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Publication numberUS3506023 A
Publication typeGrant
Publication dateApr 14, 1970
Filing dateApr 8, 1968
Priority dateApr 8, 1968
Publication numberUS 3506023 A, US 3506023A, US-A-3506023, US3506023 A, US3506023A
InventorsBogart Robert M
Original AssigneeUs Air Force
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Apparatus for controlling the flow of particles of magnetic material through an orifice
US 3506023 A
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Description  (OCR text may contain errors)

3 1 2 m 0 e 6 0 a. 5% M 3 W e Eh TCS RI AF2 R. M. BOGART FOR CONTROLLING THE FLOW OF P GNETIC MATERIAL THROUGH AN ORI SA 0 H 8 P 6 T w w 8. u H A OW MW 1 l A F R mm m0 mm W a m xgigg M April 14, 1970 R. M. BOGART 3,506,023

APPARATUS FOR CONTROLLING THE FLOW OF PARTICLES OF MAGNETIC MATERIAL THROUGH AN ORIFICE Filed April 8, 1968 2 Sheets-Sheet 2 United States Patent 3,506,023 APPARATUS FOR CONTROLLING THE FLOW OF PARTICLES OF MAGNETIC MATERIAL THROUGH AN ORIFICE Robert M. Bogart, Arlington, Mass., assignor to the United States of America as represented by the Secretary of the Air Force Filed Apr. 8, 1968, Ser. No. 719,336 Int. Cl. F16c 1/04 US. Cl. 13781.5 11 'Claims ABSTRACT OF THE DISCLOSURE An apparatus for controlling the flow of particles of magnetic material through an orifice. The apparatus has, as principal components, a valve and a hollow conduit. The valve component includes a round horseshoe permanent magnet on a rotatable shaft, a rotary solenoid energized by a power source, linkage to rotate the magnet 90 when the solenoid is energized, and a suitably placed flat coiled spring to urge the counter-rotation, and the return to the original position, of the magnet when the solenoid is de-energized. The hollow conduit includes, as an integral unit, an upper and a lower portion of magnetic material, a spacer of non-magnetic material interposed therebetween, and an orifice at each end of the hollow conduit. The valve and the conduit are in close proximity to each other, with the long axis of the conduit in a vertical position and parallel to the pole face portions of the round horseshoe magnet. When particles of magnetic material are introduced into the hollow conduit through the upper orifice, the rotational position of the horseshoe magnet relative to the conduit allows or prevents, as desired, the flow of the particles through the lower orifice.

BACKGROUND OF THE INVENTION This invention relates to the art of valves and, more particularly, to an apparatus for controlling the flow of particles of magnetic material through an orifice.

The term magnetic material, as used herein, is intended to mean material or substance which can be magnetized, i.e., the material or substance is not non-magnetic. Such magnetic materials are intended to include those which are referred to as ferromagnetic, paramagnetic and diamagnetic, but are not intended to be synonymous with magnetized materials, i.e.. magnets. Similarly, the term magnetic particle is not intended to mean magnetized particle.

A specific application of this invention is as a valve for controlling the fiow of ballast, in magnetic particle form, used for changing the altitude of large high-altitude balloons, such as the type used in scientific research and in experiments.

With reference to such use for my invention, it is noted that the ballast container is tethered near the mouth, i.e., the appendix, of the balloon, that the ballast consists of particles of magnetic material, that such particles are in the order of from .0049 to .0394 inch in diameter, that such particles are referred to as dust or grit or clean shot, that the altitude of the balloon is controlled by release of quantities of the particletype ballast, and that the present state-of-the-art devices of this type permit the flow of only a maximum of seven pounds of the particles per minute, but do not prevent the clumping or bunching of the particles, withsresultant malfunction of the ballast flow device due to clogging of the output orifice, and, thereby, causes loss of control of the altitude of the balloon and, perhaps, loss of the balloon.

3,505,023 Patented Apr. 14, 1970 "ice My invention prevents clumping or bunching of the particles, permits uninterrupted, but controlled flow of them, and increases the flow of the particles to approximately fifty pounds per minute, if such rate .of flow is desired.

Therefore, my invention obviates current problems in balloon ballast magnetic particle control devices.

