Shock improvement for an electroacoustic transducer

Information

  • Patent Grant
  • 6658134
  • Patent Number
    6,658,134
  • Date Filed
    Monday, August 16, 1999
    25 years ago
  • Date Issued
    Tuesday, December 2, 2003
    21 years ago
Abstract
A transducer comprising a coil having a first air gap, a magnetic member having a second air gap and an armature. The armature includes an armature leg that extends through the first and second air gaps. The armature leg is capable of movement-within the air gaps. The magnetic member includes at least one nub extending into the second air gap. The nub limits the movement of the armature leg within the second air gap.
Description




FIELD OF THE INVENTION




The present invention relates generally to a transducer and, more particularly, to a shock resistant transducer particularly suitable for hearing aids.




BACKGROUND OF THE INVENTION




Transducers are particularly useful in hearing aids. The transducer may be used as a microphone to convert acoustic energy into electrical energy or as a receiver to convert electrical energy into acoustic energy. Typical transducers suitable for hearing aids comprise a coil having a first air gap, a magnetic member having a second air gap and an armature with an armature leg that extends through both of the air gaps. A diaphragm connects to the armature leg.




The operation of the transducer follows. Vibrations of the diaphragm are transmitted to the armature leg, and the vibrating armature leg causes an electric alternating electric current in the coil. Conversely, an alternating current supplied to the coil causes a vibration of the armature leg, which is transmitted to the diaphragm. Under normal conditions the vibrations of the armature leg are relatively small displacements. In extreme cases, however, the armature leg may deflect a large amount and touch the magnetic member.




One problem with the conventional transducers is that a shock or impact load exerted on the transducer may cause plastic deformation of the armature leg. For example, when the transducer falls and contacts a solid object, the armature leg deflects or bends so far that undesirable plastic deformation can occur in the armature leg. Once the armature leg is plastically deformed such that it is closer to one side of the magnetic member than the other in a steady-state condition, the transducer does not function properly.




Some conventional transducers have attempted to address this shock problem. For example, Knowles Electronics, Inc. produces a transducer (e.g. Model ED1913) with deformations on a central portion of the armature leg that is positioned within the air gap of the coil. When the Knowles transducer suffers a shock, the armature leg deflects until the deformations contact the surface of the coil, thus limiting the freedom of movement of the armature leg. One example of the Knowles transducer is generally disclosed in U.S. Pat. No. 5,647,013. Another example of a conventional transducer with shock resistance is produced by the assignee of the present applicant Microtronic BNV. The Microtronic transducer (2300 series) has a rotated coil with respect to the magnetic member. This rotation forms a stop for the armature leg to inhibit excessive bending of the armature leg in the occurrence of a shock. One example of the Microtronic transducer is generally disclosed in European Patent Application No. 847,226.




One disadvantage of the above transducers is that the shock resistance, though improved, does not meet the increasing shock standards of the hearing aid industry. Furthermore, especially for the Knowles transducer, special and/or additional parts must be used to provide the shock resistance which increase the expense of the transducer.




It is a general object of the present invention to solve the above problems. More particularly, there is desired a transducer with superior shock resistance, and which can be easily assembled from standard parts at a low cost.




SUMMARY OF THE INVENTION




According one aspect of the present invention, there is provided a transducer comprising a coil having a first air gap, a magnetic member having a second air gap and an armature. The armature includes an armature leg extending through the first air gap and the second air gap. The armature leg is capable of movement within the air gaps. The magnet member has at least one nub extending into the second air gap that limits the range of motion of the armature leg to inhibit large deflections of the armature leg and plastic deformation. The nubs may be comprised of a drop of adhesive.




In another aspect of the present invention, there is provided a transducer suitable for hearing aids comprising a coil having a first air gap, a magnetic assembly having a second air gap and an armature. The armature includes an armature leg that extends through both the first air gap and the second air gap. The armature leg is capable of movement within the second air gap. The magnetic assembly has a cushioning element secured to the magnetic assembly that extends into the second air gap. When the transducer is subjected to a shock, the movement of the armature leg is limited as it engages the cushioning element. Furthermore, the cushioning element may comprise a soft material to absorb a portion of an impact of the armature leg when the armature leg moves into contact with the cushioning element.











