CN210101997U

CN210101997U - Standard ammunition throwing device for unmanned aerial vehicle

Info

Publication number: CN210101997U
Application number: CN201920694775.1U
Authority: CN
Inventors: 胡上杰; 王凯; 王六灵; 赵惠芳
Original assignee: Taizhou Public Security Bureau; Zhejiang Linhang Intelligent Technology Co Ltd
Current assignee: Taizhou Public Security Bureau; Zhejiang Linhang Intelligent Technology Co Ltd
Priority date: 2019-05-15
Filing date: 2019-05-15
Publication date: 2020-02-21
Anticipated expiration: 2029-05-15

Abstract

The utility model discloses a device is put in to standard ammunition for unmanned aerial vehicle, including unmanned aerial vehicle microscope carrier and year bullet device, carry the bullet device including carrying the bullet organism, being located a plurality of barrel in the year bullet organism with be used for putting in the device of throwing of standard ammunition in the barrel, be equipped with on the barrel and throw the bullet window, it includes a plurality of the control unit that throws the bullet to throw the bullet device, it includes steering wheel body and spacing block tongue to throw the bullet control unit, the steering wheel body is used for driving spacing block tongue stretches into or stretches out throw in the bullet window to the realization is to being located the loading restriction or the input of standard ammunition in the barrel. The utility model adopts the independent projectile throwing control structure of a single gun barrel through the optimized design, thereby improving the convenience and effectiveness of projectile throwing and realizing the single or multi-projectile throwing at one time; in addition, the bullet loading machine body is optimized, the loading stability of standard ammunition is improved, the external interference on the standard ammunition is reduced, and the subsequent secondary loading is facilitated.

Description

Standard ammunition throwing device for unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle loads technical field, in particular to device is put in to standard ammunition for unmanned aerial vehicle.

Background

At present, set up in unmanned aerial vehicle's below and put in the device and be used for putting in article, for example can be used for the area air-drop goods and materials that arrive to the inconvenient arrival of ground traffic, but the device of putting in that appears at present generally can only be used for the general goods and materials of air-drop, and this kind of device structure of putting in moreover is complicated, and the fault rate is than higher.

In some special fields, such as military field, fire field, police service field or criminal investigation field, an unmanned aerial vehicle is required to perform a projectile throwing task, and different types of ammunition are usually thrown according to different task targets, wherein the types of ammunition can be used for throwing gas ammunition, fire extinguishing ammunition, smoke bomb, signal bomb and the like.

For example, publication number CN206601073U discloses a cartridge and a cartridge chamber and a fire control unmanned aerial vehicle applying the cartridge. The ammunition barrel comprises a barrel body and a bullet throwing mechanism arranged at the lower end of the barrel body, wherein the bullet throwing mechanism comprises a connecting barrel, a cover plate, a folding connecting piece and a bullet throwing switch, the connecting barrel is connected with the lower end of the barrel body, the folding connecting piece and the bullet throwing switch are respectively arranged on the barrel wall of the lower end of the connecting barrel, the cover plate is connected with the folding connecting piece, and the bullet throwing switch controls ammunition in the ammunition barrel to throw. However, in the above structure, the standard ammunition is usually hung in an exposed manner, so that the ammunition is easily interfered by the external environment; and the bullet throwing mechanism is complex in linkage, the problem of bullet blocking is easy to occur, and the subsequent secondary loading of standard ammunition is complex, so that the use is influenced.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a device is put in to standard ammunition for unmanned aerial vehicle for solve above-mentioned technical problem, have that the bullet is swiftly convenient, load convenient, ammunition put in and stabilize effectual characteristics.

The utility model provides a technical problem can adopt following technical scheme to realize:

the bomb carrying device comprises a bomb carrying body, a plurality of barrels and a bomb projecting device, the barrels are located in the bomb carrying body, the bomb projecting device is used for projecting standard ammunition in the barrels, a bomb projecting window is arranged on each barrel, the bomb projecting device comprises a plurality of bomb projecting control units, each bomb projecting control unit comprises a steering engine body and a limiting clamping tongue, the steering engine body is used for driving the limiting clamping tongues to extend into or out of the bomb projecting window, and loading limitation or projection of the standard ammunition located in the barrels is achieved.

The gun barrel comprises a gun barrel body and a compression spring positioned in an inner cavity of the gun barrel body, the gun barrel body is of a tubular structure with two through ends, the compression spring is attached to the wall of the inner cavity of the gun barrel body and can be compressed upwards along the wall of the inner cavity of the gun barrel body, the upper part of the standard ammunition abuts against the lower part of the compression spring, and when the standard ammunition is loaded in the gun barrel body, the compression spring is in a compression state.

