The present invention relates generally to an electromagnetic accelerator. More specifically, the present invention is an electromagnetic tube gun for creating projectile motion within a barrel via Lorentz force.
Electromagnetic launchers (EML), commonly referred to as railguns, operate by generating projectile motion through an electromagnetic force known as Lorentz force. A conventional electromagnetic launcher comprises a first conducting rail and a second conducting rail that are oriented parallel to each other as well as a direct current (DC) power supply that is connected to one end of each conducting rail. Two currents travel in opposite directions to each other through the first conducting rail and the second conducting rail. A sliding conductive armature bridges the gap in between the two conducting rails and remains in contact with the two conducting rails, completing the circuit. A projectile is placed in between the conducting rails and is driven by the conductive armature. The conductive armature may be integral to the projectile. Lorentz force is generated by the interaction between the electric current in the accelerated sliding armature and the magnetic induction field (B-field) generated by the flow of current in the closed loop. Because the electric current in the conductive armature and the B-field are oriented at a right angle relative to each other, the Lorentz force is maximized and oriented normal to the plane of electric current and B-field intensity. As such, the projectile is launched in a straight line parallel to the pair of conducting rails at a high muzzle velocity suitable for straight free flight.
Electromagnetic accelerators are particularly notable in military applications due to the much greater achievable muzzle velocities relative to conventional firearms using chemical propellants. However, there are several drawbacks that are inherent to the aforementioned mechanism used by conventional electromagnetic launchers. One such drawback is the energy loss and inefficiency due to mechanical friction between the conducting rails and the conductive armature, electric arcing due to increasing distance between the conducting rails, and thermal expansion of the conducting rails and the projectile. Proper heat dissipation is particularly important as well as extreme heat may result in degradation of equipment material and system failure during operation.
The present invention is a dynamic B-field accelerator that addresses the drawbacks that are inherent to conventional electromagnetic accelerators. The present invention eliminates the need for the conductive armature in between the conducting rails. In lieu of the conductive armature, the present invention implements a power supply and a solenoid coil with ferromagnetic core that are integrated into a projectile that is positioned in between a pair of conducting rails. Electric current within the conducting rails travels from the first conducting rail to the second conducting rail through an upper conducting sheet above the projectile and a lower conducting sheet below the projectile. The coil is offset by a short distance above the plane of the lower conducting sheet and a short distance below the plane of the upper conducting sheet, enabling the coil to move. Lorentz force is generated by the interaction of the current in the conducting sheet directly under the coil with the central B-field generated by the current within the coil. External magnetic induction outside the coil is present in the opposite direction to the central B-field. However, the central B-field is much stronger than the external magnetic induction, in essence negating the external magnetic induction in both force and direction.
All illustrations of the drawings are for the purpose of describing selected versions of the present invention and are not intended to limit the scope of the present invention.
The present invention is an electromagnetic tube gun for creating projectile motion through Lorentz force. With reference to
This magnetic field B in the magnetic field induction coil 3 is oriented normal to the cross current Ic and therefore, the magnetic field B generated by the magnetic field induction coil 3 is able to interact with the cross current Ic in order to generate a Lorentz force for launching a projectile.
The first conductive rail 1 and the second conductive rail 2 are positioned parallel to each other. As such, a Lorentz force generated from the interaction between the cross current Ic and the magnetic field B in the magnetic field induction coil 3 is oriented parallel to the first conductive rail 1 and the second conductive rail 2. This allows a projectile driven by the movement of the magnetic field induction coil 3 to travel freely in between the first conductive rail 1 and the second conductive rail 2. The magnetic field induction coil 3 is positioned offset from the at least one conductive sheet 4, enabling the magnetic field induction coil 3 to freely move. The magnetic field induction coil 3 is positioned in between the first conductive rail 1 and the second conductive rail 2 in order to allow the magnetic field induction coil 3 to move parallel to the first conductive rail 1 and the second conductive rail 2 due to the Lorentz force.
As shown in
Again with reference to
The present invention further comprises a projectile case 8 as shown in
In order to generate a Lorentz force, magnetic field B must be generated in the magnetic field induction coil 3. As such, the present invention further comprises a coil power supply 9. The coil power supply 9 provides DC electrical power to the magnetic field induction coil 3. In the preferred embodiment of the present invention, the projectile is a self-contained unit and, as such, the coil power supply 9 is mounted within the projectile case 8. The coil power supply 9 is electrically connected to the magnetic field induction coil 3 in order to drive the third electrical current I3 through the magnetic field induction coil 3 and consequently generate the magnetic field B.
