Safe space trajectory imaging carrier emitter device

Abstract

The invention discloses a safe space trajectory imaging carrier emitter device, and belongs to the field of amusement equipment. The device comprises a launching module, and a launching bomb storage area, a bomb feeding mechanism and a heat dissipation module are all arranged in a launching fixer; a plurality of toy bullets are arranged in the launch bullet storage area; an ammunition increasing opening is formed above the launching ammunition storage area, and an ammunition outlet below the launching ammunition storage area is connected with an ammunition inlet of the launching module through an ammunition feeding mechanism; a launching port of the launching module is formed in one side of the launching fixer and can launch toy bullets to the outside of the launching fixer; the irradiation device is arranged on the outer side of the launching fixer, the irradiation area of the irradiation device covers the trajectory path of the toy bullet launched by the launching port, and the trajectory path of the toy bullet launched by the launching port can be irradiated; and the calibration device is arranged outside the emission fixer, is positioned above the emission module, is coaxial with an emission port of the emission module, and can emit guide type laser to calibrate an irradiation area of the irradiation device. The device has the advantages of being small in size, free of open fire, easy to maintain, capable of guaranteeing continuity, high in simulation performance and the like.

Description

Technical Field

[0001] The invention relates to the technical field of amusement equipment, and in particular to a safe space ballistic imaging carrier launcher device. Background Art

[0002] Shooting amusement equipment or shooting entertainment performances are common items in various theme parks or amusement parks. These items all belong to ballistic entertainment performance items. However, the current ballistic entertainment performance items are limited by the structure of the performance equipment and cannot safely display the high-speed flight trajectory and direction of the trajectory to the audience. The audience cannot see the high-speed flight trajectory and direction of the launched object, and cannot provide the audience with a more realistic viewing experience.

[0003] In view of this, the present invention is proposed. Summary of the invention

[0004] The purpose of the present invention is to provide a safe space ballistic imaging carrier launcher device, which can clearly and accurately display the high-speed flight trajectory and direction of the launched object to the audience while ensuring the personal safety of the audience, giving the audience a simulated viewing experience of watching the real bullet trajectory, thereby solving the above-mentioned technical problems existing in the prior art.

[0005] The objective of the present invention is achieved through the following technical solutions:

[0006] A safe space ballistic imaging carrier launcher device, comprising:

[0007] A launch fixture, a launch module, a launch bullet storage area, a bullet feeding mechanism, a heat dissipation module, an irradiation device and a calibration device; wherein,

[0008] The launch module, the launch bullet storage area, the bullet feeding mechanism and the heat dissipation module are all arranged in the launch fixture;

[0009] The heat dissipation module is located below the emission module;

[0010] The launch bullet storage area is located at the front and lower part of the launch module, and contains a plurality of toy bullets;

[0011] A bullet loading port is provided above the projectile storage area, and the bullet discharge port of the projectile storage area is connected to the bullet feed port of the launch module through the bullet feeding mechanism;

[0012] The launch port of the launch module is arranged on one side of the launch fixture, and can launch toy bullets out of the launch fixture;

[0013] The irradiation device is arranged outside the launch fixture, and the irradiation area of ​​the irradiation device covers the ballistic path of the toy bullet launched from the launch port, and can irradiate the ballistic trajectory of the toy bullet launched from the launch port;

[0014] The calibration device is arranged outside the emission fixture, above the emission module, coaxial with the emission port of the emission module, and can emit a guided laser to calibrate the irradiation area of ​​the irradiation device.

[0015] Compared with the prior art, the safe space ballistic imaging carrier launcher device provided by the present invention has the following beneficial effects:

[0016] By arranging an irradiation device on the outside of a launching fixture so that it is coaxial with the launching port of a launching module and its irradiation area covers the ballistic path of a toy bullet launched from the launching port, the emitted light of the irradiation device can be illuminated when the toy bullet is launched from the launching port, so that the viewer can clearly and accurately view the high-speed flight trajectory and direction of the launched toy bullet, giving the viewer the experience of viewing the real bullet trajectory. The launcher device achieves the goal of minimizing dangerous special effects performances without reducing the special effects performances. The launcher device can be used in indoor entertainment facility performance projects that have certain requirements for personal safety, and has the characteristics of small size, no open flame, easy maintenance, guaranteed continuity, uninterrupted operation, and high simulation. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings required for use in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other accompanying drawings can be obtained based on these accompanying drawings without paying creative work.

[0018] Figure 1 A schematic diagram of the structure of a safe space ballistic imaging carrier launcher device provided in an embodiment of the present invention.

[0019] Figure 2 A front cross-sectional schematic diagram of a safe space ballistic imaging carrier launcher device provided by an embodiment of the present invention.

