CN110645829A - Annular accelerating missile electromagnetic gun - Google Patents

Abstract

An annular accelerating missile electromagnetic gun comprises an electric gun wheel, a hub type speed reducing motor, an annular baffle, an annular steel plate, an electromagnetic switch, an advance switch, an infrared transmitting head, an infrared receiving head, an intelligent controller, an annular gun bore, a spherical missile and an electromagnetic annular accelerator, wherein the electromagnetic annular accelerator consists of 6 same single electromagnetic drivers, after the power of the annular accelerator is increased, the spherical shell rotates more and more quickly, a shell outlet at the head end and the tail end of the annular steel plate is opened in advance instantaneously, the spherical shell flies out from the outlet by virtue of strong centrifugal force, so that the linear flight at ultra-high pitch speed is realized and then flies according to a trajectory track, the spherical missile automatically becomes the shell head, a square extending pipe becomes a shell body, a plurality of sensors search and lock a target together, a control signal is sent to the intelligent controller, and vertical wings and horizontal wings are controlled to change the flight direction of, the target is automatically tracked.

Description

Annular accelerating missile electromagnetic gun

Technical Field

The invention relates to the technical field of electromagnetic coil guns, in particular to an annular accelerating missile electromagnetic gun.

Background

The electromagnetic gun technology is divided into an electromagnetic rail gun and an electromagnetic coil gun, compared with the traditional gunpowder gun, the electromagnetic gun has the advantages of high projectile speed and long shooting range, the electromagnetic rail gun technology in China is at the world leading level at present, and the electromagnetic rail gun is encouraged to be equipped on a military warship in China to be tested successfully.

At present, some military strong countries including the United states do not equip the electromagnetic orbital cannon on a military warship and are only in the research and experiment stage, because the electromagnetic orbital cannon has the defects that: the electromagnetic cannonball of the prior art moves in the length of the limited electrified guide rail, and the high speed is accelerated in a short time and the difficulty is high.

Disclosure of Invention

In order to overcome the defects of the existing electromagnetic rail gun, the invention discloses a brushless annular electromagnetic accelerating electromagnetic gun for launching missiles.

The annular accelerating missile electromagnetic gun mainly comprises an electric gun wheel, a hub type speed reducing motor, an annular baffle, an annular steel plate, a spherical missile, an electromagnetic switch, an electromagnetic annular accelerator, a lead switch, an infrared transmitting head, an infrared receiving head, an intelligent controller, a convex base, a U-shaped support, a sliding ring, an electric brush and a missile launching operation platform, and is characterized in that: the annular accelerating missile electromagnetic gun is provided with an electric gun wheel, the center of the electric gun wheel is provided with a hub type speed reducing motor, the shell of the hub type speed reducing motor is provided with a left end cover and a right end cover, the left end cover is provided with a high circular platform, the excircle of the high circular platform is provided with a left annular baffle, the left annular baffle is fixed on the left end cover by 4 screws, the right end cover is provided with a low circular platform, the excircle of the low circular platform is provided with a right annular baffle, the right annular baffle is fixed on the right end cover by 4 screws, an annular steel plate is arranged between the left annular baffle and the right annular baffle, the annular steel plate is an annular spring processed by an elastic steel plate, the inner circle of the right view of the annular steel plate is a closed circle in an original state without stress, the head end of the annular steel plate is provided with an upper connecting hole and a lower screw hole, the left annular baffle and the right annular baffle are respectively provided with an upper connecting, the left annular baffle, the annular steel plate and the right annular baffle are fastened into an integrated annular barrel by upper screws and lower screws, the annular barrel and the hub type speed reducing motor are integrated to form an electric barrel wheel, the width of the annular barrel is equal to that of the annular steel plate and equal to that between a left end cover and a right end cover of a shell of the hub type speed reducing motor, a spherical missile is arranged in the inner circle of the annular barrel and is a deformable iron ball, the diameter of the spherical missile is slightly smaller than that of the annular steel plate, the spherical missile can roll along the inner circle of the annular steel plate between the left annular baffle and the right annular baffle, a round inlet of the spherical missile is arranged on the right annular baffle, the head end of the annular steel plate is thicker, the tail end of the annular steel plate is gradually thinner, when the head end and the tail end of the annular steel plate are subjected to external force in the horizontal direction, the head end and the tail end are in an open, the opening between the head end and the tail end is set as an outlet of a spherical missile, after external force of the head end and the tail end of the annular steel plate disappears, the inner circle of the annular steel plate restores to be closed round, the left annular baffle and the right annular baffle are made of high-strength plastics, the front ends of the left annular baffle and the right annular baffle are respectively provided with a track groove, the left track groove and the right track groove are equal in size and are bilaterally symmetrical, the tail end of the annular steel plate is provided with a left sliding shaft and a right sliding shaft, the left sliding shaft and the right sliding shaft are equal in size and are bilaterally symmetrical, the left sliding shaft is arranged in the left track groove, the right sliding shaft is arranged in the right track groove, the left end of the left annular baffle is provided with a left electromagnetic switch, the right end of the right annular baffle is provided with a right electromagnetic switch, the left electromagnetic switch and the right electromagnetic switch are equal in size and, the electromagnetic switch comprises an iron-absorbing coil, an annular magnetic conduction cover is arranged at the front end of a coil framework and welded with a magnetic conduction cylinder into a whole, the inner circle of the annular magnetic conduction cover is consistent with the inner circle of the coil framework, the magnetic conduction cylinder is provided with an upper connection lug and a lower connection lug, the outer ends of a left annular baffle and a right annular baffle are respectively provided with an upper screw rod and a lower screw rod, the upper connection lug and the lower connection lug are fixed by an upper screw cap and a lower screw cap, a left electromagnetic switch is fixed at the left end of the left annular baffle, a right electromagnetic switch is fixed at the right end of the right annular baffle, the inner circle of the annular magnetic conduction cover and the inner circle of the coil framework are provided with a sliding iron core, the front end of the sliding iron core is provided with a connection hole, the connection hole of the left sliding iron core of the left electromagnetic switch is connected with a left sliding shaft, the connection hole of the right sliding iron core of the, the left sliding shaft and the right sliding shaft are instantaneously pulled to the rear ends of the left track groove and the right track groove, the tail end of the annular steel plate is pulled, the head end and the tail end of the annular steel plate are opened, when the iron-attracting coils of the left electromagnetic switch and the right electromagnetic switch are simultaneously powered off, the left sliding iron core and the right sliding iron core lose magnetic force, the restoring elastic force of the annular steel plate instantaneously pulls the left sliding shaft and the right sliding shaft to the front ends of the left track groove and the right track groove respectively, the left sliding iron core and the right sliding iron core are simultaneously pulled to the front ends of the left iron-attracting coil and the right iron-attracting coil, the head end and the tail end of the annular steel plate are closed, and the inner circle of the; the electric gun wheel is provided with a central wheel shaft, the central wheel shaft and the central shaft of a hub type speed reducing motor are the same shaft, the central wheel shaft is concentric with a left annular baffle plate and a right annular baffle plate, the left end and the right end of the central wheel shaft are respectively provided with 2 parallel screw caps, the electric gun wheel is provided with a U-shaped bracket, the left parallel screw cap fixes the left end of the central wheel shaft at the upper left end of the U-shaped bracket, the right parallel screw cap fixes the right end of the central wheel shaft at the upper right end of the U-shaped bracket, the lower end of the U-shaped bracket is connected with a large rotating disc, the lower end of the large rotating disc is welded with an inner gear ring, the center of the large rotating disc is provided with a vertical shaft, the electric gun wheel is provided with a convex base, the vertical shaft is arranged in a central hole of the convex base, the front end of the convex base is provided with a steering motor, the upper, the hub type speed reducing motor is a harmonic speed reducing motor with a large speed reducing ratio, a harmonic speed reducer is arranged in the middle of the hub type speed reducing motor, an outer rotor brushless permanent magnet motor is arranged on the periphery of the harmonic speed reducer, the rotating speed of the hub type speed reducing motor is very low, the electric gun wheel is driven to rotate up and down in the elevation angle range in the vertical direction during forward and reverse rotation, the hub type speed reducing motor is in a starting state of an annular accelerating missile electromagnetic gun during clockwise rotation, a connecting ring is arranged in the center of a low circular table of a right end cover of the hub type speed reducing motor, an insulating sleeve is arranged on the excircle of the connecting ring, a left sliding ring and a right sliding ring are arranged on the excircle of the insulating sleeve, electric brushes are arranged at the lower ends of the left and right sliding rings, a carbon brush frame is arranged at the left end of a right support of a U-shaped support and is fastened by upper and lower screws, a left carbon brush, the upper ends of the left spring and the right spring are provided with a left carbon brush and a right carbon brush, the lower ends of the left carbon brush and the right carbon brush are respectively provided with a lead, the left carbon brush and the right carbon brush are respectively tightly attached to the left sliding ring and the right sliding ring under the pressure of the springs, the upper end of the hub type speed reducing motor shell is provided with a first intelligent controller, and a wireless signal transmitting and receiving module, a brushless motor control module, an electromagnetic driving control module, a shell speed sensing conversion module, a horizontal steering angle sensing conversion module and an elevation angle sensing conversion module in the vertical direction are arranged in the first intelligent controller; the annular accelerating missile electromagnetic gun is provided with a missile launching operation table, a data information display, a power supply button, a horizontal steering button, an elevation steering button, a starting button, an accelerating button and a launching button are arranged on the missile launching operation table, an intelligent controller II and an adjustable direct-current power supply are arranged in the missile launching operation table, a wireless signal transmitting and receiving module and a brushless motor control module are arranged in the intelligent controller II, wherein the output ends of the horizontal steering button, the elevation steering button, the starting button and the launching button are respectively connected with the relevant input ends of the wireless signal transmitting and receiving module in the intelligent controller II, the wireless signal of the intelligent controller II is transmitted to the relevant input end of the wireless signal transmitting and receiving module in the intelligent controller I, and the adjustable direct-current power supply input end in the missile launching operation table is connected with a generator power supply with common power, the adjustable direct current power supply is a switching power supply and supplies power to the annular accelerating missile electromagnetic gun, the accelerating button is connected with the control input end of the adjustable direct current power supply, the voltage of the adjustable direct current power supply is adjusted, the positive and negative output ends of the adjustable direct current power supply are respectively connected with the lead of the left carbon brush and the lead of the right carbon brush, the left carbon brush and the right carbon brush are connected with the left slip ring and the right slip ring, the left slip ring and the right slip ring are respectively welded with a power transmission line, the power transmission line is led out through a wire groove of an insulating sleeve, the right annular baffle is provided with a threading hole, the power transmission line is connected with the power supply end of the intelligent controller I through the threading hole, and the output end of the brushless motor; the electromagnetic ring accelerator is composed of 6 same single electromagnetic drivers, each single electromagnetic driver is composed of a left electromagnetic coil, a right electromagnetic coil, an infrared transmitting head I, an infrared receiving head I, an infrared transmitting head II, an infrared receiving head II and a bistable switch circuit, a left annular baffle circular surface of the electric gun wheel is provided with a left setting circle, the left setting circle is provided with 6 equally divided left electromagnetic coils, the right annular baffle circular surface is provided with a right setting circle, the right setting circle is provided with 6 equally divided right electromagnetic coils, the left setting circle and the right setting circle are equal, the setting circle is concentric with an inner circle of a closed annular steel plate, the diameter difference between the diameter of the inner circle of the closed annular steel plate and the diameter of the setting circle is equal to the diameter of the spherical missile, the setting circle is concentric with the left annular baffle and the right annular baffle, each electromagnetic coil is provided with a cylindrical iron core, a coil framework is installed on the outer circle of, the setting circles of the left annular baffle and the right annular baffle are respectively provided with 6 equal mounting holes, 12 electromagnetic coils are respectively mounted in the mounting holes, the 6 mounting holes of the left annular baffle are mutually aligned with the 6 mounting holes of the right annular baffle, the excircles of 12 cylindrical iron cores are respectively mounted in the 12 mounting holes in a tight fit manner, the right end plane of the left annular baffle is consistent with the right end planes of the 6 cylindrical iron cores, the left end plane of the right annular baffle is consistent with the left end planes of the 6 cylindrical iron cores, the centers of the 6 cylindrical iron cores of the left annular baffle are respectively provided with a transmitting hole, an infrared transmitting head I is mounted in each 6 transmitting holes, the centers of the 6 cylindrical iron cores of the right annular baffle are respectively provided with a receiving hole, an infrared receiving head I is mounted in each 6 receiving hole, the 6 infrared transmitting heads I are mutually aligned with the 6 infrared receiving heads I, and on the setting circle of the left annular baffle, emitting holes are arranged between each electromagnetic coil and each electromagnetic coil, infrared emitting heads II are arranged in 6 emitting holes, on the set circle of the right annular baffle, a receiving hole is arranged between each electromagnetic coil and each electromagnetic coil, a second infrared receiving head is arranged in each 6 receiving holes, the 6 second infrared emitting heads and the 6 second infrared receiving heads are aligned with each other, in the intelligent controller I, 6 identical bistable switch circuits are arranged in the electromagnetic drive control module, the electromagnetic ring accelerator consists of 6 same single electromagnetic drivers, each single electromagnetic driver consists of a left electromagnetic coil, a right electromagnetic coil, an infrared transmitting head I, an infrared receiving head I, an infrared transmitting head II, an infrared receiving head II and a bistable switch circuit, the bistable switch circuit consists of a bistable trigger and a switch triode, and the circuit connection of the single electromagnetic driver is as follows: the input end I of the bistable trigger is connected with the infrared receiving end I, the input end II of the bistable trigger is connected with the infrared receiving end II, the output end of the switching triode is connected with the left electromagnetic coil and the right electromagnetic coil which are connected in parallel, the directions of the magnetic poles of the left electromagnetic coil and the right electromagnetic coil are consistent, the grounding end of the bistable switching circuit is connected with the negative pole of the adjustable direct-current power supply, and the power end of the bistable switching circuit is connected with the positive pole of the adjustable direct-; the electromagnetic ring accelerator is provided with an advance switch, an advance switch circuit is arranged in the electromagnetic drive control module, the advance switch circuit is provided with a monostable timer and a switch triode, and the circuit connection of the advance switch is as follows: the intelligent control device is characterized in that a transmitting hole is formed in a setting circle between two electromagnetic coils at the front end of a left annular baffle plate, a third infrared transmitting head is installed in the transmitting hole, a receiving hole is formed in a setting circle between two electromagnetic coils at the front end of a right annular baffle plate, a third infrared receiving head is installed in the receiving hole, the third infrared transmitting head is aligned to the third infrared receiving head, the monostable timer is a timer which is temporarily stable for a period of time, the third infrared receiving head is connected to the input end of the monostable timer, a left electromagnetic switch and a right electromagnetic switch which are connected in parallel are connected to the output end of a switch triode, a switch signal of a transmitting button is wirelessly transmitted to the relevant input end of a first intelligent controller, the third infrared receiving head is controlled by an output signal of the first intelligent controller, an adjustable direct-current power supply cathode is connected to a grounding end of a switch circuit in advance, an adjustable direct-current power supply anode is connected to a power The output line of the steering motor is connected with the output end of a brushless motor control module in the intelligent controller II, and wireless signal transmitting and receiving modules are respectively arranged in the intelligent controller I and the intelligent controller II and are used for realizing data information interconnection in an interactive communication mode so as to realize the wireless remote control of the electric cannon wheel by the missile launching console; the steering motor and the hub type speed reducing motor both belong to brushless permanent magnet motors, phase change pulses are generated during forward and reverse rotation, the frequency of the phase change pulses is in direct proportion to the rotating speed, the phase change pulses of the steering motor output data information of a horizontal steering angle to a display through a horizontal steering angle sensing conversion module, the phase change pulses of the hub type speed reducing motor output data information of an elevation steering angle to the display through an elevation sensing conversion module, coordinate information of a target is obtained according to detection and calculation means, a horizontal steering button and an elevation steering button are operated, the display displays the data information of the horizontal direction and the vertical direction of the electric gun wheel, the data information of the horizontal direction and the data information of the vertical direction of the electric gun wheel are aligned to the coordinate position of the target, and finally, an acceleration button and a; and finally, operating a starting button and a launching button to launch the missile.

