The present invention relates generally to the field of an electrical discharge weapon for immobilizing a live target. More specifically, the present invention is related to an electrical discharge weapon having an improved shock circuit and a method for operating the same.
Electrical discharge weapons are weapons that connect a shocking power to a remote live target by means of darts and/or trailing wires fired from the electrical discharge weapons. The shocks debilitate violent suspects, so peace officers can more easily subdue and capture them. Stun guns, by contrast, connect the shocking power to the live target that are brought into direct contact with the stun guns to subdue the target. Electrical discharge weapons and guns are far less lethal than other more conventional firearms.
In general, the basic idea of the above described electrical discharge weapon s is to disrupt the electric communication system of muscle cells in a live target. That is, an electrical discharge weapon generates a high-voltage, low-amperage electrical charge. When the charge passes into the live target's body, it is combined with the electrical signals from the brain of the live target. The brain's original signals are mixed in with random noise, making it very difficult for the muscle cells to decipher the original signals. As such, the live target is stunned or temporarily paralyzed. The current of the charge may be generated with a pulse frequency that mimics a live target's own electrical signal to further stun or paralyze the live target.
To dump this high-voltage, low-amperage electrical charge, the electrical discharge weapon includes a shock circuit having multiple transformers and/or autoformers that boost the voltage in the circuit and/or reduce the amperage. The shock circuit may also include an oscillator to produce a specific pulse pattern of electricity and/or frequency. In one embodiment, the charge is then released to the live target via a charge electrode and a ground electrode respectively positioned on a charge dart and a ground dart that are both connected to the weapon by long conductive wires. In the embodiment, the long conductive wires are considered necessary to maintain low force factors necessary for a weapon delivery system which is presumed incapable of seriously injuring a human target, but which is also capable of propelling a projectile at a target for a practical range. That is, it is desirable to use a small propellant charge and a light weight projectile.
However, a disadvantage to such a design of using two wired darts is that both minimum and maximum range are sacrificed. That is, as known to those skilled in the art, depending on the angle between the weapon's bores, the charge and ground darts will not spread enough at closer ranges to insure an adequately large current path through the target, unless the marksman is lucky enough to impact a particularly sensitive area of the body. At further ranges the darts will have spread too far apart for both of them to impact the target as needed to complete the current path through the target. In addition, the wired darts could not pass down the bore of most conventional firearms.
Moreover, if the wires are not deployed to their maximum range and length, they will hang from the cartridge over the bottom of the port or firing bay and frequently rest laxly on the ground in close proximity to each other or even resting upon or overlapping each other for portions of their lengths. Accordingly, the wires have to be insulated by heavy insulation to prevent them from being shorted with each other. The weight of the insulation further limits the range of the darts and the type of firearms that can project these darts.
In view of the foregoing, it would be highly desirable to create a weapon for immobilization and capture of a live target having projectiles or missiles that do not require trailing wires connected to the weapon while still allowing the projectiles or missiles to maintain a low less lethal force factor (i.e., being light in weight and capable of being propelled using a small propellant change) and to provide a sufficient stun (shock) power. Also, it would be desirable to provide a light weight shock circuit for such a weapon that shocks with sufficient power to disable, but that can be entirely located in the less lethal projectile itself.
The present invention relates to a system and/or an associated method for providing an electrical discharge weapon and/or a method for using the same that includes a shock circuit having a low power consumption, a high power efficiency, and/or a low weight. In one embodiment, the electrical discharge weapon includes a high efficiency circuit that would reduce the weights of shock circuits while providing a more effective and safer power level, so that the circuits may be entirely contained in a projectile of the weapon and the need for range limiting trailing wires can be eliminated.
In one embodiment of the present invention, a wireless projectile projected from an electrical discharge weapon for immobilizing a live target is provided. The wireless projection includes a projectile shell and a shock circuit. The shock circuit is integrated within the projectile shell and includes a battery source, an inverter transformer, an independent oscillator, and a switch. The inverter transformer has a primary coil of the inverter transformer and a secondary coil of the inverter transformer. The switch is connected between the inverter transformer and a common voltage node (or a ground) and is also connected to the independent oscillator. In the shock circuit, the independent oscillator triggers and re-triggers the switch to supply an energy pulse from the battery source to the primary coil of the inverter transformer for a predetermined time period.