BRIEF DESCRIPTION OF THE DRAWINGS




The forgoing and other advantages of the invention will become apparent upon reading the following detailed description and upon reference to the drawings in which:





FIG. 1

is a cross-sectional side view of a shock resistant transducer according to one embodiment of the present invention;





FIG. 2

is a cross-sectional front view of the transducer of

FIG. 1

;





FIG. 3

is a perspective view of the transducer in

FIG. 1

;





FIG. 4

is a perspective view of the armature of the transducer in

FIG. 1

;





FIG. 5

is a schematic diagram of a mechanical shock test apparatus; and





FIG. 6

is a graph of shock resistance test results.




While the invention is susceptible to various modifications and alternative forms, specific embodiments have been shown by way of example in the drawings and will be described in detail herein. However, it should be understood that the invention is not intended to be limited to the particular forms disclosed. Rather, the invention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the invention as defined by the appended claims.











DESCRIPTION OF SPECIFIC EMBODIMENTS




Turning now to the drawings and referring initially to

FIG. 1

, there is depicted a longitudinal sectional view of a shock resistant transducer


10


according to the present invention. The transducer


10


comprises a magnetic member


12


and a coil


14


. In the illustrated embodiment, the magnetic member


12


comprises a magnet housing


16


and two spaced apart magnetic elements


18


and


20


. The coil


14


has a first air gap


22


. As depicted in

FIG. 2

, the cross section of the first air gap


22


is substantially rectangular; however, the first air gap may have a different cross sectional shape in other embodiments. The magnetic elements


18


and


20


define a second air gap


24


. The cross section of the second air gap


24


is substantially rectangular; however, the second air gap may have a different cross sectional shape in other embodiments. As shown in

FIG. 1

, the two air gaps


22


and


24


are substantially aligned with each other. When viewed in the cross section of

FIG. 2

, the edges of the rectangular first air gap are parallel to the respective edges of the rectangular second air gap


24


. In other embodiments, one of the air gaps may be rotated relative to the other air gap. When the rotated embodiment is viewed in the cross section, the edges of the rectangular first air gap are not parallel to the respective edges of the rectangular second air gap.




The transducer


10


further comprises an armature


26


. The armature


26


, as more completely illustrated in

FIG. 4

, is an E-shaped armature. In other embodiments, the armature may have a U-shape. In general, the E-shaped armature


26


has three legs


28


,


30


and


32


, lying generally parallel with each other and interconnected at one end by a leg connecting part


34


. As illustrated in

FIG. 3

, the middle armature leg


30


is positioned within the two aligned air gaps


22


and


24


with the leg connecting part


34


being located on the side of coil


14


. The two outer armature legs


28


and


32


extend on the outer side along the coil


14


and the magnet housing


12


. Although not shown, the two outer armature legs


28


and


32


are affixed to the magnet housing


12


. The free end of the middle armature leg


30


is connected to a diaphragm with a connecting element (not shown).




The operation of the transducer


10


follows. When an electrical signal, originating from an amplifier (not shown) is supplied to the coil


14


, the middle armature leg


30


vibrates in cooperation with a magnetic field of the magnetic member


12


. The movement of vibration of the middle armature leg


30


is transmitted via the connecting element to the diaphragm, which causes sound vibrations. Conversely, sound vibrations vibrate the diaphragm causing the middle armature leg


30


to vibrate via the connecting element. This vibration generates an electrical signal in the coil


14


. The electrical signal may then be detected and processed accordingly.




Under normal conditions the vibrations of the armature leg are relatively small displacements. However, sometimes the transducer


10


may be subjected to a shock such as the result of an impact after a fall. The shock causes a large acceleration that is exerted on the middle armature leg


30


. The shock deflects the middle armature leg


30


further from its state of equilibrium and beyond the typical vibrations of normal operation. To prevent the middle armature leg


30


from striking the magnetic elements


18


and


20


and potentially becoming plastically deformed, the transducer


10


includes a pair of nubs


36


and


38


secured to the magnetic elements


18


and


20


. As illustrated in

FIG. 2

, the nubs


36


and


38


protrude into the second air gap


24


to inhibit an unduly large deflection of the middle armature leg


30


. The nubs


36


and


38


provide a nub air gap identified by “d” in

FIG. 2

that is smaller than the second air gap


24


.




