阅读说明：本技术 一种电磁贯性推进器 (Electromagnetic coherence propeller ) 是由 江华志 何应龙 何应君 于 2021-08-10 设计创作，主要内容包括：本发明公开了一种电磁贯性推进器,包括检测控制器、超导线圈、导磁环管、永磁体、转向轴、转向控制架,导磁环管共设有两个,每个导磁环管上均缠绕有超导线圈,导磁环管内两安装有两个或两个以上相同的永磁体,具体个数按需装配,两个导磁环管里装配的个数相同即可,每个导磁环管内磁体的磁极相同且悬浮在环内不与环内壁相接触。本发明与现有技术相比的优点在于：克服了以上所述的各类反冲式推进器的缺点,通过增加一个维度实现对因反作用力而损耗的“质量和能量”再循环利用,推进效率更高,实现了对传统飞行器因反作用力而失掉的动能的回收利用,无工质损耗,其动能的载体做循环的二维圆周运动,方向控制简便。(The invention discloses an electromagnetic coherence propeller which comprises a detection controller, superconducting coils, two magnetic conduction ring pipes, permanent magnets, a steering shaft and a steering control frame, wherein the number of the magnetic conduction ring pipes is two, the superconducting coils are wound on each magnetic conduction ring pipe, two or more than two same permanent magnets are arranged in each magnetic conduction ring pipe, the specific number of the permanent magnets is assembled according to the requirement, the number of the permanent magnets assembled in each magnetic conduction ring pipe is the same, and the magnetic poles of the magnets in each magnetic conduction ring pipe are the same and are suspended in the rings and are not contacted with the inner walls of the rings. Compared with the prior art, the invention has the advantages that: the defects of various recoil propellers are overcome, the mass and energy lost due to the reaction force are recycled by adding one dimension, the propulsion efficiency is higher, the kinetic energy lost due to the reaction force of the traditional aircraft is recycled, no working medium is lost, the carrier of the kinetic energy does circular two-dimensional circular motion, and the direction control is simple and convenient.)

1. The utility model provides an electromagnetism coherence propeller, includes detection controller (1), superconducting coil (2), magnetic conduction ring canal (3), permanent magnet (5), steering spindle (6), steering control frame (7), its characterized in that: the number of the magnetic conduction ring pipes (3) is the same, and the magnetic poles of the magnets in each magnetic conduction ring pipe (3) are the same and are suspended in the ring and not contacted with the inner wall of the ring; four detection controllers (1) are mounted on each magnetic conduction ring pipe (3), the detection controllers (1) control the current direction and the current magnitude of the superconducting coils (2) outside the magnetic conduction ring pipes (3), and can detect the temperature in the magnetic conduction ring pipes (3) and the motion position of the permanent magnets (5);

the two magnetic conduction ring pipes (3) are overlapped, symmetrically placed and fixed, air in the assembled two magnetic conduction ring pipes (3) is pumped out, reverse torque of the two magnetic conduction ring pipes (3) can be offset, and resistance of the air ring to an internal high-speed moving magnet is reduced.

2. An electromagnetic coherence thruster according to claim 1, wherein: the four detection controllers (1) divide the superconducting coil (2) into four equal arc structures on average.

3. An electromagnetic coherence thruster according to claim 1, wherein: the magnetic conduction ring pipe (3) is of a hollow circular ring structure, and the superconducting square ring (4) can be manufactured as required to meet different use requirements.

4. An electromagnetic coherence thruster according to claim 1, wherein: the magnetic conductive ring pipe (3) is made of materials with low temperature resistance, good magnetic conductivity, firmness and light weight.

5. An electromagnetic coherence thruster according to claim 1, wherein: the magnetic conduction ring pipe (3) is used as an output device of electromagnetic energy, an internal guide rail structure can guide the internal permanent magnet (5) to do circular motion, and the magnetic conduction ring pipe (3) can be used as a controller of the thrust direction of the propeller.

Technical Field

The invention relates to a propulsion device, in particular to an electromagnetic coherence propeller.

