Adjustable trip solenoid

Information

  • Patent Grant
  • 6404314
  • Patent Number
    6,404,314
  • Date Filed
    Tuesday, February 29, 2000
    24 years ago
  • Date Issued
    Tuesday, June 11, 2002
    22 years ago
Abstract
An adjustable solenoid having an enclosure containing a winding through which a current is passed. The winding defines an area and a plunger is positioned at one end of the area with a mechanical biasing mechanism for providing a biasing force to the plunger, the mechanical biasing mechanism is secured to the plunger at one end and a support at the other end. A stator having a first threaded portion engaged within a threaded opening of the enclosure causes the stator to travel between a first position and a second position as a rotational force is applied to the stator. The first position is closer to the plunger than the second position, and the stator is in a facially spaced relationship with respect to the plunger and the stator has a second threaded portion for engaging a threaded portion of the support, the second threaded portion of the stator causes the support to travel between a first position and a second position, the second position of the support provides the mechanical biasing mechanism with a greater biasing force than the first position.
Description




BACKGROUND OF THE INVENTION




The present invention relates to an adjustable magnetic device.




BACKGROUND




A magnetic tripping device such as a solenoid generally comprises a coil or winding of wire through which a current is passed. The solenoid is configured to manipulate an actuator when the electromagnetic force generated by the coil exceeds a predetermined value of the solenoid.




The actuator is generally biased by a mechanical force in an opposite direction of the force generated by the electromagnetic field of the coil. This force is typically provided by a spring or other mechanical means wherein a plunger of the actuator is biased with respect to a stator positioned opposite to the actuator.




In addition, an air gap is positioned in between the actuator and a stator. The air gap is also located within the coil and provides an insulating barrier to the force generated by the electromagnetic field of the coil.




Accordingly, the tripping or predetermined tolerances of a solenoid are dependent upon the mechanical biasing force and the size and positioning of the air gap.




Moreover, the required range or predetermined tolerances of a magnetic tripping device vary in accordance with user's requirements such as the circuit loading.




Most solenoids are either fixed (nonadjustable) or have a single means of adjustment for either the air gap or biasing force.




In an attempt to accommodate these varying tolerances, an adjustable trip solenoid has been developed wherein the air gap between the stator and the actuator can be varied. However, the varying of this air gap also causes the spring biasing force to vary. Moreover, these changes are opposite with respect to each other. For example, increasing the air gap will also decrease the biasing force of a spring.




Accordingly, there is a need for an adjustable solenoid wherein the air gap and mechanical biasing force can be varied so that as the air gap is decreased the mechanical biasing force is also decreased, and vice versa.




SUMMARY OF THE INVENTION




In an exemplary embodiment of the invention, an adjustable solenoid provides an adjustable air gap where the mechanical biasing force of the solenoid is either decreased or increased as the air gap is increased or decreased.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a front cross-sectional view of a solenoid constructed in accordance with the instant application;





FIG. 2

is a front cross-sectional view illustrating movement of a solenoid constructed in accordance with the instant application;





FIG. 3

is a view along lines


3





3


of

FIG. 1

;





FIG. 4

is a front perspective view of a portion of an alternative embodiment;





FIG. 5

is a front perspective view of the

FIG. 4

embodiment illustrating movement thereof;





FIG. 6

is a front perspective view of the

FIG. 4

embodiment illustrating movement thereof; and





FIG. 7

is a front perspective view of circuit breaker with an adjustable trip solenoid.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring now to

FIGS. 1 and 2

, an adjustable trip solenoid


10


is illustrated. In an exemplary embodiment, solenoid


10


is coupled to a circuit interruption mechanism


70


of a circuit breaker


72


(

FIG. 7

) wherein the movement or actuation of solenoid


10


causes a tripping mechanism


74


to trip circuit breaker


72


.




