US3500079A - Electromagnetic machines - Google Patents

Electromagnetic machines Download PDF

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US3500079A
US3500079A US594191A US3500079DA US3500079A US 3500079 A US3500079 A US 3500079A US 594191 A US594191 A US 594191A US 3500079D A US3500079D A US 3500079DA US 3500079 A US3500079 A US 3500079A
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magnetic
armature
piston
machine
air gap
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Maurice Barthalon
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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K33/00—Motors with reciprocating, oscillating or vibrating magnet, armature or coil system
    • H02K33/12—Motors with reciprocating, oscillating or vibrating magnet, armature or coil system with armatures moving in alternate directions by alternate energisation of two coil systems
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K33/00—Motors with reciprocating, oscillating or vibrating magnet, armature or coil system
    • H02K33/02—Motors with reciprocating, oscillating or vibrating magnet, armature or coil system with armatures moved one way by energisation of a single coil system and returned by mechanical force, e.g. by springs

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  • This invention concerns electro-magnetic variable reluctance machines, that is machines that comprise an electro-magnetic circuit comprising a fixed circuit and an armature of magnetic material which is a relatively poor conductor movable relative to the fixed circuit the movement being rectilinear.
  • This invention concerns especially the structure and assembly of such machines.
  • Electro-magnetic machines having linear movement and variable reluctance in a magnetic cirruit are already known.
  • the most interesting comprise an armature in a metal preferably a poor conductor but possessing good magnetic characteristics, sliding with a clearance practically independent of the stroke'in an air gap in which the lines of force are transverse relative to the direction of movement.
  • An arrangement of this type gives a very high force per unit of mass of the magnetic armature for a given current, this force varying little with the stroke except at the ends where it suddenly becomes zero and at the centre where it suddenly changes sign for a small variation of stroke.
  • the magnetic armature p-referably a poor conductor, being connected to this piston and being alternatively drawn into the air gap of the magnetic circuit under the action of a magnetic field created by successive electrical impulses feeding a coil, and on the other hand drawn out of this air gap, either by elastic means or by a second magnetic circuit acting on the same moving assembly.
  • the circuits fed alternatively by electric impulses dephased by 180 may each comprise an armature, the two armatures being rigidly connected.
  • Variable reluctance machines are also known operating in a reverse manner from the preceding, in which the piston and the cylinder form a reciprocating combustion engine, the piston driving at least one armature which causes the reluctance of a magnetic circuit to vary alternatively, and having a movement perpendicular to the lines of force created in the air gap by an excitation coil or magnet.
  • a further well-known difiiculty is the tendency of the poles to move towards each other under the influence of the considerable electro-magnetic forces of attraction which requires the use of mechanical means to maintain constant the distance between the poles and, therefore, the lateral clearance of the magnetic armature.
  • the parallelepiped forms of the magnetic armature, preferably a poor conductor, and of the circuits and therefore the form of the fixed magnetic circuit do not lend themselves easily to inexpensive quantity production in view of the tolerances required for reliable and satisfactory operation.
  • the object of the present invention is to achieve machines having variablereluctance and a field perpendicular to the movement of the armature which overcome the disadvantages referred to above.
  • Another object of the invention is to achieve for such machines a simple, accurate and cheap construction and easy assembly.
  • the electro-mechanical energy converting machine of the type comprising at least one magnetic circuit with a fixed part comprising a coil supplied from a source of electrical energy and with a moving part constituting a magnetic electrically weakly conducting armature moving in the field created between the pole surfaces of the fixed magnetic circuit and trans versely with respect to said field, the said armature having rectilinear movement and being directly coupled to an operating slide, is characterised in that said magnetic armature has a tubular cylindrical structure, in that said pole surfaces are also cylindrical and in that at least one part of said fixed magnetic circuit is located within said armature for at least a part of the stroke of said magnetic armature.
  • the poles and the armature having a cylindrical structure can only make line contact and not over the whole and surface of the poles; as a result the lateral force acting on the armature, when it departs slightly from the central position in the air gap, cannot reach serious value.
  • the external surface of the air gap is formed by a closed cylindrical tube, it is well able to resist crushing which practically eliminates movement of the poles towards each other.
  • Machines according to the invention may in the first place form driving machines in which the armature drives an operating slide and thus form reciprocating electric motors such as actuators, electro-compressors, electro-pumps and reciprocating electric motors.