[0020] Figure 3 A schematic rear cross-sectional view of a safe space ballistic imaging carrier launcher device provided by an embodiment of the present invention.

[0021] Figure 4 A schematic diagram of the positional relationship of an irradiation device of a safe space ballistic imaging carrier launcher device provided in an embodiment of the present invention.

[0022] Figure 5A schematic diagram of the actual application state of the safe space ballistic imaging carrier launcher device provided by the embodiment of the present invention. The marks in the figure are: 1-launching fixture; 2-launching bullet storage area; 21-observation window; 22-adding port; 3-feeding mechanism; 31-pulsator; 32-transmission pipeline; 33-control circuit board; 4-heat dissipation module; 5-launching module; 6-irradiation device; 7-toy bullet; A-ballistic path; B-irradiation area. DETAILED DESCRIPTION

[0023] The following is a clear and complete description of the technical solutions in the embodiments of the present invention in combination with the specific content of the present invention; it is obvious that the described embodiments are only part of the embodiments of the present invention, not all of the embodiments, which does not constitute a limitation of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the protection scope of the present invention.

[0024] First, the terms that may be used in this article are explained as follows:

[0025] The term “and / or” means that either or both of them can be realized at the same time. For example, X and / or Y means both “X” or “Y” and “X and Y”.

[0026] The terms "include", "comprises", "contains", "has" or other descriptions with similar semantics should be interpreted as non-exclusive inclusion. For example, including certain technical feature elements (such as raw materials, components, ingredients, carriers, dosage forms, materials, dimensions, parts, components, mechanisms, devices, steps, procedures, methods, reaction conditions, processing conditions, parameters, algorithms, signals, data, products or products, etc.) should be interpreted as including not only certain technical feature elements explicitly listed, but also other technical feature elements known in the art that are not explicitly listed.

[0027] The term "consisting of..." means excluding any technical feature elements not explicitly listed. If this term is used in a claim, it will make the claim closed, so that it does not contain technical feature elements other than the technical feature elements explicitly listed, except for the conventional impurities related to them. If this term only appears in a clause of a claim, it only limits the elements explicitly listed in the clause, and the elements recorded in other clauses are not excluded from the overall claim.

[0028] Unless otherwise specified or limited, the terms "installed", "connected", "connected", "fixed" and the like should be understood in a broad sense, for example: it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in this article can be understood according to specific circumstances.

[0029] The orientation or position relationship indicated by terms such as "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", etc. are based on the orientation or position relationship shown in the drawings and are only for the convenience and simplification of description, and do not explicitly or implicitly indicate that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation of this document.

[0030] The scheme provided by the present invention is described in detail below. The contents not described in detail in the embodiments of the present invention belong to the prior art known to professionals in the field. If the specific conditions are not specified in the embodiments of the present invention, they are carried out according to the conventional conditions in the field or the conditions recommended by the manufacturer. If the manufacturers are not specified in the reagents or instruments used in the embodiments of the present invention, they are all conventional products that can be purchased commercially.

[0031] like Figures 1 to 5 As shown, an embodiment of the present invention provides a safe space ballistic imaging carrier launcher device, comprising:

[0032] A launch fixture 1, a launch module 5, a launch bullet storage area 2, a bullet feeding mechanism 3, a heat dissipation module 4, an irradiation device 6 and a calibration device 8; wherein,

[0033] The launch module 5, the launch bullet storage area 2, the bullet feeding mechanism 3 and the heat dissipation module 4 are all arranged in the launch fixture 1;

[0034] The heat dissipation module 4 is located below the emission module 5;

[0035] The projectile storage area 2 is located at the front and lower part of the launch module 5, and contains a plurality of toy bullets 7;

[0036] A bullet loading port 22 is provided above the projectile storage area 2, and the bullet discharge port of the projectile storage area 2 is connected to the bullet feed port of the launch module through the bullet feeding mechanism;

[0037] The launching port of the launching module 5 is arranged at one side of the launching fixture 1, and can launch the toy bullet 7 out of the launching fixture 1;

[0038] The irradiation device 6 is arranged outside the launch fixture 1, and the irradiation area B of the irradiation device 6 covers the ballistic path A of the toy bullet 7 launched from the launch port, and can irradiate the ballistic trajectory of the toy bullet launched from the launch port;

[0039] The calibration device 8 is arranged outside the emission fixture 1, above the emission module 5, coaxial with the emission port of the emission module 5, and can emit a guided laser to calibrate the irradiation area of ​​the irradiation device 6.

[0040] Preferably, in the above-mentioned emitter device, the irradiation device 6 comprises: a light source assembly, a base and a universal head;

[0041] The light source assembly is connected to the base via the universal head, and the direction of the irradiated light can be adjusted on the base;

[0042] The base is fixedly arranged on the launching fixture 1 .