Solenoid


10


has a support structure


12


into which a coil


14


is received. Coil


14


consists of a copper wire through which a current is passed. In accordance with the direction of the current being passed through coil


14


, a magnetic field is generated by solenoid


10


.




A plunger


16


for movement within solenoid


10


has an actuating member


18


. Actuating member


18


is configured to pass through an opening


20


in support structure


12


of solenoid


10


. In addition, actuating member


18


is configured to have a planar member


19


, which in conjunction with actuating member


18


provides a receiving area for a portion of an actuating arm


21


. The movement of plunger and accordingly actuating member


18


causes actuating arm


21


to move from a first position to a second position (illustrated by the dashed lines in FIG.


1


). See also FIG.


2


.




It is intended that actuating arm


21


is to be coupled to a mechanism


74


(

FIG. 6

) that in accordance with the movement of actuating arm


21


from the first position to a second position, will cause an intended result of the mechanism. For example, the movement of the mechanism will cause a circuit breaker to trip. Other uses may be the activation of warning lights, indication lights, status indicators and audible alarms, etc.




In addition, actuating arm


21


is provided with a biasing force in the direction of arrow


23


that must be overcome by the movement of plunger


18


. In addition, the biasing force in the direction of arrow


23


also provides stability to actuating arm


21


. Moreover, the biasing force causes actuating arm


21


to return to the position illustrated in

FIG. 1

, once plunger


16


returns to its initial position. A spring


25


or other bias producing means causes the biasing force to be placed upon arm


21


.




As an alternative, and as illustrated by the dashed lines in

FIG. 1

, actuating arm


21


is positioned to rest upon plunger


18


and the biasing force of spring


25


is in a direction opposite to arrow


23


. In addition, and as yet another alternative, actuating arm


21


may be replaced by a pair of actuating arms or planar member in which a portion is received and engaged by planar members


19


of plunger


18


.




The movement of plunger


16


is caused by electromagnetic forces, which are generated by a current running through coil


14


.




One end of a pair of springs


22


are secured to plunger


16


and the other end of springs


22


are secured to a pair of spring position stands


24


. Springs


22


are positioned to provide a biasing force in the direction of arrow


26


. Accordingly, and in order to position plunger


16


as illustrated by the dashed lines in

FIG. 1

, the electromagnetic force generated by solenoid


10


must overcome the biasing force of springs


22


.




A stator


28


is positioned opposite to plunger


16


and an air gap


30


is defined between plunger


16


and stator


28


. In addition, air gap


30


is positioned within coil


14


.




Stator


28


is configured to have a first threaded portion


32


and a second threaded portion


34


. An engagement surface


36


of spring position stands


24


also has a threaded portion


38


. Threaded portion


38


is configured to have the same configuration (i.e. angle, size and slope) of first threaded portion


32


.




Second threaded portion


34


of stator


28


is received and engaged in an opening


40


of support structure


12


. The inner surfaces of opening


40


are configured to have a threaded engagement surface


42


that is sized and configured to engage second threaded portion


34


of stator


28


.




An end portion


44


of stator


28


has an engagement opening


46


. (

FIG. 2

) Engagement opening


46


is configured to receive and engage a tool such as a screwdriver, Allen wrench or other item for applying a rotational force to stator


28


.




The pitch or angle of engagement of first pair of threads


32


and


38


is substantially opposite to second pair of threads


34


and


42


. In addition, the size of threads


34


and


42


is substantially smaller than threads


32


and


38


. In an exemplary embodiment, the size of threads


32


is 10 threads per inch, and the size of threads


34


is 32 threads per inch. Accordingly, there is approximately a 3 to 1 thread ratio between threads


32


and


34


. Of course, it is contemplated that the dimensions; size and configuration of threads


32


and


34


may be larger or smaller than the dimensions mentioned above. Accordingly, and as a rotational force is applied to engagement opening


46


in a first direction, stator


28


will move in the direction of arrow


48


. This movement of stator


28


will cause the size of air gap


30


to decrease. However, since the angle of engagement of first pair of threads


32


is opposite to that of second pair of threads


34


, the movement of stator


28


in the direction of arrow


48


, caused by the rotation of stator


28


in a first direction, will also cause spring position stands


24


to move in an opposite direction or in the direction of arrow


50


. Moreover, and since the size of threads


32


is substantially larger than the size of threads


34


, this movement is at a much greater rate with respect to each revolution of stator


28


.