  • the invention also refers to the realisation of electric generating machines such as motor alternators, motor pulsegenerators, etc.
  • the fixed magnetic circuit and the armature have sections in directions orthogonal to the direction of movement which are circular. Considerable resistance to deformation arising from the magnetic attraction of the poles is thus obtained. At the same time this structure lends itself well to rapid, precise and inexpensive machining.
  • the circular section cylindrical structure also gives symmetrical temperature distribution when the machines warms up during operation, thus reducing distortion when hot, allowing clearances to be reduced and the unit power of the machine to be increased.
  • the magnetic circuit completely envelops the coil which is formed by a toroid of revolution co-axial with the circuit.
  • the mean distance between one turn and the circuit thus reaches a very low value and each segment of a turn remains perpendicular to the movement of the armature.
  • Another advantageous characteristic of the invention consists in providing a certain number of non-conducting volumes traversing from side to side and from the exterior to the interior the parts forming the magnetic circuit. These non-conducting volumes preferably have their axial planes passing through the axis of the cylinder and form separations between the magnetic sheets of the fixed or moving parts of the magnetic circuit. This disposition avoids the formation of annular eddy currents which in the case of the moving armature can be sufiiciently intense almost to suppress the magnetic attraction in the air gap.
  • non-conducting volumes can be used in the case of machines of a certain size as cooling air circulation ducts in the circuit.
  • the cylindrical static and moving parts are made using stampings having a profile corresponding to the section of the said circuits on a plane passing through the axis.
  • stampings are assembled by casting a non-magnetic and non-conductive material, such as for example epoxy resin, into the spaces which separate them.
  • the elements forming either the static or the moving part of the electro-magnetic circuit are assembled by means of a single piece comprising coaxial bores in which such elements are inserted.
  • the axis of the machine and so the alignment of the parts are precisely fixed which allows very small clearances to be used, ensuring precise guiding avoiding lateral hunting of the moving parts.
  • a particularly simple machine may be realised which is easy to machine and assemble with precision and speed.
  • Another preferred characteristic of the invention consists in covering at least one of the faces of the air gap with a film of non-magnetic anti-friction material such as polytetrafluoroethylene, which completely prevents any contact between the poles and the armature even along a line contact and which practically eliminates lateral forces on the armature.
  • a film of non-magnetic anti-friction material such as polytetrafluoroethylene
  • the magnetic circuit should be formed by means of an assembly of a certain number of elements of simple geometric form, which facilitates assembly.
  • This method has the particular advantage of allowing the form or the quality of the metal used in the different parts of the magnetic circuit to be adapted to the values necessary to obtain optimum performance.
  • the thickness of the laminations used for the poles may difier from that for the rest of the machine.
  • FIG. 1 shows a first industrial embodiment on axial section II of FIG. 2.
  • FIG. 2 shows sections of FIG. 1 respectively on IIa Ila on the left hand side and IIb-IIb on the right hand side, the armature having been removed.
  • FIG. 3 is a variant of the first embodiment shown partly as an external view, and partly in section, the moving parts being in half section.
  • FIG. 4 shows the third industrial embodiment on axial section IVIV of FIG. 8.
  • FIG. 5 is an axial section of the same machine on VV of FIG. 7.
  • FIG. 6 is a part section on IVIV of FIG. 5.
  • FIG. 7 is a section on VII-VII of FIG. 5.
  • FIG. 8 is another part section on VIII-VIII of FIG. 5 after removal of valve.
  • FIG. 9 is a plan view of a valve blade from the preceding embodiment.
  • FIG. 10 is an axial section of a fourth embodiment on XX of FIG. 11.
  • FIG. 11 is a half section on XIXI of FIG. 10.
  • FIG. 12 is another half section on XIIXII of FIG. 10.
  • FIG. 13 is an axial section on XIII-XIII of FIG. 14 of a variant of FIG. 10.
  • FIG. 14 is a section on XIVXIV of FIG. 13.
  • FIG. 15 is a partial transverse section, large scale, of part of the armature of the preceding embodiment.
  • the machine comprises a fixed magnetic circuit preferably manufactured from sintered material, which combines high induction saturation, high permeability and high resistivity which sensibly prevents eddy currents.
  • a composition comprising pure iron oxide and manganese oxide and whose grain size is of the order of 10 microns could be used advantageously.