In one embodiment of the present invention, a method to immobilize a live target through electricity is provided. The method includes: oscillating an independently controlled waveform from a positive voltage to a ground voltage; driving a transistor via the independently controlled waveform to turn ON and OFF; energizing and de-energizing an energy from a battery source through a primary coil of an inverter transformer via the transistor driven by the independently controlled waveform; coupling the energized and de-energized energy from the primary coil of the inverter transformer to a secondary coil of the inverter transformer; stepping up a voltage of the energized and de-energized energy from the secondary coil of the inverter transformer to immobilize the live target; and providing the stepped-up energy to the live target to immobilize the live target. In the present method, the energy provided to the live target is not greater than nine watts.
A more complete understanding of the electrical discharge weapon will be afforded to those skilled in the art and by a consideration of the following detailed description. Reference will be made to the appended sheets of drawings which will first be described briefly.
These and other features and aspects of the present invention will be more fully understood when considered with respect to the following detailed description, appended claims, and accompanying drawings.
In the following detailed description, only certain exemplary embodiments of the present invention are shown and described, by way of illustration. As those skilled in the art would recognize, the described exemplary embodiments may be modified in various ways, all without departing from the spirit or scope of the present invention. Accordingly, the drawings and description are to be regarded as illustrative in nature, and not restrictive.
There may be parts shown in the drawings, or parts not shown in the drawings, that are not discussed in the specification as they are not essential to a complete understanding of the invention. Like reference numerals designate like elements.
Referring to
In operation, an electrical charge which travel into the wire 16 and the dart 50 is activated by squeezing the trigger 20. The power for the electrical charge is provided by the battery 30. That is, when the trigger 20 is turned on, it allows the power to travel to the shock circuit 10. The shock circuit 10 includes a first transformer that receives electricity from the battery 30 and causes a predetermined amount of voltage to be transmitted to and stored in a storage capacitor (e.g., a Mylar cap). Once the storage capacitor stores the predetermined amount of voltage, it is able to discharge an electrical pulse into a second transformer and/or autoformer. The output from second transformer then goes into the first wire 16 and the dart 50. The darts 50, 60 are also projected through the air to the target by the squeeze of the trigger 20. When the darts 50, 60 contact the target, charges from the dart 50 travel into tissue in the target's body, then through the tissue into the second dart 60 and the second conducting wire 17, and then to a ground in the housing 1. Pulses are delivered from the dart 50 into target's tissue for a predetermined amount of seconds. The pulses cause contraction of skeletal muscles and make the muscles inoperable, thereby preventing use of the muscles in locomotion of the target.
Typically, the shocks from an electrical discharge weapon are generated by a classic relaxation oscillator that produces distorted saw tooth pulses as is shown in
Referring to
In addition, a secondary coil 120 of the inverter transformer T1 between PAD5 and PAD6 is connected to a pair of diodes D4 and D5 that forms a half-wave rectifier. The pair of diodes D4 and D5 are then serially connected with a Mylar cap 130 and then with a primary coil 140 of the output transformer T2. The primary coil 140 of the output transformer T2 is connected between PAD7 and PAD 8. The Mylar cap 130 is selected to have particular ionization characteristics tailored to a specific spark gap breakover voltage to “tune” the output of the shock circuit.
In operation and as described above, the classic relaxation oscillator produces distorted saw tooth pulses as is shown in
Referring also to a waveform 130′ of
In addition, since the self actualizing relaxation oscillator includes a bipolar transistor Q1, switching losses may occur. That is, the oscillator fly back or tickler coil 110 is slow to reverse bias the transistor Q1 because of its magnetic feedback. This slow ramping or rise time limits how fast the transistor Q1 can switch without burning up. The slow switching causes power losses. Moreover, because of the slow switching speed, the shock circuit requires larger and bulkier transformers T1, T2, as transformer size is directly proportional to switching speed. As such, the shock circuit of
In an embodiment of the present invention and referring to
In the shock circuit 200 of
In more detail, the primary coil 240 of the inverter transformer T1′ is energized as current flows through the coil 240 from PAD10 to PAD11 as the switch (or transistor) 250 is turned ON. The independent oscillator 210 is coupled to the switch 250 (e.g., at the base or the gate of the switch 250) to turn the switch 2500N and OFF. A secondary coil 260 of the inverter transformer T1′ between PAD 12 and PAD 13 is connected to a full-wave rectifier 270. The full-wave rectifier 270 is then serially connected with a Mylar cap 280 and then with a primary coil 290 of the output transformer T2′. The primary coil 290 of the output transformer T2′ is connected between PAD14 and PAD 15.