[0043] Preferably, in the above-mentioned launcher device, the bullet feeding mechanism 3 includes: a pulsator 31, a transmission pipeline 32, a driving motor and a control circuit board 33; wherein,

[0044] The impeller is arranged at the bullet outlet of the projectile storage area, the transmission pipeline is located above the impeller, and the upper end of the transmission pipeline is connected to the bullet compartment entrance of the launch module;

[0045] The driving shaft of the driving motor is connected to the impeller and can drive the impeller to rotate;

[0046] The control circuit board 33 is electrically connected to the drive motor and the transmitting module 5 respectively, and can control the drive motor to drive the impeller 31 to rotate according to the transmitting signal of the transmitting module 5 to supply ammunition to the bullet chamber of the transmitting module 5.

[0047] Preferably, in the above-mentioned transmitter device, the heat dissipation module 4 adopts a fan-shaped heat dissipation component.

[0048] Preferably, in the above-mentioned launcher device, the toy bullet 7 is a water bullet.

[0049] Preferably, in the above-mentioned launcher device, the projectile storage area 2 is a funnel-shaped structure, the upper part of which is a projectile loading port 22, and the bottom is a projectile discharge port, and an observation window 21 is arranged outside the projectile storage area 2 near the projectile feeding mechanism 3.

[0050] Preferably, in the above-mentioned transmitter device, the calibration device 8 adopts a laser transmitter.

[0051] In summary, the launcher device of the embodiment of the present invention can be used in indoor entertainment facilities performance projects that have certain requirements for personal safety, and has the characteristics of small size, no open flame, easy maintenance, guaranteed continuity, uninterrupted, high simulation, etc. Through the illumination of the illumination device, when the toy bullet is launched from the launch port, the emitted light of the illumination device can be illuminated, so that the viewer can clearly and accurately see the high-speed flight trajectory and direction of the launched toy bullet, giving the viewer the experience of watching the real bullet trajectory. The launcher device achieves the maximum reduction of dangerous special effects performances without reducing the special effects performances.

[0052] In order to more clearly demonstrate the technical solution and technical effects provided by the present invention, the solution provided by the embodiment of the present invention is described in detail with specific embodiments below.

[0053] Example 1

[0054] like Figure 1 As shown, the embodiment of the present invention provides a safe space ballistic imaging carrier launcher device, which can be used in indoor entertainment performance projects that have certain requirements for personal safety. It is a performance mechanism device in which the flight trajectory of the projectile can be seen by the naked eye in real space. The launcher device includes:

[0055] A launching fixture, a launching module, a launching bullet storage area, a bullet feeding mechanism, a heat dissipation module, an irradiation device and a calibration device. The calibration device can calibrate the irradiation device outside the launching fixture, and adjust the irradiation area of ​​the irradiation device to cover the ballistic trajectory of the toy bullet launched by the launching module, so that the viewer can clearly and accurately observe the high-speed flight trajectory and direction of the launched object.

[0056] As an implementable solution of the present invention, the launch fixture is an integrated mounting shell fixture for the safe space ballistic imaging carrier launcher device.

[0057] As an implementable solution of the present invention, the heat dissipation module is a fan-shaped heat dissipation component for dissipating heat from the motor inside the transmitter device.

[0058] As an implementable solution of the present invention, the funnel-shaped structure of the projectile storage area can conveniently check the storage amount of the launched toy bullets during use by providing an observation window on the outside of the storage area adjacent to the bullet feeding mechanism.

[0059] As an implementable solution of the present invention, the projectile feeding assembly includes a pulse wheel and an upward transmission pipe, and the projectile is transported upward through the pulse wheel to reach the launching module.

[0060] The bullet feeding mechanism provided according to the embodiment of the present invention also includes a driving motor and a control circuit board, which are electrically connected to the launching module through the control circuit board to change the launching speed and complete the bullet feeding in coordination with the actual length of the upward transmission pipeline to avoid the launching module from firing blank bullets.

[0061] On the other hand, toy bullets can use bullet-shaped projectiles, and the ballistic trajectory display effect can be enhanced by enhancing the reflection conditions of the surface of the bullet-shaped projectiles, including material and color conditions.

[0062] As an implementable solution of the present invention, the toy bullet adopts a water-absorbing bullet, hereinafter referred to as a "water bullet". The water bullet is a spherical water-absorbing resin polyacrylate-polyacrylamide polymer. The water bullet is made of a transparent or translucent material. The light emitted by the laser is projected on the trajectory of the water bullet to illuminate the water bullet, which can improve the shooting experience and the visual experience at the same time.

