CN219172699U - Compressed gas individual soldier transmitting system capable of being combined in modularized mode - Google Patents

Abstract

The utility model relates to a modularized combined compressed gas individual emission system which comprises an emission cylinder base, an emission cylinder top seat and an excitation assembly, wherein the bottom and the top of the emission cylinder are respectively fixed through the emission cylinder base and the emission cylinder top seat, the emission cylinder base and the emission cylinder top seat are modularized assembled structural members, and the excitation assembly is fixedly connected with the emission cylinder base. According to the compressed gas individual firing system, on one hand, the problems that the direction inconsistency of the gun barrel in the existing firing process and the vibration of the gun barrel after firing affect the firing state and the firing precision are solved; on the other hand, the problems of huge structure, insufficient maneuverability and long retransmission preparation time of the existing transmission technology are solved; furthermore, the problem that the existing cluster transmitting technology cannot be assembled in a rapid modularized mode and used by individual soldiers is solved.

Description

Compressed gas individual soldier transmitting system capable of being combined in modularized mode

Technical Field

The utility model relates to the technical field of compressed gas emission, in particular to a compressed gas individual emission system capable of being combined in a modularized manner.

Background

In recent years, along with the maturity of unmanned aerial vehicle related technology, unmanned aerial vehicle has all obtained wide application in each field, especially the development of bee colony technique has had a qualitative promotion to unmanned aerial vehicle application. The transmitting technology is one of key technologies of unmanned aerial vehicles, and directly influences the service performance of unmanned aerial vehicle systems.

The existing unmanned aerial vehicle emission modes have various, but have obvious defects: the runway is required to be fixed during running and taking off; the ejection rack is needed for zero-length emission, and the system is huge and heavy; the rocket boosting and the gas emission have higher requirements on safety and higher cost, and relate to initiating explosive devices, and the emission device needs to be maintained after the rocket boosting and the gas emission; the existing compressed gas emission systems are bulky and have long re-emission preparation time.

At present, most unmanned aerial vehicle cluster transmitting devices transmit in a fixed mode, a transmitting system is fixed by transmitting pipes during production, the quantity of the transmitting pipes cannot be quickly adjusted or detached according to actual conditions during training and use, and mobility is insufficient. In order to meet the requirement of quick disassembly, a scheme with one end fixed is adopted, and the scheme has the problem of insufficient emission precision.

The Chinese patent with application number 201810463627.9 discloses a multi-gun-tube arbitrary combination method and a free combination type multi-tube rocket gun, wherein the gun tube is in a form that one end is fixed and the other end is free, and the emitted vibration can influence the uniformity of the gun tube direction, so that the state and the precision of the next round of emission can be influenced. Meanwhile, the middle gun barrel is small in radial space of the modularized fixing bolt, so that smooth taking out of the bolt is affected.

The 201911148476.9, 201810535872.6, 201920034488.8 and 202020484248.0 patents adopt a fixed mode for clustered emission, and the emission cylinder cannot be detached for individual soldier use. Meanwhile, the gas storage and energy storage module is huge, the flexibility is insufficient, and the energy storage time is long again after the emission. The 201911195689.7 patent adopts the fixed transmission of launching frame, can't carry out modularization equipment and dismantlement individual soldier and use, and the launching frame structure is huge.

Disclosure of Invention

In view of the above, the utility model aims to provide a modularized combined compressed gas individual firing system, which solves the problems that the inconsistency of the gun barrel direction and the gun barrel vibration influence the firing state and the precision in the prior firing process; on the other hand, the problems of huge structure, insufficient maneuverability and long retransmission preparation time of the existing transmission technology are solved; furthermore, the problem that the existing cluster transmitting technology cannot be assembled in a rapid modularized mode and used by individual soldiers is solved.

The utility model solves the problems by the following technical means:

the utility model provides a but compressed gas individual soldier transmitting system of modularization combination, includes transmission section of thick bamboo base, transmission section of thick bamboo footstock and excitation subassembly, transmission section of thick bamboo's bottom and top are fixed through transmission section of thick bamboo base and transmission section of thick bamboo footstock respectively, transmission section of thick bamboo base and transmission section of thick bamboo footstock are the structure that can modularly assemble, excitation subassembly and transmission section of thick bamboo base fixed connection.

Further, the side walls of the transmitting cylinder base and the transmitting cylinder top seat are circumferentially provided with a plurality of spliced lower bosses and a plurality of spliced upper bosses, and the spliced lower bosses and the spliced upper bosses are circumferentially staggered and vertically staggered; when assembling the emission cylinder bases, the assembled lower boss of one emission cylinder base is vertically overlapped with the assembled upper boss of the other emission cylinder base and then locked by a fixing piece; when assembling between the transmitting cylinder top seats, the assembling lower boss of one transmitting cylinder top seat is vertically overlapped with the assembling upper boss of the other transmitting cylinder top seat and then locked by the fixing piece.