Accordingly, and as spring position stands


24


move in the direction of arrow


50


, biasing force of springs


22


is decreased. A pair of shoulder portions


52


are located on the inner surface of support structure


12


. Shoulder portions


52


provide an area into which spring position stands


24


can move as they move in the direction of arrows


50


.




Accordingly, and as a rotational force is applied to stator


28


in a first direction, the size of air gap


30


is reduced while the biasing force of springs


22


is also reduced.




Conversely, and as a rotational force is applied to stator


28


in a second direction, the size of air gap


30


will increase, while the biasing force of springs


22


is also increased.




Thus, for a low X-setting on the solenoid, it is desirable to have a high-efficiency solenoid that can generate a high output force per Ampere-turn for any given construction. To accomplish this, it is desirable to have a small air gap with a low reverse bias force.




On the other hand, and for a high X-setting on the same solenoid, it is desirable to lower the efficiency of the solenoid and thereby lower the output force per ampere-turn for the same given construction. To accomplish this, it is desirable to have a large air gap with a large reverse bias force.




Accordingly, the solenoid of the instant application allows such adjustments to be made in a quick and convenient manner. Moreover, the same solenoid can be used for such applications.




In addition, and as contemplated in accordance with the instant application, the size and configuration of threaded portions


32


and


34


are configured to obtain a desired result. For example, each revolution of stator


28


, or portion thereof, will cause stator


28


to move in a first direction of a known magnitude, while spring position stands


24


move in an opposite direction of a known magnitude. Therefore, and as a rotational force is applied to stator


28


, the movement of stator


28


and spring position stands


24


will adjust the trip setting of solenoid


10


to a known value.




Referring now to

FIG. 3

, and as an alternative, surface


44


of stator


28


is marked with an indication arrow


54


while the surrounding surface of support structure


12


is also marked with a plurality of markings


56


which will indicate the trip setting of solenoid


10


when arrow


54


is pointing thereto. Of course, alternative marking arrangements are contemplated, such as, demarcations on the inner surface of opening


40


and stator


28


which will indicate the trip setting of solenoid


10


as stator


28


moves within opening


40


. For example, such indications may be a color oriented scheme that provides a user with a quick and convenient means of determining the solenoid's trip setting.




Referring now to

FIG. 4

, an alternative embodiment of the instant application is illustrated. Here, component parts performing similar or analogous functions are numbered in multiples of 100.




Here, a solenoid


110


is configured to have a flux shifter


160


. Flux shifter


160


is an elongated sleeve portion constructed out of a ferromagnetic material that is configured to be placed over plunger


116


and is capable of movement in the direction indicated by arrows


162


.




Flux shifter


160


is secured to stator


128


by a pair of connection rods


164


. Accordingly, and as a rotational force is applied to stator


128


, through a tool inserted into engagement opening


146


, the threaded portion


134


of stator


128


will travel through the threaded portion


142


of opening


140


which, depending on the direction of the rotational force, will cause stator


128


and accordingly flux shifter


160


to move in either direction of arrows


162


.




Accordingly, and as stator


128


is moved in a direction away from plunger


116


, air gap


130


increases in size and flux shifter


160


is repositioned to cover a portion or all of air gap


130


. Since flux shifter


160


is constructed out of a ferromagnetic material, once it is positioned in close proximity to air gap


130


, flux shifter


160


creates a path of lesser reluctance for the magnetic flux of solenoid


110


to travel.




