Force actuator with dual magnetic operation

• US 5,896,076 A
• Filed: 12/29/1997
• Issued: 04/20/1999
• Est. Priority Date: 12/29/1997
• Status: Expired due to Term

• Current Assignee: Motran Industries Inc.
• Original Assignee: Motran Industries Inc.
• Inventors: van Namen, Frederik T.
• Primary Examiner(s): Gellner, Michael L.
• Assistant Examiner(s): Nguyen, Tuyen T.
• Application Number:
  US08/998,731
• Time in Patent Office: 477 Days
• Field of Search: 335/229-235, 335/222, 335/251, 335/255, 310/13, 310/14, 310/15
• US Class Current: 335/229
• CPC Class Codes: H01F 7/122 by permanent magnets H01F7/1615, H01F7/1646 take precedence
• CPC Class Codes: H01F 7/1615 Armatures or stationary parts of magnetic circuit having permanent magnet

Abstract

An electromagnetic active vibration actuator configuration combines two modes of operation to obtain the advantages of long stroke and linearity of voice coil type actuators and high efficiency of dual-gap solenoid type actuators. A coaxial stator shell surrounds an axially vibratable armature. Either the stator or the armature can carry one or more coils and/or permanent magnets, however usually the magnets are located on the armature for their contribution to vibrating mass. Alternate coils and alternate magnets are made opposite in polarity, the stator armature pole pieces being held symmetrically staggered relative to the stator pole pieces by end springs or flexures that allow axial vibration when AC is applied to the coils. Two different types of flux loop paths are associated with each pair of permanent magnet prominent poles: a voice-coil-effect flux loop path including two air gaps, each traversing a coil, that remain relatively constant in separation distance and permeability under vibration, and a solenoid-effect loop flux path traversing a pair of gaps in series flanking a coil prominent pole, that vary in separation distance and permeability in a complementary manner under vibration in the manner of a solenoid type actuator. These two magnetic modes operate in a cooperative additive efficient manner. Multiples of a typical magnet/coil pair can be easily tandemed using common building block component elements, typically being made to have in total an odd number of prominent poles. Wide flexibility is provided in design and manufacture to customize the performance of the actuator by manipulating the proportion of voice coil effect and solenoid effect along with the mechanical spring effect and the vibrating mass.

Claims

1. An electromagnetic force actuator, for active vibration control, motivated in a dual magnetic manner by a combination of voice-coil-effect and solenoid-effect flux paths, comprising;

an electromagnetic coil structure of magnetically permeable material constructed and arranged to have a typical cross-sectional shape defining at least one prominent pole facing a common reference line at a predetermined spacing distance and separating two of a plurality of adjacent channels formed in the magnetically permeable material each filled with an oppositely polarized coil winding oriented such that wire ends appear in the cross-sectional shape;

a magnet structure having at least one permanent magnet with a pair of magnetically opposed prominent poles of magnetically permeable material having a cross sectional shape such as to face the common reference line from a direction opposite the coil structure, disposed along the common reference line such that the prominent pole(s) of the coil structure and those of the magnet structure are located in a staggered symmetric disposition about the common reference line so as to be mutually centered axially;

suspension means constructed and arranged to retain the coil structure and the magnet structure facing the common reference line at a constant distance therefrom while providing freedom for the electromagnetic coil structure and the magnet structure to vibrate relative to each other in an axial direction along the common reference line;

magnetic flux path conducting means, including magnetically permeable material, for conducting magnetic flux, configured and arranged to conduct portions of magnetic flux paths extending from a first prominent pole of each magnet through a path to a second and opposite prominent pole thereof, the flux paths including (1) a voice-coil-effect flux path that traverses first and second air gaps serially, each gap being made to have substantially constant separation distance under vibration and each containing respectively a central portion of a first and second one of two adjacent ones of said oppositely polarized coil windings, and (2) a solenoid-effect flux path that traverses serially (a) a first air gap containing an end portion of the first coil winding, (b) a prominent pole of the coil structure that is axially movable with respect to the magnet poles, and (c) a second air gap containing an end portion of the second coil winding;

the first and second air gaps being constructed and arranged to have respective separation spacings and permeabilities that vary with vibration in a complementary manner;

said actuator being made to have an odd total number of prominent poles and thus to have at least three prominent poles;

adjacent magnets being oppositely polarized and adjacent coils being oppositely polarized; and

