CN107328309B - Multi-warhead remote non-lethal electric shock device - Google Patents
Multi-warhead remote non-lethal electric shock device Download PDFInfo
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- CN107328309B CN107328309B CN201710754099.8A CN201710754099A CN107328309B CN 107328309 B CN107328309 B CN 107328309B CN 201710754099 A CN201710754099 A CN 201710754099A CN 107328309 B CN107328309 B CN 107328309B
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- rocker arm
- warhead
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
- F41H13/0012—Electrical discharge weapons, e.g. for stunning
Abstract
The invention discloses a multi-warhead long-distance non-lethal electric shock device, which comprises: a high voltage discharge control module (210) for generating a high voltage current and controlling an output, and displaying a remaining number of discharges; the trigger electrode switching mechanism (200) is used for sequentially switching on the three electrodes respectively, outputting high voltage to corresponding warheads, and switching by continuously pressing the trigger so that high voltage current of the high-voltage discharge control module sequentially passes through the electrodes at different positions; the flying needle electrode switching mechanism (300) is used for controlling whether the switching of the electric shock device needs electrode discharge or needs to eject a flying needle to send high-voltage current to a target, and 3 groups of warheads are installed at the same time; the battery pack (601) is used for supplying power to the high-voltage discharge control module; the laser sighting device is used for indicating the target position through the upper laser lamp and the lower laser lamp; the bullet (400) is used for fixing the high-voltage current flying needle, a device for providing kinetic energy for the flying needle, a trigger control circuit and an electrode for high-voltage output of near-body defense; and the shell is used for protecting and fixing the above modules and mechanism parts.
Description
Technical Field
The invention belongs to a multi-warhead remote non-lethal electric shock device, and belongs to an anti-riot device for police.
Background
At present, one bullet is shot at a time, and the bullet needs to be filled again after being shot, so that people can catch an elbow when attacking or grouping events happen, and the bullet is not free from the mind. On the basis of the above, an electric shock device which can be used by simultaneously mounting three warheads and can be replaced is developed.
Disclosure of Invention
The invention aims to solve the technical problem of providing a multi-warhead long-distance non-lethal electric shock device.
The technical scheme adopted by the invention for solving the technical problems is as follows:
a multi-warhead remote non-lethal electric stunner, comprising:
a high voltage discharge control module (210) for generating a high voltage current and controlling an output, and displaying the remaining number of discharges; the trigger electrode switching mechanism (200) is used for sequentially switching on the three electrodes respectively, outputting high voltage to corresponding warheads, and switching by continuously pressing the trigger so that high voltage current of the high-voltage discharge control module sequentially passes through the electrodes at different positions; the flying needle electrode switching mechanism (300) is used for controlling whether the switching of the electric shock device needs electrode discharge or needs to eject a flying needle to send high-voltage current to a target, and 3 groups of warheads are installed at the same time; the battery pack (601) is used for supplying power to the high-voltage discharge control module; the laser sighting device is used for indicating the target position through the upper laser lamp and the lower laser lamp; the bullet (400) is used for fixing the high-voltage current flying needle, a device for providing kinetic energy for the flying needle, a trigger control circuit and an electrode for high-voltage output of near-body defense; and the shell is used for protecting and fixing the above modules and mechanism parts, providing the moving range thereof, and completing installation, fixing and implementation operations.
Preferably, the high-voltage discharge control module (210) is fixed in a main body (206) of the trigger electrode switching mechanism (200), the fly needle electrode switching mechanism (300) is sleeved in the trigger electrode switching mechanism (200) and matched, then a positioning groove (103-1) of the left housing (103) is installed, the trigger electrode switching mechanism (200) is fixed on the left housing (103) through screws, and the first laser sight (501) and the second laser sight (502) are respectively fixed on the left housing (103) through screws.
Preferably, the battery pack (601) is a detachable piece, is installed after the left shell (103) and the right shell (104) are fixed, and is buckled and fixed by the battery system (602).
Preferably, the bullet (400) is arranged in a bullet bin (302-1) of a bullet clip bracket (302) of the flying-pin electrode switching mechanism (300), an elastic sheet (400-1) on the bullet is guided in through a groove position 302-4 below the bullet clip bracket (302) until the elastic sheet is clamped on the bullet clip bracket (302), the detachable bullet (400) is pushed out reversely by pressing the elastic sheet (400-1), and the bullet clip bracket (302) is provided with three bin positions (302-1, 302-2 and 302-3).