The nubs


36


and


38


provide shock resistance for the transducer


10


by inhibiting large deflections of the middle armature leg


30


. During a large shock, the middle armature leg


30


will deflect and potentially strike one of the nubs


36


or


38


. Without the nubs


36


and


38


during a shock, the middle armature leg


30


may deflect a large amount and possibly strike the magnetic element that may cause plastic deformation. The nubs


36


and


38


are positioned to limit the movement of the middle armature leg


30


to inhibit plastic deformation.




As depicted in

FIG. 1

, the nubs


36


and


38


are located on the magnetic elements


18


and


20


away from the free end of the middle armature leg


30


to allow freedom of movement of the middle armature leg


30


during normal operation of the transducer


10


. This positioning of the nubs


36


and


38


avoids the nubs


36


and


38


from rubbing the free end of the middle armature leg


30


during normal operation to ensure maximum output of the transducer


10


. Preferably, the nubs


36


and


38


are positioned at the coil end of the magnetic elements


18


and


20


to allow the free end of the middle armature leg


30


greater freedom of movement. This orientation of the nubs


36


and


38


also supports the middle armature leg


30


in the middle of its length during the shock. However, the nubs


36


and


38


may be positioned anywhere along the magnetic elements


18


and


20


such that the middle armature leg


30


has free movement during normal operation, but does not experience large deflections during shock.




As depicted in

FIGS. 1 and 2

, the nubs


36


and


38


are substantially symmetrically positioned around a longitudinal plane through the middle armature leg


30


. This longitudinal plane is perpendicular to the direction of the operational motion of the middle armature leg


30


. In other embodiments, the nubs may be asymmetrical to the longitudinal plane and have different orientations as long as the middle armature leg has freedom of movement in normal operation and large deflections of the middle armature leg are inhibited. In

FIGS. 1 and 2

, the nubs


36


and


38


have a rounded exterior (i.e. a drop shape). In other embodiments, the nubs may have a different shape. Although only one pair of nubs is illustrated, additional pairs of these nubs may be applied to the magnetic elements


18


and


20


to provide shock resistance.




In one embodiment, the nubs


36


and


38


comprise drops of UV-cured adhesive adhered to the magnetic elements


18


and


20


. In other embodiments, different materials secured to the magnetic elements may be used to meet the movement limiting function of the nubs


36


and


38


. Furthermore, the nubs


36


and


38


may be unitary with the magnetic elements


18


and


20


such as deformations on the surface of the magnetic elements


18


and


20


.




Not only do the nubs


36


and


38


limit large deflections of the middle armature leg


30


, but the nubs


36


and


38


may be configured to also cushion the middle armature leg


30


during shocks. In the cushioning embodiment, the nubs


36


and


38


comprise a softer material such as an elastoner, an epoxy, or a plastic. When the nubs are comprised of softer material, the nubs


36


and


38


may be considered a cushioning element. For cushioning, the approximate hardness for the material comprising the nubs


36


and


38


may be less than about Shore D 90. In some embodiments, the material comprising the nubs may be about Shore A 60. One example of a cushioning element is the Epoxy Technology UV-cured adhesive OG115 from Billerica, Mass. with a Shore D hardness of approximately 86 that tends to absorb shock. When the middle armature leg


30


deflects and strikes one of the cushioning elements or nubs


36


,


38


, the cushioning element would absorb a portion of the impact of the middle armature leg


30


. The cushioning nature of the nubs


36


and


38


further inhibits plastic deformation and damage to the middle armature leg


30


providing greater shock resistance.




The nubs


36


and


38


of the present invention are easy to apply to the transducer


10


. In one embodiment, drops of adhesive are simply applied to the surface of the magnetic elements


18


and


20


prior to assembly of the transducer


10


. The present invention requires no additional parts, apart from these simple nubs. The transducer


10


may be easily assembled, and the armature may be adjusted with a rather high degree of accuracy.




