CN103196331A

CN103196331A - Gyroscope cannon

Info

Publication number: CN103196331A
Application number: CN201210022609XA
Authority: CN
Inventors: 葛泓杉
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-01-05
Filing date: 2012-01-05
Publication date: 2013-07-10

Abstract

The invention provides a gyroscope cannon which applies an initial velocity to an object ready to be launched through high-velocity circular motion of a gyroscope. The launching parameters of the object to be shot are controlled by adjusting the rotating angle, acceleration, launching velocity and other parameters of the launching surface of the gyroscope to meet launching requirements. As the gyroscope cannon utilizes current mature technologies, the launching velocity is greatly increased. Air resistance is changed into propulsion power due to the through structure, so that the air resistance is greatly reduced. Particularly, by utilizing the magnetic control plasma technology, the internal energy of plasmas can be extracted to be used as auxiliary power during high-velocity motion, so that the high initial velocity is maintained for a long time under the action of inertia so as to meet the launching requirements.

Description

The gyro big gun

One, technical field

A kind of emitter is in order to space flight, aviation and emissions such as shell, guided missile.

Two, technical background

When object moved in a circle, as long as centripetal force and centrifugal force balance, object just moved in a circle around the center of circle.When centripetal force disappears, object just certain a bit on, under centrifugal action, do rectilinear motion along the circle of contact.Speed when rectilinear motion begins, the linear velocity when equaling this object and moving in a circle.Use this principle, can make object accelerate to a certain speed by circular motion after, and become the rectilinear motion of circular motion into carrying out along tangent line at this speed lower edge tangent line, the purpose that object is dished out by straight line with initial velocity greatly.

Being launched logical structure in the object use, is the crux factor of gyro big gun performance ideal effect.

Three, summary of the invention

The high speed top launcher, in logical object to be launched, magnetic control plasma generating boost motor.

1, high speed top launcher is the equipment that accelerates for the emitting substance rotation.Ultimate load and limit rotary speed have directly determined the potentiality of this emitter.Suppose that the high speed gyro can make the initial velocity of the object that it carries and launch reach the first universal speed, just can directly launch a man-made satellite..When not reaching the first universal speed, just can only make carrier provide the part of fuel boosting for oneself.

Object to be launched is fixed on the surface of emission of gyro by suitable fixture.Gyro can be cylinder, also can be the young body of circle, also can be round platform.Any surface of gyro all may be as the surface of emission.Once emission can be launched an object, also can accelerate simultaneously, launches a plurality of objects respectively.When gyro accelerated, speed was by zero to emission rate, and acceleration is changeable, regulates arbitrarily as required.Emission angle can be as required, by the surfaces of revolution angle of speed governing gyro, any adjusting.

2, logical object to be launched in.The object of gyro emission, can only be in logical structure, otherwise air drag will reduce the necessity of gyro emission greatly, make it can not to bring into play succinctly, at a high speed, the purpose of lower resistance emission.

3, magnetic control plasma generating boost motor places the appropriate location of logical emission interior of articles, when being used for the emission object and reaching certain linear velocity, by extracting the interior energy of plasma, provides the purpose of thrust.If emission object itself also need push away carrying fuel, the plasma boost motor then needs to mate with burner.

Four, the specific embodiment

Make and be used as an explanation below by ground use, space base use, space-based use, submarine use, sea base

1, use on ground

With launch long-range in the admittance bullet be example.According to the trajectory needs, by adjusting the gyro surface of emission, set the angle of departure.By setting the gyro rotary acceleration, satisfy the needs of emission afterburning load that object bears.By setting the linear velocity of emitting substance, determine the launch velocity of emitting substance.If the speed in the gyro accelerator is enough high, guided missile in accelerator, in logical structure just start working, electromagnetism plasma generating boost motor just may produce certain power, the boosting gyro accelerates to rotate.

