CN217716149U - Rotary ejection target - Google Patents

Abstract

The utility model discloses a rotary ejection target, which comprises a rocket barrel and a base arranged at the bottom of the rocket barrel; the rocket launcher comprises a rocket launcher main body and a rotating target surface; the rotary target surface is sleeved on the rocket tube main body and can rotate and slide downwards along the spiral sliding track on the outer surface of the rocket tube main body, and the rotary target surface rotates for a certain angle every time the rotary target surface is hit; the bottom acousto-optic control switch is arranged at the bottom of the rocket tube main body, and when the rotating target surface reaches the bottom layer, the rotating target surface can impact the bottom acousto-optic control switch. The rotary ejection target also comprises a rocket head connected to the top of the rocket tube, and when the target surface of the rocket head is hit, the warhead arranged in the rocket head is ejected. The rotary ejection target of the utility model can realize multi-angle shooting through the rotary target surface, and achieve different shooting experiences; in addition, still can shoot the ejection of hot arrow target face realization warhead, provide another kind of shooting experience of shooter, be different from the gunnery target on the existing market, be suitable for using widely.

Description

Rotary ejection target

Technical Field

The utility model relates to a recreation articles for use field especially relates to a rotatory target that launches.

Background

At present, the gunshots on the market are mainly used for realizing scoring or moving (rotating) through electronic control; the device has the advantages that the device has light response and dynamic realization or has static and dynamic reaction for attracting shooters, and obtains the fun of shooting; the disadvantages of the product are that the shooting direction is single and the reaction result is single (the target surface hits and makes a sound and overturns the target surface) in the shooting game.

It is therefore apparent that the above-mentioned conventional target still has inconvenience and drawbacks in structure and use, and further improvement is needed. How to create a new target which can shoot at multiple angles to achieve different shooting experiences on a target becomes an extremely improved target in the current industry.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is to provide a rotatory ejection target, make it can the multi-angle shooting, reach different shooting experiences to overcome the not enough that the target exists on the current market.

In order to solve the technical problem, the utility model adopts the following technical scheme:

a rotary ejection target comprises a rocket barrel and a base arranged at the bottom of the rocket barrel; the rocket launcher comprises a rocket launcher main body and a rotating target surface; the rotary target surface is sleeved on the rocket tube main body and can rotate and slide downwards along the spiral sliding track on the outer surface of the rocket tube main body, and the rotary target surface rotates for a certain angle every time the rotary target surface is hit.

As a further improvement of the invention, the rotary target surface comprises a positioning ring, three movable positioning tongue buckles, a soft rubber ring and three target surfaces; the positioning ring is sleeved on the rocket tube main body; the three target surfaces are connected to the periphery of the positioning ring and are uniformly distributed at 120 degrees; three vertical openings are formed in the positioning ring, and a transverse shaft is arranged at the upper part in each vertical opening; the three movable positioning tongue buckles are respectively installed in the vertical opening, the middle parts of the movable positioning tongue buckles protrude inwards, the upper ends of the movable positioning tongue buckles are rotatably connected to the transverse shaft, the lower ends of the movable positioning tongue buckles are clamped at the outer side of the bottom of the vertical opening, and the lower ends of the movable positioning tongue buckles are positioned through the soft rubber ring sleeved on the periphery of the positioning ring; steps which are turned downwards are arranged on the spiral sliding track every 120 degrees of rotation, and a vertical raised baffle is arranged at the bottom of the spiral sliding track below each step in an inclined manner; when the target surface is hit once, the rotating target surface rotates, the movable positioning tongue buckles collide with the vertical raised baffle after rotating for 120 degrees, and the rotating target surface descends by one step.

Furthermore, the rotary target surface further comprises a target surface clamping piece, the target surface is detachably connected with the target surface clamping piece, and the target surface clamping piece is detachably clamped with the positioning ring.

Furthermore, a bottom acousto-optic control switch is arranged at the bottom of the rocket tube main body, and an electronic component connected with the bottom acousto-optic control switch is arranged on the inner side of the bottom of the rocket tube main body; when the rotating target surface reaches the bottom layer, it can hit the bottom acousto-optic control switch.

Further, the base comprises a central supporting seat and three supporting feet which are arranged around the central supporting seat.