For example, and referring now to

FIG. 5

, as flux shifter


160


covers air gap


130


, the flux of solenoid


110


is partially illustrated by the dashed lines in FIG.


4


. This positioning of flux shifter


160


will allow solenoid


110


to be able to accept a higher current value through coil


114


before plunger


116


is actuated. Moreover, the size of air gap


130


is also increased in the position illustrated by

FIG. 5

this also increases in the amount of flux required to actuate plunger


116


.




Conversely, and as flux shifter


160


and stator


128


are moved back into the position illustrated by

FIG. 4

, the flux of solenoid


110


is illustrated partially by the dashed lines in FIG.


6


.




Comparing solenoid


110


of

FIGS. 5 and 6

shows a high-efficiency electromagnetic system in

FIG. 6 and a

low efficiency electromagnetic system in FIG.


5


. Since higher magnetic forces are generated from a solenoid having high efficiency, the magnetic forces generated by solenoid


110


of

FIG. 6

will be greater than those of

FIG. 5

at a given solenoid current value. Alternatively, for a given trip force, the solenoid


110


of

FIG. 6

will have a trip point (activation threshold) at a lower solenoid current than will the solenoid


110


of FIG.


5


.




Therefore, solenoid


110


provides the user with a single means of adjustment for introducing flux shifter


160


while concurrently increasing air gap


130


and vice versa. This configuration provides a wide range of trip settings for solenoid


110


.




In an exemplary embodiment, solenoid


110


has a low gradient compression spring or springs


122


that has a de minimus change in bias force as stator


128


moves.




While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.



