable platform is unfolded or folded through the hydraulic supporting mechanism, and the vehicle-mounted vertical take-off and landing aircraft parking apron is convenient to use. And a folding sealing cover effect is formed, the protection effect can be achieved during transportation, and the practicability of the parking apron is further improved.

Description

Technical Field

[0001] This utility model relates to the field of aircraft technology, specifically to a vehicle-mounted vertical take-off and landing aircraft landing pad. Background Technology

[0002] Currently, drones are being used more and more frequently in various fields such as civilian, military, and search and rescue. Drone technology is also constantly being updated and iterated. Long-term hovering will cause insufficient endurance of the aircraft. As the environmental conditions required for application become more and more complex, the requirements for energy saving, endurance and multi-purpose use are constantly increasing, and some small aircraft that can move on the ground and fly in the air have emerged.

[0003] However, in the existing technology, the take-off and landing platforms of aircraft are all in fixed positions, which limits their scope of use and can only be used in a certain location. When performing a mission, it is necessary to constantly observe the flight distance and endurance. When approaching the extreme point, it is necessary to return to the base for resupply before taking off again. This makes it impossible to carry out outdoor operations for a long time, resulting in a reduction in functionality. Utility Model Content

[0004] The purpose of this invention is to provide a vehicle-mounted vertical take-off and landing (VTOL) aircraft landing pad to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a vehicle-mounted vertical take-off and landing (VTOL) aircraft landing pad, comprising a foldable platform, a generator, a platform hinge, a charging gun, and a landing pad. The outer edge of the landing pad is movably connected to the foldable platform via the platform hinge. A hydraulic support mechanism is also provided between the foldable platform and the edge of the landing pad. A generator is provided below the landing pad, and the generator is electrically connected to a charging pile. A charging gun is provided on the charging pile.

[0006] Preferably, a rope is provided on the helipad, the rope is installed on a fixing buckle, and the fixing buckle is fixedly installed on the helipad.

[0007] Preferably, both the generator and the charging pile are installed on the vehicle, and the charging pile is located on one side of the helipad.

[0008] Preferably, the helipad is fixedly mounted on the vehicle.

[0009] Preferably, both ends of the hydraulic support mechanism are movably installed with the foldable platform and the helipad.

[0010] The beneficial effects of this utility model are:

[0011] 1. This vehicle-mounted vertical take-off and landing (VTOL) aircraft helipad places the helipad on a vehicle, forming a platform that can support the parking of VTOL aircraft. It has a vehicle-mounted mobility effect and is equipped with a power source or generator to charge the aircraft. It can not only provide daily supplies but also carry out long-term outdoor operations. The location of the take-off and landing platform is no longer restricted, and it has high flexibility, applicability and functionality.

[0012] 2. The vehicle-mounted vertical takeoff and landing aircraft landing pad uses ropes installed on its surface to lock and secure the aircraft. The foldable platform is designed to unfold or fold using a hydraulic support mechanism, forming a foldable sealed cover that provides protection during transportation, further enhancing the practicality of the landing pad. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of the structure of this utility model;

[0014] Figure 2 This is a diagram showing the effect of folding a single foldable platform structure of this utility model;

[0015] Figure 3 The image shows the folded effect of the entire foldable platform structure of this utility model.

[0016] In the diagram: 1 Foldable platform, 2 Generator, 3 Platform hinge, 4 Charging gun, 5 Helipad, 6 Rope, 7 Fixing buckle, 8 Hydraulic support mechanism, 9 Charging pile. Detailed Implementation

[0017] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0018] Please see Figure 1-3This utility model provides a technical solution: a vehicle-mounted vertical take-off and landing (VTOL) aircraft landing pad, comprising a foldable platform 1, a generator 2, a platform hinge 3, a charging gun 4, and a landing pad 5. The landing pad 5 is fixedly mounted on a vehicle, forming a platform that can support the parking of a VTOL aircraft, and has a vehicle-mounted mobility effect. The outer edge of the landing pad 5 is movably connected to the foldable platform 1 through the platform hinge 3. A hydraulic support mechanism 8 is also provided between the edges of the foldable platform 1 and the landing pad 5. Both ends of the hydraulic support mechanism 8 are movably installed to the foldable platform 1 and the landing pad 5. Through the extension and retraction of the hydraulic support mechanism 8, the foldable platform 1 can be driven to unfold or fold, forming a foldable sealed cover effect on the vehicle, which can play a protective role during transportation.

[0019] Specifically, a generator 2 is installed below the helipad 5. The generator 2 is electrically connected to the charging pile 9. The charging pile 9 is equipped with a charging gun 4. Both the generator 2 and the charging pile 9 are installed on the vehicle, and the charging pile 9 is located on one side of the helipad 5.

[0020] As a preferred option, the vehicle is equipped with a charging pile 9 or a generator 2 to charge the aircraft, which can not only provide daily supplies but also carry out long-term outdoor operations. The location of the take-off and landing platform is no longer restricted, making it highly flexible and adaptable.

[0021] Specifically, a rope 6 is installed on the helipad 5, and the rope 6 is installed on a fixing buckle 7, which is fixedly installed on the helipad 5.

[0022] As a preferred solution, the ropes 6 and fixing buckles 7 are used to lock and secure the aircraft on the apron 5.

[0023] In specific implementation of this utility model: the helipad 5 is installed on the vehicle. At this time, the aircraft is parked on the helipad 5, and the foldable platform 1 is in a folded state. After the vehicle arrives at the work site, when carrying out outdoor operations, the hydraulic support mechanism 8 is extended and retracted (existing technology), and the foldable platform 1 is unfolded, so that the aircraft can take off vertically at any time to perform the mission. When the aircraft is parked and landing, it can be controlled to park at the position of the helipad 5, and the position of the aircraft is fixed by the rope 6. Energy is replenished by the charging gun 4 on the charging pile 9. At the same time, the hydraulic support mechanism 8 can be extended and retracted (existing technology), so that the foldable platform 1 is folded to form a sealed cover effect, and then moved and transported.

[0024] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A vehicle-mounted vertical takeoff and landing (VTOL) aircraft landing pad, comprising a foldable platform (1), a generator (2), a platform hinge (3), a charging gun (4), and a landing pad (5), characterized in that: The outer edge of the helipad (5) is movably connected to the foldable platform (1) via a platform hinge (3). A hydraulic support mechanism (8) is also provided between the foldable platform (1) and the edge of the helipad (5). A generator (2) is provided below the helipad (5). The generator (2) is electrically connected to the charging pile (9). A charging gun (4) is provided on the charging pile (9).

2. The vehicle-mounted vertical takeoff and landing aircraft landing pad according to claim 1, characterized in that: A rope (6) is provided on the helipad (5), and the rope (6) is installed on a fixing buckle (7), which is fixedly installed on the helipad (5).

3. The vehicle-mounted vertical takeoff and landing aircraft landing pad according to claim 1, characterized in that: The generator (2) and the charging pile (9) are both installed on the vehicle, and the charging pile (9) is located on one side of the parking apron (5).

4. The vehicle-mounted vertical takeoff and landing aircraft landing pad according to claim 1, characterized in that: The helipad (5) is fixedly installed on the vehicle.

5. The vehicle-mounted vertical takeoff and landing aircraft landing pad according to claim 1, characterized in that: Both ends of the hydraulic support mechanism (8) are movably installed with the foldable platform (1) and the helipad (5).

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