The spherical missile is made of iron materials, the spherical missile is provided with a left hemisphere and a right hemisphere, the left hemisphere and the right hemisphere are combined and then welded into a sphere, the center of the spherical missile is provided with a square hole, a square pipe is installed in the square hole in a loose fit mode, the rear end of the square pipe is provided with a spherical end cover, the left hemisphere is provided with a left half-square hole, the right hemisphere is provided with a right half-square hole, the left half-square hole and the right half-square hole are combined into a square hole, the left end of the left half-square hole is provided with a left guide groove, the right end of the right half-square hole is provided with a right guide groove, the front end of the square pipe is provided with a sliding shaft, the left end of the sliding shaft is installed in the left guide groove, the right end of the sliding shaft is installed in the right guide groove, the square hole slides back and forth in the square hole, the sliding shaft slides back and forth in the range of the left guide groove and the right guide groove, the front end of the spring retaining frame is provided with a spring shaft, a reset spring is installed on the spring shaft, the lower end of a left half-square hole is provided with a left coil groove, the lower end of a right half-square hole is provided with a right coil groove, the left and right coil grooves are combined into a coil cavity, a coil framework is arranged in the coil cavity, an enameled wire is wound in the coil framework, a tapered electromagnetic coil is manufactured, a cylindrical iron core is arranged in the coil framework, a lock hole is arranged between a left hemisphere and a right hemisphere which are positioned at the lower end of the coil cavity, the lower end of a square tube is provided with a lock hole, when the lock hole is aligned with the cylindrical iron core, the cylindrical iron core slides upwards to enter the lock hole to be matched with the lock hole to lock the square tube, a left horizontal wing motor is arranged in the square tube, a left driving shaft is arranged in the center of the left horizontal wing motor, the square, the right driving shaft penetrates into the right shaft hole, the right driving shaft is provided with a right horizontal wing, the left horizontal wing and the right horizontal wing are the same in type and are bilaterally symmetrical, the front ends of the left horizontal wing and the right horizontal wing are provided with a vertical wing motor, the center of the vertical wing motor is provided with a vertical driving shaft, a square pipe is provided with an upper shaft hole and a lower shaft hole, the upper end and the lower end of the vertical driving shaft respectively penetrate into the upper shaft hole and the lower shaft hole, the upper end and the lower end of the vertical driving shaft are provided with an upper vertical wing and a lower vertical wing, the left horizontal wing motor and the vertical wing motor are harmonic reducer motors which are low-rotating-speed motors integrating a harmonic reducer and a permanent magnet motor, the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are all tail wings which are the same in size, the left horizontal wing motor and the right horizontal wing motor drive the left horizontal wing and the right, the rear end of the left half hole is provided with a left wing groove, the rear end of the right half hole is provided with a right wing groove, an upper wing groove is arranged between the left hemisphere and the right half ball which are positioned at the upper end of the square opening, a lower wing groove is arranged between the left hemisphere and the right half ball which are positioned at the lower end of the square opening, the square tube slides forwards, the reset spring is compressed, the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are respectively arranged in the left wing groove, the right wing groove, the upper wing groove and the lower wing groove, when a lock hole of the square tube is aligned with the cylindrical iron core, a steel bar penetrates into the lock hole to push the cylindrical iron core to slide upwards to enter the lock hole to lock the square tube in the square hole, the spherical surface at the rear end of the square tube and the rear ends of the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are all consistent with the spherical surface of the missile, so that the, the square tube is ejected backwards by the reset spring, so that the spherical missile becomes a warhead, the square tube becomes a missile body, the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing become missile tails, the front end in the square tube is provided with an intelligent control box, a gyro level sensor, a brushless motor control module and an intelligent control module are arranged in the intelligent control box, the rear end of the intelligent control box is provided with a storage battery box, the front end of the square hole of the spherical missile is provided with a round concave surface, a spherical surface end cover is embedded in the round concave surface, the center of the spherical surface end cover is provided with a camera hole, a camera is arranged in the camera hole, 4 sensor holes are arranged on the spherical surface end cover around the camera hole, an upper infrared sensor, a lower infrared sensor, a left laser radar sensor and a right laser radar sensor are respectively arranged in the 4 sensor holes, the lower end of the spherical surface end cover is provided, the upper end of the steel bar is magnetic, the steel bar triggers the Hall sensor to be in a switch-on or switch-off state when approaching the Hall sensor, the front end of the square tube is provided with a wire notch, a wire hole is arranged between the left hemisphere and the right hemisphere, the output line of the Hall sensor and the output line of the lock electromagnetic coil pass through the wire hole and the wire notch and the camera, the upper infrared sensor, the lower infrared sensor, the left laser radar, the right laser radar and the output line of the gyro level sensor are converged into a telescopic sensor cable, the sensor cable reaches the inside of the intelligent control box, the output line of each sensor is respectively connected with the related input end of the intelligent control module, a plurality of output ends of the brushless motor control module are respectively connected with the left horizontal wing motor, the right horizontal wing motor and the vertical wing motor, a plurality of output, Lock head solenoid and start indicator lamp.