In operation, the capacitor C and the primary coil 240 of the embodiment of
This oscillation will continue until the circuit runs out of energy and will oscillate at an predetermined amplitude and frequency that depends on the size of the primary coil 240 and the capacitor C. As such, the capacitor C can turn the significant energy in the second half of the total train of waves of
In more detail, when the tank circuit 220 is triggered by 250, it begins to resonate. The resonation would thereafter trail off as is shown in
Referring to
In operation, the oscillator 210′ creates a periodic output that varies from a positive voltage (V+) to a ground voltage. This periodic waveform creates the drive function for the PNP transistor 290′. The output voltage of the oscillator 210′ is not a square wave but a pulse waveform that is low for about one third of its period. When the oscillator 210 switches low, it causes zener diode D27 to conduct, and in turn, causes the transistor 290′ to saturate. The zener diode D27 is needed because the voltage Vcc, that powers the transistor 290′ and the positive voltage (V+) that powers the oscillator 210′ are at different potentials. When 290′ turns on, it in turn causes the transistor 250′ to saturate. This, in turn causes current to flow through the primary coil 240′ of the transformer T1″. This current flow causes current to flow in the secondary coil 260′ of the transformer T1″ based on the turn ratio of the transformer T1″. In this particular situation, the transformer T1″ has a turn ratio of about 110:1 (or 110 to 1). A power current from the battery source 230′ then flows in the primary coil 240′ of the transformer T1″ only when the transistor 250″ is turned on and is in the process of conducting. Residual current, however, can also be flown through the primary coil 240′ as the magnetic field, initially generated by the current flow from the battery source 230′, collapses and the tank circuit 220′ mechanized with the primary coil 240′ of the transformer T1″ and capacitor C15 begins to resonate. This “resonant current” is also coupled through the transformer T1″ from the primary coil 240′ to the secondary coil 260′ and, in turn, also is stepped up by the turn ratio of the transformer T1″.
The full wave bridge rectifier 270′, mechanized with the four high voltage diodes D1, D2, D3, and D4, therefore rectifies the initial voltage and current from the power source 230′ when the transistor 250′ is caused to conduct, and then the resonant voltage and current created as the tank circuit 220′ resonates. The effect of this is to cause the Mylar cap 280′ to charge more quickly and with more efficiency, thereby requiring less energy drawn from the power source 230′ than if the tank circuit 220′ was not present in the design.
An additional feature of this shock circuit 200′ is that the transistor 250′ is a high voltage transistor with a Vcc of greater then 1000 volts. This eliminates the need for a “snubber” diode across the transformer primary. A diode D6 is required, however, because as the tank circuit 220′ resonates, it would have the capability to break down the transistor 250′ over in the reverse direction thereby potentially damaging the transistor 250′ and “snubbing” the tank circuit 220′ resonance prematurely.
In a generalized exemplary embodiment of the present invention, a portion of a shock circuit that is employed to generate a high voltage used to deliver a current pulse to an output transformer utilizes a resonant tank circuit. The tank circuit assists in the creation of the high voltage level necessary to charge the Mylar cap through the fact that it resonates at a frequency determined by the inductance of the primary coil of an inverter transformer and the capacitor that is placed in parallel with it. However, the present invention is not limited to the above described exemplary embodiment. For example, referring to
In view of the foregoing, certain high efficiency circuits can be employed to form electrical discharge weapons with higher energy shocks with similar sizes to weapons with circuits having self actualizing relaxation oscillators. However, the propriety of forming weapons capable of producing such high powered shocks may be in question because the enhanced shocks may increase the weapons lethality, especially where circuits operating at a fraction of the power ranges that can be achieved by these circuits (e.g., at power levels as low as 1.5 watts and 0.15 joules per pulse at ten pps) were demonstrated to completely disable test subjects as early as 1971. In addition, some seventy deaths have occurred proximate to use of such weapons. As such, using these pistols at high power ranges may run contrary to the idea that electrical discharge weapons are intended to subdue and capture live targets without seriously injuring them. Therefore, a more laudable purpose for such high efficiency circuits would be to reduce the weights of shock circuits at the lower and safer power levels, so that the circuits can be entirely contained in projectiles and to eliminate the need for range limiting trailing wires.