Background

As is known, many vehicles invented and created today, including marine or submarine vehicles, aircraft, rockets, including some satellite-mounted hall thrusters, etc., all utilize recoil to achieve efficient propulsion, and there must be a great deal of working fluid and energy loss. This is because these inventions obey the law of conservation of momentum and power that the direction of the force in one dimension and the direction of the momentum are one-dimensionally symmetrical.

Disclosure of Invention

The invention aims to solve the technical problem that the conventional propelling device has large energy loss and cannot meet the conventional use requirement.

In order to solve the technical problems, the technical scheme provided by the invention is as follows: the electromagnetic coherence propeller comprises a detection controller, superconducting coils, magnetic conduction ring pipes, permanent magnets, steering shafts and a steering control frame, wherein the number of the magnetic conduction ring pipes is two, the superconducting coils are wound on each magnetic conduction ring pipe, two or more than two identical permanent magnets are installed in each magnetic conduction ring pipe, the specific number of the permanent magnets is assembled as required, the number of the permanent magnets assembled in each magnetic conduction ring pipe is the same, and the magnetic poles of the magnets in each magnetic conduction ring pipe are the same and are suspended in the ring and are not in contact with the inner wall of the ring; each magnetic conduction ring pipe is provided with four detection controllers, the detection controllers control the current direction and the current magnitude of the superconducting coils outside the magnetic conduction ring pipes and can detect the temperature inside the magnetic conduction ring pipes and the movement positions of the permanent magnets;

the two magnetic conduction ring pipes are overlapped, symmetrically placed and fixed, air in the two magnetic conduction ring pipes which are assembled is pumped out, the reverse torque of the two magnetic conduction ring pipes can be offset, and the resistance of the air ring to the magnet moving at high speed in the magnet is reduced.

Compared with the prior art, the invention has the advantages that: the defects of various recoil propellers are overcome, the mass and energy lost due to the reaction force are recycled by adding one dimension, the propulsion efficiency is higher, the kinetic energy lost due to the reaction force of the traditional aircraft is recycled, no working medium is lost, the carrier of the kinetic energy does circular two-dimensional circular motion, and the direction control is simple and convenient.

As an improvement, the four detection controllers divide the superconducting coil into four equal arc structures on average.

As an improvement, the magnetic conduction ring pipe is of a hollow circular ring structure, and the superconducting square ring can be manufactured as required to meet different use requirements.

As an improvement, the performance of the manufacturing material of the magnetic conduction ring pipe requires low temperature resistance, good magnetic conduction performance, firmness and light weight.

As an improvement, the magnetic conduction ring pipe is used as an output device of electromagnetic energy, an internal guide rail structure can guide an internal permanent magnet to do circular motion, and the magnetic conduction ring pipe can be used as a controller of the thrust direction of the propeller.

Drawings

Fig. 1 is a schematic structural diagram of a magnetic conductive ring pipe of an electromagnetic coherence thruster.

FIG. 2 is a schematic diagram of a superconducting square ring of an electromagnetic coherence thruster.

Fig. 3 is a schematic diagram of the counterclockwise rotation of the permanent magnet of the electromagnetic coherence thruster.

Fig. 4 is a schematic diagram of clockwise rotation of a permanent magnet of an electromagnetic coherence thruster.

Fig. 5 is a schematic diagram of a finished structure of an electromagnetic coherence thruster.

Fig. 6 is a schematic structural diagram of the embodiment.

As shown in the figure: 1. the device comprises a detection controller, 2, superconducting coils, 3, a magnetic conduction ring pipe, 4, a superconducting square ring, 5, a permanent magnet, 6, a steering shaft, 7, a steering control frame, 8, a propeller, 9, a cab, 10, a large propulsion ring I, 11, a large propulsion ring II, 12 and an energy bin.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings.