Preferably, the trigger electrode switching mechanism (200) specifically includes: the trigger switch comprises a trigger switch (201), a sliding mechanism (202), a torsion spring (203), a draw hook (204), a ratchet wheel (205), a main body (206), a rocker arm (207), a rocker arm torsion spring (208), a check piece (209) and a slider pressing plate (225), wherein the trigger switch (201) is inserted into the main body (206), and the trigger switch (201) and the sliding mechanism (202) are fixed by screws; the draw hook (204) is arranged in a slot position (206-6) of the main body (206), the torsion spring (203) is arranged in the sliding mechanism (202), and the draw hook (204) blocks the torsion spring (203); the check piece (209) is arranged in the main body (206), the slide block pressing plate (225) is arranged in the main body (206), and the slide block pressing plate is clamped in the main body (206) and then fixed by screws; the rocker arm (207) is arranged in the main body (206), and after the rocker arm torsion spring (208) of the rocker arm (207) is arranged in the main body (206), the rocker arm (207) is clamped and then fixed by screwing in a meson and a screw. The ratchet wheel (205) is arranged on a column of the main body (206), and is provided with an upper meson and a screw for limiting and fixing the height but rotating; when the trigger is pressed down, the ratchet rotates clockwise by 60 degrees, the ratchet controls the rocker arm to switch the electrodes, the high-voltage discharge control module does not output high-voltage current in the switching process, and the high-voltage current can be output only when the trigger is pressed down to a position 2mm away from the target position and is continuously pressed down, so that the safety and the reliability of the switching process are ensured.
Preferably, the flying-needle electrode switching mechanism is switched by a tension spring and a self-locking switch, the tension spring is in an electrode discharge mode when in a compression state, the tension spring is in a flying-needle mode with high-voltage current for emission when being stretched to a drawing locking position, the electrode on the warhead can only emit high-voltage electric arc without flying needles when the trigger is pressed in place in the electrode discharge mode, and the flying needles are emitted to send the high-voltage electric current to a target when the trigger is pressed in place in the flying-needle mode with high-voltage current for emission.
Preferably, the trigger electrode switching mechanism (200) includes: the trigger switch (201), the trigger switch (201) is connected and drives the sliding mechanism (202), the torsion spring (203) and the draw hook (204) to move, the draw hook (204) hooks the ratchet (205) to rotate clockwise, the draw hook (204) moves to a limit (206-1) on the main body (206) and stops moving, at the moment, the ratchet (205) rotates clockwise by 60 degrees, the upper cylinder (205-1) of the ratchet drives the rocker (207) to move to a first limit (206-2) position, because the ratchet (205) only rotates clockwise, the rocker torsion spring (208) on the rocker (207) is required to press the rocker tail rod (207-1) of the ratchet to the upper cylinder (205-1), and the swinging of the rocker (207) is controlled by the rotation of the ratchet (205).
Preferably, the trigger switch (201) releases to drive the draw hook (204) to move the draw hook inclined plane (204-1) in the opposite direction to slide over the ratchet wheel inclined plane (205-2) and be blocked by the backstop (209), and the ratchet wheel (205) does not rotate.
Preferably, when the trigger switch (201) is pressed down again, the ratchet wheel (205) rotates clockwise, and the ratchet wheel upper cylinder 205-1 rotates beyond the range of the rocker arm tail rod 207-1, the rocker arm tail rod 207-1 leans against the ratchet wheel lower cylinder 205-3 due to the pressure of the rocker arm torsion spring (208), and the rocker arm (207) reaches the second limit (206-3); every time the trigger switch (201) is pressed and released, the ratchet wheel (205) rotates clockwise by 60 degrees, and the trigger switch (201) is repeatedly pressed and released.
Preferably, the rocker arm (207) is controlled to circularly switch the electrode positions, the upper electrode 211 and the lower electrode 212 of the high-voltage discharge control module (210) transmit high-voltage current to the clip upper electrode 401 and the clip lower electrode 402 of each bullet (400) according to the switching of the rocker arm (207) from the bracket electrodes 213 and 214 to the rocker arm electrodes 223 and 215 of the rocker arm (207) to the middle electrodes 216 and 224 or the left and right electrodes 217, 218, 219 and 220, and the high-voltage current is conducted by air gap arc with the distance of 0.3-0.6 mm between the electrodes.
The invention uses a group of high-voltage discharge control modules to respectively and sequentially connect three electrodes and output high voltage to corresponding warheads. The electrode discharge can be selected to be the flying needle with high voltage current, the electrode discharge discharges on the warhead without flying needle, three warheads are filled once, the warhead can be detached and refilled after the flying is finished, and law enforcement officers can first scare violent molecules in actual use to make uniform non-lethal electric shocking devices.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
Drawings
The present invention will be described in detail below with reference to the accompanying drawings so that the above advantages of the present invention can be more clearly understood. Wherein, the first and the second end of the pipe are connected with each other,
fig. 1 is an external view of the product 100.
Figure 2 is a cross-sectional view illustrating the design and implementation method.
