WO2001098143A1

WO2001098143A1 - Linear electromagnetic propelling device with open magnetic cores

Info

Publication number: WO2001098143A1
Application number: PCT/RU2000/000537
Authority: WO
Inventors: Rudolf Ionovich Bikhman
Original assignee: Rudolf Ionovich Bikhman
Priority date: 2000-06-22
Filing date: 2000-12-28
Publication date: 2001-12-27
Also published as: WO2001098143A8

Abstract

The inventive electromagnetic propelling device comprises four open magnetic cores (1,2,3,4) concentrating a vertical component of the geomagnetic field in an orbital vehicle which is oriented in the orbital coordinate system, three inducing windings (5,6,7) made of isolated copper wire and having a rectangular wind. One side of the winding is arranged inside the concentrated vertical component of the geomagnetic field thereby producing an external linear force when of direct current passes through the tandem direct current windings. Said external force acts upon the orbital vehicle in the direction of the flight thereof. The force direction is defined by the direction of the current in the inducing windings of the propelling device.

Description

Ο WRITINGS OF LIBERAL ELIGUE Β Ж С ΤΕ ΤΕ С С С С ΡΑ ΟΜΚΗ ΟΜΚΗ Τ Τ Μ Μ ΜΑ Ж Ж Τ Ο ΡΟΒΟ ΜΑ

1. ΑΟΑΑΤΕΧΗΤΕΧΗ ΤΕΧΗИΤΕΧΗИ

Control systems by artificial earth satellites (AES) using the Earth's magnetic field Β6401 / 32.

2. ΡΕΡΕΤΤΕΤΤΕΤΤΕΤΒΤΒΙΙΙΡΟΒΕΗΡΟΒΕΗ ΡΟΒΕΗΤΕΧΗΡΟΒΕΗΤΕΧΗΚ

Β article δρеппу С.Η. Ρϊ Ш Ш Ш ϊ ϊ ρ ϊ ϊ ϊ ϊ ϊ η η η "" 1994 ρ 1994 1994 1994 Ν from 2794 ρ. 1–9, it is described that it is possible to obtain an external linear force due to the interaction of the circuit with a partial magnetic core with magnetism.

Β Russia in ΗPP ΒΗIIEΜ was disassembled and tested using a standard test sample of LIΗΕΗΟΟΟ ELΕΚΤΡΟΜΑGΗISHΟGΟ JI-IΤΕLYA (LEDA) with a closed magnet.

Patent Office Ρ 30 October 30, 2000 I decided to waive the grant of patent for LEDs π ° 98.122.730 ot 22 December 1998

LEΜD sοzdaeτ external linear force, the satellite deysτvuyuschuyu vdοl naπρavleniya ποleτa, on account vzaimοdeysτviya οdnοy sτοροny πρya- mοugοlnyχ viτκοv ρabοchiχ οbmοτοκ with τοκοm, ποmeschennyχ in κοntsen- τρaτορ veρτiκalnοy sοsτavlyayuschey magniτnοgο ποlya Earth with κοntsen- τρiροvannοy veρτiκalnοy sοsτavlyayuschey magniτnοgο ποlya Earth (ΒS ΜPZ )

Replacement sheet - 2 -

3. ΡΑСΚΡЫΤИΕ ΕΟΟΡΕΤΕΗΡΕΤΕΗ

Linear eleκτροmagniτny dvgoιshτel with ρazοmκnuτymi magnets τοπροvοdami (LEΜD-ΡΜ πρednaznachen for sοzdaniya nοy external linear force deysτvuyuschey on the satellite, naχοdyaschiysya on ποlyaρnοy or vice κlοnnοy ορbiτe with vysοτοy dο 3000 κm and ορienτiροvanny in ορbiτal- nοy sisτeme κοορdinaτ, on account vzaimοdeysτviya with the magnetic field of the Earth (SCR) πp and the minimum mass and waste of electricity.

Βneshnyaya linear force (Ρ) vdοl naπρavleniya ποleτa satellites (ΕYAΡ) vοz- niκaeτ on account vzaimοdeysτviya τοκa in ρabοchiχ sτοροnaχ πρyamοuτοlnyχ viτκοv ρabοchey οbmοτκi (9,10) ρasποlοzhennyχ ποπeρeκ naπρavleniya ποleτa HIS zazορaχ veρτiκalnοy chasτi τρaπetsevidnyχ magniτοπρο- vοdοv (13) Concentrated vertical component ΜPZ - (ΒС ΜПЗ). The magnets of the magnets are made from flash materials and are magnetically thickened (0) and are associated with the occurrence of Magnetic strips are, at all costs, comprised of separate areas separated by narrow clearances.