The annular accelerating missile electromagnetic gun has the beneficial effects that: before the annular accelerating missile is loaded into the electromagnetic gun, a steel bar penetrates into a lock hole of the spherical missile to trigger a Hall sensor, a spherical missile power supply is turned on, a starting indicator lamp of the spherical missile is on, the spherical missile starts to work according to a control program, the spherical missile is loaded into the bottom of an annular gun bore from a circular inlet, an electric gun wheel rotates clockwise according to a starting button, the spherical missile rolls anticlockwise along the inner circle of the annular gun bore by virtue of gravity, when the spherical missile rolls to a position between an infrared emission head II and an infrared receiving head II to block infrared rays, the infrared receiving head II triggers an input end II of a bistable trigger, a switching triode outputs direct-current voltage to a left electromagnetic coil and a right electromagnetic coil which are connected in parallel, a magnetic field space between the left electromagnetic coil and the right electromagnetic coil attracts the spherical missile, when the spherical missile attracts to a position between the infrared emission head I of the, the spherical missile can automatically rotate around the annular accelerator after being attracted and accelerated for multiple times by a plurality of electromagnetic drivers, the intelligent controller controls the hub type speed reducing motor to stop rotating, the spherical missile is driven by the relay of the annular electromagnetic accelerator to be accelerated step by step and rotates in a circle of the annular gun bore repeatedly, and the rotating speed of the spherical missile can be increased to the limit without the limitation of distance and time and without large electric power; the mechanism for starting, aiming and launching the annular accelerating missile electromagnetic gun is simple and controllable, the horizontal steering button and the elevation steering button are operated to enable the missile outlet of the electric gun wheel to be aligned with a target, the accelerating button is pressed after the target is aligned to be determined, the voltage of an adjustable direct current power supply is increased, the power of the annular accelerator is increased, the rotating speed of the spherical missile is increased, the pulse frequency output by the infrared receiving head I represents the rotating speed of the spherical missile, the pulse output by the infrared receiving head I outputs the data information of the missile speed through the missile speed sensing conversion module and is transmitted to the display through radio, when the missile speed displayed on the display reaches ultrahigh sound speed, the infrared transmitting head III is remotely controlled to launch an infrared signal according to the launching button, when the spherical missile flies to the position between the infrared transmitting head III and the infrared receiving head III to block infrared rays, the infrared receiving head III triggers the input end of the monostable, the monostable trigger outputs a pulse trigger switch triode, the switch triode outputs direct current voltage which is temporarily stabilized for a period of time to a left electromagnetic switch and a right electromagnetic switch which are connected in parallel, the left electromagnetic switch and the right electromagnetic switch drive the tail end of an annular steel plate, the outlet of the missile is opened in advance, the spherical missile flies out from the outlet of the missile in the linear direction after flying for one circle, the time for the spherical missile to fly for one circle is longer than the time for the outlet of the missile to be opened completely, the spherical missile is ensured to pass through the outlet of the missile without obstacles, the switch triode is recovered to the cut-off state after the monostable trigger is temporarily stabilized for a period of time, the annular accelerating missile electromagnetic gun is stopped, the inner circle of the annular steel plate is recovered to be circular, the process is repeated when a second spherical missile is launched, the initial speed for the spherical missile to fly out from the outlet is equal to the accelerated linear, the linear flight at ultra-high pitch speed is realized, then the missile flies according to the trajectory by means of the inertia of the missile, when the missile flies to the highest stage, the gyro level sensor triggers the intelligent controller according to the change of the horizontal angle of the missile, the intelligent controller turns on the power supply of the electromagnetic coil of the lock head to dislocate the lock head, the reset spring ejects the square tube backwards to change the spherical missile into a bullet head and change the square tube into a missile body, the intelligent controller receives the instruction of the gyro level sensor to drive the left horizontal wing and the right horizontal wing to keep a horizontal state, the camera sends out a control signal of the flight direction to the intelligent controller according to the image information of the target, the upper infrared sensor and the lower infrared sensor according to the heat source information of the target, the left laser radar and the right laser radar jointly search and lock the target according to the reflection information of the target, and controls the upper, the spherical accelerating missile electromagnetic gun is suitable for being equipped on warships or land battle teams, and the spherical accelerating missile electromagnetic gun is large in mass, large in kinetic energy injury killing power and strong in penetrating power and is suitable for hitting targets in the air, on the sea or on the land.

Drawings

Fig. 1 is a right-view overall structure schematic diagram of an annular accelerating missile electromagnetic gun in a starting stage.

Fig. 2 is a right-view structural schematic diagram of the annular accelerating missile electromagnetic gun in a launching stage.

FIG. 3 is a schematic diagram of a rear view section structure of an annular accelerating missile electromagnetic gun.

FIG. 4 is an electrical schematic of a single electromagnetic actuator attracting a spherical missile.

FIG. 5 is an electrical schematic diagram of the advance switch of a spherical missile when blocking infrared rays.

Fig. 6 is a right structural schematic diagram of the opened flying state of the spherical missile.

FIG. 7 is a right view of the spherical missile in storage.

FIG. 8 is a rear view of a spherical missile.

FIG. 9 is a schematic view of the front view structure of a spherical missile.