FIG. 3 is an external view of the parts of the trigger electrode switching mechanism (200) and the fly needle electrode switching mechanism (300).
FIG. 4 is a cross-sectional view illustrating the design and implementation of the method.
FIG. 5 is an external view of a structural part illustrating the design and implementation method.
Fig. 6 is an external view of a structural part of the trigger electrode switching mechanism (200).
Fig. 7 is an external view of a structural part of the trigger electrode switching mechanism (200).
Fig. 8 is an external view of a structural part of the trigger electrode switching mechanism (200).
FIG. 9 is an external view of a ratchet part in the structure of the trigger electrode switching mechanism (200).
FIG. 10 is an external view of a part of the structure of the trigger electrode switching mechanism (200).
FIG. 11 is a partial external view showing the structure of the trigger electrode switching mechanism (200) in a state where the swing arm is moved.
FIG. 12 is a partial external view showing the structure of the trigger electrode switching mechanism (200) in a state in which the swing arm is moved.
FIG. 13 is a partial external view showing the structure of the trigger electrode switching mechanism (200) in a state in which the swing arm is moved.
Fig. 14 is a sectional view showing an embodiment of the trigger electrode switching mechanism (200).
FIG. 15 is an external view of the structural parts of the trigger electrode switching mechanism (200) and the fly needle electrode switching mechanism (300).
Fig. 16 is a diagram showing the connection relationship of the electrodes among the high-voltage discharge control module (210), the swing arm (207), the holder 221, and the bullet.
Fig. 17 is a structural diagram of the fly needle electrode switching mechanism (300) and the bullet (400).
Fig. 18 is a sectional view illustrating a mode switching method of the flying-needle electrode switching mechanism (300) and the bullet (400).
Fig. 19 is a sectional view illustrating a mode switching method of the flying-needle electrode switching mechanism (300) and the bullet (400).
Fig. 20 is a sectional view illustrating a mode switching method of the flying-needle electrode switching mechanism (300) and the bullet (400).
Fig. 21 is an external view of a structural part of the bullet (400).
Detailed Description
The following detailed description will be given with reference to the accompanying drawings and examples to explain how to apply the technical means to solve the technical problems and to achieve the technical effects. It should be noted that, as long as there is no conflict, the embodiments and the features of the embodiments of the present invention may be combined with each other, and the technical solutions formed are within the scope of the present invention.
Additionally, the steps illustrated in the flow charts of the figures may be performed in a computer system such as a set of computer-executable instructions and, although a logical order is illustrated in the flow charts, in some cases, the steps illustrated or described may be performed in an order different than here.
The invention discloses a multi-warhead remote non-lethal electric shock device, which comprises: a high voltage discharge control module (210) for generating a high voltage current and controlling an output, and displaying the remaining number of discharges; the trigger electrode switching mechanism is used for sequentially switching on the three electrodes respectively, outputting high voltage to the corresponding warheads, and switching by continuously pressing the trigger so that high-voltage current of the high-voltage discharge control module sequentially passes through the electrodes at different positions; the flying needle electrode switching mechanism is used for controlling whether the switching electric shock device needs to discharge electrodes or needs to eject flying needles to send high-voltage current to a target, and 3 groups of warheads can be installed at the same time; the battery pack supplies power to the high-voltage discharge control module; the laser sighting device is used for indicating the target position through the upper laser lamp and the lower laser lamp; the warhead is used for fixing the high-voltage current flying needle, a device for providing kinetic energy for the flying needle, a trigger control circuit and an electrode for high-voltage output of near-body defense; and the shell is used for protecting and fixing the above modules and mechanism parts, providing the moving range thereof, and completing installation, fixing and implementation operations.
The invention can continuously control the three warheads in sequence by the trigger electrode switching mechanism and can select electrode discharge or launch high-voltage current flying needles by the flying needle electrode switching mechanism.
The trigger electrode switching mechanism adopts a ratchet wheel one-way stepping principle, when a ratchet wheel rotates clockwise by 60 degrees in the process of pressing down the trigger, the ratchet wheel controls a rocker arm to switch the electrodes, a high-voltage discharge control module does not output high-voltage current in the switching process, and the high-voltage current can be output only when the trigger is pressed to a position section 2mm away from the position in place, so that the switching process is safe and reliable.
The flying-needle electrode switching mechanism adopts a tension spring and a self-locking switch for switching, the tension spring is in an electrode discharge mode when in a compression state, the tension spring is in a transmitting high-voltage current flying-needle mode when being stretched to a drawing locking position, the electrode on the warhead can only emit high-voltage electric arc without transmitting the flying needle when the trigger is pressed in place in the electrode discharge mode, the flying needle is transmitted to a target when the trigger is pressed in place in the transmitting high-voltage current flying-needle mode, and the function that law enforcement officers stop violent molecules before making clothes is achieved.