The transducer


10


of the present invention also provides excellent shock resistance. Shock resistance tests were performed on several samples of the transducer


10


depicted in

FIGS. 1-4

“Inventive” hereinafter). For the Inventive transducers, the middle armature leg


30


has a thickness of about 0.2 mm, and the second air gap


24


is approximately 0.35 mm. Drops of UV-cured adhesive from the Lord Corporation having a hardness of about Shore D 75 formed the nubs


36


and


38


on the magnetic elements


18


and


20


. The nubs


36


and


38


have a size that provides the nub air gap “d” between the tips of the nubs of approximately 0.26 to 0.27 mm. The nubs


36


and


38


have a diameter of approximately 0.5 mm. The nubs


36


and


38


are secured to the magnetic elements


18


and


20


with an edge of the nub's rounded exterior aligned with the end of the magnetic elements


18


and


20


adjacent to the coil.




To compare the shock resistance of the transducer


10


to conventional transducers, a transducer similar to the transducer


10


but without the nubs


36


and


38


“Nubless” hereinafter) was tested. Additionally, transducers produced by Knowles (Model ED1913) having deformations on the armature leg within the coil “Knowles” hereinafter) was tested. Furthermore, a Microtronic transducer (Model 2313) was tested which had a coil rotated at about 7°-8° to limit the deflection of the armature “Microtronic” hereinafter) was tested.




A free fall drop test was conducted to compare shock resistance of the Inventive, Nubless and Microtronic transducers. The test was conducted by dropping from varying heights (0 to 175 centimeters) the transducers upon a laboratory floor comprised of concrete covered by vinyl. The orientation of the transducers toward the floor was random. The distortion of the dropped transducers was measured after the free fall with a nominal input of 0.35 mVA at 1150 Hz. Table 1below illustrates the results of the free fall test with the data within the table representing percentage distortion at 1150 Hz. Table 1 also illustrates the distortion levels with symbols. No symbol represents a distortion level less than 5% distortion, an asterisk symbol (*) represents 5-10% distortion, an at symbol (@) represents 10-15% distortion and a number symbol (#) represents greater than 15% distortion.












TABLE 1











Free Fall Test Results


















Trial




Height




Height




Height




Height




Height




Height




Height






No.




0 cm




50 cm




75 cm




100 cm




125 cm




150 cm




175 cm














Nubless Transducer Percentage Distortion from Free Fall Test


















1




2.1




1.7




3.9




2.9




27.1#




#




#






2




3.6




3.7




2.3




30.1#




34#




#




#






3




2.7




1.4




14.3@




17.4#




15.2#




#




#






4




2.4




3.1




2.1




35#




40.8#




#




#






5




1.5




1.6




14.7@




8.1*




51.3#




#




#






6




2.3




2.3




4.3




34.6#




47.1#




#




#






7




1.6




1.6




1.2




1.6




33#




#




#






8




3.7




26.9#




9.3*




56.1#




80#




#




#






9




4.2




4.1




7.3*




1.3




50#




#




#






10




2.9




4.6




4.3




13.6*




54.8#




#




#











Microtronic Transducer Percentage Distortion from Free Fall Test


















1




2.9




1.7




2.6




2.6




1.9




8.7*




10.3@






2




0.9




1.3




5.8*




2.6




5.3*




11.6@




16.9#






3




1




5




3.1




1.4




1.8




2.8




1.9






4




0.9




1.2




1.3




1.7




1.3




1.2




6






5




1.7




1.7




1.7




1.6




13.1@




3.8




13.1@






6




0.9




1.3




5.4*




10@




8.6@




16#




20.3#






7




1.3




1.7




2.1




1.9




16.4#




35.7#




37.4#






8




2.6




2.6




3.1




2.2




2.4




3.5




16.9#






9




2.3




3.2




1.8




15.6#




1.8




1.6




2.2






10




1.7




4.4




2.5




1.5




1




1.1




17#











Inventive Transducer Percentage Distortion from Free Fall Test


















1




1.5




1.1




1.2




1.4




2.2




0.9




1.9






2




1.1




1.3




1.3




1.5




1.2




1.2




8.8*






3




1.6




1.9




2




2.5




4.6




2.2




16.9#






4




0.9




1.4




1.3




0.7




0.9




13.1@




16.4#














Table 1 illustrates that the Inventive transducers suffered the least distortion as of the free fall and impacts. The Microtronic transducer performed better than the Nubless transducer. Thus, the Inventive transducer provides superior shock resistance.