Although reference has been made to the use of my invention in balloon art, it is obvious, as noted above, that this is but one specific application of my invention. My invention may be used in any art where the control of flow of magnetic particles is desired.

SUMMARY OF THE INVENTION This invention provides for an apparatus which allows or prevents the flow of particles of magnetic material through an orifice.

Therefore, an object of this invention is to permit the uninterrupted, but controlled, flow of magnetic particles through an orifice.

Another object, obviously, is to prevent the flow of magnetic particles through an orifice.

A further object of my invention is to provide an apparatus which will permit a much higher rate of flow, than is obtainable by present state-of-the-art devices, of magnetic particles through an orifice.

A still further object of my invention is to provide a highly reliable, and yet economical, apparatus for controlling the fiow of magnetic particles through an orifice.

These, and still other, objects of my invention will become readily apparent after a consideration of the description of my invention and of the drawings.

DESCRIPTION OF THE DRAWINGS FIGURE 1 is a plan view, partially schematic and with a fragmented portion, of a preferred embodiment of my invention;

FIGURE 2 is a perspective view of the embodiment shown in FIGURE 1, with cover tilted back and fragmented in part;

FIGURE 3 is a side elevation view with some portions in vertical cross-section and some in fragmentary form, of a schematic representation of my invention in use as a balloon ballast magnetic particle flow control device;

FIGURE 4 is a side elevation view, partially in vertical cross-section and schematic in form, of the principal components of my invention, and how they interact as a result of the applicable magnetic phenomena, when in a no-flow, i.e., closed, mode; and

FIGURE 5 is an end elevation view, partially in vertical cross-section and schematic in form, of the principal components of my invention, and how they interact as a result of the applicable magnetic phenomena, when in a flow, i.e., open, mode.

DESCRIPTION OF A PREFERRED EMBODIMENT With reference to FIGURES 1 and 2, wherein the same components are similarly numbered, a rotary solenoid 10, such as the commercially available Ledex No. 129737- 026, with drive gear 11, is mounted on plate 51 and retained by nut 12 on shaft 13. Interposed between rotary solenoid 10, and nut 12, is coiled fiat spring 14 which, at one of its ends, is affixed to shaft 13.

Leads 21 connect power source 20 to rotary solenoid 10'.

On shaft 33 are positioned, as shown, round horseshoe permanent magnet 30, such as General Electric No. 5U35B, driven gear 31, and set screw collar 32. Shaft 33 is mounted on, and through, plate 52 with bearing 53 and plate 51. Horseshoe magnet 30 is preferably of the Alnico type with a holding force of from 5 to 11 pounds and the face of magnet 30 is normal to the axis of shaft 33.

Hollow conduit assembly 40, i.e. orifice tube assembly, includes, as an integral unit, two conduit sections 4} and 42 of magnetic material, such as iron, with a spacer 43, preferably of brass, interposed between conduitsection 41 and 42 and silver soldered to them at their interfaces, thereby making the unit or assembly an integral one. The hollow portion 44 of conduit assembly 40 extends throughout the assembly, is cylindrical in shape, and has a diameter of approximately /4 inch. Conduit assembly 40 has an outlet or orifice portion 45 and 46 at each end. A push in type ping, such as 47 in FIGURE 1, may be used as an adapter to vary the diameter of either orifice 45 or 46.

All components of my invention are mounted on a base plate 50 and are covered with cover 54, except that base plate 50 has an opening to permit orifice 46 of conduit assembly 40 to protrude and, similarly, cover 54 has an opening to permit orifice 45 to protrude through. Cover 54 protects the components from the elements and prevents dust and the back iiow of magnetic particles 62 from interfering with the operation of the components.

It is to be noted that the pole face portions of magnet 30 are parallel to the long axis of conduit assembly 40 and approximately .032-.035 inch therefrom.

MODE OF OPERATION OF THE EMBODIMENT As has been previously stated, one specific application of .my invention is in the balloon art where my apparatus may be effectively used as a ballast flow control device. That utilization is pictorially represented in FIGURE 3.