The following is a description of a specific design implementation of the present invention.
1. Trigger electrode switching mechanism (200)
The trigger switch (201) is pressed down to drive the sliding mechanism (202), the torsion spring (203) and the draw hook (204) to move, the draw hook (204) hooks the ratchet wheel (205) to rotate clockwise, the draw hook (204) moves to the limit 206-1 on the main body (206) to stop moving, at the moment, the ratchet wheel (205) rotates clockwise by 60 degrees, and the upper cylinder 205-1 of the ratchet wheel drives the rocker arm (207) to a position (shown in figure 8). As the ratchet wheel (205) only rotates clockwise, the rocker arm (207) needs the rocker arm torsion spring (208) to press the rocker arm tail rod 207-1 to the ratchet wheel upper cylinder 205-1, and the swinging of the rocker arm (207) is controlled by the rotation of the ratchet wheel (205).
The trigger switch (201) is loosened to drive the draw hook (204) to move the draw hook inclined plane (204-1) and the ratchet wheel inclined plane (205-2) in the opposite direction to slide through and be blocked by the backstop (209), and the ratchet wheel (205) does not rotate (figure 9).
When the trigger switch (201) is pressed again, the ratchet wheel (205) rotates clockwise (figure 10) to a position, and the ratchet wheel upper cylinder (205-1) rotates beyond the range of the rocker tail rod (207-1), the pressure of the rocker torsion spring (208) can lean against the ratchet wheel lower cylinder (205-3) (figure 10). Every time the trigger switch (201) is pressed and released once, the ratchet (205) rotates clockwise by 60 degrees, and the trigger switch (201) is repeatedly pressed and released, and the ratchet (205) and the rocker (207) are changed as shown in fig. 11, 12 and 13.
The control rocker arm (207) cyclically switches the electrode positions, the upper electrode 211 and the lower electrode 212 of the high-voltage discharge control module (210) transmit high-voltage current to the clip upper electrode 401 and the clip lower electrode 402 of each bullet (400) according to the switching of the rocker arm (207) through the bracket electrodes 213 and 214 → the rocker arms 223 and 215 of the rocker arm (207), the intermediate electrodes 216 and 224, or the left and right electrodes 217, 218, 219 and 220 (note that the intermediate electrodes and the left and right electrodes are determined according to the switching of the rocker arm (207). Air gaps of 0.3-0.6 mm are arranged between the electrodes of the high-voltage for electric arc energization.
The positions, moving ranges and moving modes of the parts are fixed and limited by the main body 221 and the clip support 222, and the mounting, fixing and implementing operations are completed (fig. 14, 15 and 16).
2. A fly needle electrode switching mechanism (300) and a bullet (400).
When the drawing 301 is in the position (fig. 15), the electrode discharge mode is set, the tension spring 403 is in the contracted state, and the electric arc is generated in the high-voltage loop of the bullet (400) when the distance between the output ends 401-1 and 402-1 of the upper pole 401 and the lower pole 402 of the cartridge clip is nearest, so that the electrode discharge is realized. In order to ensure that the electrode discharge mode can reliably discharge between 401-1 and 402-1, the design is that a conducting strip 418 (figure 21) is additionally arranged on the door cover 417.
The movement of the draw 301 to the latched position 222-1 (fig. 15) of the clip holder 222 is a launch band high voltage current fly pin mode. The extension spring 403 is extended to the input end 401-2 of the cartridge clip upper pole 401, the electric arc is electrified to the extension spring through the conductive copper foil 414, and the high-voltage loop of the bullet (400): such as the cartridge upper pole 401 → the conductive copper foil 414 → the tension spring 403 → the wire 415 → the miniature explosive 404 → the gas cylinder 405 → the conductive copper foil 416 → the flying pin 408 → the wire 410 → the cartridge lower pole 402. The high-voltage circuit triggers the miniature explosive 404 to push the gas cylinder 405 to move and press the puncture needle 406, the punctured gas cylinder instantly releases compressed nitrogen to eject flying needles 407 and 408, the tail parts 407-1 and 408-1 of the flying needles are provided with leads 409 and 410 in a penetrating manner, the other ends 409-1 and 410-1 of the leads are respectively electrified with the upper pole 401 and the lower pole 402 of the cartridge clip, and the flying needles with high voltage current are shot to a target.
The positions, the line arrangement and the movement mode of the parts are fixed by the cartridge clip 411, the rear cover 412 and the air bottle gland 413, and the movement range is limited, so that the installation, the fixation and the implementation operation are completed.
The high-voltage discharge control module, the trigger electrode switching mechanism, the flying needle electrode switching mechanism, the battery pack, the laser sighting devices 101 and 102 and the warheads are mounted, fixed, protected and operated by the shells 103 and 104.
