CN1870400A

CN1870400A - Variable magnetic pole linear accelerator

Info

Publication number: CN1870400A
Application number: CN 200510120548
Authority: CN
Inventors: 宋云卿; 黄谷
Original assignee: Individual
Current assignee: Individual
Priority date: 2005-12-28
Filing date: 2005-12-28
Publication date: 2006-11-29
Anticipated expiration: 2025-12-28
Also published as: CN1870400B

Abstract

This invention discloses a pole-variable linear accelerator relating to structures of supply guideway and a synchronous core composing a pole device including a pole device, an orbit and a movement electromagnet, in which, the orbit is set on the magnetic device, the movement electromagnet is on the orbit, said magnetic device includes a first, a second, a third and the nth electromagnets arrayed in line and the pole directions of the magnets are the directions enabling the movement magnet to move along the orbit.

Description

Variable magnetic pole linear accelerator

Technical field

The present invention relates to the linear accelerator in a kind of electromagnetic propulsion technical field, relate in particular to a kind of variable magnetic pole linear accelerator; Specifically, relate to the structure that composition becomes the electrical supply rail and the synchronous core of magnetic device.

Background technology

Along with the develop rapidly of aeronautical technology, at present, the domestic rocket that can utilize starts the punching type aircraft, but rocket can only use once the cost height.And developed countries such as the U.S., France utilize B52 aircraft+rocket to start the punching type aircraft, and are more advanced than China, but because of the use of B52 aircraft repeated multiple times, thereby it is very low to start total cost, but still undesirable; In order to find high-tech with practical value, the U.S. has planned development test punching type aircraft startup in three stages new technology, i.e. X-43A, X-43B, X-43C.In a word, the U.S. studies stage by stage and its objective is:

(1) starting punching type aircraft one-tenth should be very low;

(2) fail safe is good;

(3) linear thrust is big;

(4) space rate height has 2～5 overtone speed (M);

(5) electrical source of power requires very little;

(5) no difficulty is easily gone in operation.

The U.S. has entered second stage at present; Phase III still can't carry out, difficult labour.

Summary of the invention

The objective of the invention is to overcome the shortcoming and defect that prior art exists, and a kind of variable magnetic pole linear accelerator is provided.

The object of the present invention is achieved like this: the synchronization principles of main utilization " linear accelerator " and the mutual grafting of the expansion of DC motor running principle form.

As Fig. 1, Fig. 2, the present invention mainly is made up of change magnetic device 1, orbit 2, motion electromagnet 3;

Become magnetic device 1 and be provided with orbit 2, motion electromagnet 3 is arranged on orbit 2;

Described change magnetic device 1 is the 1st electromagnet the 1.1, the 2nd electromagnet the 1.2, the 3rd electromagnet 1.3 along linear array ... N electromagnet 1.N; The direction of the magnetic pole of each electromagnet is to make motion electromagnet 3 along the direction of orbit 2 continuous accelerated motions (among Fig. 1 for to the right).

Operation principle of the present invention is:

As Fig. 1, suppose that motion electromagnet 3 upper ends are the S utmost point, then the upper end of the 1st electromagnet 1.1 should be the S utmost point, and the upper end of the 2nd electromagnet 1.2 should be the N utmost point.According to the same sex is repelled each other, there is a natural attraction between the sexes principle as can be known, then motion electromagnet 3 leaves 2nd electromagnet 1.2 motions of the 1st electromagnet 1.1 to the right.

As Fig. 3, the upper end strain of crossing the 2nd electromagnet 1.2, the 2 electromagnet 1.2 when motion electromagnet 3 one is the S utmost point, and the upper end strain of the 3rd electromagnet 1.3 is the N utmost point.According to the same sex is repelled each other, there is a natural attraction between the sexes principle as can be known, then motion electromagnet 3 leaves 3rd electromagnet 1.3 motions of the 2nd electromagnet 1.2 to the right.

And the like, make motion electromagnet 3 along the continuous accelerated motion of the direction of orbit 2.

Feature of the present invention and technique effect:

1, the present invention utilizes direct current machine to launch principle, make two magnetic poles near the time interaction force maximum (axiom) that produced, thereby linear thrust is big.