Claims
  • 1. An adjustable solenoid, comprising:a) an enclosure containing a winding through which a current is passed, said winding defining an area; b) a plunger being positioned at one end of said area, said plunger having an actuating member positioned to pass through an opening in said enclosure, said plunger being configured for movement between an actuating position and a non-actuating position; c) a mechanical biasing mechanism for providing a biasing force to said plunger, said mechanical biasing mechanism being secured to said plunger at one end and a support at the other; d) a stator having a first threaded portion being engaged within a threaded opening of said enclosure, said first threaded portion and said threaded opening of said enclosure causing said stator to travel between a first position and a second position as a rotational force is applied to said stator, said first position being closer to said plunger than said second position, said stator being in a facially spaced relationship with respect to said plunger and having a second threaded portion for engaging a threaded portion of said support, said second threaded portion of said stator causing said support to travel between a first position and a second position, said second position of said support provides said mechanical biasing mechanism with a greater biasing force than said first position.
  • 2. The solenoid as in claim 1, wherein said mechanical biasing mechanism is a spring having one end fixedly secured to said plunger and the other end being fixedly secured to said support.
  • 3. The solenoid as in claim 2, wherein said first and second threaded portions of said stator are positioned on a generally circular portion of said stator and said threaded opening in said enclosure is also generally circular in configuration.
  • 4. The solenoid as in claim 3, wherein said support is an annular collar having an inner surface with a threaded portion for engaging said second threaded portion of said stator.
  • 5. The solenoid as in claim 4, wherein said enclosure is configured to have a receiving area to allow for the movement of said annular collar.
  • 6. The solenoid as in claim 1, wherein said enclosure is configured to have a receiving area to allow for the movement of said support.
  • 7. The stator as in claim 3, wherein said stator has an engagement surface with an engagement opening positioned to be engaged from outside of said enclosure.
  • 8. The stator as in claim 7, wherein said engagement surface is marked with indicia and said enclosure is also marked with indicia in close proximity to said indicia of said engagement surface, said indicia of said engagement surface and said indicia of said enclosure indicating the trip setting of said solenoid.
  • 9. The stator as in claim 1, wherein said second threaded portion has a pitch opposite to said first threaded portion.
  • 10. The stator as in claim 9, wherein the thread size of said second threaded portion is substantially larger than said first threaded portion.
  • 11. The stator as in claim 10, wherein said mechanical biasing mechanism is a pair of springs, each of said springs having one end secured to said plunger and the other secured to said support.
  • 12. The stator as in claim 3, wherein said support is a pair of supports and said mechanical biasing mechanism is a pair of springs, each having one end secured to said plunger and the other end secured to one of said supports.
  • 13. The stator as in claim 12, wherein said enclosure is configured to have a receiving area to allow for the movement of said supports.
  • 14. A method for varying the trip setting in a solenoid, comprising:simultaneously adjusting the size of an air gap between a stator and a plunger of said solenoid and the biasing force of a spring providing a biasing force to said plunger, said biasing force decreases as said air gap decreases.