spring means constructed and arranged to provide a spring force tending to establish and maintain the mutually centered relationship between each prominent pole of the coil structure and corresponding prominent poles of the magnet structure;

whereby, in response to alternating current applied to the coil windings, at least one of said structures is caused to vibrate relative to the other, operating in first part according to principles of a voice coil type actuator due to e.m.f. of the voice-coil-effect flux path having substantially constant permeability and acting directly on the said oppositely polarized coil windings as a force in an axial direction, and operating in second part according to principles of a dual-gap solenoid type actuator in the solenoid-effect flux path due to magnetic attraction forces typically between a stator prominent pole and an adjacent movable armature prominent pole, with recurrent complementary flux redistribution in the two air gaps from the complementary variation of respective gap separation distances and permeabilities under vibration.

2. The electromagnetic force actuator as defined in claim 1, wherein said coil structure, constituting a stator assembly, comprises:

a tubular shell, of permeable magnetic material;

a pair of end plates disposed one at each end of said tubular shell;

a quantity of n+1 annular coils, connected alternately in opposite phase polarity relationship, disposed around an inner peripheral region of said shell, each centered axially about a corresponding one of said pole pieces of the armature; and

a quantity of n annular stator rings of magnetically permeable material disposed between said coils in an interleaved manner, extending inwardly from said shell so as to constitute the prominent poles of the coil structure;

and wherein said magnet structure, constituting a cylindrical armature assembly disposed coaxially and centrally within said shell, comprises;

a quantity of n identical short cylindrical permanent magnets, each having a pair of parallel magnetically opposite flat pole faces, said magnets, if n>

1, being stacked coaxially in alternating polarity directions; and

a quantity of n+1 identical short cylindrical armature pole pieces of permeable magnetic material interleaved with said permanent magnets, each adjacent pair of pole pieces flanking and interfacing with pole faces of a corresponding one of said magnets, said pole pieces extending radially outwardly so as to constitute corresponding prominent poles facing the common reference line and forming an annular air gap extending to said shell.

3. The electromagnetic force actuator as defined in claim 2 wherein the stator assembly further comprises an additional pair of said stator rings, disposed at opposite ends of said stator assembly between a corresponding one of said end plates and a corresponding adjacent outermost one of said coils.

4. The electromagnetic force actuator as defined in claim 2 wherein said suspension means comprises a cylindrical support shaft, secured at each end to a corresponding one of the end plates, traversing a cylindrical passageway provided through said armature assembly, made and arranged to allow said armature assembly to vibrate axially.

5. The electromagnetic force actuator as defined in claim 2 wherein said suspension means comprises a cylindrical support shaft, secured concentrically to said armature assembly with two opposite ends each supported slidably by extending through a corresponding one of the end plates, whereby axial vibration of said armature is enabled and whereby such vibration may be transmitted to an external object via an end portion of said support shaft.

6. The electromagnetic force actuator as defined in claim 2 wherein said spring means comprises a pair of coil springs, each disposed between a corresponding end plate and a corresponding outermost one of said armature pole pieces so as to exert a spring force therebetween.

7. The electromagnetic force actuator as defined in claim 1 wherein said suspension means comprises a pair of spring flexure assemblies, each disposed between a corresponding one of the end plates and a corresponding outermost one of said armature pole pieces, each flexure assembly comprising:

at least one pair of flat spring strips crossing each other centrally so as to form a star-shaped pattern with uniformly spaced ends, secured to a corresponding end of said armature assembly such that the ends extend radially from the central axis; and

a concentric flexure ring of resilient material constructed and arranged to captivate the extending ends of the star pattern and to be secured against an inner surface of a corresponding end plate, and to thusly support said armature disposed coaxially in said shell and centered between the end plates in a manner that allows said armature assembly to vibrate axially in response to alternating current applied to said coils.

8. The electromagnetic force actuator as defined in claim 7 wherein said suspension means further comprises:

a pair of screw fasteners, one disposed centrally at each end of the armature assembly, traversing a central opening provided in each of said spring strips and threadedly engaging the corresponding end of said armature so as to secure said spring strips to the armature assembly.

9. The electromagnetic force actuator as defined in claim 8 wherein said spring means consist of said spring strips in said suspension means.