Detailed Description

In the figures 1-6, the ring-shaped accelerating missile electromagnetic gun is provided with an electric gun wheel, the center of the electric gun wheel is provided with a hub-type speed reducing motor 1, the shell of the hub-type speed reducing motor is provided with a left end cover 2 and a right end cover 3, the left end cover is provided with a high round table 4, the excircle of the high round table is provided with a left ring-shaped baffle plate 5, the left ring-shaped baffle plate is fixed on the left end cover by 4 screws 6, the right end cover is provided with a low round table 7, the excircle of the low round table is provided with a right ring-shaped baffle plate 8, the right ring-shaped baffle plate is fixed on the right end cover by 4 screws 9, a ring-shaped steel plate 10 is arranged between the left ring-shaped baffle plate and the right ring-shaped baffle plate, the ring-shaped steel plate is a ring-shaped spring processed by an elastic steel plate, the inner circle of the right view of the ring-shaped steel plate is, the upper screw hole and the lower screw hole are respectively aligned with the upper connecting hole and the lower connecting hole, the left annular baffle, the annular steel plate and the right annular baffle are fastened into an integrated annular barrel 13 by the upper screw 11 and the lower screw 12, the annular barrel and the hub type speed reducing motor are integrated into an electric barrel, the width of the annular barrel is equal to that of the annular steel plate and equal to that between the left end cover and the right end cover of the shell of the hub type speed reducing motor, the inner circle of the annular barrel is provided with a spherical missile 14 which is a deformable iron ball, the diameter of the spherical missile is slightly smaller than that of the annular steel plate, so that the spherical missile can roll along the inner circle of the annular steel plate between the left annular baffle and the right annular baffle, the right annular baffle is provided with a circular inlet 15 of the spherical missile, the head end of the annular steel plate is thicker, the tail end is thinner gradually, when the head end and the tail end of the, the head and the tail ends are in an open state, the right view of the annular steel plate is in an involute shape of a circle, an opening between the head and the tail ends is provided with an outlet 16 of a spherical missile, after external force of the head and the tail ends of the annular steel plate disappears, the inner circle of the annular steel plate returns to a closed circle, the left annular baffle and the right annular baffle are made of high-strength plastics, the front ends of the left annular baffle and the right annular baffle are respectively provided with a track groove 17, the left track groove and the right track groove are equal in size and are bilaterally symmetrical, the tail end of the annular steel plate is provided with a left sliding shaft and a right sliding shaft 18, the left sliding shaft and the right sliding shaft are equal in size and are bilaterally symmetrical, the left sliding shaft is arranged in the left track groove, the right sliding shaft is arranged in the right track groove, the left end of the left annular baffle is provided with a left electromagnetic switch, the right end of the, the electromagnetic switch is provided with a magnetic conduction cylinder 19, a coil framework 20 is arranged in the magnetic conduction cylinder, enameled wires are wound in the coil framework to manufacture an iron-absorbing coil 21, the front end of the coil framework is provided with an annular magnetic conduction cover 22, the annular magnetic conduction cover and the magnetic conduction cylinder are welded into a whole, the inner circle of the annular magnetic conduction cover is consistent with the inner circle of the coil framework, the magnetic conduction cylinder is provided with an upper connecting lug 23 and a lower connecting lug 24, the outer ends of a left annular baffle plate and a right annular baffle plate are respectively provided with an upper screw rod and a lower screw rod, the upper connecting lug and the lower connecting lug are fixed by an upper screw cap 25 and a lower screw cap 26, a left electromagnetic switch is fixed at the left end of the left annular baffle plate, a right electromagnetic switch is fixed at the right end of the right annular baffle plate, the inner circle of the annular magnetic conduction cover and the inner circle of the coil framework are provided with a sliding iron, when the left and right iron attracting coils are simultaneously electrified, the left sliding iron core and the right sliding iron core are simultaneously attracted into the bottoms of the left iron attracting coil and the right iron attracting coil, the left sliding shaft and the right sliding shaft are instantly pulled to the rear ends of the left track groove and the right track groove, the tail end of the annular steel plate is pulled, the head end and the tail end of the annular steel plate are opened, when the iron attracting coils of the left electromagnetic switch and the right electromagnetic switch are simultaneously powered off, the left sliding iron core and the right sliding iron core lose magnetic force, the restoring elastic force of the annular steel plate instantly pulls the left sliding shaft and the right sliding shaft to the front ends of the left track groove and the right track groove respectively, the left sliding iron core and the right sliding iron core are simultaneously pulled to the front ends of the left iron attracting coil and the right iron attracting coil, the head end and the tail end of the annular steel plate are closed; the electric cannon wheel is provided with a central wheel shaft 28, the central wheel shaft and the central shaft of a hub type speed reducing motor are the same shaft, the central wheel shaft is concentric with a left annular baffle plate and a right annular baffle plate, the left end and the right end of the central wheel shaft are respectively provided with 2 parallel screw caps, the electric cannon wheel is provided with a U-shaped bracket 29, the left parallel screw caps 30 and 31 fix the left end of the central wheel shaft at the upper left end of the U-shaped bracket, the right parallel screw caps 32 and 33 fix the right end of the central wheel shaft at the upper right end of the U-shaped bracket, the lower end of the U-shaped bracket is connected with a large turntable 34, the lower end of the large turntable is welded with an inner gear ring 35, the center of the large turntable is provided with a vertical shaft 36, the center of the vertical shaft is provided with a wire hole 37, the electric cannon wheel is provided with a convex base 38, the vertical, the large turntable is driven to enable the electric gun wheel to turn left and right within 360 degrees in the horizontal direction when the steering motor rotates forwards and backwards, the hub type speed reducing motor is a harmonic speed reducing motor with a large speed reducing ratio, a harmonic speed reducer 41 is arranged in the middle of the hub type speed reducing motor, an outer rotor brushless permanent magnet motor 42 is arranged on the periphery of the harmonic speed reducer, the rotating speed of the hub type speed reducing motor is low, the electric gun wheel is driven to turn up and down within an elevation angle range in the vertical direction when the steering motor rotates forwards and backwards, and the hub type speed reducing motor rotates clockwise to enable the annular accelerating missile electromagnetic gun to be in a starting state; the center of the low circular platform of the right end cover of the hub type speed reducing motor is provided with a connecting ring 43, the excircle of the connecting ring is provided with an insulating sleeve 44, the excircle of the insulating sleeve is provided with a left sliding ring 45 and a right sliding ring 46, the lower ends of the left and right sliding rings are provided with electric brushes, the electric brushes are provided with carbon brush holders 47, the carbon brush holders are arranged at the left end of the right bracket of the U-shaped bracket and are fastened by upper and lower screws 48 and 49, a left carbon brush cavity and a right carbon brush cavity are arranged inside the carbon brush holders, a left spring 50 and a right spring 51 are arranged inside the left and right carbon brush cavities, a left carbon brush 52 and a right carbon brush 53 are arranged at the upper ends of the left and right springs, the lower ends of the left carbon brush and the right carbon brush are respectively provided with a power line 54, the power line is led out from the outside through a vertical shaft wire hole, the left and right carbon brushes are respectively tightly attached to the left sliding ring and the, The device comprises a brushless motor control module, an electromagnetic drive control module, a shell speed sensing conversion module, a horizontal steering angle sensing conversion module and an elevation angle sensing conversion module in the vertical direction; the annular accelerating missile electromagnetic gun is provided with a missile launching operation table 56, a data information display 57, a power supply button, a horizontal steering button, an elevation steering button, a starting button, an accelerating button and a launching button 58 are arranged on the missile launching operation table, an intelligent controller II 59 and an adjustable direct current power supply 60 are arranged in the missile launching operation table, a wireless signal transmitting and receiving module and a brushless motor control module are arranged in the intelligent controller II, wherein the output ends of the horizontal steering button, the elevation steering button, the starting button and the launching button are respectively connected with the relevant input ends of the wireless signal transmitting and receiving module in the intelligent controller II, the wireless signal of the intelligent controller II is transmitted to the relevant input ends of the wireless signal transmitting and receiving module in the intelligent controller I, the adjustable direct current power supply input end in the missile launching operation table is connected with a generator power supply with common power, the adjustable direct current power supply is a switching power supply and supplies power to the annular accelerating missile electromagnetic gun, the accelerating button is connected with the control input end of the adjustable direct current power supply, the voltage of the adjustable direct current power supply is adjusted, the positive and negative output ends of the adjustable direct current power supply are respectively connected with the power line of the left carbon brush and the power line of the right carbon brush, the left carbon brush and the right carbon brush are connected with the left slip ring and the right slip ring, the left slip ring and the right slip ring are respectively welded with the power transmission line 61, the power transmission line is led out through a wire groove of the insulating sleeve, the right annular baffle is provided with a threading hole 62, the power transmission line is connected with the power supply end of the intelligent controller I through the threading hole, and the output end of the; the electromagnetic ring accelerator consists of 6 same single electromagnetic drivers, each single electromagnetic driver consists of a left electromagnetic coil, a right electromagnetic coil, an infrared transmitting head I, an infrared receiving head I, an infrared transmitting head II, an infrared receiving head II and a bistable switch circuit, a left annular baffle circular surface of the electric gun wheel is provided with a left set circle, the left set circle is provided with 6 equally-divided left electromagnetic coils, the right annular baffle circular surface is provided with a right set circle 63, the right set circle is provided with 6 equally-divided right electromagnetic coils, the left set circle and the right set circle are equal, the set circle is concentric with the inner circle of a closed annular steel plate, the diameter difference between the diameter of the inner circle of the closed annular steel plate and the diameter of the set circle is equal to the diameter of the spherical missile, the set circle is concentric with the left annular baffle and the right annular baffle, each electromagnetic coil is provided with a cylindrical iron core 64, and the outer circle, enameled wires are wound in the coil framework, 6 equal mounting holes are formed in the set circles of the left annular baffle and the right annular baffle, 12 electromagnetic coils are mounted in the mounting holes respectively, the 6 mounting holes of the left annular baffle are aligned with the 6 mounting holes of the right annular baffle, the excircles of 12 cylindrical iron cores are mounted in the 12 mounting holes in a tight fit mode respectively, the right end plane of the left annular baffle is consistent with the right end planes of the 6 cylindrical iron cores, the left end plane of the right annular baffle is consistent with the left end planes of the 6 cylindrical iron cores, the centers of the 6 cylindrical iron cores of the left annular baffle are provided with transmitting holes, first infrared transmitting heads are mounted in the 6 transmitting holes, receiving holes are formed in the centers of the 6 cylindrical iron cores of the right annular baffle, first infrared receiving heads 65 are mounted in the 6 receiving holes, and the first 6 infrared transmitting heads are aligned with the 6 infrared receiving heads, on the setting circle of the left annular baffle, a transmitting hole is arranged between each electromagnetic coil and each electromagnetic coil, an infrared transmitting head II is arranged in 6 transmitting holes, a receiving hole is arranged on the setting circle of the right annular baffle, an infrared receiving head II 66 is arranged in 6 receiving holes, 6 infrared transmitting heads II and 6 infrared receiving heads II are aligned with each other, in the intelligent controller I, 6 identical bistable switch circuits are arranged in the electromagnetic drive control module, the electromagnetic annular accelerator consists of 6 identical single electromagnetic drivers, each single electromagnetic driver consists of a left electromagnetic coil, a right electromagnetic coil, an infrared transmitting head I, an infrared receiving head I, an infrared transmitting head II, an infrared receiving head II and a bistable switch circuit, and the bistable switch circuit consists of a bistable trigger and a switching triode, the circuit connections of the single electromagnetic driver are: the input end I of the bistable trigger 67 is connected with the infrared receiving end I65, the input end II of the bistable trigger is connected with the infrared receiving end II 66, the output end of the switching triode 68 is connected with the left electromagnetic coil 69 and the right electromagnetic coil 70 which are connected in parallel, the directions of the magnetic poles of the left electromagnetic coil and the right electromagnetic coil are consistent, the grounding end of the bistable switching circuit is connected with the negative pole of the adjustable direct-current power supply, and the power supply end 71 of the bistable switching circuit is connected with the positive pole of the adjustable direct-; the electromagnetic ring accelerator is provided with an advance switch, an advance switch circuit is arranged in the electromagnetic drive control module, the advance switch circuit is provided with a monostable timer and a switch triode, and the circuit connection of the advance switch is as follows: the infrared emission head III 72 is arranged in the emission hole, the receiving hole is arranged on the setting circle between the two electromagnetic coils at the front end of the left annular baffle plate, the infrared receiving head III 73 is arranged in the receiving hole, the infrared emission head III is aligned to the infrared receiving head III, the monostable timer 74 is a timer which is temporarily stable for a period of time, the input end of the monostable timer is connected with the infrared receiving head III, the output end of the switching triode 75 is connected with the left electromagnetic switch 76 and the right electromagnetic switch 77 which are connected in parallel, the switching signal of the emission button is wirelessly transmitted to the relevant input end of the intelligent controller I, the output signal of the intelligent controller I controls the infrared receiving head III, the grounding end of the advance switching circuit is connected with the cathode of the adjustable direct-current power supply, the power end 78 of the advance switching circuit is connected with the anode of the adjustable direct-current power supply, the output lines of the 6 infrared emission heads I and the 6 infrared emission heads II and the output line of the infrared emission head III are respectively connected with the relevant output end of the intelligent controller I, the output line of the steering motor is connected with the output end of the brushless motor control module in the intelligent controller II, wireless signal transmitting and receiving modules are respectively arranged in the intelligent controller I and the intelligent controller II, and the intelligent controller I and the intelligent controller II realize data information interconnection in an interactive communication mode, so that the missile launching console can wirelessly remotely control the electric gun wheel; the steering motor and the hub type speed reducing motor both belong to brushless permanent magnet motors, phase change pulses are generated during forward and reverse rotation, the frequency of the phase change pulses is in direct proportion to the rotating speed, the phase change pulses of the steering motor output data information of a horizontal steering angle to a display through a horizontal steering angle sensing conversion module, the phase change pulses of the hub type speed reducing motor output data information of an elevation steering angle to the display through an elevation sensing conversion module, coordinate information of a target is obtained according to detection and calculation means, a horizontal steering button and an elevation steering button are operated, the display displays the data information of the horizontal direction and the vertical direction of the electric gun wheel, the data information of the horizontal direction and the data information of the vertical direction of the electric gun wheel are aligned to the coordinate position of the target, and finally, an acceleration button and a.