  • This circuit comprises a magnetic core 1 forming a first pole piece and including a solid central cylinder 1a and an external annular cylinder 1b. On the magnetic core 1 is centered the second pole piece 2 of circular cylindrical section.
  • the single magnetising coil 3 which is thus surrounded by the magnetic circuit and which is of toroidal form, which gives a good efiiciency, low flux loss and low manufacturing cost.
  • the coil 3 is fed by successive electric impulses provided by conductors 3a from a source 3b of alternating current (for example at 50 cycles), this circuit further comprising a rectifier 30 such as a diode, allowing only one out of the alternations to pass.
  • the cylindrical section magnetic armature 4 perpendicular to the radial magnetic field created in the cylindrical annular air gap 21 and with residual clearance less than /5 of this air gap, the armature being made in a magnetic material (that is with high saturation induction) and which is furthermore arranged to have an appreciable electrical resistance in respect of currents circulating along an annular path.
  • a sintered magnetic material having high permeability and high resistivity.
  • the radial clearance of piston 6 in cylinder 7 is preferably less than half the magnetic clearance between the armature and the surface of the poles. This limits the transverse magnetic force which acts upon the armature when it leaves its axial position, to a small value.
  • the operating slide is formed by piston 6.
  • the moving assembly is thus especially simple to machine and manufacture.
  • the ratio between the air gap and the residual clearance which is greater than 5, results in a high flux variation and thus in high unit power.
  • the compresor is closed by a cylinder head 9 in which valve housings 10 and 11 are screwed, the housings carrying the suction valve 12 (and its spring 13) and the delivery valve 15 (and its spring 16).
  • the annular armature 4 has ports 17 which at the end of the stroke are opposite ports 18 drilled in cylinder 7, so as to ensure the distribution of cooling air pumped by the under face of piston 6.
  • Cylinder 7 is also provided with cooling fins 19. Channels 20 supply cooling air through the air gap 21 to the air jacket 22 surrounding the coil 3.
  • a non-magnetic spacer 24 is interposed between the cylinder 7 and the pole piece 2 and ensures their respective centering.
  • Another non-magnetic spacer 25 is interposed between the coil 3 and the pole piece 2. In the case of small machines without cooling air circulation the spacer 25 may hermetically seal the volume containing coil 3 which is thus protected against corrosive gases or liquids from the other half of the machine.
  • the machine thus arranged is of the type which delivers fluid during the return stroke, that is, the electro-magnetic energy created by the excitation of coil 3 is first entirely transformed into spring energy in cushion 5 in the form of compressed air.
  • Armature 4 then closes channel 20 and the air contained in the cushion volume 5 is compressed, thus storing spring energy.
  • the excitation of coil 3 decreases very rapidly and the moving assembly is returned towards the right, in direction H by the energy of the compressed air contained in cushion volume 55.
  • the fluid contained in the compressor volume 8 is compressed and then delivered through delivery valve 15 in the same way as in a conventional machine.
  • the structure of the compressor it self differs very little from that of a conventional compressor, particularly in its essential parts (cylinder, piston, cylinder head, valves) which is advantageous and economical for mass production manufacture.
  • At the end of the stroke cushion 5 is at a lower pressure then atmospheric pressure which results in the admission of fresh air into this volume when ports 17 and 18 coincide.
  • the characteristics of the structure intended for the pole pieces, the armature and the coil of the machine ensure the advantages of economy of material, thermal symmetry resistance to the movement of the poles'towards each other, and good centering of the static and moving parts as explained above.
  • the magnetic circuit 30, which is symmetrical on plane C-C, comprises on each side annular poles 31 and 32 of revolution defining the annular air gap 47.
  • the magnetic circuit is formed from two identical parts 33 and 34, in which an annular channel is hollowed on the face opposite the poles, in the form of a circular section toroid 35.
  • a magnetised coil 36 is located in this channel 35 and is fed by successive electrical impulses as in the preceding variant.
  • the magnetic armature 37 is formed of lamination separated in planes orthogonal to the axis of movement (for example by varnished sheets of annular sector shape) and also on planes passing through the axis of movement, so as to reduce the losses and parasitic forces due to eddy currents.
  • the longitudinal separation of the laminations are further used as grooves for anti-friction material 38, such as polytetrafluoroethylene, formed as bands.