Less lethal wireless projectiles could not, heretofore, be launched to optimally desired tactical ranges while maintaining safe force factors, because, as currently produced by various manufactures, the shock circuits that might be contained within the projectile have too great a weight.
The primary consideration when assessing the relative lethality of a non-lethal projectile is the kinetic energy that is transferred to the target upon impact. The energy is equal to one-half the mass of the projectile times the square of the velocity:
K.E.=½ mv2
This equation shows the strong dependence on velocity and a lesser dependence on the mass of the projectile. It is desirable to keep the velocity high to deliver the maximum kinetic energy, within the constraints of non-lethal impact to the body (blunt impact trauma and penetration). Higher velocities also have the desirable effect of maximizing the accuracy and flight stability of the projectile, for improved flight characteristics and trajectory.
Much research has been done to characterize the blunt trauma and penetration characteristics of non-lethal projectiles, and these results have been correlated with specific ranges of kinetic energy and kinetic energy per unit of impact area. Acceptable impact properties can usually be achieved by controlling the kinetic energy delivered to the target, maximizing the impact area that contacts the target, or by designing features into the projectile that absorb or dissipate energy upon impact.
When trying to find a compromise between the competing goals of maximum kinetic energy, optimum flight characteristics, and non-lethal impact properties, the designer is usually faced with sacrificing performance in one area to satisfy requirements in another when adjusting the velocity. One way to control the kinetic energy while keeping the velocity as high as possible for optimum flight considerations is to decrease the mass of the projectile. While this has a smaller effect on the kinetic energy than the velocity, it allows the designer some flexibility to decrease the impact energy without affecting performance.
In one embodiment of the present invention, a shock circuit includes a non-self actualizing oscillator. The shock circuit can be less than or equal to forty-five grams, produce a shock power that is less than nine watts, and/or produce each pulse at an energy range that is less than 0.9 joules. In one embodiment, each pulse is produced at an energy range that is not less than 0.15 joules and not greater than 0.75 joules.
In more detail, the profile of pulses used in an exemplary embodiment should be within the following ranges. First, the energy produced by the pulses should be in the range of about 0.01 to 0.8 joules or about 0.5 to 0.75 joules. Second, the width of each pulse should be about one to nine microseconds or about seven and a half to nine microseconds. Third, the root-mean-square (rms) current of the pulses should be in the range of about twenty to ninety milliamps or about sixty-five to ninety milliamps. In addition, the pulses should be delivered to a target having a travel spacing (or distance) within the target to induce enough skeletal muscles contractions such that the live target subjected to the pulses is actually disabled.
Referring to
In more detail and referring to
A passage 522 is covered with a Mylar tape 521 where it opens adjacent end cap 513. The tape 521 protects a primer 528 shown in
The terminal operation of the projectile 512 as it nears and engages the target 520, is illustrated sequentially in
This secondary propelling of the second connector 525 only when the projectile 512 is close to or in contact with the target 520 assures that, irrespective of the distance to the target 520, the spacing between connectors 515 and 525 will be substantially the same. Moreover, the spacing will be within a range to virtually assure optimal disabling effect on the target.
In one embodiment, the wire tether 530 can be about forty-six cm or eighteen inches long and the passage 522 can be at an angle greater than forty-five degrees, or about seventy degrees with respect to the axis of the projectile 512.
An embodiment of the projectile 512 can be configured as a fixed ammunition shell which can be fired through a conventional thirty-eight mm or forty mm bore or which can be between 38 to 40 mm in caliber. An embodiment of the projectile 512 can also be launched by gas expansion in the launching cartridge or casing in the chamber of a firearm. In one embodiment, the projectile 512 should be less than 110 grams and should produce a force of less than about twelve newtons or ninety ft-lb/s2 (pdl) on the target 520. The shock circuit integrated into the projectile 512 should not be greater than 45 grams or about 25 grams and should produce a shock power that is less than nine watts or between about two to six watts. Otherwise, the operation of the projectile 512 should act like a standard shell when it is desired to immobilize a target.
While the invention has been described in connection with certain exemplary embodiments, it is to be understood by those skilled in the art that the invention is not limited to the disclosed embodiments, but, on the contrary, is intended to cover various modifications included within the spirit and scope of the appended claims and equivalents thereof.