In fig. 7-9, the spherical missile is made of ferrous material, the spherical missile is provided with a left hemisphere 79 and a right hemisphere 80, the left hemisphere and the right hemisphere are welded into a sphere after being combined, the center of the spherical missile is provided with a square hole, a square pipe 81 is loosely fitted in the square hole, the rear end of the square pipe is provided with a spherical end cover 82, the square hole is provided with a left half-square hole at the left hemisphere, the right hemisphere is provided with a right half-square hole, the left half-square hole and the right half-square hole are combined into a square hole, the left end of the left half-square hole is provided with a left guide groove 83, the right end of the right half-square hole is provided with a right guide groove 84, the front end of the square pipe is provided with a sliding shaft 85, the left end of the sliding shaft is arranged in the left guide groove, the sliding shaft is arranged in the right guide groove, the square pipe slides back and forth in the square hole, the sliding shaft slides back and forth in the left and right guide grooves, the left half, a return spring 86 is arranged in a spring hole, a spring baffle frame 87 is arranged at the upper end of the square tube, a spring shaft 88 is arranged at the front end of the spring baffle frame, the return spring is arranged on the spring shaft, a left coil groove is arranged at the lower end of the left half-square hole, a right coil groove is arranged at the lower end of the right half-square hole, the left and right coil grooves are combined into a coil cavity, a coil framework 89 is arranged in the coil cavity, an enameled wire is wound in the coil framework to manufacture a tapered electromagnetic coil 90, a cylindrical iron core 91 is arranged in the inner circle of the coil framework, a lock hole 92 is arranged between the left hemisphere and the right hemisphere at the lower end of the coil cavity, a lock hole 93 is arranged at the lower end of the square tube, when the lock hole is aligned with the cylindrical iron core, the cylindrical iron core slides upwards to enter the lock hole to lock the square tube, a left horizontal wing motor 94 is arranged in the square tube, the center of the right horizontal wing motor is provided with a right driving shaft 97, a square pipe is provided with a right shaft hole, the right driving shaft penetrates into the right shaft hole, the right driving shaft is provided with a right horizontal wing 98, the left and right horizontal wing motors have the same model and are bilaterally symmetrical, the front ends of the left and right horizontal wing motors are provided with a vertical wing motor 99, the center of the vertical wing motor is provided with a vertical driving shaft 100, the square pipe is provided with an upper shaft hole and a lower shaft hole, the upper end and the lower end of the vertical driving shaft respectively penetrate into the upper shaft hole and the lower shaft hole, the upper vertical wing 101 is arranged at the upper end of the vertical driving shaft, the lower vertical wing 102 is arranged at the lower end of the vertical driving shaft, the left and right horizontal wing motors and the vertical wing motor are harmonic reducer motors, the harmonic reducer motor is a low-speed motor with a harmonic reducer and a permanent magnet brushless motor, the left horizontal wing, the right horizontal wing, the upper vertical, when the vertical wing motor rotates forwards and backwards, the upper vertical wing and the lower vertical wing are driven to synchronously turn left and right, the rear end of the left half hole is provided with a left wing groove, the rear end of the right half hole is provided with a right wing groove, an upper wing groove is arranged between the left hemisphere and the right hemisphere which are positioned at the upper end of the square opening, a lower wing groove is arranged between the left hemisphere and the right hemisphere which are positioned at the lower end of the square opening, the square tube slides forwards, the reset spring is compressed, the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are respectively arranged in the left wing groove, the right wing groove, the upper wing groove and the lower wing groove, when a lock hole of the square tube is aligned with the cylindrical iron core, a steel bar penetrates into the lock hole to push the cylindrical iron core to slide upwards to enter the lock hole to lock the square tube, the rear end spherical surface of the square tube, the rear ends of the left horizontal wing, the right horizontal wing, the upper vertical wing, the cylindrical iron core is sucked into the lower end of the inner circle of the coil framework by electromagnetic force, the cylindrical iron core slides downwards to be separated from the keyhole, the return spring ejects the square tube backwards, the spherical missile becomes a warhead, the square tube becomes a missile body, and the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing become missile tails; the intelligent control box 103 is arranged at the front end in the square tube, the gyro level sensor, the brushless motor control module and the intelligent control module are arranged in the intelligent control box, the storage battery box 104 is arranged at the rear end of the intelligent control box, the round concave surface is arranged at the front end of the square hole of the spherical missile, the spherical end cover 105 is embedded in the round concave surface, the camera hole is arranged at the center of the spherical end cover, the camera 106 is arranged in the camera hole, 4 sensor holes are arranged on the spherical end cover around the camera hole, the upper infrared sensor 107, the lower infrared sensor 108, the left laser radar sensor 109 and the right laser radar sensor 110 are respectively arranged in the 4 sensor holes, the lower end of the spherical end cover is provided with an indicator lamp hole, the starting indicator lamp 111 is arranged in the indicator lamp hole, the hall sensor 112 is arranged at the front upper end of the lock hole, the upper end of the, square pipe front end is equipped with wire breach 113, be equipped with the line hole between left hemisphere and the right hemisphere, hall sensor's output line 114 and tapered end solenoid's output line 115 passes through line hole and wire breach and camera, go up infrared sensor, infrared sensor and left laser radar down, telescopic cable 116 is assembled into to right laser radar and top level sensor's output line, in the sensor cable reachs the intelligent control box, the output line of each sensor is connected with intelligent control module's relevant input respectively, left horizontal wing motor is connected respectively to a plurality of outputs of brushless motor control module, right horizontal wing motor and vertical wing motor, brushless motor control module input is connected respectively to a plurality of outputs of intelligent control module, tapered end solenoid and start indicator.