  • 15. A method for varying the trip setting in a solenoid, comprising:adjusting the size of an air gap between a stator and a plunger of said solenoid and the biasing force of a spring providing a biasing force to said plunger, said biasing force decreases as said air gap decreases, wherein said stator is movably mounted within said solenoid and said air gap and said biasing force are adjusted by a rotational force applied to said stator.
  • 16. A method for varying the trip setting in a solenoid, comprising:a) adjusting the size of an air gap between a stator and a plunger of said solenoid by applying a rotational force to said stator; and b) adjusting the biasing force of a spring providing a biasing force to said plunger, said biasing force increases as said rotational force is applied to said stator and said air gap increases.
  • 17. The method as in claim 16, wherein said air gap increases at lesser rate than said biasing force.
  • 18. The method as in claim 16, wherein said stator is movably mounted within said solenoid.
  • 19. The method as in claim 14, wherein said stator is movably mounted within said solenoid.
  • 20. The method as in claim 14, wherein said spring is secured to said plunger at one end and a support member at the other and said stator moves in a opposite direction with respect to said support member as said biasing force decreases and said air gap decreases.
  • 21. An adjustable solenoid, comprising:a) a plunger being positioned at one end of said solenoid, said plunger being configured for movement between an actuating position and a non-actuating position in response to a magnetic field generated by said solenoid; b) a biasing member for providing a biasing force to said plunger, said biasing member being secured to said plunger at one end and a support at the other; d) a stator being movably received within said solenoid, said stator being adapted to move between a first position and a second position, said first position being closer to said plunger than said second position, said stator being in a facially spaced relationship with respect to said plunger and having a means for moveably engaging said support, the movement of said stator towards said first position causes said support to travel from a first position to a second position, said second position of said support provides said biasing member with a lesser biasing force than said first position of said support.
  • 22. The adjustable solenoid as in claim 21, wherein said support moves in an opposite direction with respect to said stator.
  • 23. The adjustable solenoid as in claim 21, wherein said support is an annular ring configured for engaging a threaded portion of said stator.
  • 24. The adjustable solenoid as in claim 23, wherein said adjustable solenoid is configured to have a receiving area for accommodating a range of movement for said annular ring.
  • 25. The adjustable solenoid as in claim 23, wherein said biasing member is a pair of springs each having one end secured to said plunger and the other secured to said annular ring.
  • 26. An adjustable solenoid, comprising:a) a plunger being positioned at one end of said solenoid, said plunger being configured for movement between an actuating position and a non-actuating position in response to a magnetic field generated by said solenoid; b) a biasing member for providing a biasing force to said plunger, said biasing member being secured to said plunger at one end and a support at the other; and c) a means for decreasing an air gap between a stator and said plunger while decreasing said biasing force.
  • 27. The adjustable solenoid as in claim 26, wherein said biasing force decreases at a factor of three times that of the decreasing of said air gap.