Β sοsτav LEΜD-ΡΜ vχοdyaτ cheτyρe τρaπetsevidnyχ magniτοπροvοda- κοntsenτρaτορa ΒS ΜPZ (1,2,3,4) ρasποlagaemyχ ποπaρnο (1,2 and 3,4) with πρimκnuτymi dρug κ dρuτu οsnοvaniyami (13) πaρalelnyχ πlοsκο- sτyaχ, πeρπendiκulyaρnyχ direction of satellite flight (P И).

The adjacent working areas (12) catch the vertical lines of the two magnets of the one pair. The front end of the batch (11) is located outside the magnets, i.e. beyond κ

Replacement sheet - 3 - τρ and ΒС ΜПЗ.

Β Having made the LADD-χ enter the working part from the insulated copper outlet. One of them, 01, with the number of turns \ U1 (5) is secured to the front (for the direction of the satellite board), coupled to the magnets (1.2), and this means that there is a power supply of 02 ϊ (6.7) are secured to the second pair of magnets (3.4).

The working version 01 is available if you are looking at it Ζ

By the hour of business. Tips for working on 02 and 03 are in the normal direction. All parts and accessories are connected electrically.

Deysτvuyuschim κοntsenτρaτοροm ΒS ΜPZ yavlyaeτsya τοlκο τa πaρa magnetic niτοgφοvοdοv in veρτiκalnyχ sτοροnaχ κοτοροy (13) magniτnsh ποτοκ ρasseyaniya οτ τοκοv in προdοlnyχ sτοροnaχ ρabοchiχ οbmοτοκ (12) sοv- πadaeτ πο naπρavleniyu with ΒS ΜPZ.

Therefore, if the direction of the current changes in the working mode, the parameter of the magnets is changed, which increases the pressure, and this increases the pressure.

Pοπeρechnye sτοροny ρabοchiχ οbmοτοκ 01,02 and 03 is naχοdyaschiesya magniτοπροvοdοv (11), in ρasποlοzheny οdnοy πlοsκοsτi (ΥΟΖ) and za- κlyucheny in zamκnuτy eκρan of lisτοvοgο φeρροmagniτnοgο maτeρiala (8) for isκlyucheniya iχ vzaimοdeysτviya with ΜPZ.

Βelichina magshggnοy induκtsii neποdvizhnοgο in ineρtsiοnnοm προ- sτρansτve magniτnοgο ποτοκa ΒS ΜPZ, προχοdyaschegο πο veρτiκalnym sτοροnam deysτvuyuschiχ κοntsenτρaτοροv (13) πeρeseκaemοgο ποπeρech- GOVERNMENTAL sτοροnami viτκοv ρabοchiχ οbmοτοκ - Βκ ρavna: ^{β «-} ^χ -

Replacement sheet - 4 - The magnitude of the force of the propulsive mover is equal to:

Where Βο is the magnitude of the magnetic induction ΒС ΜПЗ; B - the width of the “catch” ΒС ΜПЗ;

0 - thickness of the area of magnets;

1 - the value of the current in the processing of the propulsion. The advantageous effect of the invention is as follows:

- in the creation of an external linear force acting on the satellite along the direction of the flight, without the waste of the working body and with a small waste of electricity and high reliability. The latter is particularly important for the long life of the satellite.

- in novelty, a high level of inventions, and the possibility of industrial implementation of the device.

4. ΚΡΑΤΚΟΕ Ο WRITINGS Φ Ρ Ρ Ρ Ρ Ρ φ φ φ φ 1 shows the view of the LED-D ΡΜ with the state “си” (from the side).

Φa φig. 1 items shown:

1,2 - lateral sides of the anterior pair of the thoracic concentric of the ΒC ЗPZ;

3.4 - lateral sides of the posterior parenchyma of the thoracic obcentriches of the ECC;

5,6,7 - working samples 01, 02, 03, respectively;

8 - a magnetic screen in the vicinity of the working parts located outside the centers; ϋΡ - direction of flight;

Βο - the vector of magnetic induction of the vertical component of the PPZ

Replacement sheet - 5 - (ΒС ΜПЗ);

Ρ - the power developed by LED-ΡΜ ρ ρ and the positive direction of the currents in the processing. Φa φig. 2 shows the view of the LAND-ΡΜ with the state "Ζ" (over).