Additionally, to compare the shock resistance of the Inventive transducer to the conventional transducers, a mechanical shock test was performed. The mechanical shock test is illustrated in FIG.


5


. The test apparatus


50


comprises a steel ball


52


having a weight of approximately one kilogram connected to a steel bar


54


having a length of approximately one meter by a string


56


. A steel block


58


weighing approximately 100 kg reinforces the base of the bar


54


. The shock test was conducted by fixing the transducers on the flat side of the ball


52


using double-sided tape. Although the tape most likely added mechanical damping, all transducers were tested using the same tape. Also adhered to the ball


52


is an accelerometer (B&K 8300 accelerometer)


60


to measure peak acceleration of the ball


52


. The shock test comprises releasing the ball


52


at a certain distance such that the ball


52


will strike the block


58


reinforced bar


54


with the desired acceleration.




The Inventive transducer was tested with five samples being mounted to the ball


52


“cover up” and five samples mounted “cover down.” When the transducers are mounted “cover down,” the cover side of the transducer is affixed with the double tape to the flat side of the ball


52


. When the transducers are “mounted cover up,” the cover side of the transducer is opposite the flat side of the ball


52


. The reason for these separate measurements is that if the armature is asymmetrically mounted, the armature can move more freely in one direction and much less in the other direction, thus the shock resistance is also asymmetrical. Ten samples of each the Nubless, Microtronic and Knowles transducers were also tested.





FIG. 6

illustrates a graph of the shock resistance test with acceleration on the x-axis and percentage distortion at 1150 Hz on the y-axis. The distortion of the tested transducers was measured after the shock with a nominal input of 0.35 mVA at 1150 Hz. Referring to

FIG. 6

, the cluster of the lines I represents the test results for five Inventive transducers tested “cover down.” The cluster of the Lines


2


represents the test results for five Inventive transducers tested “cover up.” If the results of the Inventive transducers were graphed as an average, it would be nearly a horizontal line across the y-axis at less than 2% distortion. If the results of the Inventive transducers were graphed as an average, it would be nearly a horizontal line across the y-axis at less than 2% distortion. Line


3


illustrates the average test results for the Microtronic transducer. Line


4


illustrates the average test results for the Knowles transducer. Line


5


illustrates the average test results for the Nubless transducer.





FIG. 6

clearly illustrates the improved shock resistance of the Inventive transducer over the conventional transducers. The Nubless transducers have a level of 10% distortion at approximately 6000 g. The Knowles transducers have a level of 10% distortion at approximately 10500 g. The Microtronic transducers have a level of 10% distortion at approximately 11500 g. None of the Inventive transducers have a distortion of greater than a 5% distortion over the entire test range of 16000 g. Shock resistibility is generally defined as the level for which the distortion exceeds 10%. Thus, the Inventive transducers provide significantly more shock resistance then the other transducers.




It will be appreciated that the present invention has been generally described with reference to a particular embodiment illustrated in the figures, but the present embodiment is not limited to the particular embodiments described herein. For example, the present invention may include a U-shaped armature or other suitable form instead of the illustrated E-shaped armature. For the U-shaped armature embodiment, one of the nubs


36


may be mounted on the left on the upper magnetic element


18


and the other nub


38


on the right on the lower magnetic element


20


. Additionally, it is also possible that the first air gap and/or the second air gap has a non-rectangular cross section. Similarly, the nubs may have varying positions, shapes and compositions.




While particular embodiments and applications of the present invention have been illustrated and described, it is to be understood that the invention is not limited to the precise construction and compositions disclosed herein and that various modifications, changes, and variations will be apparent from the foregoing descriptions without departing from the spirit and scope of the invention as defined in the appended claims.