2. The long-distance non-lethal electric stunner with multiple warheads according to claim 1, wherein the high-voltage discharge control module (210) is fixed in the main body (206) of the trigger electrode switching mechanism (200), the flying-needle electrode switching mechanism (300) is sleeved in the trigger electrode switching mechanism (200) and is matched, then the positioning groove (103-1) of the left shell (103) is arranged, and then 200-1 and 200-2 of the trigger electrode switching mechanism (200) are fixed on the left shell (103) by screws; the first laser sight (501) and the second laser sight (502) are fixed at the positions 103-2, 103-3, 103-4 and 103-5 of the left shell (103) by screws respectively. The battery pack (601) is a detachable piece, is installed after the left shell (103) and the right shell (104) are fixed, and is buckled and fixed by the battery system (602). The bullet (400) is loaded into a bullet bin (302-1) of a bullet clip bracket (302) of the flying-pin electrode switching mechanism (300), an elastic sheet (400-1) on the bullet is guided in through a groove position 302-4 below the bullet clip bracket (302) until the elastic sheet blocks the 302-5 position of the bullet clip bracket (302), the detachable bullet (400) is pushed out reversely by pressing the elastic sheet (400-1), and the method for installing and detaching the bullet (400) in the bullet clip bracket (302) is the same as that for installing and detaching the bullet (400) in three bin positions 302-1, 302-2 and 302-3;
2. the multi-warhead remote non-lethal electric stun device of claim 1, wherein said trigger electrode switching mechanism comprises: the specific components comprise a trigger switch (201), a sliding mechanism (202), a torsion spring (203), a draw hook (204), a ratchet wheel (205), a main body (206), a rocker arm (207), a rocker arm torsion spring (208), a check piece (209) and a slider pressing plate (225) (figure 6 and figure 7).
The specific structure is that the main body (206) is taken as the main body, 201-1 of the trigger switch (201) is inserted into the position 206-5 of the main body (206), and 201-2 of the trigger switch (201) and 202-1 of the sliding mechanism (202) are fixed by screws. The draw hook (204) is arranged in a slot position (206-6) of the main body (206), the torsion spring (203) is arranged at a position 202-3 and a position 203-1 of the sliding mechanism (202) and is arranged at a position 202-4, and the position 204-1 of the draw hook (204) blocks a position 203-2 of the torsion spring (203). The check piece (209) is installed at the positions of 206-7 and 206-8, the slide block pressing plate (225) is installed in the main body (206), and the slide block pressing plate is clamped into the positions of 206-9 and 206-10 of the main body (206) and then fixed with screws 206-11 and 206-12. The rocker arm (207) is arranged in the main body (206), the rocker arm (207) is positioned at the positions of 206-13 and 206-14, after the rocker arm torsion spring (208) is arranged in the position of 206-13 of the main body (206), the rocker arm (207) is clamped at the same time of clamping 206-15, and then the rocker arm (207) is fixed by screwing in the position of 206-13 by using a meson and a screw. The ratchet wheel (205) is arranged on the 206-16 columns of the main body (206) and is provided with a middle piece and a screw for limiting and fixing the height but rotating.
The ratchet wheel unidirectional stepping mechanism rotates clockwise by 60 degrees in the process of pressing down the trigger, the ratchet wheel controls the rocker arm to switch the electrodes, the high-voltage discharge control module does not output high-voltage current in the switching process, and the high-voltage current can be output only when the trigger is pressed to a position 2mm away from the target position and is continuously pressed down, so that the safety and the reliability of the switching process are ensured.
The flying-needle electrode switching mechanism adopts a tension spring and a self-locking switch for switching, the tension spring is in an electrode discharging mode when in a compressed state, the tension spring is in a flying-needle mode with high-voltage current emission when being stretched to a drawing locking position, the electrode on the warhead can only emit high-voltage electric arc without flying needles when the trigger is pressed in place in the electrode discharging mode, and the flying-needle is emitted to a target when the trigger is pressed in place in the flying-needle mode with high-voltage current emission.
The trigger electrode switching mechanism (200) comprising: the trigger switch (201), the trigger switch (201) is connected and drives the sliding mechanism (202), the torsion spring (203) and the draw hook (204) to move, the draw hook (204) hooks the ratchet (205) to rotate clockwise, the draw hook (204) moves to a limit (206-1) on the main body (206) and stops moving, at the moment, the ratchet (205) rotates clockwise by 60 degrees, the upper cylinder (205-1) of the ratchet drives the rocker (207) to move to a first limit (206-2) position (shown in figure 8), because the ratchet (205) only rotates clockwise, the rocker torsion spring (208) on the rocker (207) is required to press the rocker tail rod 207-1 against the upper cylinder (205-1) of the ratchet, and the swinging of the rocker (207) is controlled by the rotation of the ratchet (205).
