Patent classifications
F41B6/00
Device, method and energy product-by-process for launching magnetic projectiles and motivating linear and rotational motion, using permanent magnets or magnetized bodies
A magnetic apparatus and related method and energy product-by-process to motivate linear or rotational motion, comprising: at least one magnet ring tier comprising a ring of a plurality of permanent magnets; a central core comprising a permanent magnet projectile movement channel, an axis of the channel aligned in a direction normal to a geometric plane defined by the magnet ring, and running through a geometric center of the magnet ring; and each of the permanent magnets mounted in the ring at a mount angle thereof, with the components of their polar alignments parallel to the central core all oriented in the same direction; wherein: if the polar alignment of a permanent magnet projectile was introduced with a particular duality-dependent orientation into the permanent magnet projectile movement channel, the magnetic forces between the ring magnets and the projectile would be capable of motivating the permanent magnet projectile relative to the channel.
Device, method and energy product-by-process for launching magnetic projectiles and motivating linear and rotational motion, using permanent magnets or magnetized bodies
A magnetic apparatus and related method and energy product-by-process to motivate linear or rotational motion, comprising: at least one magnet ring tier comprising a ring of a plurality of permanent magnets; a central core comprising a permanent magnet projectile movement channel, an axis of the channel aligned in a direction normal to a geometric plane defined by the magnet ring, and running through a geometric center of the magnet ring; and each of the permanent magnets mounted in the ring at a mount angle thereof, with the components of their polar alignments parallel to the central core all oriented in the same direction; wherein: if the polar alignment of a permanent magnet projectile was introduced with a particular duality-dependent orientation into the permanent magnet projectile movement channel, the magnetic forces between the ring magnets and the projectile would be capable of motivating the permanent magnet projectile relative to the channel.
ELECTROMECHANICAL GUN
The present disclosure provides systems, devices, and techniques that can be implemented at a gun, such as an electromechanical gun. The gun may include a barrel located within a slide and a cylindrical spring enveloping the barrel. The barrel may be configured to act as a guide rod for the cylindrical spring, and the cylindrical spring may be configured to bias the slide in a forward battery position. The gun may include an electronic component such as an energy store, a processor, or a circuit board, located under the barrel and forward of the trigger when the gun is in an upright position. The gun may include a physical transmission medium that electronically couples the electronic component with an additional electronic component located rearward of the trigger, and the physical transmission medium may be at least partially encapsulated by a trigger guard.
Electromechanical gun
The present disclosure provides systems, devices, and techniques that can be implemented at a gun, such as an electromechanical gun. The gun may include a barrel located within a slide and a cylindrical spring enveloping the barrel. The barrel may be configured to act as a guide rod for the cylindrical spring, and the cylindrical spring may be configured to bias the slide in a forward battery position. The gun may include an electronic component such as an energy store, a processor, or a circuit board, located under the barrel and forward of the trigger when the gun is in an upright position. The gun may include a physical transmission medium that electronically couples the electronic component with an additional electronic component located rearward of the trigger, and the physical transmission medium may be at least partially encapsulated by a trigger guard.
ELECTROMAGNETIC LAUNCHER WITH SPIRAL GUIDEWAY
An electromagnetic launcher with a curved or spiral-shaped, open-ended guideway and conductors for launching a projectile. The projectile, movably retained on or within the guideway, is accelerated along the guideway using electromagnetic forces until it reaches an end of the guideway, then the projectile is launched in a desired direction. The direction of the launch of the projectile is determined by orienting the guideway in the desired direction using an actuator.
AUTONOMOUS AUTOMATIC ELECTROMAGNETIC LAUNCH SYSTEM WITH ADJUSTABLE LAUNCH VELOCITY, LOW RECOIL FORCE, LOW ACOUSTIC REPORT, AND LOW VISIBLE AND INFRA-RED SIGNATURE
Apparatus for electromagnetic launching system for the linear acceleration of macro particles. The apparatus disclosed is autonomously-powered, compact, and lightweight. The apparatus disclosed has low recoil force, low acoustic report, and low visible and infra-red signature. The apparatus disclosed is capable of automatic operation and the maximum particle velocity can be adjusted. The apparatus disclosed includes a trigger, controller, component power source, particle container, particle loader, propellant container, propellant loader, igniter, combustion chamber, sound suppressor, linear electrical generator, linear electrical motor, and thermal barrier.
Hybrid propellant electromagnetic gun system
A hybrid gun device composed of two barrels (1,10) that accept energy from combustion of standard propellant (6), one barrel (10) being operative to produce a high intensity electric current to add accelerating energy to a projectile (7) in the second barrel (1) and at least one coil (8) stage to convert energy between electrical and kinetic to cause the projectile (7) to be launched at hypervelocity.
Electromagnetic rifle with compact armature
An EM driver for accelerating an object may be configured as an EM rifle for accelerating, rotating to spin-stabilize, and releasing a projectile. A core includes a stator coil, forward and reverse coils, a railed shaft, and a transfer shaft. The stator coil generates a first EM field, and the forward and reverse coils generate second and third EM fields which interact with the first EM field to accelerate the armature in forward and reverse directions, respectively. The railed shaft is elongated along a central axis through the armature and includes multiple rails arranged helically around a central shaft. The armature remains in contact with the rails during acceleration so as to impart a turning motion. The transfer shaft is physically coupled with and projects forwardly from the armature and transfers to the projectile the acceleration and the turning motion of the armature in the forward direction.
Linear motor based on radial magnetic tubes
A liner motor based on radical magnetic tubes includes: a dynamicer (mover, QDZ) and a stator (STA), the structure of the stator (STA) is: a stator magnetic tube (SCG) is nested into the inner wall of a pure iron tube (DTG), the stator magnetic tube (SCG) provides a radial magnetic field, a stator tube (DZGD) is formed within the stator magnetic tube (SCG), the dynamicer can travel in the stator tube; the dynamicer iron core is a tube of a radial magnetic field and installed on a tubular coil skeleton, on which winding the dynamicer coil to form the dynamicer main body; the sliders (HDZ) are installed on both ends of the dynamicer main body load.
Relay based system to launch a projectile
A series of the relay of the electromagnetic launcher with a gun and a floating launch platform to launch projectiles in space, wherein the projectile is accelerated along a path using electromagnetic force until the projectile reaches a desired direction and position. The direction of the path is determined by orienting the path in the desired direction using a catcher. the catcher and rail gun projectile as high above as possible, coming close to near space. When the said projectile will reach the last platform, it will be launched by the railgun and ignite its rocket engine to take the payload in space or as required to eliminate the need for large rocket boosters to launch the projectile.