  • the magnetic armature 37 is attached to the skirt 39 of compressor piston 40, which has a different diameter and is of non-magnetic material.
  • the piston 40 which can be equipped with sealing means 41, slides in cylinder 42, closed by cylinder 43 carrying the suction and delivery valves of any known type and not shown.
  • the compressor volume 48 is defined by piston 40, cylinder 42, and cylinder head 43.
  • a non-magnetic spacer 44 separates the cylinder from the magnetic circuit and ensures their respective centering.
  • a spring located in piston 40 ensures the return of the latter to the top dead point.
  • the assembly mounted on the other side of plane CC is exactly symmetrical with that already described.
  • the two parts 33 and 34 of the magnetic circuit and the two spacers 44 are assembled by tie rods 46.
  • piston 40 attached to the armatures, draws the fluid into the compressor volumes 48 and at the same time compress springs 45.
  • springs 45 giving back the energy stored during the power stroke, push pistons 40 away from the centre in direction 1 while compressing the fluid in volume 48 and delivering it to the exterior through the delivery valves.
  • the two preceding embodiments thus provide two machines, One having twice the power of the other while using the same parts for the compressor assembly (cylinder, cylinder head, pistons, springs, armature).
  • the machine is entirely of revolution and is symmetrical With respect to the central plane. It comprises (FIG. 4) two magnetic cores 51a, 51b in which are mounted two pole pieces 52a, 52b thus completing the two static magnetic circuits which are assembled by means of the external cylinder 73 of non-magnetic material whose axis precisely determines the axis of the machine.
  • the magnetic circuits are excited by coils 53a, 53b supplied from an alternating source 530 across inverted diodes 53d, 53e mounted in parallel.
  • the piston skirts 61 comprise two magnetic armatures 56a, 56b, relatively poor conductors sliding in the annular air gaps 57w, 57b whose external extremities 58a, 58b form return cushions.
  • the skirts 56a, 56b, piston 61 and magnetic cores 51a, 51b define two compressor volumes 59a, 59b.
  • a peripheral extension of piston 61 forms a ventilation piston 62 sliding in the non-magnetic cylinder 63 and thus defining two ventilation volumes 60a, 60b, which avoids complicating the machine by an external source of ventilation.
  • Volumes 60a and 60b are fed through single piece suction valves 64 formed from a disc of spring steel whose external part 76 (FIG. 9) is trapped between cylinder 63 and pole piece 51 and whose annular central part is cut away to form a certain number of blades 79 by slots 77, themselves rounded at their ends 78.
  • External air passes through ports 74 drilled in the cylindrical casing 73 and through the channels 69 formed in the cores 51a, 51b and the pole pieces 52a, 52b.
  • Air passes from the ventilation volume 60a or 60b in skirt 56a or 56b.
  • the compressed air is delivered through the delivery valve 65a or 65b. This is advantageously located in the central pole piece 51a or 51b with its return spring 66a or 66b.
  • the air is then evacuated through the axial drilling 67a or 67b.
  • Channels 71a, 71b and, 72a, 72b and 75a, 75b form the cooling air circuit, communicate with the atmosphere through posts 75a, 75b in the casing 73, and act as laminations to avoid annular eddy currents.
  • the walls of the channels 71a, 71b, 72a and 72b are formed of molded plastic, such as an epoxy resin. Joints 80a and 80b of flexible non-magnetic material ensure complete separation of the electric part from the pump part which is advantageous in case of corrosive fluids.
  • Valve 64 opens and allows external air to enter under the action of the depression created in volume 6011 by the movement of the piston 62 to the right in direction J
  • Valve 65a closes under the action of spring 66a.
  • Pistons 61 and 62 compress the air contained in volumes 59b and 60b. This air is delivered through canals 71b and 72b, cooling the delivery valve and the core.
  • Fresh air entering through the valve 64a cools skirt 56a directly, then towards the end of the stroke, ports 68a open, the external fresh air flows directly into the compressor cylinder 59a owing to the depression created in this volume by the movement of the piston 61.
  • the air compressed in volume 59b is delivered through valve 65b and axial channel 67b. Also during this end of stroke, skirt 56b closes volume 58b which forms a cushion return means and closes off channel 71b which transforms volumes 60b and 58b into a cushion return means.
  • the return stroke in direction J is entirely symmetrical.