Further, the rocket launcher comprises a rocket launcher body and a rocket head, wherein the rocket launcher comprises a rocket launcher body and a rocket head; the rocket body comprises a rocket body inner structure and a rocket target surface; the interior of the rocket head main body is of a cylindrical structure, the upper part of the outer surface of the rocket head main body is provided with a set of linkage piece, and the linkage piece is provided with a positioning clamping piece extending into the cylindrical structure and a rocket head target surface triggering end; the lower part of the bullet is provided with a bullet buckle, and when the bullet is pressed into the rocket body, the bullet buckle is clamped with the positioning clamping piece of the linkage piece; a bottom spring is arranged at the bottom of the inner structure of the rocket head main body; the rocket body is installed to the rocket body inner structure periphery, and when the rocket body was hit, the rocket body target surface trigger end was triggered, and the location fastener that drives the linkage outwards removes, detains with the warhead of warhead and breaks away from, and the warhead that breaks away from pops out through the bottom spring.

Further, the linkage piece comprises two first connecting rods, two second connecting rods and two trigger tongues; the middle parts of the two first connecting rods and the two second connecting rods are respectively fixed at the outer side of the inner structure of the rocket head main body through lever shafts; one end of the second connecting rod is a positioning clamping piece which extends into the opening at the upper part of the structure in the rocket head main body from outside to inside; the other end of the second connecting rod is rotatably connected with the trigger tongue, and the outer side of the trigger tongue is also provided with a convex rocket target surface trigger end; the two first connecting rods, the two second connecting rods and the two trigger tongues are symmetrically arranged on the outer side of the inner structure of the rocket head body respectively, and two ends of each second connecting rod are coaxially and rotatably connected with one end of one first connecting rod respectively; when the rocket head target surface is hit, the rocket head target surface moves inwards to touch the rocket head target surface triggering end, the rocket head target surface triggering end drives one end of the first connecting rod to move inwards, the other end of the first connecting rod moves outwards around the lever shaft, then the positioning clamping piece of the second connecting rod is driven to move outwards to be separated from the bullet buckle, and the bullet is popped out.

Furthermore, the warheads are multiple, each warhead is provided with a warhead track groove, and the warhead track grooves are curved; the trigger tongue is also provided with a trigger tongue piece extending to the inner side of the inner structure of the rocket head main body, when a plurality of bullets are pressed into the inner structure of the rocket head main body, the trigger tongue piece extends into the bullet rail groove at the lower part, the bent bullet rail groove drives the trigger tongue piece to swing, and then the positioning clamping piece of the second connecting rod is driven to extend into or extend out, so that the clamping or the separation from the bullet buckle is realized until the bullet buckle of the bullet at the top is clamped with the positioning clamping piece; when the target surface of the rocket head is hit, the trigger tongue piece is driven to move inwards to the bullet rail groove of the next bullet close to the top bullet, so that the positioning clamping piece is driven to move outwards to be separated from the bullet buckle of the top bullet, and the separated bullet is ejected under the stress of the bottom spring; and the bent bullet track groove drives the trigger tongue piece to swing, so as to drive the positioning clamping piece of the second connecting rod to clamp the bullet buckle of the next bullet.

Furthermore, two fire arrow target surfaces are arranged and are respectively and symmetrically arranged on the outer sides of the linkage pieces outside the inner structure of the fire arrow main body; the two rocket head target surfaces are connected through two rotating plates which are symmetrically and crossly arranged, and the two rotating plates are connected to the rocket head main body inner structure through rotating shafts; the two rotating plates are connected to realize the synchronous inward or outward movement of the target surfaces of the two fire arrow heads; and the inner side of the target surface of the rocket head is also provided with a return spring for returning the target surface of the rocket head after being hit.

Further, the fire arrow main body also comprises two fire arrow main body shells; each upper surface is provided with a target surface window, the fire arrow head target surface is exposed through the target surface window, and the fire arrow head main body shell is correspondingly arranged in a buckling position; and/or the bottom of the rocket head is provided with symmetrical rotary buckles, and the rocket head can be directly inserted into the rocket tube to rotate to be connected with the rocket tube into a whole.