2, because introduced the synchronization principles of linear accelerator, magnetic pole change-over time is zero, and space rate is fast.

3, the preliminary experiment by power is measured, every 12V automobile batteries can produce the linear thrust of 10Kg.If it is 15～20 tons that certain punching type aircraft needs thrust, then need automobile batteries 1500-2000 only; Electrical source of power of the present invention requires very little, just 8～10% of U.S.'s electromagnetic propulsion test (with the power contrast of Lauren).

4, operating cost of the present invention is low, can repeatedly use (rocket can only use once).

5, security performance is good, can not explode.

6. the present invention is an open type, processing ease.

This shows that the present invention is the desirable technique that starts the punching type aircraft, is the high-tech that fills the domestic gaps, surmounts U.S. X-43C, thereby, can reduce the start-up cost of punching type aircraft greatly, and fail safe is good, economical and practical, the cost performance height, defense spending is saved in useful national defense construction; Realize catching up with and surpassing the target of U.S.'s high-tech technically.

Description of drawings

One of Fig. 1-operation principle schematic diagram of the present invention (front view);

Fig. 2-operation principle schematic diagram of the present invention (left view);

Two of Fig. 3-operation principle schematic diagram of the present invention (front view);

Fig. 4-motion electromagnet operation principle schematic diagram;

One of Fig. 5-change magnetic device operation principle schematic diagram;

Two of Fig. 6-change magnetic device operation principle schematic diagram.

Wherein:

1-becomes magnetic device,

1.1-the 1st electromagnet, 1.2-the 2nd electromagnet, 1.N-N electromagnet;

2-moves track;

3-motion electromagnet;

The 4-electrical supply rail;

The synchronous core of 5-.

Embodiment

Be further described below in conjunction with drawings and Examples.

1, operation track 2

Orbit 2 supports and slides for motion electromagnet 3, makes a kind of smooth track with non-magnet material.

2, the motion electromagnet 3

As Fig. 4, motion electromagnet 3 is made up of electromagnet 3.1, winding 3.2, brush 3.3, ball bearing 3.4;

The ball bearing 3.4 that electromagnet 3.1 is provided with places on the operation track 2;

The two ends of the winding 3.2 on the electromagnet 3.1 are connected with brush 3.3, and a guide rail, the b guide rail of brush 3.3 contact electrical supply rails 4 get.

3, become magnetic device 1

Become magnetic device 1 by the 1st electromagnet the 1.1, the 2nd electromagnet the 1.2, the 3rd electromagnet 1.3 along linear array ... N electromagnet 1.N; Electrical supply rail 4 and synchronous core 5 are formed, and the pole orientation that guarantees each electromagnet is to make the direction of motion electromagnet 3 along orbit 2 accelerated motions.

1) electrical supply rail 4

As Fig. 5, Fig. 6, electrical supply rail 4 is made up of the passive synchronous core guide rail of 2 active guide rails and 6 segmentations:

A guide rail, b guide rail are power rail, connect the positive and negative electrode of power supply respectively;

C guide rail, d guide rail, e guide rail, f guide rail, g guide rail, h guide rail are passive synchronous core guide rail, and all breaking before the central axis of each electromagnet that becomes magnetic device 1 is the 1st section, the 2nd section, the 3rd section ... the N section;

E guide rail, f guide rail the 1st section with c guide rail, d guide rail the 2nd section is electrically connected respectively,

G guide rail, h guide rail the 1st section with e guide rail, f guide rail the 2nd section is electrically connected respectively,

Thereafter again and the like be electrically connected;

The winding of the 1st electromagnet 1.1 connects c guide rail, d guide rail the 1st section,

The winding of the 2nd electromagnet 1.2 connects c guide rail, d guide rail the 2nd section,

The winding of the 3rd electromagnet 1.3 connects c guide rail, d guide rail the 3rd section;

Thereafter again and the like be electrically connected.

2) synchronous core 5

As Fig. 5, Fig. 6, core 5 places between motion electromagnet 3, the electrical supply rail 4 synchronously, is connected as a single entity with motion electromagnet 3; Core 5 is made up of 8 groups of brushes synchronously, contacts with 6 passive synchronous core guide rails with 2 active guide rails of electrical supply rail 4 respectively from top to bottom; From top to bottom, 1,3,6,7 group of brush is connected, and 2,4,5,8 groups of brushes are connected.