[0063] The last aspect is to calibrate the illumination range of the illumination device through the calibration device, control the light source and the space environment, and realize the range condition of the light in the process of enhancing the trajectory of the toy bullet.

[0064] As an implementable solution of the present invention, the calibration device is installed outside the launch fixture and is coaxial with the launch port to perform a guided laser calibration function.

[0065] According to the calibration device and the external illumination device provided in the embodiment of the present invention, the illumination range and the degree of brightness and darkness of the light source assembly of the illumination device can be adjusted to make the motion effect of the water bullet trajectory more layered from the perspective of light perception and vision.

[0066] In summary, the launcher device of the embodiment of the present invention can enable viewers to clearly and accurately view the high-speed flight trajectory and direction of the projectile, giving viewers the experience of viewing the trajectory of a real bullet. It can minimize the dangerous special effects without reducing the special effects. The launcher device has the characteristics of small size, no open flame, easy maintenance, continuous, uninterrupted, and high simulation.

[0067] The above is only a preferred specific embodiment of the present invention, but the protection scope of the present invention is not limited thereto. Any changes or substitutions that can be easily thought of by any technician familiar with the technical field within the technical scope disclosed in the present invention should be included in the protection scope of the present invention. Therefore, the protection scope of the present invention should be based on the protection scope of the claims. The information disclosed in the background technology section of this article is only intended to deepen the understanding of the overall background technology of the present invention, and should not be regarded as an admission or in any form that the information constitutes prior art known to those skilled in the art.

Claims

1. A safe space ballistic imaging carrier launcher device, characterized in that: include: A launching fixture (1), a launching module (5), a launching bullet storage area (2), a bullet feeding mechanism (3), a heat dissipation module (4), an irradiation device (6) and a calibration device (8); wherein: The launching module (5), the launching bullet storage area (2), the bullet feeding mechanism (3) and the heat dissipation module (4) are all arranged in the launching fixture (1); The heat dissipation module (4) is located below the emission module (5); The projectile storage area (2) is located at the front and lower part of the launch module (5), and contains a plurality of toy bullets (7); A bullet loading port (22) is provided above the projectile storage area (2), and a bullet discharge port of the projectile storage area (2) is connected to a bullet feed port of the launch module via the bullet feeding mechanism; The launching port of the launching module (5) is arranged on one side of the launching fixture (1) and can launch a toy bullet (7) out of the launching fixture (1); The irradiation device (6) is arranged outside the launch fixture (1), and the irradiation area (B) of the irradiation device (6) covers the ballistic path (A) of the toy bullet (7) launched from the launch port, and can irradiate the ballistic trajectory of the toy bullet launched from the launch port; The calibration device (8) is arranged outside the emission fixture (1), above the emission module (5), coaxial with the emission port of the emission module (5), and can emit a guided laser to calibrate the irradiation area of ​​the irradiation device (6).

2. The safe space ballistic imaging carrier launcher device according to claim 1, characterized in that: The irradiation device (6) comprises: a light source assembly, a base and a universal head; The light source assembly is connected to the base via the universal head, and the direction of the irradiated light can be adjusted on the base; The base is fixedly arranged on the launching fixture (1).

3. The safe space ballistic imaging carrier launcher device according to claim 1 or 2, characterized in that: The bullet feeding mechanism (3) comprises: a pulsator (31), a transmission pipeline (32), a driving motor and a control circuit board (33); wherein: The impeller is arranged at the bullet outlet of the projectile storage area, the transmission pipeline is located above the impeller, and the upper end of the transmission pipeline is connected to the bullet compartment entrance of the launch module; The driving shaft of the driving motor is connected to the impeller and can drive the impeller to rotate; The control circuit board (33) is electrically connected to the drive motor and the transmitting module (5) respectively, and can control the drive motor to drive the impeller (31) to rotate according to the transmitting signal of the transmitting module (5), so as to supply ammunition to the bullet chamber of the transmitting module (5).

4. The safe space ballistic imaging carrier launcher device according to claim 1 or 2, characterized in that: The heat dissipation module (4) adopts a fan-shaped heat dissipation component.

5. The safe space ballistic imaging carrier launcher device according to claim 1 or 2, characterized in that: The toy bullet (7) is a water bullet.

6. The safe space ballistic imaging carrier launcher device according to claim 1 or 2, characterized in that: The projectile storage area (2) is a funnel-shaped structure, the upper part of which is a projectile loading port (22) and the bottom part is a projectile discharge port. An observation window (21) is arranged outside the projectile storage area (2) near the projectile feeding mechanism (3).

7. The safe space ballistic imaging carrier launcher device according to claim 1 or 2, characterized in that: The calibration device (8) uses a laser transmitter.

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