By adopting the technical scheme, the utility model discloses at least, following advantage has:

1. the utility model discloses a rotatory ejection target sets up the spiral that can follow rocket main part surface and slides the gliding rotatory target surface of track spin down, can realize the multi-angle shooting, reaches different shooting experience.

2. By adopting the movable positioning tongue buckle to match with the step and the vertical raised baffle, the device can stop after rotating 120 degrees and descend by one step.

3. By adopting the soft rubber ring matched with the movable positioning tongue buckle, after the rotating target surface moves to the bottommost layer, the rotating target surface can be directly pushed upwards to avoid the spiral sliding track and return to the topmost end again.

4. Be provided with bottom acousto-optic control switch and rather than complex electronic component in rocket tube main part bottom, can realize the light and the effect of harmony sound that reach the bottom, promote shooter's experience.

5. Be provided with the arrow point target surface and rather than the complex linkage, when the arrow point target surface is hit, the arrow point target surface trigger end is triggered, drives the outside removal of location fastener of linkage, makes the warhead break away from and pop out through the bottom spring, and above-mentioned special design provides the second kind shooting target of rotatory ejection target, can realize the ejection of warhead through shooting arrow point target surface, provides another kind of shooting of shooter and experiences.

Drawings

The foregoing is only an overview of the technical solutions of the present invention, and in order to make the technical means of the present invention more clear, the present invention will be further described in detail with reference to the accompanying drawings and the detailed description.

Fig. 1 is a schematic view of an overall structure of a rotary ejection target according to an embodiment of the present invention;

FIG. 2 is a schematic view of the joint between the main body of the rocket tube and the rotating target;

FIGS. 3 and 4 are partial exploded views of a rocket tube;

FIG. 5 is a schematic view of a base structure;

FIG. 6 is a schematic view of a rocket head;

FIG. 7 is a schematic view of the inner structure of the warhead and the body of the rocket head;

FIGS. 8 and 9 are schematic views of the internal structure of the fire arrow body at different angles;

FIG. 10 is a partial exploded view of the body of the rocket head;

FIG. 11 is a schematic view of the internal structure of the warhead at another angle to the body of the fire arrow;

fig. 12 is a schematic view of a warhead configuration;

FIG. 13 is a schematic view of another angled internal configuration of the body of the hot arrow;

FIG. 14 is a schematic view of the assembly structure of the body with the fire-point and the bullet;

FIG. 15 is a partial exploded view of a body of the fire arrow (including the housing);

fig. 16 is a schematic view showing the structure of the connection of the rocket head to the upper part of the rocket tube.

Detailed Description

Exemplary embodiments of the present invention will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the invention are shown in the drawings, it should be understood that the invention can be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

The rotatory target that launches that this embodiment provided, as shown in fig. 1, including rocket tube 1, base 2 and rocket head 3 three major parts, base 2 installs in rocket tube 1 bottom, and rocket head 3 installs at rocket tube 1 top, and rocket tube 1 plays the bearing effect.

The rocket launcher 1 comprises a rocket launcher main body 11 and a rotating target surface 12; rotatory target surface 12 cover is on rocket tube main part 11, can follow the spiral sliding track 111 of rocket tube main part 11 surface and rotate the slip downwards, and rotatory target surface 12 is once hit once, rotates certain angle (the preferred 120 degrees of this embodiment), and rocket tube main part 11 bottom is provided with bottom acousto-optic control switch, when rotatory target surface 12 reaches the bottom, can strike bottom acousto-optic control switch.

Through the arrangement, the first shooting target of the rotary ejection gun target can be realized, namely the rotary target surface 12 which can spirally descend on the shooting rocket tube main body 11 is shot, the rotary target surface 12 is shot each time, the rotary target surface 12 rotates for 120 degrees, and descends by one layer (5 layers are adopted in the embodiment), and when the rotary target surface 12 reaches the bottom layer, the rotary target surface can impact the bottom acousto-optic control switch to trigger the internal light and sound effect; through this kind of setting, shooter can the multi-angle shooting, reaches different shooting and experiences, and the light audio developments when having the success simultaneously are amazing, further promote the shooting and experience.