The releasing process of the trigger switch (201) drives the draw hook (204) to move the draw hook inclined plane (204-1) and the ratchet wheel (205) -2 in opposite directions to slide through and be blocked by the backstop (209), and the ratchet wheel (205) does not rotate (figure 9).
When the trigger switch (201) is pressed again, the ratchet wheel (205) rotates clockwise, the ratchet wheel upper cylinder 205-1 rotates beyond the range of the rocker arm tail rod 207-1, the rocker arm tail rod 207-1 leans against the ratchet wheel lower cylinder 205-3 due to the pressure of the rocker arm torsion spring (208), and the rocker arm (207) reaches the second limit 206-3 position (fig. 10). Every time the trigger switch (201) is pressed and released once, the ratchet (205) rotates clockwise by 60 degrees, and the trigger switch (201) is repeatedly pressed and released, and the ratchet (205) and the rocker (207) are changed as shown in fig. 11 → 12 → 13.
The control rocker arm (207) cyclically switches the electrode positions, the upper electrode 211 and the lower electrode 212 of the high-voltage discharge control module (210) transmit high-voltage current to the clip upper electrode 401 and the clip lower electrode 402 of each bullet (400) according to the switching of the rocker arm (207) through the bracket electrodes 213 and 214 → the rocker arms 223 and 215 of the rocker arm (207), the intermediate electrodes 216 and 224, or the left and right electrodes 217, 218, 219 and 220 (note that the intermediate electrodes and the left and right electrodes are determined according to the switching of the rocker arm (207). Air gaps of 0.3-0.6 mm are arranged between the electrodes of the high-voltage for arc energization.
The positions, moving ranges and moving modes of the parts are fixed and limited by the main body 221 and the clip support 222, and the mounting, fixing and implementing operations are completed (fig. 14, 15 and 16).
A fly needle electrode switching mechanism (300) and a bullet (400).
When the drawing 301 is in the 222-1 position, an electrode discharge mode is set (fig. 15), the tension spring 403 is in a contracted state (fig. 19), an arc is generated in a high-voltage loop of the bullet (400) when the distance between the output ends 401-1 and 402-1 of the upper pole 401 and the lower pole 402 of the cartridge clip is nearest, the electrode discharge is realized (fig. 16 and 17), and in order to ensure that the electrode discharge mode can reliably discharge between the output ends 401-1 and 402-1, a conductive sheet 418 (fig. 21) is additionally arranged on the door cover 417.
The movement of the draw 301 to the latched position 222-2 (fig. 15) of the clip holder 222 is a launch band high voltage current fly pin mode. Extension spring 403 is elongated to near the input end 401-2 of the cartridge holder top pole 401 (fig. 18, fig. 19), the arc energizes the extension spring through the conductive copper foil 414, the high voltage loop of the warhead (400): such as the upper pole 401 of the clip → the conductive copper foil 414 → the tension spring 403 → the wire 415 → the miniature explosive 404 → the gas cylinder 405 → the conductive copper foil 416 → the flying pin 408 → the wire 410 → the lower pole 402 of the clip (fig. 20). The high-voltage circuit triggers the miniature explosive 404 to push the gas cylinder 405 to move and press the puncture needle 406, the punctured gas cylinder instantly releases compressed nitrogen to eject flying needles 407 and 408, the tail parts 407-1 and 408-1 of the flying needles are provided with leads 409 and 410 in a penetrating manner, the other ends 409-1 and 410-1 of the leads are respectively electrified with the upper pole 401 of the cartridge holder and the lower pole 402 of the cartridge holder, and the flying needles with high voltage current are shot to a target (fig. 18, fig. 19 and fig. 20).
The positions, the line arrangement and the movement mode of the parts are fixed by the cartridge clip 411, the rear cover 412 and the air bottle gland 413, and the movement range is limited, so that the installation, the fixation and the implementation operation are completed.
The high-voltage discharge control module, the trigger electrode switching mechanism, the flying needle electrode switching mechanism, the battery pack, the laser sighting devices 101 and 102, and the bullet are used for completing the installation, fixation, protection and implementation operation of the whole machine by a left shell (103) and a right shell (104).
