Unmanned aerial vehicle launch canister device

Abstract

The utility model belongs to the field of unmanned aerial vehicle launch canisters, and particularly relates to an unmanned aerial vehicle launch canister device. The utility model provides an unmanned aerial vehicle launch canister device which comprises an unmanned aerial vehicle launch canister, and the tail end of the launch canister is provided with a first valve capable of being communicated with the outside; the piston is used for boosting the unmanned aerial vehicle to launch in the launch canister and is sealed with the launch canister; and the gas storage tank is communicated with the tail end of the launching cylinder, and a second valve is arranged at the communication part. According to the unmanned aerial vehicle launch canister device, the technical characteristic that the piston and the launch canister are sealed but can slide relatively is utilized, the principle that space gas needs to be exhausted when the space of the launch canister is compressed is ingeniously utilized, and the piston slowly and stably slides to the tail end of the launch canister from an opening of the launch canister; the device can be remotely operated, so that the safety is improved.

Description

TECHNICAL FIELD

[0001] The utility model belongs to unmanned aerial vehicle launching tube field, concretely relates to an unmanned aerial vehicle launching tube device. BACKGROUND

[0002] The unmanned aerial vehicle launching tube adopting pneumatic force is pushed by the expansion force of compressed gas or directly acts on the tail of unmanned aerial vehicle to push it out of the launching tube at high speed.

[0003] The existing unmanned aerial vehicle launching tube adopting pneumatic force has a problem that the piston cannot be slowly lowered from the launching port of the launching tube to the tail end of the launching tube.

[0004] In order to solve this problem, some buffering devices are usually added in the launching tube to achieve the purpose of piston buffering, but this will make the structure of the launching tube and increase the manufacturing cost, and the impact force when launching the unmanned aerial vehicle will also damage the buffering device. UTILITY MODEL CONTENTS

[0005] The unmanned aerial vehicle launching tube device can effectively solve the problems in the background art.

[0006] The unmanned aerial vehicle launching tube device comprises:

[0007] The unmanned aerial vehicle launching tube is provided with a first valve door which can be connected with the outside at the tail end of the launching tube;

[0008] The piston is used for assisting the launching of the unmanned aerial vehicle in the launching tube and is sealed with the launching tube;

[0009] The gas storage tank is connected with the tail end of the launching tube and is provided with a second valve door at the connecting position.

[0010] As a further optimization of the utility model, the gas charging tank which is connected with the gas storage tank and is provided with a third valve door at the connecting position is further included.

[0011] As a further optimization of the utility model, the pipeline which is connected with the gas storage tank at one end and is connected with the gas charging tank at the other end is further included.

[0012] As a further optimization of the utility model, the sealing cavity which connects the tail end of the launching tube with the gas storage tank is further included, and the sealing cavity is provided with a fourth valve door which can be connected with the outside; the second valve door is arranged at the connecting position of the gas storage tank and the sealing cavity.

[0013] As a further optimization of the utility model, the base is further included, and the sealing cavity is arranged in the base; the base is provided with a sealing connection boss which is inserted into the tail end of the launching tube and is connected with the launching tube; the boss is provided with a concave groove in a reverse conical shape corresponding to the piston, and the concave groove is connected with the sealing cavity.

[0014] As a further optimization of the utility model, the control button which is connected with the second valve door is further included.

[0015] As a further optimization of the utility model, the gas tank is filled with high-pressure nitrogen.

[0016] As a further optimization of the utility model, the piston is cylindrical, and the arc surface of the piston is sleeved with not less than two sealing rings.

[0017] As a further optimization of the utility model, the device further comprises a base, the sealing cavity is arranged in the base, the base is provided with a convex platform which is inserted into the tail end of the launching barrel and sealingly connected with the launching barrel, the convex platform is provided with a concave groove in the shape of an inverted cone corresponding to the piston, and the concave groove is communicated with the sealing cavity.

[0018] The utility model provides a launching barrel device of unmanned plane, utilizes the technical features that the piston is sealing but can relatively slide, ingeniously utilizes the principle that the space of launching barrel compresses the space gas to be discharged, makes the piston slowly slide from the opening of the launching barrel to the tail end of the launching barrel slowly and reliably, and the utility model can also be remotely operated, and the safety is improved. BRIEF DESCRIPTION OF DRAWINGS

[0019] Figure 1 It is the shape structure schematic diagram of this embodiment;

[0020] Figure 2 It is Figure 1 It is another perspective view and the structure schematic diagram of the hidden launching barrel;

[0021] Figure 3 Make Figure 1 It is the piston structure schematic diagram in the middle;

[0022] Among them, the launching barrel 1, the piston 2, the sealing ring 2a, the gas tank 3, the inflation tank 4, the pipeline 5, the control button 6, the base 7, the convex platform 7a, the concave groove 7b, the fourth valve 8. SPECIFIC EMBODIMENT

[0023] As Figures 1-3 Indicated, this embodiment includes the launching barrel 1, the piston 2, the gas tank 3 and the inflation tank 4.

[0024] The launching barrel 1 is cylindrical, the launching barrel 1 is erected on the ground at a certain elevation angle, and the launching barrel 1 is used to launch unmanned plane.

[0025] The piston 2 is arranged in the launching barrel 1, the piston 2 is used to hold and boost unmanned plane, and the piston 2 can slide up and down in the launching barrel 1.