The projectile throwing device further comprises a controller and a power supply, the power supply is used for supplying power to the controller and the steering engine body, and the controller is used for controlling the steering engine body to realize rotary driving, so that rotary driving of the limiting clamping tongue is realized.

The single projectile control unit is used for correspondingly matching the single barrel.

The device comprises a bomb carrying machine body and is characterized in that a top plate is arranged on the upper portion of the bomb carrying machine body, a plurality of first gun barrel through cavities are formed in the top plate, a carrier mounting frame and at least one bollard are arranged on the top plate, the upper portion of the carrier mounting frame is used for being installed in a matched mode with an unmanned aerial vehicle carrier, the bollard is used for being connected with a trigger line of standard ammunition, a gun barrel mounting groove is formed in the bottom of the top plate, and the upper end of the gun barrel is correspondingly installed.

The bomb carrying machine body is further internally provided with an objective table which is used for being installed in a matched mode with the bomb projecting device, and the objective table is provided with a plurality of second gun barrel through cavities.

The outer side of the bomb carrying machine body is provided with a shell, and the shell is used for completely or partially covering the outer sides of the plurality of gun barrels.

When the compression spring is in a compressed state, the horizontal plane of the bottom end part of the compression spring is higher than the horizontal plane of the projectile shooting window.

When the compression spring is in a compressed state, the upper end of the compression spring is abutted against the bottom surface of the top plate.

The single mooring bollard is used for mooring 1-4 standard ammunitions.

Compared with the prior art, the utility model have following outstanding advantage and effect: the utility model adopts the independent projectile throwing control structure of a single gun barrel through the optimized design, thereby improving the convenience and effectiveness of projectile throwing and realizing the single or multi-projectile throwing at one time; in addition, the bullet loading machine body is optimized, the loading stability of standard ammunition is improved, the external interference on the standard ammunition is reduced, and the subsequent secondary loading is facilitated.

The features of the present invention will be apparent from the accompanying drawings and from the detailed description of the preferred embodiments which follows.

Drawings

Fig. 1 is a schematic view of an overall installation structure of the present invention;

FIG. 2 is a schematic view of the overall installation structure of the present invention;

FIG. 3 is a first schematic view of the mounting structure of the bullet-loading device of the present invention;

fig. 4 is a second schematic view of the mounting structure of the bullet-loading device of the present invention;

fig. 5 is a third schematic view of the mounting structure of the bullet-loading device of the present invention;

FIG. 6 is a schematic view of the structure of the bullet-projecting window and the limit latch of the present invention;

fig. 7 is a schematic overall sectional structure diagram of the present invention;

fig. 8 is a schematic structural view of a second projectile firing control unit of the present invention;

fig. 9 is a schematic structural view of the barrel body of the present invention;

fig. 10 is a schematic sectional structural view of the barrel body of the present invention;

fig. 11 is a schematic structural diagram of standard ammunition of the present invention;

wherein, 1, a bullet loading device; 11. a cartridge carrier body; 111. a top plate; 1111. mooring bollards; 1112. a stage mounting frame; 1113. a first barrel is communicated with the cavity; 1114. a gun barrel mounting groove; 112. a housing; 113. an object stage; 1131. a second barrel is communicated with the cavity; 12. a barrel; 121. shooting windows; 122. a barrel body; 123. a compression spring; 13. a projectile throwing device; 131. a projectile feeding control unit; 1311. a limiting clamping tongue; 1312. a steering engine body; 132. a controller; 133. a power source; 2. an unmanned aerial vehicle carrying platform; 3. preparing ammunition; 31. triggering a line; 32. and (7) clamping the table.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand and understand, the present invention is further explained by combining with the specific drawings.

It should be noted that all directional indicators (such as up, down, left, right, front, and back) in the embodiments of the present invention are only used to explain the relative position relationship between the components, the motion situation, and the like in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indicator is changed accordingly. In addition, the descriptions related to "first", "second", etc. in the present invention are for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicit ly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature.