As shown in fig. 2 and 3, the rotary target surface 12 includes a positioning ring 121, three movable positioning tongue fasteners 122, a soft rubber ring 123 and three target surfaces 124; the positioning ring 121 is sleeved on the rocket tube main body 11; the three target surfaces 124 are connected to the periphery of the positioning ring 121 and are uniformly distributed at 120 degrees; the positioning ring 121 is provided with three vertical openings 1211, and a transverse shaft 1212 is arranged at the upper part in each vertical opening 1211; the three movable positioning tongue buckles 122 are respectively installed in the vertical opening 1211, the middle parts of the movable positioning tongue buckles 122 protrude inwards, the upper ends of the movable positioning tongue buckles 122 are rotatably connected to the transverse shaft 1212, the lower ends of the movable positioning tongue buckles 122 are clamped at the outer side of the bottom of the vertical opening 1211, and the lower ends are positioned by a soft rubber ring 123 sleeved on the periphery of the positioning ring 121; on the spiral sliding track 111, a step 112 turning downwards is arranged every 120 degrees of rotation, and a vertical raised baffle 113 is arranged at the bottom of the spiral sliding track 111 obliquely below each step 112.

In the shooting process, when the target surface 124 is hit once, the rotating target surface 12 rotates, and after rotating for 120 degrees, the movable positioning tongue 122 collides with the vertical raised baffle 113, so that the vertical raised baffle 113 decelerates and stops, descends downwards along the vertical raised baffle 113, and descends to the next floor, which is equivalent to that the rotating target surface 12 descends by one step at the moment. In order to ensure smooth descending, the width between the upper vertical raised baffle 113 and the next step should be slightly larger than the width of the movable positioning tongue 122, and the vertical raised baffle 113 cannot be too long. When the next shot is fired, the above-described actions are repeated until the rotating target surface 12 has rotated to the very bottom. When the rotating target surface 12 reaches the bottom and needs to be fired again, the rotating target surface can be directly pushed upwards from the bottom, at the moment, the bottom of the movable positioning tongue buckle 122 is pushed away, the soft rubber ring 123 is expanded, the movable positioning tongue buckle 122 leaves the spiral sliding track 111 on the rocket tube main body 11, and finally the rotating target surface is pushed to the top of the rocket tube main body 11.

As shown in the accompanying fig. 2 and 3, the rotary target surface 12 further comprises a target surface clamping piece 125, the target surface 124 is detachably connected with the target surface clamping piece 125, the target surface clamping piece 125 and the positioning ring 121 are detachably clamped, and the target surface clamping piece is detachably arranged to facilitate the replacement of the target surface 124.

As shown in fig. 4, an electronic component 13 connected to the bottom acousto-optic control switch is disposed on the inner side of the bottom of the rocket tube main body 11, and when the bottom acousto-optic control switch is impacted, the electronic component realizes the effects of light, sound effect and the like.

As shown in fig. 5, the base 2 includes a central support base 21 and three support legs 22 installed around the central support base 21. The central support seat 21 and the three support legs 22 are matched, so that the whole gun target can keep a stable state in the shooting process.

As shown in fig. 6 and 7, the fire arrow 3 includes a fire arrow body 31 and a bullet head 32; the rocket body 31 comprises a rocket target surface 311 and a rocket body inner structure 312; the rocket head main body inner structure 312 is a cylindrical structure, the upper part of the outer surface of the rocket head main body inner structure is provided with a set of linkage members 313, and the linkage members 313 are provided with positioning clamping pieces extending into the cylindrical structure and rocket head target surface triggering ends; the lower part of the bullet 32 is provided with a bullet buckle 321, and when the bullet 32 is pressed into the rocket body inner structure 312, the bullet buckle 321 is clamped with the positioning fastener of the linkage 313; the bottom of the fire arrow head body inner structure 312 is provided with a bottom spring 314.

The fire arrow target surface 311 is arranged on the periphery of the inner structure 312 of the rocket body, when the fire arrow target surface 311 is hit, the trigger end of the fire arrow target surface is triggered to drive the positioning clamping piece of the linkage piece 313 to move outwards and separate from the warhead buckle 321 of the warhead 32, and the separated warhead 32 is ejected through the bottom spring 314.

The structural design of the above fire arrow 3 provides a second kind of shooting target of the rotary ejection gun target, the ejection of the warhead can be realized by shooting the target surface of the fire arrow, and another kind of shooting experience of shooters is provided.

