CN1535895A - Rotor type electromagnetic power space propeller - Google Patents

Abstract

The present invention relates to a rotor type electromagnetic power space propeller. It is an equipment capable of providing thrust force for space vehicle, and is mainly formed from two geared ring rotors mounted on the base seat and three coils which are passed through central hole of the rotor and formed by means of coiling process. On the rotor is mounted a moving-iron block, after the coil is powdered on, an electric field can be produced, and the attractive power for attracting moving-iron assembly can be produced so as to make the rotor accelerate, after the acceleration is up to rated value, another coil can produce attractive power to make the rotor reduce speed, in the process of accelerating speed and reducing speed the rotor can produce reactive force to system whole body, and said system can have thrust force.

Description

Rotor-type electromagnetic power space propulsion

The present invention relates to a kind ofly can be space vehicle, the propeller system of propelling thrust effect is provided.

In the present prior art, the aircraft that moves in the space has propeller formula and jet-propelled two kinds of thrust modes.The mode that propeller formula aircraft utilizes paddle to promote air backward obtains propelling thrust forward.The shortcoming of this mode is to use under the space vacuum condition.Jet-propelled aircraft obtains forward propelling thrust by the mode that sprays at a high speed gas backward, and its shortcoming is the cost height, and complex structure, and under the space vacuum condition is in case use up can not repeated usage for standby ejected matter.

Task of the present invention provide a kind of cost low simple in structure, can be under the space vacuum condition reusable propeller system.

The object of the present invention is achieved like this: be on the plane of pedestal at the rectangular planes plate, with two structures and garden annular gear ring identical in quality as rotor, be installed on the rotor shaft by ball bearing of main shaft, two rotors are meshed in the gear mode, and rotor shaft and pedestal are connected mutually.On the ring end face of two rotor gardens, fixedly mounting the moving iron assembly of polylith evenly and at intervals.Pass rotor garden ring centre hole, twining the three branch circle, the three branch circle is arranged in parallel within on the same horizon, and wherein middle coil is installed in two rotor engaged places, and it twines simultaneously and has crossed over two rotor gear rings.Two rotors and moving iron assembly can rotate flexibly, pass freely through the three branch circle.During work, the main supply switch on the closed base at first, so the self-starting motor that is fixed on the pedestal rotates, make rotor begin rotation, when epitrochanterian moving iron assembly reaches the coil upper end position, the contact of the switch controlling device on the moving iron assembly, connect the first period contact switch, make the first period coil electricity produce magnetic field, and attract moving iron assembly, the beginning work done.The moving suffered magnetic force of iron is near zero the time, and the contact on the moving iron assembly disconnects with contact switch because of rotation.This process continues to take place, and just makes rotor reach the maximum speed of regulation gradually.When rotor reaches maximum speed, the push rod of the switch controlling device on the moving iron assembly, because of making contact, moves centnifugal force, make the second period contact switch, just passed for second period during hub of a spool hole at moving iron assembly, be switched on circuit, so moving iron assembly is subjected to the magnetic field suction of this coil and underspeeds gradually, at this moment the contact switch of first period was no longer connected all the time in second period.When rotor speed reduces to zero, pull bar on the moving iron assembly returns because of elastic force, and the second period contact switch is no longer connected, simultaneously by the far infrared teleswitch that is fitted on the moving iron assembly, make the self-starting motor rotation, begin the work done process of above two periods heavily again.Self-starting motor has the intermittent operation function, and after starting, its time control setup can make the trigger circuit outage at short notice, and this moment, self-starting motor promptly broke away from the rotor gear ring automatically.In above two period working processs, two rotor speeds are opposite sign but equal magnitude all the time, therefore aggregate momentum moment vector and be always zero, but two rotor kinetic energy gross energies by zero to maxim, get back to zero at last again, therefore rotor has antagonistic force to entire system, and this power is two period direction unanimities, and is all consistent with the intermediate coil centerline direction.Need to prove according to above method, two rotors also can be in the coaxial installation in pedestal two sides, and this mode needs four coils to be wrapped on two rotor gear rings, and distributes in rotor shaft line of centers bilateral symmetry, simultaneously always make two rotor speeds identical, switched in opposite.

Since the present invention utilize rotor to the antagonistic force of total system as propelling thrust, thereby jet-propelledly compare with propeller formula propelling unit with existing, have cost hang down simple in structure, can be in the advantage of sustained use under the vacuum condition.

Below in conjunction with accompanying drawing and concrete embodiment, the present invention is described in further detail.

Fig. 1 is a structural representation of the present invention.

Fig. 2 is the circuit diagram of three branch circle of the present invention and self-starting motor.

Fig. 3 is the switch controlling device scheme drawing on the moving iron assembly of the present invention.

Fig. 4 is the structure diagrams of the present invention's two rotors when coaxial.