As shown in fig. 1 to 11, a system ammunition throwing device for an unmanned aerial vehicle comprises an unmanned aerial vehicle carrying platform 2 and an ammunition carrying device 1, wherein the ammunition carrying device 1 comprises an ammunition carrying body 11, a plurality of barrels 12 positioned in the ammunition carrying body 1 and a throwing device 13 used for throwing system ammunition 3 in the barrels 12, an ammunition throwing window 121 is arranged on each barrel 12, the throwing device 13 comprises a plurality of throwing control units 131, each throwing control unit 131 comprises a steering engine body 1312 and a limiting clamping tongue 1311, the steering engine body 1312 is used for driving the limiting clamping tongue 1311 to extend into or out of the ammunition throwing window 12, and loading limitation or throwing of the system ammunition 3 positioned in the barrels 12 is realized.

Unmanned aerial vehicle microscope carrier 2 is used for hanging in unmanned aerial vehicle bottom, makes things convenient for unmanned aerial vehicle to carry, and there is certain difference in the unmanned aerial vehicle model of specific carry structural design foundation difference, and carries structural design and belongs to common design among the prior art, consequently no longer detailed description in this scheme.

The ammunition carrying device 1 is used for carrying standard ammunition and mainly comprises an ammunition carrying body 11, gun barrels 12 and an ammunition throwing device 13, wherein the ammunition carrying body 11 is of a main body framework structure, so that the fixed installation of the gun barrels 12 is facilitated, in addition, the ammunition carrying body is also conveniently matched with an unmanned aerial vehicle carrying platform 2 for installation, and meanwhile, the assembly and installation of the ammunition throwing device 13 are also facilitated; the gun barrel 12 is used for loading standard ammunition 3, the specific shape structure of the gun barrel 12 is preferably matched with the specific standard ammunition generally, the conventional selection is a cylindrical structure design, the number of the gun barrel 12 can be set to be 4 barrels, 8 barrels, 12 barrels, 16 barrels, 9 barrels and the like according to requirements, the shape of the gun barrel body 122 can be in different specifications such as a circle, a square and a polygon, the preferred gun barrel 12 is provided with a shooting window 121, and the shooting window 121 is matched with a shooting device 13 conveniently, so that the standard ammunition 3 in the gun barrel 12 can be limited in a clamping mode conveniently; the projectile throwing device 13 comprises a plurality of projectile throwing control units 131, preferably one-to-one matching is adopted, namely, a single projectile throwing control unit 131 is used for correspondingly matching a single barrel 12, but the design is not limited to the matching design, a steering engine body 1312 with a double-station driving structure can be selected, and the single steering engine body 1312 can control two limiting clamping tongues 1311, so that the single projectile throwing control unit 131 can synchronously or asynchronously control two barrels 12; the steering engine body 1312 preferably adopts a digital steering engine or an analog steering engine commonly used in the prior art, and the model of the steering engine body can be JX PDI-6221MG, but is not limited to the above.

In the above structure, the projectile principle of the standard ammunition 3 is as follows: when unmanned aerial vehicle microscope carrier 2 is mounted on an unmanned aerial vehicle, the unmanned aerial vehicle is controlled to fly through an unmanned aerial vehicle controller, when the unmanned aerial vehicle flies to a target area and the putting of standard ammunition needs to be completed, the unmanned aerial vehicle controller is utilized to remotely control the steering engine body 1312 to rotate, or the steering engine body 1312 is controlled in a timing control mode, the specific control mode can refer to the control mode for the steering engine in the prior art, after the steering engine body 1312 receives a signal, the driving is completed, and therefore the limiting clamping tongue 1311 is driven to extend outwards from the shooting window 121 of the gun barrel 12, the limitation on the standard ammunition 3 in the gun barrel 12 is contacted, and the putting of the standard ammunition is completed.

Preferably, in the present embodiment, the barrel 12 includes a barrel body 122 and a compression spring 123 located in an inner cavity of the barrel body 122, the barrel body 122 is a tubular structure with two through ends, the compression spring 123 is attached to the inner cavity wall of the barrel body 122 and can be compressed upwards along the inner cavity wall of the barrel body 122, the upper portion of the system ammunition 3 abuts against the lower portion of the compression spring 123, the system ammunition 3 is preferably provided with a catch 32 conveniently engaged with the limiting catch 1311, the catch 32 can also be used for abutting against the compression spring 123, and when the system ammunition 3 is loaded in the barrel body 122, the compression spring 123 is in a compressed state; when the compression spring 123 is in a compressed state, the horizontal plane of the bottom end part of the compression spring 123 is higher than the horizontal plane of the projectile launching window 121, so that the limiting clamping tongue 1311 can conveniently extend in or out; preferably, a compression spring 123 structure is arranged in the gun barrel 12, when the gun barrel body 122 needs to load the standard ammunition 3, the upper part of the standard ammunition 3 abuts against the lower part of the compression spring 123, the compression spring 123 is pressed into the upper end of the gun barrel body 122, so that the compression spring 123 is always in a stressed state, when the clamping table 32 of the standard ammunition 3 is slightly higher than the projectile launching window 121, the limit clamping tongue 1311 is extended into the projectile launching window 121 by controlling the steering engine body 1312, so that the limit clamping tongue 1311 limits and clamps the standard ammunition 3, and the loading of the standard ammunition 3 is completed; in addition, this structure utilizes compression spring 121's restoring force, can provide a driving force when system ammunition 3 is put in, can avoid system ammunition 3 to appear the card bullet phenomenon, improves the stability and the validity of throwing.