It should be noted that for simplicity of description, the above method embodiments are described as a series of acts, but those skilled in the art should understand that the present application is not limited by the described order of acts, as some steps may be performed in other orders or simultaneously according to the present application. Further, those skilled in the art should also appreciate that the embodiments described in the specification are preferred embodiments and that the acts and modules referred to are not necessarily required in this application.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. A multi-warhead remote non-lethal electric stun device, comprising:
a high voltage discharge control module (210) for generating a high voltage current and controlling an output, and displaying the remaining number of discharges; the trigger electrode switching mechanism (200) is used for sequentially switching on the three electrodes respectively, outputting high voltage to corresponding warheads, and switching by continuously pressing the trigger so that high voltage current of the high-voltage discharge control module sequentially passes through the electrodes at different positions; the flying needle electrode switching mechanism (300) is used for controlling whether the switching of the electric shock device needs electrode discharge or needs to eject a flying needle to send high-voltage current to a target, and 3 groups of warheads are installed at the same time; the battery pack (601) is used for supplying power to the high-voltage discharge control module; the laser sighting device is used for indicating the target position through the upper laser lamp and the lower laser lamp; the bullet (400) is used for fixing the high-voltage current flying needle, a device for providing kinetic energy for the flying needle, a trigger control circuit and an electrode for high-voltage output of near-body defense; the shell is used for protecting and fixing each module and mechanism parts, providing the moving range of the shell, and completing installation, fixation and implementation operation; the high-voltage discharge control module (210) is fixed in a main body (206) of the trigger electrode switching mechanism (200), the fly needle electrode switching mechanism (300) is sleeved into the trigger electrode switching mechanism (200) and matched, then a positioning groove (103-1) of a left shell (103) is arranged, the trigger electrode switching mechanism (200) is fixed on the left shell (103) through screws, and a first laser sighting device (501) and a second laser sighting device (502) are respectively fixed on the left shell (103) through screws;
the trigger electrode switching mechanism (200) specifically comprises: the trigger switch comprises a trigger switch (201), a sliding mechanism (202), a torsion spring (203), a draw hook (204), a ratchet wheel (205), a main body (206), a rocker arm (207), a rocker arm torsion spring (208), a check piece (209) and a slider pressing plate (225), wherein the trigger switch (201) is inserted into the main body (206), and the trigger switch (201) and the sliding mechanism (202) are fixed by screws; the draw hook (204) is arranged in a slot position (206-6) of the main body (206), the torsion spring (203) is arranged in the sliding mechanism (202), and the draw hook (204) blocks the torsion spring (203); the check piece (209) is arranged in the main body (206), the slide block pressing plate (225) is arranged in the main body (206), and the slide block pressing plate is clamped in the main body (206) and then fixed by screws; the rocker arm (207) is arranged in the main body (206), and after a rocker arm torsion spring (208) of the rocker arm (207) is arranged in the main body (206), the rocker arm (207) is clamped and then is screwed in by a meson and a screw to be fixed;
the ratchet wheel (205) is arranged on a column of the main body (206), and is provided with an upper meson and a screw for limiting and fixing the height but rotating; when the trigger is pressed down, the ratchet rotates clockwise by 60 degrees, the ratchet controls the rocker arm to switch the electrodes, the high-voltage discharge control module does not output high-voltage current in the switching process, and the high-voltage current can be output only when the trigger is pressed down to a position 2mm away from the target position and is continuously pressed down, so that the safety and the reliability of the switching process are ensured.
2. The multi-warhead remote non-lethal electric stun device according to claim 1, wherein the battery pack (601) is a detachable piece which is installed after the left housing (103) and the right housing (104) are fixed and is buckled and fixed by the battery (602).
3. The multi-warhead remote non-lethal electric shocker according to claim 2, wherein the warhead (400) is loaded into a magazine of a cartridge holder (302) of the flying-pin electrode switching mechanism (300), a spring plate (400-1) on the warhead is guided through a slot position (302-4) below the cartridge holder (302) until the spring plate is clamped on the cartridge holder (302), the detachable warhead (400) is reversely pushed out by pressing the spring plate (400-1), and the cartridge holder (302) has three magazine positions (302-1, 302-2 and 302-3).
4. The multi-warhead remote non-lethal electric shock device of claim 1, wherein said flying-probe electrode switching mechanism is switched by a tension spring and a self-locking switch, the tension spring is in an electrode discharge mode when in a compressed state, the tension spring is in a flying-probe mode with high voltage current for emission when being stretched to a drawing locking position, the electrode on the warhead can only emit high voltage arc without flying probe when the trigger is pressed in place in the electrode discharge mode, and the flying probe can only emit high voltage current to a target when the trigger is pressed in place in the flying-probe mode with high voltage current for emission.
5. The multi-warhead remote non-lethal electric stun device of claim 1, wherein said trigger electrode switching mechanism (200) comprises: the trigger switch (201), the trigger switch (201) is connected and drives the sliding mechanism (202), the torsion spring (203) and the draw hook (204) to move, the draw hook (204) hooks the ratchet (205) to rotate clockwise, the draw hook (204) moves to a limit (206-1) on the main body (206) to stop moving, at the moment, the ratchet (205) rotates 60 degrees clockwise, the upper cylinder (205-1) of the ratchet drives the rocker (207) to move to a first limit (206-2) position, because the ratchet (205) only rotates clockwise, the rocker torsion spring (208) on the rocker (207) is needed to press the rocker tail rod (207-1) on the ratchet to press the upper cylinder (205-1), and the swing of the rocker (207) is controlled by the rotation of the ratchet (205).