The invention is implemented in detail, the electromagnetic permeability propeller comprises a detection controller 1, two superconducting coils 2, two magnetic conduction ring pipes 3, permanent magnets 5, a steering shaft 6 and a steering control frame 7, wherein the number of the magnetic conduction ring pipes 3 is two, the superconducting coils 2 are wound on each magnetic conduction ring pipe 3, two or more same permanent magnets 5 are arranged in the magnetic conduction ring pipes 3, the specific number is assembled as required, the number of the permanent magnets assembled in the two magnetic conduction ring pipes 3 is the same, and the magnetic poles of the magnets in each magnetic conduction ring pipe 3 are the same and are suspended in the ring and are not contacted with the inner wall of the ring; four detection controllers 1 are installed on each magnetic conduction ring pipe 3, the detection controllers 1 control the current direction and the current magnitude of the superconducting coils 2 outside the magnetic conduction ring pipes 3, and can detect the temperature in the magnetic conduction ring pipes 3 and the motion positions of the permanent magnets 5;

the two magnetic conductive ring pipes 3 are overlapped, symmetrically arranged and fixed, air in the assembled two magnetic conductive ring pipes 3 is pumped out, the reverse torque of the two magnetic conductive ring pipes 3 can be offset, and the resistance of the air ring to the magnet moving at high speed in the magnet is reduced.

The four detection controllers 1 equally divide the superconducting coil 2 into four equal arc structures.

The magnetic conduction ring pipe 3 is of a hollow circular ring structure, and the superconducting square ring 4 can be manufactured as required to meet different use requirements.

The magnetic conductive ring pipe 3 is made of materials with low temperature resistance, good magnetic conductivity, firmness and light weight.

The magnetic conduction ring pipe 3 is used as an output device of electromagnetic energy, an internal guide rail structure can guide the internal permanent magnet 5 to do circular motion, and the magnetic conduction ring pipe 3 can be used as a controller of the thrust direction of the propeller.

The working principle of the invention is as follows: the invention overcomes the disadvantages of the recoil thrusters of the various types described above and achieves the recycling of the 'mass and energy' lost due to the reaction force by adding one dimension. The principle of the invention is that the impulse of an object which does circular motion (two-dimensional motion) is utilized by utilizing the momentum of the object in the tangential direction of the motion track (circle), and the specific method is as follows:

firstly, two identical magnetic conducting hollow circular rings (hereinafter referred to as superconducting rings, which can be square pipe circular rings or circular pipe circular rings) wound with superconducting coils are manufactured, and the material performance requirements are as follows: low temperature resistance, good magnetic conductivity, firmness and light weight, as shown in figures 1 and 2. The functions of the utility model are mainly as follows: 1) an output device for electromagnetic energy; 2) guide rail: guiding the inner magnet to do circular motion; 3) as a control for the thrust direction of the propeller.

Secondly, two (or more) same permanent strong magnets (hereinafter referred to as magnets) are respectively arranged in the two rings, the specific number of the permanent strong magnets is required to be assembled according to the requirement, the number of the permanent strong magnets assembled in the two rings is only required to be the same, and the magnetic poles of the magnets in each ring are the same and are suspended in the rings and are not contacted with the inner wall of the rings.

The functional function is as follows: and the high-speed circular motion is performed, and the kinetic energy is stored.

Thirdly, four detection controllers are arranged on each ring (the four detectors divide the ring into four equal circular arcs).

The functional function is as follows: 1) controlling the current direction and magnitude of the superconducting coil outside the loop; 2) the temperature within the ring and the position of movement of the magnet are detected. (the permanent magnet in the superconducting ring can be selectively applied with a resistance field to obtain the kinetic energy thereof).

Fourthly, the two circular rings are overlapped and symmetrically placed and fixed. The air inside the two rings which have been assembled is evacuated.

The purpose of the utility model is: 1) counteracting the opposing moments of the two rings; 2) the resistance of the air ring to the inner high-speed moving magnet is reduced.

The steps of the electromagnetic coherence thruster are provided above.

As shown in fig. 2, 3 and 4, the operation process of the electromagnetic coherence thruster is described as follows:

if the superconducting coils of the upper, lower, left and right segments apply force fields in the same direction to the permanent magnets moving into the segment, and the permanent magnets do circular accelerated motion in the same direction, then the state is called as the kinetic energy accumulation stage of the propeller. Because of newton's third law, the superconducting rings are subjected to a counter torque to rotate in the opposite direction. And because of the law of conservation of momentum, the sum of the momentum of the moving permanent magnet and the superconducting loop rotating in the opposite direction is zero. Therefore, we use two rings stacked together to cancel each other's opposing moments (see fig. 4), which are then converted into kinetic energy of the permanent magnets in the two superconducting rings.