Further, the excitation assembly comprises an elbow, a buffer cavity and a cold air generator which are sequentially and fixedly connected, the elbow is fixedly connected with a base of the transmitting cylinder, and an air flow hole communicated with the elbow in a butt joint mode is formed in the transmitting cylinder.

Further, one end of the bent pipe is in threaded connection with the side wall of the transmitting cylinder base, the other end of the bent pipe is in threaded connection with one end of the buffer cavity, and the other end of the buffer cavity is in threaded connection with the cold air generator.

Further, the side wall of the transmitting cylinder base is provided with a threaded hole connected with the bent pipe, and the spliced lower boss and the spliced upper boss are provided with through holes for assembling the fixing parts.

Further, a leg for the launch barrel support is included.

The utility model has the beneficial effects that:

the utility model discloses a modularized combined compressed gas individual emission system which comprises an emission cylinder base, an emission cylinder top seat and an excitation assembly, wherein the bottom and the top of the emission cylinder are respectively fixed through the emission cylinder base and the emission cylinder top seat, the emission cylinder base and the emission cylinder top seat are structural members which can be assembled in a modularized manner, and the excitation assembly is fixedly connected with the emission cylinder base. According to the transmitting system, on one hand, the problems that the existing cluster transmitting technology cannot be quickly assembled in a modularized mode and used by an individual soldier are solved, meanwhile, in a cluster transmitting state, multiple tubes are assembled in a modularized mode, the top and the bottom of a transmitting tube are respectively fixed, vibration of the transmitting tube in the transmitting process is reduced, the direction consistency of the transmitting tube in the transmitting process is ensured, and the influence of the vibration of the transmitting tube on the transmitting precision (state) in the transmitting process is avoided; on the other hand, the integrated excitation assembly is arranged, so that the compactness of the structure is improved, the preparation time for emission is also reduced, and the emission efficiency is improved.

In a word, the application range and the application of the product are expanded due to the adoption of the modularized structure, and the product can be adjusted under different emission environments so as to achieve an emission state, and has higher emission precision; meanwhile, the emission efficiency is improved, the excitation power source can be quickly replaced after the emission is finished, the next round of emission is performed, and the emission preparation time can be saved compared with other schemes; the multi-pipe type solar energy power station can be integrally installed on platforms such as vehicles, ships and planes for transportation or emission under the multi-pipe state, reaches a designated place or an area where the platforms cannot pass, can be quickly disassembled and then is carried by a single soldier to enter an emission array, and the adaptability of products is greatly improved.

Drawings

The utility model is further described below with reference to the drawings and examples.

FIG. 1 is a schematic view of the structure of a single cartridge of the present utility model;

FIG. 2 is a schematic view of a modular assembly of a plurality of launching drums according to the present utility model;

FIG. 3 is a schematic view of a launch canister base or assembled launch canister base;

FIG. 4 is a schematic diagram showing a comparison of different mounting angles of the excitation assembly.

In the figure: 1. a transmitting cylinder top seat; 2. a launch canister; 3. a launch canister base; 4. bending the pipe; 5. a buffer chamber; 6. a cold air generator; 7. a support leg; 8. a threaded hole; 9. a through hole; 10. assembling a lower boss; 11. and assembling a boss.

Detailed Description

The utility model is further described in detail below by means of the figures and examples. The features and advantages of the present utility model will become more apparent from the description. It will be apparent that the described embodiments are only some, but not all, embodiments of the utility model.

In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", "head", "tail", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.

Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present utility model, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.

As shown in fig. 1 to 4, the embodiment of the utility model discloses a modularized combined compressed gas individual emission system, which comprises an emission cylinder base 3, an emission cylinder 2, an emission cylinder top seat 1, an excitation component and a supporting leg 7 for supporting the emission cylinder, wherein the bottom and the top of the emission cylinder 2 are respectively fixed through the emission cylinder base 3 and the emission cylinder top seat 1, and the emission cylinder base 3, the emission cylinder 2 and the emission cylinder top seat 1 are connected through threads or are integrally formed.

The transmitting cylinder base and the transmitting cylinder top seat are structural members which can be assembled in a modularized mode, specifically, the side walls of the transmitting cylinder base 3 and the transmitting cylinder top seat 2 are circumferentially provided with a plurality of assembled lower bosses 10 and a plurality of assembled upper bosses 11, and the assembled lower bosses 10 and the assembled upper bosses 11 are circumferentially staggered and vertically staggered; when assembling the emission cylinder bases, the assembled lower boss of one emission cylinder base is vertically overlapped with the assembled upper boss of the other emission cylinder base and then locked by a fixing piece; when assembling between the transmission cylinder footstock, the boss is locked through the mounting after the boss is vertically coincide down in the assembling of a transmission cylinder footstock and the assembling of another transmission cylinder footstock, the through-hole 9 that is used for the mounting assembly has all been seted up to the boss under assembling and the boss is gone up in the assembling, the mounting can be the bolt spare.