  • FIGS. 4 and indicate the direction of movement of the movable armature by an arrow and the circulation of compression and cooling air by broken lines.
  • the hottest parts due to contact with hot compressed air are those where the heat given out by electromagnetic effects is least, and reciprocally, which results in uniform expansion.
  • the structure described prevents any movement of the pole piece towards one another which might reduce the air gap and require excessive clearance under stationary conditions. In the same way this structure reduces thermal distortion of the assembly to a minimum and provides the best guarantee of maintaining the symmetry with respect to the axis which is essential for obtaining symmetrical electrical and pneumatic forces, and therefore stability and a high efficiency for the machine.
  • the assembly is very compact, has high unit power and comprises very few wearing parts. Its manufacture in quantity is inexpensive.
  • the fourth industrial embodiment is an application of the invention to a motor alternator (internal combustion electric generating set) and forms an improvement in the structure of electrical generating equipment of which the principle is already well-known.
  • the structure proposed is more especially intended for machines having higher unit power than those already described (above one kw. for example).
  • a combustion volume defined by a cylinder head 91 and piston 92.
  • On the cylinder head are exhaust valves '93 and inlet ports 94 and a means of introducing and igniting fuel 95 of a type already known.
  • a return cushion volume 96 symmetrical with volume 90 with respect to the electro-magnetic part situated in the centre, is defined by a cylinder head assembly 97 and a piston 98.
  • a non-magnetic rod 99 connects pistons 92 and i
  • the cylinder piston skirts 100 and 101, of circular section, are formed by the assembly of moving armatures of a certain number of independent magnetic circuits having three branches preferably arranged radially.
  • circuits comprise interrupted branches 102, 103 on the one hand and 104, 105 on the other, which carry excitation coils 109a and 10% situated in the immediate neighbour hood of the air gap, which increases the power and the efiiciency, and the common branch 106 which carries the power coil 110.
  • Coils 109a tend to cause magnetic flux to circulate between pole pieces 102, 103 and the same thing applies for the coils 10% in respect of the pole pieces 104, 105.
  • Lateral members 107 and 108 join these three branches.
  • Non-magnetic and'non-conducting casings 111 and 112 provide the centering of the assembly.
  • the external and internal parts of the stator are defined by cylindrical rings, carrying magnetic plates 117 and 119 placed opposite the poles and in one piece with the rest of the rings which are of non-magnetic material, acting as strengthening Iltll11gS and preventing the poles from moving towards each 0 er.
  • the operation already known is as follows: The moving assembly is projected in direction 0 by the force of the combustion which takes place in volume 90 and this compresses the fluid contained in the cushion volume 96 which, at the end of the stroke, returns the moving assembly in direction N.
  • Coils 109a and 10% are excited (as shown in FIG. 10) by direct current supply such that the corresponding flux in branch 106 cancels itself out in the absence of any armature.
  • skirts 100 and 101 are introduced alternatively into the air gaps 113 and 114 alternating current is obtamed from coil in the normal way alread known.
  • the resulting electrical generating set has high unit power, easy assembly, and inexpensive manufacture in large quantities.
  • the separation into several coils results in an armature having a greater diameter and thus in machines of a higher unit power than those of the first embodiment.
  • the machine comprises a central casing 120 containing a number of magnetic 9 circuits 121a, 121b and of coils 122a, 122b, 132a, 133b, two skirts formed of annular armatures 123a, 123b attached to two pistons 124a, 1241b and two cylinders 125a, 125b.
  • FIG. shows in detail the structure of a sector of armature 123a formed for example in laminations 171 assembled with sheets 172 of epoxy resin, the groups of laminations 171 being separated by spacers 173 of epoxy resin cast between these laminations.
  • the number of stacks of laminations corresponds to the number of poles (8 in the example considered).
  • the central casing 120 is made of a non-magnetic nonconducting material and comprises a central disc 126 solid with an internal boss 127 and an external sleeve 128 projecting equally relatively to the two faces of disc 126.
  • Sleeve 127 is cut away axially to receive the inner pole piece 129a, 12'9b.
  • Sleeve 128 is cut away to receive outer pole piece 130a, 1301). These various pole pieces are equally spaced and aligned radially.
  • This assembly comprises the magnetic circuits 121a, 121b.