10. The electromagnetic force actuator as defined in claim 8 wherein wherein said spring means further comprise:

a pair of coil springs, disposed coaxially at opposite ends of armature assembly so as to exert therefrom a spring force against a corresponding end plate, and

said spring strips in said suspension means working in conjunction with said coil springs so as to establish a predetermined spring modulus.

11. The electromagnetic force actuator as defined in claim 6 further comprising an additional pair of stator rings, identical with said stator rings, disposed at opposite ends of said actuator between a corresponding end plate and an adjacent outermost one of said coils.

12. The electromagnetic force actuator as defined in claim 7 wherein each of said spring flexure assemblies is constructed and arranged to have a cross-sectional shape defining (1) a short tubular-shaped portion made to fit against an inwardly-facing surface of a corresponding outermost ring, (2) a first flange, extending radially inwardly from a first edge of the tubular portion, captivating the ends of the spring strips, and (3) a second flange, at a second edge of the tubular portion opposite the first edge, extending radially outwardly for retention between the corresponding outermost ring and the corresponding end plate.

13. The electromagnetic force actuator as defined in claim 12 wherein each of said end plates is configured with an inwardly-facing annular channel dimensioned and located to accommodate and retain the second flange of a corresponding one of said flexure rings.

14. The electromagnetic force actuator as defined in claim 1, wherein said magnet structure, constituting a cylindrical armature assembly, comprises:

a cylindrical permanent magnet having opposite magnetic poles at corresponding opposite flat parallel surfaces; and

two identical cylindrical pole pieces of permeable magnetic material, flanking said permanent magnet, configured and arranged to constitute corresponding prominent armature poles facing said shell;

and wherein said magnetic coil structure, constituting a stator assembly, comprises;

a tubular shell, of permeable magnetic material,

a pair of end plates disposed one at each end of said shell and attached thereto;

two annular coils, connected in opposite phase polarity relationship, disposed around an inner peripheral region of said shell; and

a stator ring of magnetically permeable material, disposed centrally between said two coils, extending radially inward from said shell so as to constitute a prominent pole of the magnetic coil structure;

suspension means for supporting the armature assembly in said shell with positive coaxial constraint and with spring-loaded axial constraint arranged to establish a central quiescent axial armature location at which the two armature pole pieces straddle said stator ring symmetrically and about which the armature can be driven, by alternating current applied to said coils, so as to vibrate axially against the spring-loaded axial constraint.

15. The electromagnetic force actuator as defined in claim 14 wherein the stator assembly further comprises an additional pair of said stator rings, disposed at opposite ends of said stator assembly, each retained between a corresponding one of said end plates and a corresponding one of said coils.

16. The electromagnetic force actuator as defined in claim 1, wherein:

said magnet structure is incorporated in a stator assembly comprising;

a tubular shell, of non-magnetic material, including a pair of end plates disposed one at each end thereof;

a quantity of n annular-shaped permanent magnets located peripherally inside said shell, each having two opposed parallel faces defining magnetic poles of opposite polarity, stacked adjacently with alternating polarity so that poles of like polarity face each other; and

a quantity of n+1 annular-shaped stator rings of magnetically permeable material disposed between said magnets in an interleaved manner, extending inwardly from said shell past said magnets so as to constitute the prominent poles of the magnet structure;

and wherein said coil structure is incorporated in a cylindrical armature assembly, surrounded coaxially by said stator assembly, comprising;

a generally cylindrical central core of magnetically permeable material configured and arranged to define a row of n+1 adjacent annular-shaped coil winding bobbin channels interleaved with cylindrical prominent pole pieces extending radially outward from said core and facing said shell; and

a quantity of n+1 identical annular coils, connected alternately in opposite phase polarity relationship, disposed each in a corresponding one of said bobbin channels and each centered axially about a corresponding one of said stator rings.

17. The electromagnetic force actuator as defined in claim 1 wherein said suspension means comprises a pair of spring flexure assemblies, each disposed between a corresponding one of the end plates and a corresponding outermost one of said armature pole pieces, each flexure assembly comprising:

at least one flat spring strip, secured centrally to a corresponding end of said armature assembly such that two opposite ends thereof extend radially from the central axis; and

a concentric flexure ring of resilient material constructed and arranged to captivate the extending ends and to be secured against an inner surface of a corresponding end plate, and to thusly support said armature disposed coaxially in said shell and centered between the end plates in a manner that allows said armature assembly to vibrate axially in response to alternating current applied to said coils.