By adopting the structural design, the problem that the conventional cluster emission technology cannot be assembled in a rapid modularized manner and used by an individual soldier is solved, meanwhile, in the cluster emission state, multiple tubes are assembled in a modularized manner, the top and the bottom of the emission tube are respectively fixed, the vibration of the emission tube in the emission process is reduced, the uniformity of the direction of the emission tube in the emission process is ensured, and the influence of the vibration of the emission tube on the emission precision (state) in the emission process is avoided.

The excitation assembly is fixedly connected with the emission tube base, specifically, the excitation assembly comprises an elbow 4, a buffer cavity 5 and a cold air generator 6 which are sequentially and fixedly connected, the elbow is fixedly connected with the emission tube base, and an air flow hole which is in butt joint communication with the elbow 4 is formed in the emission tube 2. In this embodiment, the one end of return bend and the lateral wall threaded connection of transmission section of thick bamboo base, the other end and the one end threaded connection of buffer chamber of return bend, the other end and the air conditioning generator threaded connection of buffer chamber, the screw hole 8 of being connected with the return bend is seted up to the lateral wall of transmission section of thick bamboo base. In the practical application process, a plurality of screw holes can be circumferentially arranged at intervals, so that the bent pipe is conveniently connected with the base of the transmitting cylinder from different directions, and the screw holes are closed in a non-connection state.

The buffer cavity 5 and the cold air generator 6 can be matched with different specifications according to the emission requirements, the bent pipe 4, the buffer cavity 5 and the cold air generator 6 are connected through threads, the state can be adjusted according to different use scenes (as shown in fig. 4, the emission cylinders can be arranged at any angle relatively), and the emission requirements of different (individual soldiers, clusters and different emission sites) are met. The cold air generator 6 is pre-filled with corresponding pressure gas according to unmanned aerial vehicle demands, and is matched with the corresponding buffer cavity 5, and the cold air generator 6 only needs to be replaced quickly during re-emission. Unmanned aerial vehicle with different requirements can be launched, and the whole buffer cavity 5 and the cold air generator 6 can be replaced to quickly adapt to the launching requirements.

Finally, it is noted that the above embodiments are only for illustrating the technical solution of the present utility model and not for limiting the same, and although the present utility model has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications and equivalents may be made thereto without departing from the spirit and scope of the technical solution of the present utility model, which is intended to be covered by the scope of the claims of the present utility model.

Claims (6)

1. A compressed gas individual soldier's transmitting system that can modularization combination, its characterized in that: the device comprises a transmitting cylinder base, a transmitting cylinder top seat and an excitation assembly, wherein the bottom and the top of the transmitting cylinder are respectively fixed through the transmitting cylinder base and the transmitting cylinder top seat, the transmitting cylinder base and the transmitting cylinder top seat are structural members which can be assembled in a modularized mode, and the excitation assembly is fixedly connected with the transmitting cylinder base.

2. The modularly combinable compressed gas individual soldier emission system of claim 1, wherein: the side walls of the transmitting cylinder base and the transmitting cylinder top seat are circumferentially provided with a plurality of spliced lower bosses and a plurality of spliced upper bosses, and the spliced lower bosses and the spliced upper bosses are circumferentially staggered and vertically staggered; when assembling the emission cylinder bases, the assembled lower boss of one emission cylinder base is vertically overlapped with the assembled upper boss of the other emission cylinder base and then locked by a fixing piece; when assembling between the transmitting cylinder top seats, the assembling lower boss of one transmitting cylinder top seat is vertically overlapped with the assembling upper boss of the other transmitting cylinder top seat and then locked by the fixing piece.

3. The modularly combinable compressed gas individual soldier emission system of claim 2, wherein: the excitation assembly comprises an elbow, a buffer cavity and a cold air generator which are sequentially and fixedly connected, the elbow is fixedly connected with a base of the emission cylinder, and an air flow hole communicated with the elbow in a butt joint mode is formed in the emission cylinder.

4. A modularly combinable compressed gas individual soldier emission system according to claim 3, characterized in that: one end of the bent pipe is in threaded connection with the side wall of the transmitting cylinder base, the other end of the bent pipe is in threaded connection with one end of the buffer cavity, and the other end of the buffer cavity is in threaded connection with the cold air generator.

5. The modularly combinable compressed gas individual soldier emission system of claim 4, wherein: the side wall of the transmitting cylinder base is provided with a threaded hole connected with the bent pipe, and the spliced lower boss and the spliced upper boss are respectively provided with a through hole for assembling the fixing piece.

6. The modularly combinable compressed gas individual soldier emission system according to any of the claims 1-5, characterized in that: and further comprises a leg for the launch canister support.

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