Container type unmanned aerial vehicle storage, transportation, launch and control integrated device

Abstract

The utility model relates to a container type unmanned aerial vehicle storage, transportation, launch and control integrated device. Comprising a container storage and transportation platform, telescopic supporting legs arranged at the four corners of the container storage and transportation platform, a universal tilting launching platform arranged in the container storage and transportation platform and a liquid-gas phase change launching system arranged on the universal tilting launching platform. The container type unmanned aerial vehicle storage, transportation, launch and control integrated device has the advantages of being convenient to transport and store, low in launch and maintenance cost, convenient to observe and overhaul, free of high-temperature ablation, high in generalization degree, self-adaptive in site and large in launch angle.

Description

TECHNICAL FIELD

[0001] The utility model belongs to unmanned plane technical field, concretely relates to a container formula unmanned plane storage and transportation launch control integration device. BACKGROUND

[0002] As an important aircraft, unmanned plane is widely used in military, civil and commercial fields because of its flexibility and multifunctionality. Especially with the development of bee colony technology, the advantage of unmanned plane bee colony is far greater than the simple superposition of single machine capacity. However, the transportation and launch of unmanned plane have been an important factor restricting its application. In the field of automatic control technology, how to realize the automatic transportation, launch and control of unmanned plane is a hot issue of current research. In the field of container transportation technology, how to use container to realize the safe, efficient transportation and rapid deployment of unmanned plane is a problem to be solved urgently.

[0003] The existing unmanned plane transportation and launch mode mainly adopts the fixed container platform mode, which transports the container unmanned plane to the designated launch site meeting the requirements, and then launches manually. These modes have some problems, such as high launch site requirements, rocket boosting mode in the container, high temperature ablation in the box, influence on other unmanned planes not launched, fixed launch angle cannot be used for multiple models, high launch cost, inconvenient observation and maintenance in the container, small launch angle in the container, etc. UTILITY MODEL CONTENTS

[0004] Therefore, the utility model aims at providing a container formula unmanned plane storage and transportation launch control integration device which is convenient to transport and store, low in launch and maintenance cost, convenient to observe and maintain, free from high temperature ablation, high in generalization degree, adaptive to site, and large in launch angle.

[0005] The utility model solves the above problems through the following technical means:

[0006] A container formula unmanned plane storage and transportation launch control integration device, which comprises a container storage and transportation platform, telescopic legs arranged at four corners of the container storage and transportation platform, a universal tilting launch platform arranged in the container storage and transportation platform, and a liquid-gas phase change launch system arranged on the universal tilting launch platform.

[0007] Further, the container storage and transportation platform comprises two European wing doors and two opposing doors, and the European wing doors are opened and closed by a first telescopic cylinder.

[0008] Further, the universal tilting launch platform comprises a plurality of overturning supports, and the overturning supports are overturned by a second telescopic cylinder.

[0009] Further, the liquid-gas phase change launch system comprises an ejection device and an unmanned plane trolley device moved by the ejection device.

[0010] Further, the long side direction of the container storage and transportation platform is a European wing door.

[0011] Further, the short side direction of the container storage and transportation platform is a double-leaf door.

[0012] The beneficial effects of the present application are as follows:

[0013] 1. Improve transportation efficiency: the container storage and transportation platform of the present application is provided with telescopic legs at four corners, which can be automatically loaded and unloaded without external hoisting equipment, and can be transported by various modes such as ship, automobile, truck and air transport, and quickly deployed. This transportation mode greatly improves the transportation efficiency of the unmanned aerial vehicle and meets the requirement of quick deployment.

[0014] 2. Reduce maintenance cost: due to the container design, the unmanned aerial vehicle is maintained, inspected and transported quickly, the maintenance time is shortened, the outer packaging and maintenance cost are reduced, the protective property of the container shell is stronger, and the service life of the unmanned aerial vehicle is prolonged.

[0015] 3. Enhance concealment: the container storage and transportation design makes the unmanned aerial vehicle have good concealment during transportation and is not easy to be detected and attacked.

[0016] 4. Strong adaptability: the container long side front and rear vertical surfaces can be expanded by one key up and down, and the left and right vertical surfaces are opened left and right by a double-leaf door, which is convenient for inspection and maintenance and observation during launching, and at the same time, the angle of the launching window is greatly improved, and more different models can be used. The unmanned aerial vehicles in the container are arranged in multiple layers, and the launching angle of each layer of bottom plate can be adjusted according to the requirement to meet the launching requirement of different unmanned aerial vehicles. The unmanned aerial vehicle is constrained by a pulley during transportation in the container to prevent the unmanned aerial vehicle from moving or falling during transportation. When launching, the pulley is unlocked by one key to enter the state of waiting for launching. This design realizes the automatic control of the unmanned aerial vehicle, reduces the manual operation, and reduces the operation difficulty and risk. BRIEF DESCRIPTION OF DRAWINGS

[0017] The present application will be further described in conjunction with the drawings and examples.