And secondly, extracting the kinetic energy of the permanent magnet which does high-speed circular motion in the two superconducting rings, referring to fig. 3, taking upward propulsion as an example. Because the permanent magnets in the two rings move in opposite directions, when the permanent magnet in the first superconducting ring moves to the right section (section D) of the ring, the moving direction of the permanent magnet is generally upward, at the same time, the permanent magnet in the second superconducting ring moves to the left section (section B') of the ring, the moving direction of the permanent magnet is generally upward, the permanent magnet in the left superconducting coil also controls the current direction of the superconducting coil to apply a resistance magnetic field to the permanent magnet moving upward in the superconducting ring, (and the superconducting coils in the other three sections can still apply a thrust field to the permanent magnet in the same moving direction as the permanent magnet). Therefore, the left and right of the propeller are pushed upwards by the upward impact inertia force of the permanent magnet. (note: each time the resistance applied to the permanent magnet must be less than its own inertial force, the permanent magnet is allowed to cycle again through the segment into the acceleration segment).

The propulsion to other directions is the same as the principle of the propulsion, and can be realized by only selecting the superconducting coil sections at different positions to apply resistance to the permanent magnets in the superconducting coil sections. The rotating angle of the propeller can be controlled by using the vertical direction of the propeller as a rotating shaft through the steering of a steering control frame (see figure four), and the propeller can be propelled to any space direction of front and back, left and right, and vertical directions by combining the exchange of the resistance superconducting coils.

(Note that at the same time, the permanent magnets in ring one and ring two are moved to positions that remain in a left-right symmetrical position about their propulsion direction axis.

Example (b):

this embodiment is a supplementary description of how to use and install the electromagnetic coherence thrusters, and is shown in fig. 5, which is a cross-sectional view of a disk-shaped aircraft equipped with four small and one large electromagnetic coherence thrusters. The four small electromagnetic coherence propellers are arranged on the inner side of a large electromagnetic coherence propeller in central symmetry and are bound and linked with the large electromagnetic coherence propeller, and the large electromagnetic coherence propeller can be used for fine adjustment of any pitch angle, so that the flexibility of the propelling direction of the aircraft is increased, and a synchronous and unified control method is adopted for controlling all the electromagnetic coherence propellers arranged on the aircraft. The most central sphere, the upper hemisphere is a driving cabin, and the lower hemisphere is an energy cabin (preferably a nuclear battery).

In the gravity environment, four small-sized electromagnetic coherence propellers mainly provide lift force for the aircraft, and the small-sized electromagnetic coherence propellers in the microgravity environment can assist the large-sized electromagnetic coherence propeller to propel, so that the propelling direction of each small-sized electromagnetic coherence propeller is consistent with that of the large-sized electromagnetic coherence propeller, and the propelling force of the whole aircraft is increased.

Compared with the traditional aircrafts such as airplanes and rockets, the invention has higher propelling efficiency because the kinetic energy lost by the traditional aircrafts due to reaction force is recycled, no working medium is lost, and because the carrier of the kinetic energy does circular two-dimensional circular motion, the direction control is simple and convenient. If the energy source adopts nuclear power, the stealth material is covered on the outer surface of the energy source, so that radar and vision stealth can be realized, and the permanent magnet does not contact with the inner wall of the superconducting pipe, so that no sound exists basically during flight. Therefore, the propeller is a revolutionary and subversive ideal propeller.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature, and in the description of the invention, "plurality" means two or more unless explicitly specifically defined otherwise.

In the present invention, unless otherwise specifically stated or limited, the terms "mounted," "connected," "fixed," and the like are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly above and obliquely above the second feature, or simply meaning that the first feature is at a lesser level than the second feature.

In the description herein, reference to the terms "one embodiment," "some embodiments," "an example," "a specific example," or "some examples" or the like means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made in the above embodiments by those of ordinary skill in the art without departing from the principle and spirit of the present invention.