With reference to FIGURE 3, my apparatus is connected, in an inverted position, to the opening 61 of ballast container, hopper or bin 60. With my apparatus in a flow mode, i.e., open position, as shown in FIGURE 3, ballast 62, which consists of magnetic particles, flows through ballast container opening 61, through input orifice 46 of hollow conduit assembly 40, through the hollow portion 44 of assembly 40., and is emitted through output orifice 45 of assembly 40.

A rotation of an integral odd multiple of 90 of magnet 30 will stop the flow.

A description of the flow and no flow action of my apparatus can best be explained by reference to FIG- URE 4 and FIGURE 5.

In FIGURE 4, the principal components of my invention are shown. These are hollow conduit assembiy 40 and round horseshoe permanent magnet 30. Their relative positioning, as shown in FIGURE 4, is a no flow mode, i.e., closed position.

The operation, and applicable theory, in the no fiow mode is as follows: Conduit sections 41 and 42 are in close proximity to magnet 30. Since conduit sections 41 and 42 are of magnetic material, they become magnetized. Further, since sections 41 and 42 are near each other and across the pole gap in magnet 30, the magnetic lines of rorce are directed and intensified across the gap be= tween sections 41 and 42. It is to be noted at this point that a brass spacer 43 is interposed between sections 41 and 42, that spacer 43 is non-magnetic, and that spacer 43 is located adjacent to the gap between the pole faces of magnet 30. Thereby, sections 41 and 42 become effectively extensions of magnet 30. If, now, magnetic particles 62 are introduced into hollow portion 44, each particle 62 will itself become a magnet, will be attracted to each other and to the walls of hollow portion 44, and will block hollow portion 44 at brass spacer 43. A no flow or closed position results.

The operation, and applicable theory, in the flow mode, i.e.,-open position, is shown in FIGURE and is as follows: If magnet 30 is rotated 90, or an integral odd multiple, the magnetic lines of force near and across spacer 43 are neutralized and particles 62 in that area are demagnetized. In addition, since each pole, i.e., N and S, of magnet 30 is attempting, at the same time, to magnetize the same conduit sections. 41 and 42, the lines of force are neutralized. As a result, conduit sections 41 and 42., and the remainder of particles 62, are demagnetized. Therefore, particles 62 flow freely from ballast bin 60, through conduit assembly 40, and from output orifice 45.

With regard to the mechanical, electromechanical, and magnetic actions involved in the actual utilization of my apparatus as a balloon ballast flow control device, it is best to return to FIGURES 1, 2 and 3, for a detailed description.

With reference to FIGURE 3, when my apparatus is connected, in an inverted position, to the ballast bin 60, it is in the no flow or closed position. After the balloon is released and is in flight, if it is desired to change the altitude of the balloon, the ballast particles 62 are released rom the ballast bin 60 and through my apparatus. This is done as follows; With reference to FIGURES 1 and 2, the power source 20 is turned on by suitable means, such as a command signal from a ground-based station. The power from power source 20 and through leads 31 energizes rotary solenoid 10 which turns drive gear 11. Driven gear 32 is thereby rotated, as are rotatable shaft 33 and magnet 30. However, since flat coiled spring 14 is constrained to permit the rotation of magnet 30 to integral odd multiples of when magnet 30 reaches that degree of rotation, it stops and remains in that position. That position, as hereinbefore described, is the flow or open position. Ballast particles 62 are thereby released and the altitude of the balloon is changed. To return my apparatus to the no flow or closed position, and thereby prevent the flow of ballast, the power source 20 is turned off. Coiled spring 14 which has been in an expanded state during the power on phase, recoils, causing the 90 rotation back of magnet 30, by causing the counter rotation of drive gear 11, driven gear 31, and shaft 33.

While there has been shown and described the fundamental features of my invention, as applied to a preferred embodiment, it is understood that various substitutions and omissions may be made by those skilled in the art without departing from the spirit of the invention. For example: (a) bar magnets or electromagnets may be substituted for the round horseshoe magnet; and (b) a motor, rather than a rotary solenoid, could be used.

I claim:

-1. An apparatus for controlling the flow of particles of magnetic material comprising:

(a) means for generating magnetic flux;

(b) means for orienting said means for generating magnetic flux, so that the direction of said magnetic flux may be changed to an integral odd multiple of 90;

(c) and a hollow conduit assembly comprising a pair of axially aligned sections, each insulated from the other, wherein each section is in close proximity to a pole of said means for generating a magnetic flux, with the passageway of each section orthogonal to the rines of magnetic flux.