Before the annular accelerating missile is loaded into the electromagnetic gun, a steel bar penetrates into a lock hole of the spherical missile to trigger a Hall sensor, a spherical missile power supply is turned on, a starting indicator lamp of the spherical missile is on, the spherical missile starts to work according to a control program, the spherical missile is loaded into the bottom of an annular gun bore from a circular inlet, an electric gun wheel rotates clockwise according to a starting button, the spherical missile rolls anticlockwise along the inner circle of the annular gun bore by virtue of gravity, when the spherical missile rolls to a position between an infrared emission head II and an infrared receiving head II to block infrared rays, the infrared receiving head II triggers an input end II of a bistable trigger, a switching triode outputs direct-current voltage to a left electromagnetic coil and a right electromagnetic coil which are connected in parallel, a magnetic field space between the left electromagnetic coil and the right electromagnetic coil attracts the spherical missile, when the spherical missile attracts to a position between the infrared emission head I of the left, the spherical missile is triggered by a pulse of an infrared receiving head I, a switch triode is cut off, a left electromagnetic coil and a right electromagnetic coil are powered off, the spherical missile is separated from magnetic field force and continuously rotates anticlockwise by means of gravity and inertia, the spherical missile can automatically rotate around an annular accelerator after being attracted and accelerated for multiple times by a plurality of electromagnetic drivers, an intelligent controller I controls a hub type speed reducing motor to stop rotating, the spherical missile is driven by the relay of the annular electromagnetic accelerator to be continuously accelerated step by step and rotates in a circle of an annular gun bore repeatedly, and the rotation speed of the spherical missile can be increased to the limit without being limited by distance and time and needing large electric power; the mechanism for starting, aiming and launching the annular accelerating missile electromagnetic gun is simple and controllable, the horizontal steering button and the elevation steering button are operated to enable the missile outlet of the electric gun wheel to be aligned with a target, the accelerating button is pressed after the target is aligned to be determined, the voltage of an adjustable direct current power supply is increased, the power of the annular accelerator is increased, the rotating speed of the spherical missile is increased, the pulse frequency output by the infrared receiving head I represents the rotating speed of the spherical missile, the pulse output by the infrared receiving head I outputs the data information of the missile speed through the missile speed sensing conversion module and is transmitted to the display through radio, when the missile speed displayed on the display reaches ultrahigh sound speed, the infrared emitting head III is remotely controlled to launch an infrared signal according to the launching button, when the spherical missile flies to the position between the infrared emitting head III and the infrared receiving head III to block infrared rays, the infrared receiving head III triggers the input end of the monostable trigger, the monostable trigger outputs a pulse trigger switch triode, the switch triode outputs direct current voltage which is temporarily stabilized for a period of time to a left electromagnetic switch and a right electromagnetic switch which are connected in parallel, the left electromagnetic switch and the right electromagnetic switch drive the tail end of an annular steel plate, the outlet of the missile is opened in advance, the spherical missile flies out from the outlet of the missile in the linear direction after flying for one circle, the time for the spherical missile to fly for one circle is longer than the time for the outlet of the missile to be opened completely, the spherical missile is ensured to pass through the outlet of the missile without obstacles, the switch triode is recovered to the cut-off state after the monostable trigger is temporarily stabilized for a period of time, the annular accelerating missile electromagnetic gun is stopped, the inner circle of the annular steel plate is recovered to be circular, the process is repeated when a second spherical missile is launched, the initial speed for the spherical missile to fly out from the outlet is equal to the accelerated linear, the linear flight at ultra-high pitch speed is realized, then the missile flies according to the trajectory by means of the inertia of the missile, when the missile flies to the highest stage, the gyro level sensor triggers the intelligent controller according to the change of the horizontal angle of the missile, the intelligent controller turns on the power supply of the electromagnetic coil of the lock head to dislocate the lock head, the reset spring ejects the square tube backwards to change the spherical missile into a bullet head and change the square tube into a missile body, the intelligent controller receives the instruction of the gyro level sensor to drive the left horizontal wing and the right horizontal wing to keep a horizontal state, the camera sends out a control signal of the flight direction to the intelligent controller according to the image information of the target, the upper infrared sensor and the lower infrared sensor according to the heat source information of the target, the left laser radar and the right laser radar jointly search and lock the target according to the reflection information of the target, and controls the upper, the spherical accelerating missile electromagnetic gun is suitable for being equipped on warships or land battle teams, and the spherical accelerating missile electromagnetic gun is large in mass, large in kinetic energy injury killing power and strong in penetrating power and is suitable for hitting targets in the air, on the sea or on the land.

Claims (2)