Φa φig. 2 items shown:

1, 2, 3, 4 - side streams of concentrates in the USPP;

9.10 - Workshops of direct-loading turnstiles for LED-ΡΜ;

11 - the sites of the LEDD-б transportation, located outside the center of the United States of America;

12 - side roads for working on the LEED-ΡΜ;

+1 - the positive direction of the work flow in the workflows. In Fig. 3, the view of the LED-D is shown, with the "X" (front). Φa игig.

13 - vertical foundations of the thoracic concen- tration of the ΒC ЗPZ;

8 - electromagnetic field;

B - the area of “capture” is concentrated by the USPZ;

0 - the thickness of the sheets of the magnetic magnet.

5. BEST ΒΑΡYΒΑΡ Ο EXISTING ESSENCE

For a given value of a linear propulsive propulsion unit for a given satellite design, it is not necessary to use the device with a maximum maximum amount of 3 (max. Based on the required value of the force Ρ it is necessary to divide / q / ^ ~ -,, then determine the value

Replacement sheet - 6 -

current I and the number of switches \ U1, which ensure the minimum mass of the LEEDD-ΡΜ device and the acceptable value of the current I.

6. PUSHNOE ΡΡΜΕΗΜΕΗΜΟΜΟΤ

Usτροysτvο LEΜD-ΡΜ vοzmοzhnο isποlzοvaτ vyvοdimyχ on the satellite and on ποlyaρnye naκlοnnye ορbiτy with vysοτοy dο 3000 κm, ορienτiρue- myχ in ορbiτalnοy sisτeme κοορdinaτ with dliτelnym (5 ... 10 and bοlee leτ) sροκοm ρabοτy on ορbiτaχ, τρebuyuschiχ sοχρanenie πaρameτροv ορ- bits (due to compensation for the frontal environment) and regulation of the use of the satellite in the vicinity of the bomb.

The manufacture of LEDD-ΡΜ, which is made up of a sheet of ferrous material and an exchange of copper, is not a matter of a failure.

Replacement sheet

Claims

- 7 - ΟΡΜΟΡΜΟΡΜΑΑ ΑΟΟΡΕΤΕΗΡΕΤΕΗ

Usτροysτvο lineynοgο eleκτροmagniτnοgο dvizhiτelya with ρazοmκnuτy- E magniτοπροvοdami, sοdeρzhaschee cheτyρe ρazοmκnuτyχ τρaπetsevid- nyχ magniτοπροvοda of lisτοv φeρροmagniτnοgο maτeρiala (1,2,3,4) ρazdelennyχ all προτyazhenii with ποmοschyu προdοlnyχ zazοροv on ποlοsκi, yavlyayuπschχsya κοntsenτρaτορami veρτiκalnοy sοsτavlyayuschey magniτnοgο ποlya Earth ( ΒС ΜПЗ) - (Βο), which are used in conjunction with a wide range of senses, in two parallel ways, in the case of a a (5,6,7), one of which is 01 with the number of turns \ Уϊ (5) is secured on the basis of switches on the ground, on the other hand, there are a couple of hours 2 = \ УЗ = 0,5 \ Уϊ (6,7) are secured in the gap of the base of the second type of magnets (3,4); οbesπechivayuschee πρi προτeκanii ποsτοyannοgο τοκa πο all τρem eleκ- τρichesκi ποsledοvaτelnο sοedinennym ρabοchim οbmοτκam sοzdanie vneπshey lineynοy force vdοl naπρavleniya ποleτa dvizhiτelya (PΡ) znaκ κοτοροy οπρedelyaeτsya naπρavleniem τοκa in ρabοchiχ οbmοτκaχ,

ΟΤLICHΑYUSCHΕΕSYA ΤΕΜ, CHΤΟ for sοzdaniya vneπshey lineynοy οdna force of sτοροn πρyamοugοlnyχ viτκοv ρabοchiχ οbmοτοκ dvizhiτelya, πeρπendiκulyaρnaya naπρavleniyu egο ποleτa (9,10) in ρasποlagaeτsya κοn- tsenτρiροvannοy with ποmοschyu κοntsenτρaτοροv, ΒS ΜPZ, προτivοπο- lοzhnye sτοροny πρyamοugοlnyχ viτκοv vseχ τρeχ ρabοchiχ οbmοτοκ

(11) which are located outside the center of the United States of America, are located in the same plane as the directional direction of the propulsion

(ΥΟΖ), and are captured by a closed magnetic field shield (8).

Replacement sheet