6. The multi-warhead remote non-lethal electric shock device according to claim 5, wherein the trigger switch (201) is released to drive the draw hook (204) to move the draw hook inclined plane (204-1) and the ratchet inclined plane (205-2) in the opposite direction to slide over and be blocked by the backstop (209), and the ratchet (205) does not rotate.
7. The multi-warhead remote non-lethal electric shocker according to claim 6, wherein when the trigger switch (201) is pressed again, the ratchet wheel (205) rotates clockwise, the upper cylinder (205-1) of the ratchet wheel rotates beyond the range of the tail rod (207-1) of the rocker arm, the tail rod (207-1) of the rocker arm leans against the lower cylinder (205-3) of the ratchet wheel due to the pressure of the torsion spring (208) of the rocker arm, and the rocker arm (207) reaches the second limit (206-3) position; every time the trigger switch (201) is pressed and released, the ratchet wheel (205) rotates clockwise by 60 degrees, and the trigger switch (201) is repeatedly pressed and released.
8. The multi-warhead remote non-lethal electric stun device according to claim 5, wherein the control rocker arm (207) cyclically switches the electrode positions, the upper electrode (211) and the lower electrode (212) of the high-voltage discharge control module (210) are switched from the bracket poles (213, 214) to the rocker poles (223, 215) of the rocker arm (207) to the middle poles (216, 224) or the left and right poles (217, 218, 219, 220), high-voltage current is delivered to the cartridge holder upper pole (401) and the cartridge holder lower pole (402) of each warhead (400) according to the switching of the rocker arm (207) positions, and air gaps of 0.3-0.6 mm are electrified between the high-voltage electrodes.
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| CN201710754099.8A CN107328309B (en) | 2017-08-29 | 2017-08-29 | Multi-warhead remote non-lethal electric shock device |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108362275A (en) * | 2018-02-02 | 2018-08-03 | 北京盈想东方科技股份有限公司 | A kind of acousto-optic-electric bore sight |
| US11041698B2 (en) * | 2019-01-18 | 2021-06-22 | Axon Enterprise, Inc. | Unitary cartridge for a conducted electrical weapon |
| AU2020299117A1 (en) | 2019-04-30 | 2022-01-06 | Axon Enterprise, Inc. | Polymorphic conducted electrical weapon |
| RU2748738C1 (en) * | 2020-03-20 | 2021-05-31 | Габлия Юрий Александрович | Electroshock weapons to immobilize several aims |
| CN112066787B (en) * | 2020-09-17 | 2021-05-14 | 观典防务技术股份有限公司 | Multifunctional electric shock gun |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104748619A (en) * | 2015-04-23 | 2015-07-01 | 成都恒安警用装备制造有限公司 | Multi-running-fire anti-riot gun |
| CN105605972A (en) * | 2014-10-28 | 2016-05-25 | 靳洪伟 | Multi-warhead controller |
| CN205957811U (en) * | 2016-08-17 | 2017-02-15 | 深圳民盾安全技术开发有限公司 | Electric shock anti -riot device |
| CN205957818U (en) * | 2016-08-17 | 2017-02-15 | 深圳民盾安全技术开发有限公司 | Electric shock anti -riot device flies needle emitter |
| CN106767174A (en) * | 2016-12-26 | 2017-05-31 | 孙景斌 | A kind of remote non-lethal electric shock device and multiple warhead base |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8261666B2 (en) * | 2008-10-26 | 2012-09-11 | Rakesh Garg | Charging holder for a non-lethal projectile |
-
2017
- 2017-08-29 CN CN201710754099.8A patent/CN107328309B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105605972A (en) * | 2014-10-28 | 2016-05-25 | 靳洪伟 | Multi-warhead controller |
| CN104748619A (en) * | 2015-04-23 | 2015-07-01 | 成都恒安警用装备制造有限公司 | Multi-running-fire anti-riot gun |
| CN205957811U (en) * | 2016-08-17 | 2017-02-15 | 深圳民盾安全技术开发有限公司 | Electric shock anti -riot device |
| CN205957818U (en) * | 2016-08-17 | 2017-02-15 | 深圳民盾安全技术开发有限公司 | Electric shock anti -riot device flies needle emitter |
| CN106767174A (en) * | 2016-12-26 | 2017-05-31 | 孙景斌 | A kind of remote non-lethal electric shock device and multiple warhead base |
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