Preferably, in this embodiment, the projectile shooting device 13 further includes a controller 132 and a power source 133, the power source 133 is used to supply power to the controller 132 and the steering engine body 1312, and the controller 132 is used to control the steering engine body 1312 to realize rotational driving, so as to realize rotational driving of the limit latch 1311; the controller 132 can control the plurality of projectile control units 131 in a centralized manner, or can control one projectile control unit 131 for the independent controller 132 singly, the design can be diversified and matched according to requirements, the controller 132 and the power supply 133 both adopt accessories matched with a specific steering engine body 1312, the purpose is to realize the control of the steering engine body 1312, the controller 132 adopts a control circuit board commonly used in the prior art, a single chip microcomputer, a wireless signal receiver and the like are arranged in the controller, signal receiving is realized, remote control of the steering engine body 1312 is realized, specific control circuits and control programs can be realized through the prior art means, and circuit control of the steering engine body does not belong to the technical innovation point of the embodiment, and detailed explanation is omitted.

Preferably, in this embodiment, a top plate 111 is arranged at the upper part of the projectile carrier 11, a plurality of first barrel through cavities 1113 are arranged on the top plate 111, a carrier mounting rack 1112 and at least one bollard 1111 are arranged on the top plate 111, the carrier mounting rack 1112 is used for being mounted in cooperation with an unmanned aerial vehicle carrier 2, the bollard 1111 is used for being connected with a trigger line 31 of standard ammunition 3, a barrel mounting groove 1114 is arranged at the bottom of the top plate 111, and the upper end of the barrel 12 is correspondingly mounted with the barrel mounting groove 1114; the single mooring bollard 1111 is used for mooring 1-4 standard ammunition 3, and the preferred single mooring bollard 1111 is usually matched with 2 standard ammunition 3; when the compression spring 123 is in a compressed state, the upper end of the compression spring 123 abuts against the bottom surface of the top plate 111; the minimum caliber of the first barrel through cavity 1113 is smaller than the minimum caliber of the upper end of the standard ammunition 3, so that the standard ammunition 3 is prevented from being exposed, and the trigger line 31 of the standard ammunition 3 is conveniently connected with the mooring bollard 1111 by utilizing the cavity structure of the first barrel through cavity 1113; the barrel mounting groove 1114 is preferably an annular blind groove structure, the bottom surface of the barrel mounting groove is an open surface, the butt joint with the barrel body 122 is facilitated, and meanwhile, the upper end of the compression spring 123 can be abutted and fixed, which is equivalent to an upper spring seat of the compression spring 123.

Preferably, in the embodiment, an object stage 113 is further disposed in the projectile carrier 11, the object stage 113 is used to cooperatively mount the projectile device 13, a plurality of second barrel through cavities 1131 are disposed on the object stage 113, generally, the object stage 113 is horizontally disposed, is located at the lower portion of the top plate 111, and is spaced from the top plate 111, so as to form a cavity for assembling the projectile device 13, and the object stage 113 is preferably divided into an upper object stage and a lower object stage; usually, the upper objective table is used for placing the steering engine body, and the lower objective table is used for correspondingly placing the controller and the power supply, and of course, the controller can also be placed on the upper objective table.

Preferably, in the embodiment, the outer side of the projectile carrier 11 is provided with a casing 112, the casing 112 is used to wholly or partially cover the outer sides of the plurality of barrels 12, and the casing 112 is used to form outer side covering protection, so that a relatively sealed structure is formed inside, and interference of an external environment to internal components can be reduced.