  • 28. An adjustable solenoid, comprising:a) a plunger being positioned at one end of said solenoid, said plunger being configured for movement between an actuating position and a non-actuating position in response to a magnetic field generated by said solenoid; b) a biasing member for providing a biasing force to said plunger, said biasing member being secured to said plunger at one end and a support at the other, the amount of said biasing force being dependant upon the size of the distance between said support and said plunger; and c) a means for varying the distance between a stator of said solenoid and said plunger while simultaneously varying in an opposite manner the distance between said support and said plunger.
  • 29. An adjustable solenoid, comprising:a) a plunger being positioned at one end of said solenoid, said plunger being configured for movement between an actuating position and a non-actuating position in response to a magnetic field generated by said solenoid; b) a biasing member for providing a biasing force to said plunger; and c) a means for varying the size of an air gap between a stator and said plunger while simultaneously varying in an opposite manner the size of said biasing force.
US Referenced Citations (173)
Number Name Date Kind
2340682 Powell Feb 1944 A
2719203 Gelzheiser et al. Sep 1955 A
2937254 Ericson May 1960 A
3158717 Jencks et al. Nov 1964 A
3162739 Klein et al. Dec 1964 A
3197582 Norden Jul 1965 A
3307002 Cooper Feb 1967 A
3517356 Hanarusa Jun 1970 A
3631369 Menocal Dec 1971 A
3803455 Willard Apr 1974 A
3883781 Cotton May 1975 A
4129762 Bruchet Dec 1978 A
4144513 Shafer et al. Mar 1979 A
4158119 Krakik Jun 1979 A
4165453 Hennemann Aug 1979 A
4166988 Ciarcia et al. Sep 1979 A
4220934 Wafer et al. Sep 1980 A
4255732 Wafer et al. Mar 1981 A
4259651 Yamat Mar 1981 A
4263492 Maier et al. Apr 1981 A
4276527 Gerbert-Gaillard et al. Jun 1981 A
4297663 Seymour et al. Oct 1981 A
4301342 Castonguay et al. Nov 1981 A
4360852 Gilmore Nov 1982 A
4368444 Preuss et al. Jan 1983 A
4375021 Pardini et al. Feb 1983 A
4375022 Daussin et al. Feb 1983 A
4376270 Staffen Mar 1983 A
4383146 Bur May 1983 A
4392036 Troehel et al. Jul 1983 A
4393283 Masuda Jul 1983 A
4401872 Boichot-Castagne et al. Aug 1983 A
4409573 DiMarco et al. Oct 1983 A
4435690 Link et al. Mar 1984 A
4463332 Everett Jul 1984 A
4467297 Boichot-Castagne et al. Aug 1984 A
4467645 Gerbert-Gaillard et al. Aug 1984 A
4470027 Link et al. Sep 1984 A
4479143 Watanabe et al. Oct 1984 A
4488133 McClellan et al. Dec 1984 A
4492941 Nagel Jan 1985 A
4541032 Schwab Sep 1985 A
4546224 Mostosi Oct 1985 A
4550360 Dougherty Oct 1985 A
4562419 Preuss et al. Dec 1985 A
4589052 Dougherty May 1986 A
4595812 Tamaru et al. Jun 1986 A
4611187 Banfi Sep 1986 A
4612430 Sloan et al. Sep 1986 A
4616198 Pardini Oct 1986 A
4622444 Kandatsu et al. Nov 1986 A
4631625 Alexander et al. Dec 1986 A
4642431 Tedesco et al. Feb 1987 A
4644438 Puccinelli et al. Feb 1987 A
4649247 Preuss et al. Mar 1987 A
4658322 Rivera Apr 1987 A
4672501 Bilac et al. Jun 1987 A
4675481 Markowski et al. Jun 1987 A
4682264 Demeyer Jul 1987 A
4689712 Demeyer Aug 1987 A
4691182 Mrenna et al. Sep 1987 A
4694373 Demeyer Sep 1987 A
4710845 Demeyer Dec 1987 A
4711255 Davis et al. Dec 1987 A
4717985 Demeyer Jan 1988 A
4733211 Castonguay et al. Mar 1988 A
4733321 Lindeperg Mar 1988 A
4764650 Bur et al. Aug 1988 A
4768007 Mertz et al. Aug 1988 A
4780786 Weynachter et al. Oct 1988 A
4831221 Yu et al. May 1989 A
4870531 Danek Sep 1989 A
4883931 Batteux et al. Nov 1989 A
4884047 Baginski et al. Nov 1989 A
4884164 Dziura et al. Nov 1989 A
4900882 Bernard et al. Feb 1990 A
4910485 Bolongeat-Mobleu et al. Mar 1990 A
4914541 Tripodi et al. Apr 1990 A
4916420 Bartolo et al. Apr 1990 A
4916421 Pardini et al. Apr 1990 A
4926282 McCline May 1990 A
4935590 Malkin et al. Jun 1990 A
4937706 Schueller et al. Jun 1990 A
4939492 Raso et al. Jul 1990 A
4943691 Mertz et al. Jul 1990 A
4943888 Jacob et al. Jul 1990 A
4950855 Bolonegeat-Mobleu et al. Aug 1990 A
4951019 Gula Aug 1990 A
4952897 Barnel et al. Aug 1990 A
4958135 Baginski et al. Sep 1990 A
4965543 Batteux Oct 1990 A
4983788 Pardini Jan 1991 A
5001313 Leclerq et al. Mar 1991 A
5004878 Seymour et al. Apr 1991 A
5029301 Nehon et al. Jul 1991 A
5030804 Abri Jul 1991 A
5057655 Kersusan et al. Oct 1991 A
5077627 Fraisse Dec 1991 A