[0026] In this embodiment, the piston 2 is cylindrical, the arc surface of the piston 2 is provided with two rings of concave grooves 7b, each ring of concave grooves 7b is sleeved with a sealing ring 2a, and the sealing ring 2a specifically adopts rubber ring.

[0027] The two rubber rings can ensure the stability of the piston 2 sliding in the launching barrel 1, so that the piston 2 will not be tilted and stuck in the launching barrel 1 to cause safety hazards when the piston 2 is suddenly impacted by the gas pressure.

[0028] In other embodiments, the sealing ring 2a can also be provided with three or more rings.

[0029] In other embodiments, the gas storage tank 3 is used to store pressure gas, and in the present embodiment, high-purity nitrogen is used, and in other embodiments, air can also be used.

[0030] In the present embodiment, the gas storage tank 3 is in communication with the tail end of the launching barrel 1, and a second valve is further arranged between the communication channels. When the second valve is opened, the high-pressure nitrogen in the gas storage tank 3 rushes into the tail end of the launching barrel 1 to impact the piston 2, so as to promote the piston 2 to push the unmanned aerial vehicle out of the launching barrel 1.

[0031] Specifically, the present embodiment is provided with a base 7, and a sealing cavity is arranged in the base 7. The tail end of the launching barrel 1 is in communication with the gas storage tank 3 through the sealing cavity, and the second valve is arranged at the communication position of the gas storage tank 3 and the sealing cavity. A fourth valve 8 is arranged on the base 7 and is in communication with the sealing cavity and the outside.

[0032] The fourth valve 8 has at least two functions. Firstly, it can be used to release the pressure of the gas storage tank 3. Secondly, when the unmanned aerial vehicle is loaded, the piston 2 slides from the opening end to the tail end of the launching barrel 1. Since the piston 2 and the launching barrel 1 have good sealing effect, the space from the piston 2 to the tail end of the launching barrel 1 is continuously compressed. The fourth valve 8 can limit the flow of gas when the compression space is compressed, so that the piston 2 can slowly slide to the tail end of the launching barrel 1 at a relatively stable speed.

[0033] In other embodiments, a first valve can be directly arranged at the tail end of the launching barrel 1 to achieve the second function of the fourth valve 8 in the present embodiment.

[0034] The present embodiment further provides a boss 7a on the base 7, which corresponds to the shape of the tail end of the launching barrel 1. The tail end of the launching barrel 1 is sleeved and fixedly sealed on the boss 7a.

[0035] The boss 7a corresponds to the shape of the piston 2 and is provided with a reverse conical groove 7b, which is in communication with the sealing cavity. When the piston 2 falls into the tail end of the launching barrel 1, it is attached to the groove 7b. The groove 7b can improve the explosive force when the gas pressure is released, improve the impact effect, and make the stress surface of the piston 2 more extensive and uniform.

[0036] The gas tank 4 is in communication with the gas storage tank 3, and a third valve is further arranged at the communication position. The third valve is provided with a pressure gauge, so that the pressure of the gas filled into the gas storage tank 3 can be known when the gas tank 4 is filled with gas.

[0037] The gas storage tank 3 is arranged beside the launching tube 1, and the gas charging tank 4 is arranged at a far position, so the pipeline 5 is arranged, one end of the pipeline 5 is communicated with the gas storage tank 3, and the other end of the pipeline 5 is communicated with the gas charging tank 4. In this way, the gas storage tank 3 can be kept at a far distance when being charged.

[0038] Further, the embodiment further comprises a control button 6 connected with the second valve, and remote operation can be realized through the control button 6.

[0039] It should be noted that the up, down, left, right, front, back, top and tail directions described in the present application are all referred to the drawings, and are only used to more clearly express the technical solutions, and do not limit the protection scope.

[0040] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, and not to limit the protection scope of the present application. Although the present application has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solutions of the present application can be modified or replaced equivalently without departing from the essence and scope of the technical solutions of the present application.

Claims

1. An unmanned aerial vehicle launcher apparatus, characterized by, The application relates to a launching device for unmanned aerial vehicles. The launching device comprises a launching cylinder, a first valve at the tail end of the launching cylinder, a piston in the launching cylinder, a gas storage tank connected to the tail end of the launching cylinder, a second valve at the connection between the launching cylinder and the gas storage tank, a gas filling tank connected to the gas storage tank, a third valve at the connection between the gas storage tank and the gas filling tank, a pipeline connected to the gas storage tank and the gas filling tank, a sealing cavity connected to the tail end of the launching cylinder and the gas storage tank, a fourth valve at the connection between the gas storage tank and the sealing cavity, a base, a boss at the tail end of the launching cylinder, a circular conical groove in the boss corresponding to the piston, and a control button connected to the second valve. The gas storage tank is filled with high-pressure nitrogen. The piston is in the shape of a cylinder, and the circular arc surface of the piston is sleeved with not less than two sealing rings.

2. The unmanned aerial vehicle launching tube apparatus of claim 1, wherein, ​ 3. The unmanned aerial vehicle launching tube apparatus of claim 2, wherein, ​ 4. The unmanned aerial vehicle launching tube apparatus of claim 1, wherein, ​ 5. The unmanned aerial vehicle launching tube apparatus of claim 4, wherein, ​ 6. The unmanned aerial vehicle launching tube apparatus of claim 1, wherein, ​ 7. The unmanned aerial vehicle launching tube apparatus of claim 1, wherein, ​ 8. The unmanned aerial vehicle launching tube apparatus of claim 1, wherein, ​

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