  • On the inner pole pieces 129a, 12% are mounted the magnetising coils 122a, 122b and on the outer pole pieces 130a, 1301; other magnetising coils 132a, 132k.
  • FIG. 14 shows an embodiment comprising 8 radial pole pieces, joined in pairs by their bases by means of sleeve 127 and equally spaced radially.
  • the extremities 133a, 133b of the pole pieces constitute the poles and form the inner part of the cylindrical air gaps 134a, 134b.
  • the outer pole pieces 130a, 1301) are arranged radially as extensions of the inner pole pieces 129a, 12%. These pole pieces are also joined in pairs. The parts of each pair are connected at their outer extremities 'by members 136 forming the arcs of a circle.
  • the inner ends 137a, 1371) of the pole pieces 129a, 1291) form the poles and form also the outer part of the air gaps 134a and 134b.
  • the magnetic circuit is thus formed by four circuits of triangular contour (FIG. 14). These magnetic circuits can be made from sintered material or in the form of laminated sheets 144 as indicated in FIG. 13. In this case, the end sheets are preferably thicker to resist the attraction of armatures 123a, 123b. The inner and outer surfaces of air gaps 134a, 134b are covered with a thin coating of polytetrafluoroethylene or other similar non-magnetic, non-conducting, anti-friction material.
  • Coils 122a and 132a on one hand 122b, 132k on the other are fed alternatively, similarly to coils 53a, 535, on FIG. 4. Furthermore the associated coils 122b and 13215 are so connected that the magnetic flux circulates in the same direction A (FIG. 14) in the corresponding pole pieces 129b, 13%. The same arrangement is adopted for the coils of the other group.
  • the axial canal 131 of sleeve 127 is threaded at each end to receive the caps 139 through which passes a rod 140 whose ends are screwed into the pistons 124a and 124! so that they move as one unit.
  • annular armatures 132a, 132b which form the skirts of pistons 124a, 124b is so arranged that the stacks of laminations 171 are situated in alignment with pole pieces 133a, 137a or 133b, 1371;.
  • Each piston 124a, 124b is equipped with piston rings or other sealing means and slides in the corresponding cylinder 125a, 125b which are equipped with suction valves 141a, 141b and delivery valves 142a, 14%.
  • the two compressor assemblies are thus situated out? side the magnetic assembly so that a very rigid machine can be achieved since the massive electro-magnetic part is in the centre.
  • the assembly of the static part of the machine is carried out by first placing the coils on the inner and outer pole pieces of the fixed magnetic circuits which are then inserted axially into the central casing 120 and held in place by the caps 139 and by the dove tail shape of the members 136 inserted into the casing 120.
  • the static parts are easily and accurately positioned in the casing.
  • the whole of the static part is then located with a non conducting non-magnetic material of epoxy resin type (indicated in FIG. 14 'by random dots) which renders it sufficiently rigid to avoid distortion due to the magnetic attraction between the poles and to with stand severe operational conditions without damage.
  • the air gap is suitably protected during this operation.
  • a coating of polytetrafluoroethylene or other material having a low coefficient of friction is then applied to the air gap and thus prevents any contact between the annular armatures 123a, 123b and the surfaces of the poles, and thus any appreciable lateral force towards the poles, which would be the consequence of contact between the armature and the poles.
  • Pistons 124a, 1241) are then attached to annular armatures 123a, 123b then to rod 140, such that when armature 123b fully occupies air gap 134b, the other armature 123a is ready to enter its corresponding air gap 134a.
  • cylinders 125a, 125b are fitted over the pistons and assembled with screws 143.
  • Electrical impulses alternatively feed coils 122a, 132a of the first half of the machine, then coils 122b and 13% -of the second half.
  • An electro-mechanical energy converting mac ine comprising at least one fixed electromagnetic circuit having spaced apart cylindrical and coaxial pole surfaces defining an annular cylindrical air gap, a field coil on the fixed magnetic circuit adapted to generate a magnetic field across the air gap, means to reduce the flow of eddy currents that tend to travel along annular paths concentric with the air gap in the fixed magnetic circuit, an operating piston incorporating a tubular cylindrical magnetic armature mounted for reciprocating movement along a path disposed transversely to the magnetic field, the magnetic armature disposed coaxially with the pole surfaces of the fixed magnetic circuit, a part of the fixed magnetic circuit being located within the armature for i at least part of the stroke of the armature, the armature formed to be a poor conductor of eddy currents to minimize the fiow of eddy currents therein, an operating cylinder having an inner surface that is coaxial with the pole surfaces, the operating piston sliding along the inner surface of the cylinder to guide the piston and center the armature in the air gap, and means including supporting structure
  • a machine according to claim 1, wherein the operating piston comprises the piston of a heat engine.