2. An apparatus for controlling the flow of particles of magnetic material comprising:

(a) means for generating magnetic flux, connected to a rotatable shaft having thereon a gear to be driven;

(b) means for orienting said means for generating magnetic flux, so that the direction of said magnetic flux may be changed 90;

(c) a drive gear adjacent to and meshing with said gear to be driven, and connected to said means for orienting said means for generating magnetic flux;

(d) means for rotating said drive gear;

(e) a hollow conduit assembly, in close proximity to said means for generating magnetic flux, vertically disposed and parallel thereto, and including, as an integral unit, sections of magnetic material with a nonmagnetic spacer interposed therebetween, with said magnetic sections and spacer hav ng a continuous cylindrical hollow portion of constant diameter throughout, with said hollow portion having an orifice at each end;

(f) means for varying the diameter of the orifices of said hollow portion of said conduit assembly;

(g) and means for housing all components.

3. The apparatus, as described in claim 2, wherein said means for generating magnetic flux is a round horseshoe permanent magnet.

4. The apparatus, as described in claim 2, wherein said means for generating magnetic flux are bar magnets of the permanent type.

5. The apparatus, as described in claim 2, wherein said means for generating magnetic flux is a solenoid with a power source. I

6. The apparatus, as described in claim 2, wherein said means for orienting said means for generating magnetic flux is a rotary solenoid, with a power source, with the shaft of said rotary solenoid having a coiled flat spring restraining rotation of said shaft to allow the direction of said magnetic flux to be changed 90 only.

7. The apparatus, as described in claim 2, wherein said means for orienting said means of magnetic flux is a motor, with a power source, with the shaft of said motor having a coiled fiat spring restraining rotation of said shaft to allow the direction of said magnetic flux to be changed 90 only.

8. The apparatus, as described in claim 2, wherein said means for rotating said drive gear is a rotary solenoid with power source.

9. The apparatus, as described in claim 2, wherein said means for rotating said drive gear is a motor with power source.

10.;The apparatus, as described in claim 2, wherein said means for varying the diameter of the orifices of said hollow portion of said conduit assembly is a push in type plug of the desired diameter.

11, The apparatus, as described in claim 2, wherein said means for housing all components includes a base plate, to which are connected said components, having a suitably located opening to allow an orifice of said hollow conduit assembly to protrude, and a cover, fitting over said components and fitting onto said base plate, with said cover having a suitably located opening to allow the other orifice of said hollow conduit assembly to protrude.

References Cited UNITED STATES PATENTS 3,417,771 12/1968 Ernst 137-815 HAROLD w. WEAKLEY, Primary Examiner US. Cl. X.R.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US3417771 *Sep 24, 1965Dec 24, 1968Hans ErnstFlow control apparatus for fluent magnetic materials
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3701357 *Sep 23, 1969Oct 31, 1972Asea AbElectromagnetic valve means for tapping molten metal
US3995661 *Sep 22, 1975Dec 7, 1976Wheelabrator-Frye, Inc.Flow control valve for magnetic particulate
US5113890 *Nov 14, 1990May 19, 1992Hylsa S.A. De C.V.Method and apparatus for regulating the flow of particulate ferromagnetic solids
US6044858 *Feb 11, 1998Apr 4, 2000Concept Engineering Group, Inc.Electromagnetic flow control valve for a liquid metal
US6321766Jan 14, 2000Nov 27, 2001Richard D. NathensonElectromagnetic flow control valve for a liquid metal with built-in flow measurement
US7249604 *May 10, 2002Jul 31, 2007Vasmo, Inc.Medical devices for occlusion of blood flow
US8087480Nov 16, 2006Jan 3, 2012Shell Oil CompanyDevice and method for feeding particles into a stream
Classifications
U.S. Classification137/807, 137/827, 137/343, 137/269, 251/194, 251/65
International ClassificationF16C33/82, F16K31/08, F16C33/76
Cooperative ClassificationF16K31/088
European ClassificationF16K31/08M2