1. The utility model provides an annular guided missile electromagnetism big gun that accelerates mainly comprises electronic barrel, wheel hub formula gear motor, ring baffle, annular steel sheet, spherical guided missile, electromagnetic switch, electromagnetism annular accelerator, advance switch, infrared emission head, infrared receiving head, intelligent control ware, convex base, U-shaped support, sliding ring, brush, guided missile transmission operation panel, its characterized in that: the annular accelerating missile electromagnetic gun is provided with an electric gun wheel, the center of the electric gun wheel is provided with a hub type speed reducing motor (1), the shell of the hub type speed reducing motor is provided with a left end cover (2) and a right end cover (3), the left end cover is provided with a high round table (4), the excircle of the high round table is provided with a left annular baffle plate (5), the left annular baffle plate is fixed on the left end cover by 4 screws (6), the right end cover is provided with a low round table (7), the excircle of the low round table is provided with a right annular baffle plate (8), the right annular baffle plate is fixed on the right end cover by 4 screws (9), an annular steel plate (10) is arranged between the left annular baffle plate and the right annular baffle plate, the annular steel plate is an annular spring processed by an elastic steel plate, the inner circle of the right view of the annular steel plate is closed and circular under the original state without stress, the head end of the annular steel plate is provided with an upper screw hole, the upper screw hole and the lower screw hole are respectively aligned with the upper connecting hole and the lower connecting hole, the left annular baffle, the annular steel plate and the right annular baffle are fastened into an integrated annular barrel (13) by the upper screw (11) and the lower screw (12), the annular barrel and the hub type speed reducing motor are integrated to form an electric barrel wheel, the width of the annular barrel is equal to that of the annular steel plate and equal to that between the left end cover and the right end cover of the shell of the hub type speed reducing motor, the inner circle of the annular barrel is provided with a spherical missile (14), the spherical missile is an iron ball capable of deforming, the diameter of the spherical missile is slightly smaller than that of the annular steel plate, so that the spherical missile can roll along the inner circle of the annular steel plate between the left annular baffle and the right annular baffle, the right annular baffle is provided with a circular inlet (15) of the spherical missile, the head end of the annular steel plate is thicker, and the tail end of the annular steel plate, the head and the tail ends are in an open state, the right view of the annular steel plate is in an involute shape of a circle, an opening between the head and the tail ends is provided with an outlet (16) of a spherical missile, after external force of the head and the tail ends of the annular steel plate disappears, the inner circle of the annular steel plate returns to a closed circle, the left annular baffle and the right annular baffle are made of high-strength plastics, the front ends of the left annular baffle and the right annular baffle are respectively provided with a track groove (17), the left track groove and the right track groove are equal in size and are bilaterally symmetrical, the tail end of the annular steel plate is provided with a left sliding shaft and a right sliding shaft (18), the left sliding shaft and the right sliding shaft are equal in size and are bilaterally symmetrical, the left sliding shaft is arranged in the left track groove, the right sliding shaft is arranged in the right track groove, the left end of the left annular baffle is provided with a left electromagnetic switch, the right end of, the electromagnetic switch is provided with a magnetic conduction cylinder (19), a coil framework (20) is arranged in the magnetic conduction cylinder, enameled wires are wound in the coil framework to manufacture an iron-absorbing coil (21), an annular magnetic conduction cover (22) is arranged at the front end of the coil framework and is welded with the magnetic conduction cylinder into a whole, the inner circle of the annular magnetic conduction cover is consistent with the inner circle of the coil framework, the magnetic conduction cylinder is provided with an upper connecting lug (23) and a lower connecting lug (24), the outer ends of a left annular baffle plate and a right annular baffle plate are respectively provided with an upper screw rod and a lower screw rod, the upper connecting lug and the lower connecting lug are fixed by an upper nut (25) and a lower nut (26), the left electromagnetic switch is fixed at the left end of the left annular baffle plate, the right electromagnetic switch is fixed at the right end of the right annular baffle plate, the inner circle of the annular magnetic conduction cover and the inner circle of the coil framework, the connecting hole of the right sliding iron core of the right electromagnetic switch is connected with a right sliding shaft, when the left and right iron attracting coils are simultaneously electrified, the left sliding iron core and the right sliding iron core are simultaneously sucked into the bottoms of the left iron attracting coil and the right iron attracting coil, the left sliding shaft and the right sliding shaft are instantly pulled to the rear ends of the left track groove and the right track groove, the tail end of the annular steel plate is pulled, the head end and the tail end of the annular steel plate are opened, when the iron attracting coils of the left and right electromagnetic switches are simultaneously powered off, the left sliding iron core and the right sliding iron core lose magnetic force, the restoring elastic force of the annular steel plate instantly pulls the left sliding shaft and the right sliding shaft to the front ends of the left track groove and the right track groove respectively, the left sliding iron core and the right sliding iron core are simultaneously pulled to the front ends of the left iron attracting coil and the right iron attracting coil, the head end and the tail end of the; the electric cannon wheel is provided with a central wheel shaft (28), the central wheel shaft and a central shaft of a hub type speed reducing motor are the same shaft, the central wheel shaft is concentric with a left annular baffle plate and a right annular baffle plate, the left end and the right end of the central wheel shaft are respectively provided with 2 parallel screw caps, the electric cannon wheel is provided with a U-shaped bracket (29), the left end of the central wheel shaft is fixed at the left upper end of the U-shaped bracket by the left parallel screw caps (30 and 31), the right end of the central wheel shaft is fixed at the right upper end of the U-shaped bracket by the right parallel screw caps (32 and 33), the lower end of the U-shaped bracket is connected with a large turntable (34), the lower end of the large turntable is welded with an inner gear ring (35), the center of the large turntable is provided with a vertical shaft (36), the center of the vertical shaft is provided with a wire hole (37), the small driving gear is meshed with the inner gear ring, the steering motor is a speed reduction brushless motor, the large turntable is driven to enable the electric gun wheel to steer left and right within 360 degrees in the horizontal direction when the steering motor rotates forwards and backwards, the hub type speed reduction motor is a harmonic speed reduction motor with a large speed reduction ratio, a harmonic speed reducer (41) is arranged in the middle of the hub type speed reduction motor, an outer rotor brushless permanent magnet motor (42) is arranged on the periphery of the harmonic speed reducer, the rotating speed of the hub type speed reduction motor is low, the electric gun wheel is driven to steer up and down within an elevation angle range in the vertical direction when the steering motor rotates forwards and backwards, and the hub type speed reduction motor is in a starting state of the annular accelerating electromagnetic; a connecting ring (43) is arranged at the center of a low circular truncated cone of a right end cover of the hub type speed reducing motor, an insulating sleeve (44) is arranged on the excircle of the connecting ring, a left sliding ring (45) and a right sliding ring (46) are arranged on the excircle of the insulating sleeve, electric brushes are arranged at the lower ends of the left and right sliding rings, the electric brushes are provided with carbon brush holders (47), the carbon brush holders are arranged at the left end of a right bracket of a U-shaped bracket and are fastened by upper and lower screws (48 and 49), a left carbon brush cavity and a right carbon brush cavity are arranged inside the carbon brush holders, a left spring (50) and a right spring (51) are arranged in the left and right carbon brush cavities, a left carbon brush (52) and a right carbon brush (53) are arranged at the upper ends of the left and right springs, a power wire (54) is respectively arranged at the lower ends of the left and right carbon brushes, the power wire is led out of the hub type speed reducing motor through a vertical shaft wire, a wireless signal transmitting and receiving module, a brushless motor control module, an electromagnetic driving control module, a shell speed sensing conversion module, a horizontal steering angle sensing conversion module and an elevation angle sensing conversion module in the vertical direction are arranged in the intelligent controller I; the annular accelerating missile electromagnetic gun is provided with a missile launching operation table (56), a data information display (57), a power supply button, a horizontal steering button, an elevation steering button, a starting button, an accelerating button and a launching button (58) are arranged on the missile launching operation table, a second intelligent controller (59) and an adjustable direct current power supply (60) are arranged in the missile launching operation table, a wireless signal transmitting and receiving module and a brushless motor control module are arranged in the second intelligent controller, wherein the output ends of the horizontal steering button, the elevation steering button, the starting button and the launching button are respectively connected with the relevant input ends of the wireless signal transmitting and receiving module in the second intelligent controller, the wireless signal of the second intelligent controller is transmitted to the relevant input ends of the wireless signal transmitting and receiving module in the first intelligent controller, the adjustable direct current power supply input end in the missile launching operation table is connected with a generator power supply with common power, the adjustable direct current power supply is a switching power supply and supplies power to the annular accelerating missile electromagnetic gun, the accelerating button is connected with the control input end of the adjustable direct current power supply, the voltage of the adjustable direct current power supply is adjusted, the positive and negative output ends of the adjustable direct current power supply are respectively connected with the power line of the left carbon brush and the power line of the right carbon brush, the left carbon brush and the right carbon brush are connected with the left slip ring and the right slip ring, the left slip ring and the right slip ring are respectively welded with a power transmission line (61), the power transmission line is led out through a wire groove of an insulating sleeve, the right annular baffle is provided with a threading hole (62), the power transmission line is connected with the power supply end of the first intelligent controller through the threading hole, and the output end of the; the electromagnetic ring accelerator is composed of 6 same single electromagnetic drivers, each single electromagnetic driver is composed of a left electromagnetic coil, a right electromagnetic coil, a first infrared emitting head, a first infrared receiving head, a second infrared emitting head, a second infrared receiving head and a bistable switch circuit, a left annular baffle circular surface of the electric gun wheel is provided with a left setting circle, the left setting circle is provided with 6 equally divided left electromagnetic coils, the right annular baffle circular surface is provided with a right setting circle (63), the right setting circle is provided with 6 equally divided right electromagnetic coils, the left setting circle and the right setting circle are equal, the setting circle is concentric with an inner circle of a closed annular steel plate and is concentric with the left annular baffle and the right annular baffle, the diameter difference between the diameter of the inner circle of the closed annular steel plate and the diameter of the setting circle is equal to the diameter of a sphere of the missile, each electromagnetic coil is provided with a cylindrical iron core (64), a coil framework is installed on the outer, the setting circles of the left annular baffle and the right annular baffle are respectively provided with 6 equal mounting holes, 12 electromagnetic coils are respectively mounted in the mounting holes, the 6 mounting holes of the left annular baffle are mutually aligned with the 6 mounting holes of the right annular baffle, the excircles of cylindrical iron cores of the 12 electromagnetic coils are respectively mounted in the 12 mounting holes in a tight fit manner, the right end plane of the left annular baffle is consistent with the right end planes of the 6 cylindrical iron cores, the left end plane of the right annular baffle is consistent with the left end planes of the 6 cylindrical iron cores, the centers of the 6 cylindrical iron cores of the left annular baffle are respectively provided with a transmitting hole, a first infrared transmitting head is mounted in each 6 transmitting holes, the centers of the 6 cylindrical iron cores of the right annular baffle are respectively provided with a receiving hole, a first infrared receiving head (65) is mounted in each 6 receiving holes, the 6 first infrared transmitting heads are mutually aligned with the 6 first infrared receiving heads, the setting circle of the left annular baffle is arranged, all be equipped with the emission hole between each solenoid and the solenoid, all install infrared emission head two in 6 emission holes, on the setting circle of right ring baffle, all be equipped with the receiving hole between each solenoid and the solenoid, all install infrared receiving head two (66) in 6 receiving holes, 6 infrared emission head two and 6 infrared receiving head two align mutually, in intelligent control ware one, be equipped with 6 the same bistable switch circuit in the electromagnetic drive control module, bistable switch circuit comprises bistable trigger and switch triode, single electromagnetic drive's circuit connection is: the input end I of the bistable trigger (67) is connected with the infrared receiving end I (65), the input end II of the bistable trigger is connected with the infrared receiving end II (66), the output end of the switch triode (68) is connected with the left electromagnetic coil (69) and the right electromagnetic coil (70) which are connected in parallel, the magnetic pole directions of the left electromagnetic coil and the right electromagnetic coil are consistent, the grounding end of the bistable switch circuit is connected with the negative pole of the adjustable direct-current power supply, and the power supply end (71) of the bistable switch circuit is connected with the positive pole of the adjustable direct-current; the electromagnetic ring accelerator is provided with an advance switch, an advance switch circuit is arranged in the electromagnetic drive control module, the advance switch circuit is provided with a monostable timer and a switch triode, and the circuit connection of the advance switch is as follows: a transmitting hole is formed in a setting circle between two electromagnetic coils at the front end of the left annular baffle, a third infrared transmitting head (72) is installed in the transmitting hole, a receiving hole is formed in a setting circle between two electromagnetic coils at the front end of the right annular baffle, a third infrared receiving head (73) is installed in the receiving hole, the third infrared transmitting head is aligned with the third infrared receiving head, a monostable timer (74) is a timer which is temporarily stable for a period of time, the input end of the monostable timer is connected with the third infrared receiving head, the output end of a switching triode (75) is connected with a left electromagnetic switch (76) and a right electromagnetic switch (77) which are connected in parallel, a switching signal of a transmitting button is wirelessly transmitted to the relevant input end of a first intelligent controller, the third infrared receiving head is controlled by an output signal of the first intelligent controller, the grounding end of a lead switching circuit is connected with the negative electrode of an adjustable direct current power supply, the output lines of the 6 infrared emission heads I and the 6 infrared emission heads II and the output line of the infrared emission head III are respectively connected with the relevant output end of the intelligent controller I, the output line of the steering motor is connected with the output end of the brushless motor control module in the intelligent controller II, wireless signal transmitting and receiving modules are respectively arranged in the intelligent controller I and the intelligent controller II, and the intelligent controller I and the intelligent controller II realize data information interconnection in an interactive communication mode, so that the missile launching console can wirelessly remotely control the electric gun wheel; the steering motor and the hub type speed reducing motor both belong to brushless permanent magnet motors, phase change pulses are generated during forward and reverse rotation, the frequency of the phase change pulses is in direct proportion to the rotating speed, the phase change pulses of the steering motor output data information of a horizontal steering angle to a display through a horizontal steering angle sensing conversion module, the phase change pulses of the hub type speed reducing motor output data information of an elevation steering angle to the display through an elevation sensing conversion module, coordinate information of a target is obtained according to detection and calculation means, a horizontal steering button and an elevation steering button are operated, the display displays the data information of the horizontal direction and the vertical direction of the electric gun wheel, the data information of the horizontal direction and the data information of the vertical direction of the electric gun wheel are aligned to the coordinate position of the target, and finally, an acceleration button and a; the spherical missile is made of iron materials, the spherical missile is provided with a left hemisphere (79) and a right hemisphere (80), the left hemisphere and the right hemisphere are combined and then welded into a sphere, the center of the spherical missile is provided with a square hole, the square hole is loosely matched with a square pipe (81), the rear end of the square pipe is provided with a spherical end cover (82), the square hole is provided with a left half square hole at the left hemisphere, the right hemisphere is provided with a right half square hole, the left half square hole and the right half square hole are combined into a square hole, the left end of the left half square hole is provided with a left guide groove (83), the right end of the right half square hole is provided with a right guide groove (84), the front end of the square pipe is provided with a sliding shaft (85), the left end of the sliding shaft is arranged in the left guide groove, the sliding shaft is arranged in the right guide groove, the square pipe slides back and forth in the square hole, the sliding shaft slides back and forth in the range of the left guide groove and the right guide groove, the left, a reset spring (86) is arranged in the spring hole, a spring baffle frame (87) is arranged at the upper end of the square tube, a spring shaft (88) is arranged at the front end of the spring baffle frame, the reset spring is arranged on the spring shaft, a left coil groove is arranged at the lower end of the left half-square hole, a right coil groove is arranged at the lower end of the right half-square hole, the left and right coil grooves are combined into a coil cavity, a coil framework (89) is arranged in the coil cavity, enameled wires are wound in the coil framework to manufacture a lock electromagnetic coil (90), a cylindrical iron core (91) is arranged in the coil framework, a lock hole (92) is arranged between the left hemisphere and the right hemisphere which are positioned at the lower end of the coil cavity, a lock hole (93) is arranged at the lower end of the square tube, when the lock hole is aligned with the cylindrical iron core, the cylindrical iron core slides upwards to enter the lock, the left driving shaft is provided with a left horizontal wing (95), a right horizontal wing motor (96) is arranged in the square tube, the center of the right horizontal wing motor is provided with a right driving shaft (97), the square tube is provided with a right shaft hole, the right driving shaft penetrates into the right shaft hole, the right driving shaft is provided with a right horizontal wing (98), the models of the left horizontal wing motor and the right horizontal wing motor are the same, the left horizontal wing motor and the right horizontal wing motor are bilateral symmetry, the front end of the left horizontal wing motor and the right horizontal wing motor is provided with a vertical wing motor (99), the center of the vertical wing motor is provided with a vertical driving shaft (100), the square tube is provided with an upper shaft hole and a lower shaft hole, the upper end and the lower end of the vertical driving shaft respectively penetrate into the upper shaft hole and the lower shaft hole, the upper vertical wing (101) is arranged at the upper end of the vertical driving, The square tube type missile wing comprises a right horizontal wing, an upper vertical wing and a lower vertical wing which are missile empennages with the same size, a left horizontal wing and a right horizontal wing are respectively driven to turn up and down when a left horizontal wing motor and a right horizontal wing motor rotate positively and reversely, the upper vertical wing and the lower vertical wing are driven to turn left and right synchronously when the vertical wing motor rotates positively and reversely, a left wing groove is arranged at the rear end of a left half hole, a right wing groove is arranged at the rear end of a right half hole, an upper wing groove is arranged between a left hemisphere and a right hemisphere which are positioned at the upper end of a square opening, a lower wing groove is arranged between the left hemisphere and the right hemisphere which are positioned at the lower end of the square opening, a square tube slides forwards, a reset spring is compressed, the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are respectively arranged in the left wing groove, the right wing groove, the upper wing groove and the lower wing groove, a lock hole of the square tube is aligned with the cylindrical iron core, the rear ends of the right horizontal wing, the upper vertical wing and the lower vertical wing are all consistent with the spherical surface of the missile, so that the spherical missile is changed into a spherical shape, when the electromagnetic coil of the lock head is electrified, the cylindrical iron core is sucked into the lower end of the inner circle of the coil framework by electromagnetic force, the cylindrical iron core slides downwards to be separated from the lock hole, the square tube is ejected backwards by the reset spring, the spherical missile is changed into a warhead, the square tube is changed into a missile body, and the left horizontal wing, the right horizontal wing, the upper vertical wing and the lower vertical wing are changed into; the intelligent control box (103) is arranged at the front end in the square tube, a gyro level sensor, a brushless motor control module and an intelligent control module are arranged in the intelligent control box, the battery box (104) is arranged at the rear end of the intelligent control box, a round concave surface is arranged at the front end of the square hole of the spherical missile, a spherical end cover (105) is embedded in the round concave surface, a camera hole is arranged in the center of the spherical end cover, a camera (106) is installed in the camera hole, 4 sensor holes are formed in the spherical end cover around the camera hole, an infrared sensor (107), a lower infrared sensor (108), a left laser radar sensor (109) and a right laser radar sensor (110) are respectively installed in the 4 sensor holes, an indicator lamp hole is formed in the lower end of the spherical end cover, a starting indicator lamp (111) is installed in the indicator lamp hole, a Hall sensor (112) is arranged at the front upper end of the lock hole, square pipe front end is equipped with wire breach (113), be equipped with the line hole between left hemisphere and the right hemisphere, output line (114) of hall sensor and tapered end solenoid's output line (115) are through line hole and wire breach and camera, go up infrared sensor, infrared sensor and left laser radar down, telescopic cable (116) are assembled to right laser radar and top horizontal sensor's output line, in the sensor cable reachs the intelligent control box, the output line of each sensor is connected with intelligent control module's relevant input respectively, left horizontal wing motor is connected respectively to a plurality of outputs of brushless motor control module, right side horizontal wing motor and vertical wing motor, brushless motor control module input is connected respectively to a plurality of outputs of intelligent control module, tapered end solenoid and start indicator.