Claims
  • 1. A transducer comprising:a coil having a first air gap; a magnetic member having a second air gap, said magnetic member including at least one nub extending into said second air gap; and an armature including an armature leg extending through said first and said second air gaps, said armature leg capable of movement within said second air gap, said nub limiting the movement of said armature leg within said second air gap.
  • 2. The transducer of claim 1, wherein said nub is comprised of a shock absorbing material.
  • 3. The transducer of claim 2, wherein said nub absorbs a portion of an impact of said armature leg when said armature leg moves into contact with said nub.
  • 4. The transducer of claim 2, wherein said nub is a drop of cured adhesive secured to said magnetic member.
  • 5. The transducer of claim 1, wherein a pair of said nubs are secured to said magnetic member, said a pair of nubs are symmetrical with respect to a longitudinal plane of said armature leg that is perpendicular to a direction of said armature movement.
  • 6. The transducer of claim 1, wherein said first air gap and said second air gap are aligned.
  • 7. The transducer of claim 1, wherein said nub prevents said armature leg from plastic deformation.
  • 8. The transducer of claim 1, wherein said armature has an E-shape.
  • 9. The transducer of claim 1, wherein said armature has a U-shape.
  • 10. The transducer of claim 1, wherein said nubs are positioned on said magnetic member opposite a free end of said armature leg.
  • 11. A transducer comprising:a coil having a first air gap; a magnetic assembly having a second air gap; said magnetic assembly include at least one cushioning element extending into said second air gap; and an armature including an armature leg extending through both said first air gap and said second air gap, said armature leg capable of movement within said second air gap, said armature leg engaging said cushioning element in response to said transducer being subject to a shock.
  • 12. The transducer of claim 11, wherein said cushioning element is comprised of a soft material.
  • 13. The transducer of claim 11, wherein said cushioning element absorbs a portion of an impact of said armature leg when said armature leg moves into contact with said cushioning element.
  • 14. The transducer of claim 11, wherein said nub is a drop of cured adhesive secured to said magnetic assembly.
  • 15. The transducer of claim 11, wherein a pair of cushioning elements are symmetrical with respect to a longitudinal plane of said armature leg that is perpendicular to a direction of said armature movement.
  • 16. The transducer of claim 11, wherein said cushioning elements are positioned on said magnetic assembly away from a free end of said armature leg.
  • 17. A transducer comprising:a coil having an inner surface defining a first air gap; a magnetic member including a pair of magnetic elements, said pair of magnetic elements being spaced apart by a distance and defining a second air gap therebetween, said first air gap and said second air gap being generally aligned; an armature extending through said first and said second air gaps, said armature leg capable of moving within said second air gap; and at least one nub positioned on said magnetic member for limiting the movement of said armature within said second air gap.
  • 18. The transducer of claim 17, wherein said at least one nub is positioned on one of said pair of magnetic elements.
  • 19. The transducer of claim 18, wherein said at least one nub includes two nubs, one of said nubs being located on a first one of said pair of magnetic elements, the other of said nubs being located on a second one of said pair of magnetic elements.
  • 20. The transducer of claim 19, wherein said pair of magnetic elements have surfaces facing each other, said surfaces being substantially parallel.
  • 21. The transducer of claim 20, wherein said nubs are made of a material having a Shore D hardness of less than about 90.
  • 22. The transducer of claim 21, wherein said material has a Shore D hardness of about 75.
  • 23. The transducer of claim 21, wherein said material is a UV-cured epoxy.
  • 24. The transducer of claim 21, wherein said nubs are cushioning elements for absorbing shock.
  • 25. The transducer of claim 17, wherein each of said first and second gaps are substantially rectangular in cross-section.
  • 26. The transducer of claim 25, wherein corresponding ones of the four edges defining each of said rectangular shaped cross-sections are substantially parallel.
  • 27. The transducer of claim 17, wherein said armature has an E-shape.
  • 28. The transducer of claim 17, wherein said armature has a U-shape.
  • 29. The transducer of claim 17, wherein said nubs are positioned at a coil side of said magnetic member.
  • 30. A method of increasing the shock resistance of a transducer comprising a coil defining a first air gap, a pair of magnetic elements being spaced apart by a distance and defining a second air gap that is lateral to and generally aligned with said first air gap, and a moveable armature extending through said first and said second air gaps, said method comprising:decreasing the size of the said second air gap by adding a material to said pair of magnetic elements to absorb shock, said material being a cushioning element having a Shore D hardness of less than about 90.
  • 31. The method of claim 30, wherein said step of adding material includes the step of providing a smooth rounded shape to a surface of said material that is to contact said armature.
  • 32. The method of claim 30, wherein said material is added at a coil side of said pair of magnetic elements.
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