The present invention further comprises a firing assembly 11 that initiates the projectile launching process. The firing assembly 11 comprises an ultra capacitor 12, a first spring 13, a second spring 14, a push rod 15, a first electrical contact 16, and a second electrical contact 17. The first spring 13 and the second spring 14 are laterally mounted within the projectile case 8 in order to position the components of the firing assembly 11 within the self-contained unit of the projectile. The first spring 13 and the second spring 14 are oriented towards each other. Additionally, the first electrical contact 16 is mounted adjacent to the first spring 13, opposite the projectile case 8, while the second electrical contact 17 is mounted adjacent to the second spring 14, opposite the projectile case 8. This allows the first spring 13 and the second spring 14 to push the first electrical contact 16 and the second electrical contact 17 toward each other. The push rod 15 is slidably positioned in between the first electrical contact 16 and the second electrical contact 17. The push rod 15 serves to separate the first electrical contact 16 and the second electrical contact 17 prior to launching the projectile in order to prevent completing the circuit for the magnetic field induction coil 3. The push rod 15 may be slid out of place from in between the first electrical contact 16 and the second electrical contact 17 in order to allow the first electrical contact 16 to come into contact with the second electrical contact 17 and complete the circuit for the magnetic field induction coil 3. The push rod 15 partially traverses out of the projectile case 8 in order to allow the push rod 15 to be actuated from outside the projectile case 8.
Typically, a very large current is required in order to accelerate the projectile to the desired velocity. The ultra capacitor 12 is suitable for this application as the present invention requires a large amount of power for a short period of time. The ultra capacitor 12 stores and releases the very large amount of energy required to launch the projectile. In the preferred embodiment of the present invention, the ultra capacitor 12 and the magnetic field induction coil 3 are electrically connected in series between the first electrical contact 16 and the second electrical contact 17. This allows the first electrical contact 16, the second electrical contact 17, the ultra capacitor 12, and the magnetic field induction coil 3 to form a circuit that, when completed, generates a magnetic field B that interacts with the cross current Ic. The resulting Lorentz force causes the projectile to rapidly accelerate.
The present invention further comprises a pneumatic cylinder 19 that is utilized to actuate the push rod 15 and initiate the launch process. The pneumatic cylinder 19 is externally positioned to the projectile case 8 and thus may be utilized to launch multiple projectiles. A plunger 20 of the pneumatic cylinder 19 is pressed against the push rod 15. The pneumatic cylinder 19 is able to generate a reciprocating motion that forces the push rod 15 to slide from between the first electrical contact 16 and the second electrical contact 17, completing the circuit and launching the projectile.
With reference to
The first electrical contact 16, the second electrical contact 17, and the push rod 15 are shown in a fired configuration in
With reference to
The plurality of guide tracks 25 is internally connected along the launch tube 21 in order to guide the projectile case 8 along the length of the launch tube 21 prior to the projectile case 8 exiting the launch tube 21. The plurality of guide tracks 25 is radially distributed about the launch tube 21 as well in order to secure the projectile case 8 to the plurality of guide tracks 25 at multiple points. The plurality of guide fins 24 is externally connected along the projectile case 8 and are additionally radially distributed about the projectile case 8. The plurality of guide fins 24 is configured to correspond to the plurality of guide tracks 25. Each of the plurality of guide fins 24 is engaged to a corresponding track from the plurality of guide tracks 25. This allows the plurality of guide fins 24 to slide along the plurality of guide tracks 25, thus enabling the projectile case 8 to slide within the launch tube 21.
The launch tube 21 comprises a closed end 22 and a muzzle end 23 that are opposing ends of the launch tube 21. The muzzle end 23 is the end of the launch tube 21 through which the projectile case 8 exits the launch tube 21. The pneumatic cylinder 19 is mounted within the launch tube 21, adjacent to the closed end 22. This enables the pneumatic cylinder 19 to engage the firing assembly 11 without impeding the path of the projectile case 8 after the Lorentz force is generated. In the preferred embodiment of the present invention, the pneumatic cylinder 19 utilizes compressed gas to produce a reciprocating linear force in order to move a piston toward the push rod 15. As such, the projectile case 8 is positioned in between the pneumatic cylinder 19 and the muzzle end 23. Once the push rod 15 is actuated by the force of the pneumatic cylinder 19, the first electrical contact 16 and the second electrical contact 17 are electrically connected and the circuit is completed. The interaction between the magnetic field B and the cross current Ic generates the Lorentz force that propels the projectile case 8 along the plurality of guide tracks 25 through the launch tube 21.
Although the present invention has been explained in relation to its preferred embodiment, it is understood that many other possible modifications and variations can be made without departing from the spirit and scope of the present invention as hereinafter claimed.
The current application claims a priority to the U.S. Provisional Patent application Ser. No. 61/989,638 filed on May 7, 2014.
Number | Date | Country | |
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61989638 | May 2014 | US |