[0018] Fig. 1 The structure of the preferred embodiment of the present application is shown in the figure;

[0019] Fig. 2 The schematic diagram of the liquid-gas phase change launching system is shown in the figure. DETAILED DESCRIPTION

[0020] The present application will be further described in conjunction with the drawings and examples. Through these descriptions, the characteristics and advantages of the present application will become more clear and explicit. Obviously, the described examples are only a part of the examples of the present application, but not all the examples.

[0021] In the description of the utility model, it is understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", "head", "tail" is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the utility model and simplifying the description, and therefore cannot be understood as limiting the utility model.

[0022] In addition, the terms "first" and "second" are only for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined with "first" and "second" can explicitly or implicitly include one or more features. In the description of the utility model, the meaning of "multiple" is two or more, unless otherwise specifically limited.

[0023] As shown in Figs. 1-2 The utility model discloses a container formula unmanned plane storage and transport launch control integration device, including container storage and transport platform 1, set up telescopic support leg 2 of container storage and transport platform four corners, set up generalization tilting launch platform 3 in container storage and transport platform and set up liquid gas phase change launch system 4 on generalization tilting launch platform.

[0024] The container storage and transport platform includes two European wing doors 11 and two opposite doors 13, the European wing door is hinged with the top of the container storage and transport platform, and the European wing door is opened and closed by the first telescopic cylinder 12. In the embodiment, the long side direction of the container storage and transport platform is the European wing door, and the short side direction of the container storage and transport platform is the opposite door. Based on the combined design of the European wing door and the opposite door, the unmanned aerial vehicle launch end can be maximally guaranteed without obstacles, the launch angle can be increased, the launch angle space can be improved, the high temperature in the container can be reduced, and observation and maintenance are facilitated.

[0025] By setting the telescopic support leg, the container storage and transport platform can be raised as a whole, the bottom part is convenient for the transport vehicle to enter, the system can be quickly and mobile transferred, and when launching in the wild field such as slope, the container storage and transport platform can be leveled to reduce the dependence on the environment of the launch site.

[0026] The universal tilting launch platform 3 comprises a plurality of layers of tilting supports 31 hinged to the main support of the universal tilting launch platform, the tilting supports are pushed to tilt by the second telescopic cylinders 32, and the liquid-gas phase change launch system 4 is arranged on the tilting supports.

[0027] The liquid-gas phase change launch system 4 comprises a launching device 41 and a UAV trolley device 42 pushed to move by the launching device, wherein the launching device is of an open cylinder type structure, can realize the starting of the UAV in the container, and low-temperature launching.

[0028] The power source of the telescopic legs can be electric drive, hydraulic drive, pneumatic drive, etc.

[0029] The power source of the first telescopic cylinder and the second telescopic cylinder is also applicable to hydraulic drive, pneumatic drive, etc.

[0030] Finally, it should be pointed out that the above embodiments are only used to illustrate the technical solutions of the present application but not limit the present application, although the present application has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present application can be modified or replaced equivalently without departing from the purpose and scope of the technical solutions of the present application, and all of them should be covered in the scope of the claims of the present application.

Claims

1. A containerized unmanned aerial vehicle (UAV) storage, transportation, launch, and control integrated device, characterized in that: It includes a container storage and transportation platform, telescopic outriggers installed at the four corners of the container storage and transportation platform, a universal tilting launch platform installed inside the container storage and transportation platform, and a liquid-gas phase change launch system installed on the universal tilting launch platform.

2. The containerized UAV storage, transportation, launch, and control integrated device according to claim 1, characterized in that: The container storage and transportation platform includes two gull-wing doors and two double doors, which are opened and closed by a first telescopic cylinder.

3. The containerized UAV storage, transportation, launch, and control integrated device according to claim 2, characterized in that: The universal tilting launch platform includes a multi-layered tilting support, which is tilted by a second telescopic cylinder.

4. The containerized UAV storage, transportation, launch, and control integrated device according to claim 3, characterized in that: The liquid-gas phase change launch system includes a catapult and a drone trolley mechanism that is propelled by the catapult.

5. The containerized UAV storage, transportation, launch, and control integrated device according to claim 4, characterized in that: The long side of the container storage and transportation platform is a gull-wing door.

6. The containerized UAV storage, transportation, launch, and control integrated device according to claim 5, characterized in that: The container storage and transportation platform has double doors on its shorter side.

Images