  • a machine in which is provided two fixed magnetic circuits each of which includes an annular cylindrical air gap, each of the magnetic circuits carrying at least one magnetizing coil, two tubular cylindrical magnetic armatures respectively movable in the air gaps of the fixed magnetic circuits, and a third common magnetic branch of the two magnetic circuits carrying a coil for the generation of alternating current.
  • a machine in which is provided means forming cooling passages in the machine, and the operating piston includes a central part and an outwardly extending part, the outwardly extending part functioning as a piston of a pump that insures circulation of a cooling fluid through the cooling passages in the machine.
  • said centering means includes a cylindrical bore, the bore centering the fixed magnetic circuit with respect to the operating cylinder.
  • a machine in which is provided a cylindrical ring formed partly of magnetic material and partly of non-magnetic material to hold pole pieces of the fixed magnetic circuit in place and prevent any variation in the dimensions of the air gap under the influence of magnetic attraction forces.
  • a machine which includes a plurality of fixed magnetic circuits extending radially from the axis of the machine, each of the circuits including at least one coil whose axis is perpendicular to the axis of the magnetic armature, and said coil being located adjacent to the air gap.
  • a machine in which is provided an operating cylinder located on each side of the fixed magnetic circuit, each of the operating cylinders centering one of the operating pistons rigidly joined to the tubular cylindrical magnetic armature, the fixed magnetic circuit having two coaxial annular air gaps in which the two magnetic armatures and operating pistons are mounted to move in opposite directions.
  • a machine according to claim 1 in which two magnetic armatures extend axially in opposite directions from and form part of the operating piston.
  • the fixed magnetic circuit includes first pole pieces extending substantially radially from the air gap inwardly, the pole pieces being joined at their bases and bearing on an axial sleeve, and second pole pieces extending substantially radially from the air gap outwardly in line with the first pole pieces and interconnected by annular cores engaged by an external casing.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Linear Motors (AREA)
US594191A 1965-11-17 1966-11-14 Electromagnetic machines Expired - Lifetime US3500079A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR38798A FR1523129A (fr) 1965-11-17 1965-11-17 Machines électromécaniques transformatrices d'énergie à reluctance variable

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US3500079A true US3500079A (en) 1970-03-10

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US (1) US3500079A (sr)
BE (1) BE689152A (sr)
CH (1) CH472137A (sr)
DE (2) DE1538747A1 (sr)
ES (1) ES333436A1 (sr)
FR (1) FR1523129A (sr)
GB (1) GB1115720A (sr)
NL (1) NL6616006A (sr)
OA (1) OA02274A (sr)
SE (1) SE341427B (sr)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3947155A (en) * 1974-09-19 1976-03-30 Tecumseh Products Company Linear compressor
US4163911A (en) * 1975-01-27 1979-08-07 Sutter Hospitals Medical Research Foundation Permanent magnet translational motor for respirators
US4395649A (en) * 1978-03-20 1983-07-26 Robert Bosch Gmbh Linear electromagnetic vibrator
EP0114069A2 (en) * 1983-01-17 1984-07-25 Helix Technology Corporation Cryogenic refrigeration system with linear drive motors
US4615661A (en) * 1982-07-30 1986-10-07 King Jimmy L Magnetic pump
US5231747A (en) * 1990-12-21 1993-08-03 The Boeing Company Drill/rivet device
US5263236A (en) * 1990-12-21 1993-11-23 The Boeing Company Drill quill bearing assembly
US5349256A (en) * 1993-04-23 1994-09-20 Holliday Jeffrey C Linear transducer
US5607292A (en) * 1995-07-19 1997-03-04 Rao; Dantam K. Electromagnetic disk pump