The utility model adopts the independent projectile throwing control structure of a single gun barrel through the optimized design, thereby improving the convenience and effectiveness of projectile throwing and realizing the single or multi-projectile throwing at one time; in addition, the bullet loading machine body is optimized, the loading stability of standard ammunition is improved, the external interference on the standard ammunition is reduced, and the subsequent secondary loading is facilitated.

It will be appreciated by those skilled in the art that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The embodiments disclosed above are therefore to be considered in all respects as illustrative and not restrictive. All changes which come within the scope of the invention or which are equivalent to the scope of the invention are embraced by the invention.

Claims

1. The utility model provides a device is put in to standard ammunition for unmanned aerial vehicle, includes unmanned aerial vehicle microscope carrier (2) and year bullet device (1), its characterized in that: the bomb carrying device (1) comprises a bomb carrying body (11), a plurality of gun barrels (12) located in the bomb carrying body (11) and a bomb projecting device (13) used for projecting standard ammunition (3) in the gun barrels (12), wherein bomb projecting windows (121) are formed in the gun barrels (12), the bomb projecting device (13) comprises a plurality of bomb projecting control units (131), each bomb projecting control unit (131) comprises a steering engine body (1312) and a limiting clamping tongue (1311), the steering engine body (1312) is used for driving the limiting clamping tongues (1311) to stretch into or out of the bomb projecting windows (121), and loading limitation or projection of the standard ammunition (3) located in the gun barrels (12) is achieved.

2. A system ammunition dispensing device for unmanned aerial vehicles according to claim 1, wherein: the gun barrel (12) comprises a gun barrel body (122) and a compression spring (123) located in an inner cavity of the gun barrel body (122), the gun barrel body (122) is of a tubular structure with two through ends, the compression spring (123) is attached to the wall of the inner cavity of the gun barrel body (122) and can be compressed upwards along the wall of the inner cavity of the gun barrel body (122), the upper part of the system ammunition (3) abuts against the lower part of the compression spring (123), and when the system ammunition (3) is loaded in the gun barrel body (122), the compression spring (123) is in a compression state.

3. A system ammunition dispensing device for unmanned aerial vehicles according to claim 1, wherein: the projectile throwing device (13) further comprises a controller (132) and a power source (133), the power source (133) is used for supplying power to the controller (132) and the steering engine body (1312), and the controller (132) is used for controlling the steering engine body (1312) to realize rotary driving, so that the limiting clamping tongue (1311) is driven to rotate.

4. A system ammunition dispensing device for unmanned aerial vehicles according to claim 1, wherein: the single projectile control unit (131) is used for correspondingly matching the single barrel (12).

5. A system ammunition discharge device for unmanned aerial vehicles according to any one of claims 1 to 4, characterized in that: the missile loading device is characterized in that a top plate (111) is arranged on the upper portion of the missile loading body (11), a plurality of first barrel through cavities (1113) are formed in the top plate (111), a carrying platform mounting frame (1112) and at least one bollard (1111) are arranged on the top plate (111), the upper portion of the carrying platform mounting frame (1112) is used for being installed in a matched mode with the unmanned aerial vehicle carrying platform (2), the bollard (1111) is used for being connected with a trigger line (31) of standard ammunition (3), a barrel mounting groove (1114) is formed in the bottom of the top plate (111), and the upper end of the barrel (12) is correspondingly installed in the barrel mounting groove (1114).

6. The modular ammunition dispensing device for unmanned aerial vehicles according to claim 5, wherein: still be equipped with objective table (113) in carrier organism (11) objective table (113) are used for the cooperation installation projectile device (13), be equipped with a plurality of second barrel and lead to chamber (1131) on objective table (113).

7. The modular ammunition dispensing device for unmanned aerial vehicles according to claim 6, wherein: the outer side of the bomb carrying machine body (11) is provided with a shell (112), and the shell (112) is used for completely or partially wrapping the outer sides of the plurality of gun barrels (12).

8. A system ammunition delivery apparatus for unmanned aerial vehicles according to claim 2, wherein: when the compression spring (123) is in a compressed state, the horizontal plane of the bottom end part of the compression spring (123) is higher than the horizontal plane of the projectile shooting window (121).

9. The modular ammunition dispensing device for unmanned aerial vehicles according to claim 5, wherein: when the compression spring (123) is in a compressed state, the upper end of the compression spring (123) abuts against the bottom surface of the top plate (111).

10. The modular ammunition dispensing device for unmanned aerial vehicles according to claim 5, wherein: the single mooring bollard (1111) is used for tying 1-4 standard ammunitions (3).