As shown in fig. 8-11, the linkage 313 includes two first connecting rods 3131, two second connecting rods 3132, and two trigger tongues 3133; the middle parts of the two first connecting rods 3131 and the two second connecting rods 3132 are respectively fixed outside the fire arrow main body inner structure 312 through lever shafts 3134; one end of the second connecting rod 3132 is a positioning fastener 31321, the positioning fastener 31321 extends into the opening hole at the upper part of the fire arrow main body inner structure 312 from outside to inside; the other end of the second connecting rod 3132 is rotatably connected with a triggering tongue 3133, and a convex fire arrow target surface triggering end 31331 is further arranged on the outer side of the triggering tongue 3133; two first connecting rods 3131, two second connecting rods 3132, and two trigger tongues 3133 are symmetrically disposed outside the fire-arrow-head main body 312, and two ends of each second connecting rod 3132 are coaxially and rotatably connected to one end of one first connecting rod 3131.

When the fire arrow target surface 311 is hit, the fire arrow target surface 311 moves inward to trigger the fire arrow target surface triggering end 31331, the fire arrow target surface triggering end 31331 drives one end of the first connecting rod 3131 to move inward, the other end of the first connecting rod 3131 moves outward around the lever shaft 3134, and then the positioning fastener 31321 of the second connecting rod 3132 is driven to move outward to be separated from the bullet buckle 321, and the bullet 32 pops up.

A plurality of warheads 32 are provided, in this embodiment, 3 warheads are used in bulk, and as shown in fig. 12 and 13, each warhead 32 is provided with a warhead track groove 322, and the warhead track groove 322 is curved; the trigger tongue 3133 is further provided with a trigger tongue 31332 extending to the inner side of the fire arrow main body inner structure 312, when a plurality of bullets 32 are pressed into the fire arrow main body inner structure 312, the trigger tongue 31332 extends into the bullet rail groove 322 at the lower portion, the bent bullet rail groove 322 drives the trigger tongue 31332 to swing, and further drives the positioning fastener 31321 of the second connecting rod 3132 to extend or extend, so as to realize the engagement or disengagement with the bullet fastener 321, until the bullet fastener 321 of the bullet 32 at the top is engaged with the positioning fastener 31321.

When the target surface 311 of the rocket head is hit, the trigger tongue 31332 is driven to move inward into the bullet rail groove 322 of the next bullet 32 (the second bullet counted from top to bottom) next to the top bullet 32, and the positioning fastener 31321 is driven to move outward to be separated from the bullet fastener 321 of the topmost bullet 32, and the separated bullet 32 is forced to pop out by the bottom spring 314; at this time, the other bullet heads 32 at the bottom are also forced to move upwards, and during the movement, the curved bullet track groove 322 drives the trigger tongue 31332 to swing, and further drives the positioning fastener 31321 of the second connecting rod 3132 to lock the bullet head fastener 321 of the next bullet head 32 (the next bullet head is relative to the separated bullet head, i.e. the next bullet head is the currently topmost bullet head). By the cooperation of the curved bullet track groove 322 and the trigger tongue 31332, the next bullet can be quickly engaged after the top bullet is disengaged.

As shown in fig. 14, two fire arrow target surfaces 311 are symmetrically arranged outside the linkage 313 outside the fire arrow main body inner structure 312; the two rocket nose target surfaces 311 are connected through two symmetrical and crossed rotating plates 316, and the two rotating plates 316 are connected to the rocket nose main body inner structure 312 through a rotating shaft 317; the two fire arrow target surfaces 311 are connected through the two rotating plates 316 to synchronously move inwards or outwards; the inner side of the target surface 311 is also provided with a return spring 318 for returning the target surface 311 after being hit.

As shown in fig. 15 and 16, the fire arrow body 31 further includes two fire arrow body housings 315; each upper surface is provided with a target surface window 3151, the fire arrow target surface 311 is exposed through the target surface window 3151, and the fire arrow main body shell 315 is correspondingly arranged in a buckling position. In addition, the bottom of the shell 315 of the rocket body of the rocket 3 is provided with symmetrical rotary buckles, and the rocket body can be directly inserted into the rocket tube 1 to rotate so as to be connected with the rocket tube 1 into a whole.