With reference to two structures and identical in quality of Fig. 1, the garden annular gear ring rotor 4 that rotor inertia is enough big by ball bearing of main shaft 10, is installed on two rotor shafts 19, and two rotors are meshed by the gear teeth.Rotor 4 gardens are equipped with the moving iron assembly 3 of polylith, (among the figure being 5) evenly and at intervals on week.Two rotor shafts 19 are fixedly mounted on the pedestal 1.Coil 6, coil 5, coil 9 all twine after passing rotor bore and make.Triple coil all is fixed on the rotor shaft.The at first closed starting switch 12 that is fixed on the pedestal 1 when work, the self-starting motor 11 that then is fixed on the pedestal 1 begins rotation, makes two rotors begin rotation thus.Rotation along with rotor, when epitrochanterian moving iron assembly 3, when going to the upper port edge of coil 6, be fixed on the first period contact switch 8 on the rotor shaft, contact 14 by the switch controlling device on the moving iron assembly among Fig. 3 is just in time connected, so be fixed on power supply 2 on the pedestal 1, to coil 6 power supplies, the moving iron assembly of the magnetic field suction that coil 6 produces and work done.Moving iron assembly when technical requirement produces attractive force when coil to a moving iron, is zero to other moving iron gravitation in epitrochanterian distribution.Along with the rotation of rotor, when moving iron assembly all entered in the hub of a spool hole suffered magnetic force and is zero, switch 8 was disconnected again, and this process constantly repeats, and the rotating speed of rotor is constantly accelerated, and reached maximum rated speed.This was for first working hour, and these periods two rotor speed is identical, but switched in opposite, thereby aggregate momentum moment vector and be zero.But total kinetic energy becomes big by zero, thereby two rotors must produce antagonistic force to total system, and this force direction is the indicated direction of sight vane 13.

After rotor reaches specified maximum speed, the pull bar 15 of the switch controlling device among Fig. 3 on the moving iron assembly 3, because of centnifugal force moves, make contact 14 no longer connect the first period switch 8, and make contact 21 when moving iron assembly has just passed coil 5 and coil 9, connect the second period switch 7, and make coil 5 and line produce magnetic field than 9, moving iron assembly 3 is produced suction, when magnetic force seldom the time, contact makes the two coil outage because of motion.Repeat so incessantly, rotor speed will reduce to zero.When rotor speed was zero, the control setup contact 21 among Fig. 3 on the moving iron assembly in the return process, was pushed return infrared ray and is shaken control switch 20, and self-starting motor is started again.Thereby work endlessly.In second period work, two rotor total kinetic energies are by the maxim vanishing, and the aggregate momentum square does not change, thereby rotor must produce antagonistic force to total system, and this force direction is identical with the first period antagonistic force direction.

Above embodiment is the different axle mountings of two rotors, also can realize above effect when the coaxial installation of two rotors.With reference to Fig. 4, rotor 23 and rotor 27 are distributed in the two sides of pedestal 25, and at this moment system has 4 line charts.Wherein coil 24 is the same period with coil 28, coil 26 and 22 same periods of coil, as long as other structure and technical requirements are consistent with above embodiment principle, then total system will produce and the same effect of above embodiment like this.

Propelling unit of the present invention must a plurality ofly be united use in application, in exemplary embodiments, two propelling units are installed in parallel on the aircraft, as long as an angle of rake electric current is reduced, thereby both thrust is changed, so just can realize the turning to of aircraft, oppositely, state of kinematic motion such as prevention, the solar cell in the outer space vehicle can make propelling unit have lasting electric energy simultaneously, thereby propelling unit has the sustainability in-use performance.

The reasoning that the present invention discloses is:

When the suffered bonding force of system and bonding force square are zero, if the internal force of internal system causes the individuality of system, the change of the straight-line motion and the two kinds of state of kinematic motion powers that rotatablely move takes place, and the situation of variation will appear in the momentum of system so, and perhaps the situation of variation will appear in the rotation momentum square of system.

Claims (7)

1, a kind of by pedestal (1), two garden annular gear ring rotors (4), self-starting motor (11) coil (5), coil (6), coil (9) first period contact switches (8), the second period contact switch (7), the rotor-type electromagnetic power space propulsion of forming is characterized in that two rotors (4) are installed on the rotor shaft (19) by ball bearing of main shaft respectively, coiling formed after coil (5), coil (6), coil (9) all passed rotor bore, on the anchor ring of rotor garden, the moving iron assembly (3) of polylith is installed evenly and at intervals.

2, device according to claim 1, it is characterized in that coil (5), coil (6), coil (9) are distributed on the same horizon, coil (6) is to pass two rotor bores to stride around forming, an independent work done period of coil (6), coil (5) and coil (9) are in same period work done, and they always make two rotor speed equal directions opposite when attracting to move the iron work done.

3, device according to claim 1 is characterized in that the first period contact switch (8) and second period contact switch (7) rear end, flushes with coil (6) and coil (5) upper end respectively, so that moving iron assembly has maximum expansion space stroke when magnetic field force induced.

4, device according to claim 1 is characterized in that moving iron assembly (3), rectangular distribution on rotor, between two adjacent moving iron assemblies, angle at interval, should have only a moving iron to be subjected to the magnetic field graviational interaction when making each rotor work done more than big 15 degree of the pairing angle of coil central axe longitudinal length.

5, device according to claim 1 is characterized in that on the moving iron assembly (3) pull bar (15) being installed, and pull bar (15) passes through groove (16), ball (17), and can move back and forth.

6, device according to claim 1 is characterized in that being installed with push type infrared remote control switch (20) on the moving iron assembly 3.

7, want 1 described device according to right, it is characterized in that two rotors also can be installed on the same rotor shaft.

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