US5654596A (en) * 1992-12-22 1997-08-05 Stirling Technology Company Linear electrodynamic machine and method of making and using same
US20050082917A1 (en) * 2001-12-07 2005-04-21 Schulte Franz J. Linear generator with a swinging piston
US20170218758A1 (en) * 2014-07-31 2017-08-03 Siemens Aktiengesellschaft Linear actuator and method for operating such a linear actuator
US10030961B2 (en) 2015-11-27 2018-07-24 General Electric Company Gap measuring device
US10634131B2 (en) * 2016-12-14 2020-04-28 Dmitrij Valerevich KHACHATUROV Submersible pumping apparatus, comprising linear electric motor and double action pump

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US3536941A (en) * 1967-10-10 1970-10-27 Eaton Yale & Towne Linear synchronous electric motor with reciprocating armature
FR1582781A (sr) * 1968-01-12 1969-10-10
DE2821842C2 (de) * 1978-05-19 1983-04-21 Eckart Prof. Dr.-Ing. 3005 Hemmingen Doege Elektromagnetische Antriebsvorrichtung
FR2544926B1 (fr) * 1983-04-20 1986-05-30 Jarret Jacques Anneau magnetique pour generateurs rectilignes a pistons libres

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Cited By (22)

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Publication number Priority date Publication date Assignee Title
US3947155A (en) * 1974-09-19 1976-03-30 Tecumseh Products Company Linear compressor
US4163911A (en) * 1975-01-27 1979-08-07 Sutter Hospitals Medical Research Foundation Permanent magnet translational motor for respirators
US4395649A (en) * 1978-03-20 1983-07-26 Robert Bosch Gmbh Linear electromagnetic vibrator
US4615661A (en) * 1982-07-30 1986-10-07 King Jimmy L Magnetic pump
EP0114069A2 (en) * 1983-01-17 1984-07-25 Helix Technology Corporation Cryogenic refrigeration system with linear drive motors
EP0114069A3 (en) * 1983-01-17 1985-09-18 Helix Technology Corporation Cryogenic refrigeration system with linear drive motors
US5577315A (en) * 1990-12-21 1996-11-26 The Boeing Company Method of upsetting rivets
US5263236A (en) * 1990-12-21 1993-11-23 The Boeing Company Drill quill bearing assembly
US5752306A (en) * 1990-12-21 1998-05-19 The Boeing Company Method for upsetting a headed rivet by differential initiation of opposed electromagnetic rivet drivers
US5404633A (en) * 1990-12-21 1995-04-11 The Boeing Company Method of dynamically supporting a drill quill in a drill/rivet machine
US5231747A (en) * 1990-12-21 1993-08-03 The Boeing Company Drill/rivet device
US5685058A (en) * 1990-12-21 1997-11-11 The Boeing Company Method for direct insertion of a headed rivet into a countersunk hole
US5621963A (en) * 1990-12-21 1997-04-22 The Boeing Company Differential capacitance in an electromagnetic riveter
US5654596A (en) * 1992-12-22 1997-08-05 Stirling Technology Company Linear electrodynamic machine and method of making and using same
US5349256A (en) * 1993-04-23 1994-09-20 Holliday Jeffrey C Linear transducer
US5607292A (en) * 1995-07-19 1997-03-04 Rao; Dantam K. Electromagnetic disk pump
US20050082917A1 (en) * 2001-12-07 2005-04-21 Schulte Franz J. Linear generator with a swinging piston
US7291943B2 (en) * 2001-12-07 2007-11-06 Otag Gmbh & Co. Kg Linear generator with a swinging piston
US20170218758A1 (en) * 2014-07-31 2017-08-03 Siemens Aktiengesellschaft Linear actuator and method for operating such a linear actuator
US10731464B2 (en) * 2014-07-31 2020-08-04 Siemens Aktiengesellschaft Linear actuator and method for operating such a linear actuator
US10030961B2 (en) 2015-11-27 2018-07-24 General Electric Company Gap measuring device
US10634131B2 (en) * 2016-12-14 2020-04-28 Dmitrij Valerevich KHACHATUROV Submersible pumping apparatus, comprising linear electric motor and double action pump

Also Published As

Publication number Publication date
BE689152A (sr) 1967-05-02
ES333436A1 (es) 1967-08-01
DE1538747A1 (de) 1970-04-23
GB1115720A (en) 1968-05-29
OA02274A (fr) 1970-05-05
NL6616006A (sr) 1967-05-18
CH472137A (fr) 1969-04-30
SE341427B (sr) 1971-12-27
DE6608987U (de) 1972-01-13
FR1523129A (fr) 1968-05-03

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