In summary, the rotary ejection target of the utility model is provided with the rotary target surface which can rotate and slide downwards along the spiral sliding track on the outer surface of the rocket body, thereby realizing multi-angle shooting and achieving different shooting experiences; in addition, except the above-mentioned target surface of will rotating as the shooting target, still can shoot the ejection that the fire arrow target surface realized the warhead, provide another kind of shooting experience of shooter, be different from the gunnery on the existing market, be suitable for using widely.

The above description is only for the preferred embodiment of the present invention, and not intended to limit the present invention in any way, and those skilled in the art can make various modifications, equivalent changes and modifications using the above-described technical content, all of which fall within the scope of the present invention.

Claims (10)

1. A rotary ejection target is characterized by comprising a rocket tube (1) and a base (2) arranged at the bottom of the rocket tube (1); the rocket launcher (1) comprises a rocket launcher main body (11) and a rotating target surface (12); the rotary target surface (12) is sleeved on the rocket tube main body (11) and can rotate and slide downwards along a spiral sliding track (111) on the outer surface of the rocket tube main body (11), and the rotary target surface (12) rotates for a certain angle every time being hit.

2. The rotary ejection gun target according to claim 1, characterized in that the rotary target surface (12) comprises a positioning ring (121), three movable positioning tongue clasps (122), a soft rubber ring (123) and three target surfaces (124);

the positioning ring (121) is sleeved on the rocket tube main body (11); the three target surfaces (124) are connected to the periphery of the positioning ring (121) and are uniformly distributed at 120 degrees; three vertical openings (1211) are formed in the positioning ring (121), and a transverse shaft (1212) is arranged at the upper part in each vertical opening (1211); the three movable positioning tongue buckles (122) are respectively installed in the vertical opening (1211), the middle parts of the movable positioning tongue buckles (122) protrude inwards, the upper ends of the movable positioning tongue buckles are rotatably connected to the upper end and the lower end of the transverse shaft (1212) and clamped at the outer side of the bottom of the vertical opening (1211), and the lower ends of the movable positioning tongue buckles are positioned through a soft rubber ring (123) sleeved on the periphery of the positioning ring (121);

steps (112) turning downwards are arranged at each 120-degree rotation on the spiral sliding track (111), and a vertical raised baffle (113) is arranged at the bottom of the spiral sliding track (111) obliquely below each step (112);

when the target surface (124) is hit once, the rotating target surface (12) rotates, the movable positioning tongue buckle (122) collides with the vertical raised baffle (113) after rotating for 120 degrees, and the rotating target surface (12) descends by a step.

3. The rotary ejection gun target according to claim 2, characterized in that the rotary target (12) further comprises a target surface fastener (125), the target surface (124) is detachably connected with the target surface fastener (125), and the target surface fastener (125) is detachably clamped with the positioning ring (121).

4. The rotary ejection target according to claim 1, characterized in that the bottom of the rocket body (11) is provided with a bottom acousto-optic control switch, and the inner side of the bottom of the rocket body (11) is provided with an electronic component (13) connected with the bottom acousto-optic control switch; when the rotating target surface (12) reaches the bottom layer, it can strike the bottom acousto-optic control switch.

5. The rotary ejection target according to claim 1, characterized in that the base (2) comprises a central support base (21) and three support feet (22) mounted around the central support base (21).

6. The rotary ejection target according to any one of claims 1 to 5, characterized by further comprising a rocket head (3) attached to the top of the rocket barrel (1), said rocket head (3) comprising a rocket body (31) and a bullet (32);

the rocket body (31) comprises a rocket target surface (311) and a rocket body inner structure (312); the interior (312) of the rocket head body is of a cylindrical structure, the upper part of the outer surface of the interior is provided with a set of linkage piece (313), and the linkage piece (313) is provided with a positioning clamping piece and a rocket head target surface triggering end which extend into the cylindrical structure;

the lower part of the bullet (32) is provided with a bullet buckle (321), and when the bullet (32) is pressed into the rocket body inner structure (312), the bullet buckle (321) is clamped with the positioning clamping piece of the linkage piece (313); a bottom spring (314) is arranged at the bottom of the fire arrow head main body inner structure (312);

the rocket body is characterized in that the rocket body is provided with a rocket target surface (311) at the periphery of the rocket body inner structure (312), when the rocket target surface (311) is hit, the trigger end of the rocket target surface is triggered to drive the positioning clamping piece of the linkage piece (313) to move outwards and separate from the bullet buckle (321) of the bullet (32), and the separated bullet (32) is ejected by the stress of the bottom spring (314).