During emission, gyro is begun by zero-speed, accelerates to emission rate by namely fixed acceleration.After accelerating to emission rate, fixture moment is opened the centripetal force pop-off of fast approximately guided missile.Guided missile is just with the set angle of departure, and the initial velocity so that rotation is obtained flies to target.After guided missile breaks away from the gyro emitter, on the one hand with lower resistance, fly to target at a high speed.Because additionaling power disappears, just under the acceleration of gravity effect, make parabolic motion on the one hand.When guided missile reaches the parabola top area, as required, can start the missile-borne rocket assist.Because the deceleration effect that acceleration of gravity produces guided missile no matter guided missile begins emission with which type of initial velocity, in the top area of trajectory, can make guided missile, avoid high speed plasma shielding effect, obtain external navigation corrected signal, fly to target.If guided missile does not need self-contained fuel, after the trajectory top area obtains the navigation correction, fly to target with inertia.

When being used as the emission of manned or accurate space flight instrument, can set arbitrarily when adding the rotation acceleration, can set acceleration arbitrarily, make people or precision instrument avoid the pressure of high acceleration.Certainly with conducting oneself or during the precision instrument use, consider the people to the limit of bearing of the centrifugal force in the rotary course, and the reaction of centripetal force when suddenly disappearing.

2, space base is used

The gyro big gun fully can miniaturization, uses by installing on the aircraft.The bullet quality of emission may have only the rifle bullet size, but because high-speed, its fighting capacity will be very strong.Be installed in the miniaturization gyro big gun on the aircraft, be completely fixed with the relative parameter of carrier aircraft, the angle of shell emission, parameters such as direction determine by the state of flight of adjusting aircraft.Under the support of satellite, to goal-setting straight line trajectory, be not the bullet navigation midway.High initial speed, according to height face down, factors such as logical in the bullet, acceleration of gravity, high precision computation, when making airborne gyro big gun at large-scale water surface naval vessel or large-scale ground military base, just look like one long apart from sniper rifle, the bombardment power of high speed bullet is just as miniature nuclear bomb.

Suppose that bullet penetrates facing to sea-surface target with ten to ten tierces speed, logical structure is seldom slowed down bullet in the bullet, and under the acceleration of gravity effect, and bullet is kept even to improve initial velocity more secure.The moment that the high speed bullet hits the mark, bullet and target contact-making surface will bear super powerful pressure, this pressure is enough to make the interior of bullet and target part metals sharply to increase, the energy explosion type of strand is discharged, cause the solid gasification, the shock wave that produces might be ignited fuel and ammunition on the large ship fully, and personnel also are difficult to existence.Therefore possibility one big gun is fatal fully.Can predict, the accuracy of this attack is high.In addition, the small-sized gyro big gun of space base also can be used as anti-satellite.

3, space-based is used

Small-sized gyro big gun is installed on the spacecraft, and is identical with the dress mode of pressing on the aircraft, and parameters such as the direction by changing spacecraft and static angular satisfy the needs of run-home.It is more convenient to kill satellite.Attack over the ground, effect is better.

4, submarine uses

Submarine uses, and mainly is in order to torpedo-launching under water, and it is identical with space base to press the dress mode.During torpedo-launching, satisfy the parameter that torpedo is launched by the elevation angle and the travel direction that changes submarine.Be subjected to the influence of water body resistance, the underwater rotating speed of gyro is significantly less than the rotating speed in atmosphere or vacuum, but in order to satisfy the initial velocity of torpedo emission, better than existing radiation pattern.Can increase the operational distance of torpedo greatly.

5, sea base is used

Be installed on the large ship, identical with the occupation mode that is installed in the land, just the scope of application is subjected to bigger restriction.Be mainly used in sea and land attack.

The advantage of gyro big gun is;

1, utilizes current all mature technologies, effectively overcome the initial velocity bottleneck, significantly promote launch velocity.

2, become fuel and carry, additional for kinetic energy, significantly reduce launch mass, can accomplish the miniaturization of great emission, rapid.

3, set the acceleration of emission arbitrarily, make people or precision instrument, in accelerator, avoid too high acceleration action.

Claims

1. with the high linear speed of gyro rotation, make to be launched the object technical method of transmitted at high speed on demand.

2. by the controllability of teetotum gyration, the controllability of acceleration and emission rate makes to be launched the technical method that object obtains desirable emission parameter.