5083081 Barrault et al. Jan 1992 A
5095183 Raphard et al. Mar 1992 A
5103198 Morel et al. Apr 1992 A
5115371 Tripodi May 1992 A
5120921 DiMarco et al. Jun 1992 A
5132865 Mertz et al. Jul 1992 A
5138121 Streich et al. Aug 1992 A
5140115 Morris Aug 1992 A
5153802 Mertz et al. Oct 1992 A
5155315 Malkin et al. Oct 1992 A
5166483 Kersusan et al. Nov 1992 A
5172087 Castonguay et al. Dec 1992 A
5178504 Falchi Jan 1993 A
5184717 Chou et al. Feb 1993 A
5187339 Lissandrin Feb 1993 A
5198956 Dvorak Mar 1993 A
5200724 Gula et al. Apr 1993 A
5210385 Morel et al. May 1993 A
5239150 Bolongeat-Mobleu et al. Aug 1993 A
5260533 Livesey et al. Nov 1993 A
5262744 Arnold et al. Nov 1993 A
5280144 Bolongeat-Mobleu et al. Jan 1994 A
5281776 Morel et al. Jan 1994 A
5296660 Morel et al. Mar 1994 A
5296664 Crookston et al. Mar 1994 A
5298874 Morel et al. Mar 1994 A
5300907 Nereau et al. Apr 1994 A
5310971 Vial et al. May 1994 A
5313180 Vial et al. May 1994 A
5317471 Izoard et al. May 1994 A
5331500 Corcoles et al. Jul 1994 A
5334808 Bur et al. Aug 1994 A
5341191 Crookston et al. Aug 1994 A
5347096 Bolongeat-Mobleu et al. Sep 1994 A
5347097 Bolongeat-Mobleu et al. Sep 1994 A
5350892 Rozier Sep 1994 A
5357066 Morel et al. Oct 1994 A
5357068 Rozier Oct 1994 A
5357394 Piney Oct 1994 A
5361052 Ferullo et al. Nov 1994 A
5373130 Barrault et al. Dec 1994 A
5379013 Coudert Jan 1995 A
5424701 Castonguary et al. Jun 1995 A
5438176 Bonnardel et al. Aug 1995 A
5440088 Coudert et al . Aug 1995 A
5449871 Batteux et al. Sep 1995 A
5450048 Leger et al. Sep 1995 A
5451729 Onderka et al. Sep 1995 A
5457295 Tanibe et al. Oct 1995 A
5467069 Payet-Burin et al. Nov 1995 A
5469121 Payet-Burin Nov 1995 A
5475558 Barjonnet et al. Dec 1995 A
5477016 Baginski et al. Dec 1995 A
5479143 Payet-Burin Dec 1995 A
5483212 Lankuttis et al. Jan 1996 A
5485343 Santos et al. Jan 1996 A
D367265 Yamagata et al. Feb 1996 S
5493083 Olivier Feb 1996 A
5504284 Lazareth et al. Apr 1996 A
5504290 Baginski et al. Apr 1996 A
5510761 Boder et al. Apr 1996 A
5512720 Coudert et al. Apr 1996 A
5515018 DiMarco et al. May 1996 A
5519561 Mrenna et al. May 1996 A
5534674 Steffens Jul 1996 A
5534832 Duchemin et al. Jul 1996 A
5534835 McColloch et al. Jul 1996 A
5534840 Cuingnet Jul 1996 A
5539168 Linzenich Jul 1996 A
5543595 Mader et al. Aug 1996 A
5552755 Fello et al. Sep 1996 A
5581219 Nozawa et al. Dec 1996 A
5604656 Derrick et al. Feb 1997 A
5608367 Zoller et al. Mar 1997 A
5784233 Bastard et al. Jul 1998 A
Foreign Referenced Citations (60)
Number Date Country
819 008 Dec 1974 BE
12 27 978 Nov 1966 DE
30 47 360 Jun 1982 DE
38 02 184 Aug 1989 DE
38 43 277 Jun 1990 DE
44 19 240 Jan 1995 DE
0 061 092 Sep 1982 EP
0 064 906 Nov 1982 EP
0 066 486 Dec 1982 EP
0 076 719 Apr 1983 EP
0 117 094 Aug 1984 EP
0 140 761 May 1985 EP
0 174 904 Mar 1986 EP
0 196 241 Oct 1986 EP
0 224 396 Jun 1987 EP
0 235 479 Sep 1987 EP
0 239 460 Sep 1987 EP
0 258 090 Mar 1988 EP
0 264 313 Apr 1988 EP
0 264 314 Apr 1988 EP
0 283 189 Sep 1988 EP
0 283 358 Sep 1988 EP
0 291 374 Nov 1988 EP
0 295 155 Dec 1988 EP
0 295 158 Dec 1988 EP
0 309 923 Apr 1989 EP
0 313 106 Apr 1989 EP
0 313 422 Apr 1989 EP
0 314 540 May 1989 EP
0 331 586 Sep 1989 EP
0 337 900 Oct 1989 EP
0 342 133 Nov 1989 EP
0 367 690 May 1990 EP
0 371 887 Jun 1990 EP
0 375 568 Jun 1990 EP
0 394 144 Oct 1990 EP
0 394 922 Oct 1990 EP
0 399 282 Nov 1990 EP
0 407 310 Jan 1991 EP
0 452 230 Oct 1991 EP
0 555 158 Aug 1993 EP
0 567 416 Oct 1993 EP
0 595 730 May 1994 EP
0 619 591 Oct 1994 EP
0 665 569 Aug 1995 EP
0 700 140 Mar 1996 EP
2 410 353 Jun 1979 FR
2 512 582 Mar 1983 FR
2 553 943 Apr 1985 FR
2 592 998 Jul 1987 FR
2 682 531 Apr 1993 FR
2 697 670 May 1994 FR
2 699 324 Jun 1994 FR
2 714 771 Jul 1995 FR
387037 Feb 1933 GB
412606 Jul 1934 GB
2 233 155 Jan 1991 GB
9200598 Jan 1992 WO
9205649 Apr 1992 WO
9400901 Jan 1994 WO
Non-Patent Literature Citations (1)
Entry
International Search Report, corresponding to International Application No. PCT/US 01/0 6204, dated the Jul. 13, 2001 and a copy of each of the publications cited therein.