Specifically, when the synchronous core 5 on the motion electromagnet 3 when the 1st electromagnet 1.1 moves to the central axis of the 2nd electromagnet 1.2, obtain its 1st section all outage of c guide rail, d guide rail, e guide rail, f guide rail, g guide rail, h guide rail of power supplys from synchronous core 5; Its 2nd section on c guide rail, the d guide rail that obtains power supplys from synchronous core 5 from top to bottom electric power polarity by negative, positive become positive and negative, realized the power supply commutation of the 2nd electromagnet 1.2, the top of corresponding the 2nd electromagnet 1.2 is the S utmost point by the N pole-change, with the S utmost point formation repulsive force on motion electromagnet 3 tops.

Based on the concrete structure of above-mentioned electrical supply rail 4 and synchronous core 5, when motion electromagnet 3 moves right, from start to finish, constantly quicken.Motion electromagnet 3 is convenient to drive the aircraft moving linearly at short notice by sliding power supply, reaches M2-3 speed.When the axis of motion electromagnet 3 overlaps with two pole center axles of both sides, realize becoming magnetic by synchronous core 5, become repulsive force by former attraction.This process is finished at one time, and promptly the used time is zero.Linear accelerator synchronization principles that Here it is.

Claims

1, a kind of variable magnetic pole linear accelerator is characterized in that:

Mainly form by change magnetic device (1), orbit (2), motion electromagnet (3);

Become magnetic device (1) and be provided with orbit (2), going up at orbit (2) is motion electromagnet (3);

Described change magnetic device (1) is the 1st electromagnet (1.1), the 2nd electromagnet (1.2), the 3rd electromagnet (1.3) along linear array ... N electromagnet (1.N); The pole orientation of each electromagnet is to make the direction of motion electromagnet (3) along orbit (2) accelerated motion.

2, by the described a kind of variable magnetic pole linear accelerator of claim 1, it is characterized in that:

Become magnetic device (1) by the 1st electromagnet (1.1), the 2nd electromagnet (1.2), the 3rd electromagnet (1.3) along linear array ... N electromagnet (1.N); Electrical supply rail (4) and synchronous core (5) are formed, and the pole orientation that guarantees each electromagnet is to make the direction of motion electromagnet (3) along orbit (2) accelerated motion.

3, by the described electrical supply rail of claim 2 (4), it is characterized in that:

Electrical supply rail (4) is made up of the passive synchronous core guide rail of 2 active guide rails and 6 segmentations:

A guide rail, b guide rail are active guide rail, connect the positive and negative electrode of power supply respectively;

Thereafter again and the like be electrically connected;

The winding of the 1st electromagnet (1.1) connects c guide rail, d guide rail the 1st section,

The winding of the 2nd electromagnet (1.2) connects c guide rail, d guide rail the 2nd section,

The winding of the 3rd electromagnet (1.3) connects c guide rail, d guide rail the 3rd section;

Thereafter again and the like be electrically connected.

4, by the described synchronous core 5 of claim 2, it is characterized in that:

Core (5) places between motion electromagnet (3), the electrical supply rail (4) synchronously, is connected as a single entity with motion electromagnet (3); Core (5) is made up of 8 groups of brushes synchronously, contacts with 6 passive synchronous core guide rails with 2 active guide rails of electrical supply rail (4) respectively from top to bottom; From top to bottom, 1,3,6,7 brushes are connected, and 2,4,5,8 brushes are connected.

5, by the described a kind of variable magnetic pole linear accelerator of claim 1, it is characterized in that:

Orbit (2) supports and slides for motion electromagnet (3), makes a kind of smooth track with non-magnet material.

6, by the described a kind of variable magnetic pole linear accelerator of claim 1, it is characterized in that:

Motion electromagnet (3) is made up of electromagnet (3.1), winding (3.2), brush (3.3), ball bearing (3.4);

The ball bearing (3.4) that electromagnet (3.1) is provided with places on the operation track (2);

The two ends of the winding (3.2) on the electromagnet (3.1) are connected with brush (3.3), and a guide rail, the b guide rail of brush (3.3) contact electrical supply rail (4) get.