7. The rotary ejection target according to claim 6, characterized in that the linkage (313) comprises two first connecting rods (3131), two second connecting rods (3132), two trigger tongues (3133); the middle parts of the two first connecting rods (3131) and the two second connecting rods (3132) are respectively fixed on the outer side of the fire arrow main body inner structure (312) through a lever shaft (3134);

one end of the second connecting rod (3132) is a positioning clamping piece (31321), and the positioning clamping piece (31321) extends into the opening hole in the upper part of the fire arrow head main body inner structure (312) from outside to inside; the other end of the second connecting rod (3132) is rotatably connected with a triggering tongue (3133), and the outer side of the triggering tongue (3133) is also provided with a convex fire arrow target surface triggering end (31331);

the two first connecting rods (3131), the two second connecting rods (3132) and the two trigger tongues (3133) are respectively and symmetrically arranged on the outer side of the fire arrow head main body inner structure (312), and two ends of each second connecting rod (3132) are respectively and coaxially and rotatably connected with one end of one first connecting rod (3131);

when the fire arrow target surface (311) is hit, the fire arrow target surface (311) moves inwards to trigger the fire arrow target surface triggering end (31331), the fire arrow target surface triggering end (31331) drives one end of the first connecting rod (3131) to move inwards, the other end of the first connecting rod (3131) moves outwards around the lever shaft (3134), and then the positioning clamping piece (31321) of the second connecting rod (3132) is driven to move outwards to be separated from the bullet buckle (321), and the bullet (32) pops up.

8. The rotary ejection target of claim 7, wherein the plurality of bullets (32) are provided, each bullet (32) having a bullet track groove (322), the bullet track grooves (322) being curved;

the trigger tongue (3133) is further provided with a trigger tongue (31332) extending towards the inner side of the fire arrow main body inner structure (312), when a plurality of bullets (32) are pressed into the fire arrow main body inner structure (312), the trigger tongue (31332) extends into the bullet track groove (322) at the lower part, the bent bullet track groove (322) drives the trigger tongue (31332) to swing, and then the positioning fastener (31321) of the second connecting rod (3132) extends into or extends out to realize the clamping or separation with the bullet fastener (321) until the bullet fastener (321) of the bullet (32) at the top is clamped with the positioning fastener (31321);

when the target surface (311) of the fire arrow is hit, the triggering tongue piece (31332) is driven to move inwards to the bullet rail groove (322) of the next bullet (32) next to the top bullet (32), and then the positioning fastener (31321) is driven to move outwards to be separated from the bullet buckle (321) of the topmost bullet (32), and the separated bullet (32) is forced to pop out by the bottom spring (314); and the curved bullet track groove (322) drives the trigger tongue piece (31332) to swing, and further drives the positioning fastener (31321) of the second connecting rod (3132) to clamp the bullet buckle (321) of the next bullet (32).

9. The rotary ejection target of claim 6, wherein the two fire-arrow target surfaces (311) are symmetrically arranged outside the linkage member (313) outside the fire-arrow main body inner structure (312); the two fire arrow target surfaces (311) are connected through two symmetrical and crossed rotating plates (316), and the two rotating plates (316) are connected to the fire arrow main body inner structure (312) through a rotating shaft (317);

the two fire arrow target surfaces (311) are synchronously moved inwards or outwards through the connection of the two rotating plates (316);

and a return spring (318) is further arranged on the inner side of the fire arrow target surface (311) and is used for returning the fire arrow target surface (311) after being hit.

10. The rotary ejection gun target according to claim 9, characterized in that the fire arrow body (31) further comprises two fire arrow body housings (315); each upper surface is provided with a target surface window (3151), the fire arrow target surface (311) is exposed through the target surface window (3151), and the fire arrow main body shell (315) is correspondingly buckled and installed;

and/or symmetrical rotary buckles are arranged at the bottom of the rocket head (3), and the rocket head can be directly inserted into the rocket tube (1) to rotate so as to be connected with the rocket tube (1) into a whole.

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