2. The annular accelerating missile electromagnetic gun of claim 1, wherein: before the annular accelerating missile is loaded into the electromagnetic gun, a steel bar penetrates into a lock hole of the spherical missile to trigger a Hall sensor, a spherical missile power supply is turned on, a starting indicator lamp of the spherical missile is on, the spherical missile starts to work according to a control program, the spherical missile is loaded into the bottom of an annular gun bore from a circular inlet, an electric gun wheel rotates clockwise according to a starting button, the spherical missile rolls anticlockwise along the inner circle of the annular gun bore by virtue of gravity, when the spherical missile rolls to a position between an infrared emission head II and an infrared receiving head II to block infrared rays, the infrared receiving head II triggers an input end II of a bistable trigger, a switching triode outputs direct-current voltage to a left electromagnetic coil and a right electromagnetic coil which are connected in parallel, a magnetic field space between the left electromagnetic coil and the right electromagnetic coil attracts the spherical missile, when the spherical missile attracts to a position between the infrared emission head I of the left, the spherical missile is triggered by a pulse of an infrared receiving head I, a switch triode is cut off, a left electromagnetic coil and a right electromagnetic coil are powered off, the spherical missile is separated from magnetic field force and continuously rotates anticlockwise by means of gravity and inertia, the spherical missile can automatically rotate around an annular accelerator after being attracted and accelerated for multiple times by a plurality of electromagnetic drivers, an intelligent controller I controls a hub type speed reducing motor to stop rotating, the spherical missile is driven by the relay of the annular electromagnetic accelerator to be continuously accelerated step by step and rotates in a circle of an annular gun bore repeatedly, and the rotation speed of the spherical missile can be increased to the limit without being limited by distance and time and needing large electric power; the mechanism for starting, aiming and launching the annular accelerating missile electromagnetic gun is simple and controllable, the horizontal steering button and the elevation steering button are operated to enable the missile outlet of the electric gun wheel to be aligned with a target, the accelerating button is pressed after the target is aligned to be determined, the voltage of an adjustable direct current power supply is increased, the power of the annular accelerator is increased, the rotating speed of the spherical missile is increased, the pulse frequency output by the infrared receiving head I represents the rotating speed of the spherical missile, the pulse output by the infrared receiving head I outputs the data information of the missile speed through the missile speed sensing conversion module and is transmitted to the display through radio, when the missile speed displayed on the display reaches ultrahigh sound speed, the infrared emitting head III is remotely controlled to launch an infrared signal according to the launching button, when the spherical missile flies to the position between the infrared emitting head III and the infrared receiving head III to block infrared rays, the infrared receiving head III triggers the input end of the monostable trigger, the monostable trigger outputs a pulse trigger switch triode, the switch triode outputs direct current voltage which is temporarily stabilized for a period of time to a left electromagnetic switch and a right electromagnetic switch which are connected in parallel, the left electromagnetic switch and the right electromagnetic switch drive the tail end of an annular steel plate, the outlet of the missile is opened in advance, the spherical missile flies out from the outlet of the missile in the linear direction after flying for one circle, the time for the spherical missile to fly for one circle is longer than the time for the outlet of the missile to be opened completely, the spherical missile is ensured to pass through the outlet of the missile without obstacles, the switch triode is recovered to the cut-off state after the monostable trigger is temporarily stabilized for a period of time, the annular accelerating missile electromagnetic gun is stopped, the inner circle of the annular steel plate is recovered to be circular, the process is repeated when a second spherical missile is launched, the initial speed for the spherical missile to fly out from the outlet is equal to the accelerated linear, the linear flight at ultra-high pitch speed is realized, then the missile flies according to the trajectory by means of the inertia of the missile, when the missile flies to the highest stage, the gyro level sensor triggers the intelligent controller according to the change of the horizontal angle of the missile, the intelligent controller turns on the power supply of the electromagnetic coil of the lock head to dislocate the lock head, the reset spring ejects the square tube backwards to change the spherical missile into a bullet head and change the square tube into a missile body, the intelligent controller receives the instruction of the gyro level sensor to drive the left horizontal wing and the right horizontal wing to keep a horizontal state, the camera sends out a control signal of the flight direction to the intelligent controller according to the image information of the target, the upper infrared sensor and the lower infrared sensor according to the heat source information of the target, the left laser radar and the right laser radar jointly search and lock the target according to the reflection information of the target, and controls the upper, the spherical accelerating missile electromagnetic gun is suitable for being equipped on warships or land battle teams, and the spherical accelerating missile electromagnetic gun is large in mass, large in kinetic energy injury killing power and strong in penetrating power and is suitable for hitting targets in the air, on the sea or on the land.

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