Claims
- 1. An extruded composite having a helically twisted unitary structure, comprising: a unitary, helically twisted integral assembly of at least one axially elongated, substantially rigid inner cylindrical member having an outwardly directed wall, at least one axially elongated, substantially rigid outer tubular member, having an inwardly directed wall directed toward and radially spaced from said outwardly directed wall, and a plurality of substantially rigid struts disposed in part of the annular space and extending between the inwardly and outwardly directed walls;
wherein at least some of said struts are joined to both said inwardly and outwardly directed walls along a sufficient portion of the axial length of said walls to maintain a predetermined radial spacing between said walls; wherein at least some of said struts, that are paired next adjacent to each other, are disposed at opposite angles, other than perpendicular, with respect to said inwardly directed and said outwardly directed walls to which they are joined, and said paired struts are joined to said inwardly directed and outwardly directed walls such that there is at most a small portion of said wall(s) separating the juncture of each of said paired struts with said wall(s); wherein said composite structure has an outside diameter that is not substantially greater than the outside diameter of a fluid form extrudate from which it was made; wherein said fluid form extrudate initially comprises an axially aligned, untwisted, moldable, unitary structure comprising an inner cylindrical member having an outwardly directed wall, an outer tubular member having an inwardly directed wall radially spaced from, and directed toward, said outwardly directed wall, and angularly disposed strut pairs in supporting contact with both said inwardly directed wall and said outwardly directed wall; wherein said fluid form extrudate has been pulled and twisted as a unitary structure to produce moldable helically twisted unitary structure; wherein said moldable helically twisted unitary structure has been solidified by cooling from inside said inner cylindrical member and outside said outer tubular member into said substantially rigid, helically twisted unitary structure; and wherein the alignment of said helically twisted has longitudinal and circumferential alignment components.
- 2 CANCELLED
- 3. A composite tube as claimed in claim 1 wherein at least some of said struts are simultaneously contacted with and adhered to said inwardly directed and said outwardly directed walls, respectively, at location(s) that are spaced from the location where the next adjacent struts are contacted with and adhered to said inwardly and outwardly directed walls, respectively, so as to form generally longitudinal/circumferential strut-defining cells having a substantially trapezoidal cross section.
- 4. A composite tube as claimed in claim 3 wherein all of said struts are angularly disposed at alternating positive and negative angles away from normal with respect to said inwardly and outwardly directed walls.
- 5. A composite tube as claimed in claim 1 wherein all of said struts extend the entire longitudinal length of said composite tube.
- 6. A composite tube as claimed in claim 1 wherein said inner cylinder is a hollow tube.
- 7. A drainage pipe comprising a plurality of composite tubes as claimed in claim 6 joined together end to end.
- 8. A composite tube as claimed in claim 6 having at least one perforation in at least one of said tubular members.
- 9. A drainage pipe as claimed in claim 7 wherein said composite tubes are perforated.
- 10. A composite tube as claimed in claim 6, further comprising at least one perforation through said outer tubular member.
- 11. A composite tube as claimed in claim 6, further comprising a plurality of perforations through said inner and outer tubular members, said perforations being positioned such that a volume inside said inner tubular member is adapted to communicate with a volume outside said outer tubular member.
- 12. A pipe comprising a plurality of joined together composite tubes as claimed in claim 11.
- 13. A septic field comprising a plurality of composite tubes as claimed in claim 11.
- 14. A septic field comprising a plurality of composite tubes as claimed in claim 11, wherein some of said composite tubes are joined together end to end.
- 15. A method of draining underground water comprising burying at least one composite tube as claimed in claim 11 proximate to a source of said water and in a position adapted to permit said water to drain by gravity and in a condition adapted to cause underground water to seep into said inner tube through said perforations, and providing an outlet for said composite tube.
- 16. A method of making a helically twisted unitary cylindrical stricture, comprising an outer tubular member, an inner cylindrical member and a plurality of struts disposed in an annular space the between said inner and outer members, and in spacing and supporting relationship to said inner cylindrical member and said outer tubular member, said method comprising:
extruding a unitary, moldable cylindrical profile extrudate, having an outer cross sectional size, comprising, as the extrudate, a moldable inner cylindrical member, a moldable outer tubular member and moldable struts in spacing and supporting contact with said inner cylindrical member and said outer tubular member; while in a moldable condition, drawing in a downstream direction and twisting, said extrudate passing said twisted and drawn extrudate through a cooling zone, along a twisting path that has longitudinal and circumferential directional components that substantially correspond to a rate of circumferential twisting and a rate of down stream drawing, and cooling said structure from inside said inner cylindrical member and from outside said outer tubular member an amount sufficient to solidify said unitary extrudate in said drawn and twisted orientation; downstream of said cooling step, drawing said solidified composite unitary structure downstream while simultaneously twisting it so as to cause said molten extrudate, at a location between said extrusion and said cooling, to be pulled downstream and twisted, whereby causing said structure to become oriented in both longitudinal and circumferential directions prior to cooling/solidifying it; and carrying out said method under conditions such that the outer cross sectional size of said solid unitary structure is not substantially larger than the outer cross sectional size of said moldable extrudate.
- 17. A method as claimed in claim 16 wherein said inner cylindrical member is tubular and further comprising drawing said inner tubular member over a cooling mandrel and through a cooling sleeve under conditions sufficient to cool and solidify said extrudate from the inside as well as from the outside.
- 18. A method as claimed in claim 17 further comprising cooling and solidifying said inner tubular member, said outer tubular member and said struts at substantially the same time.
- 19. A method as claimed in claim 17 further comprising cooling said outer tubular member and proximate portion(s) of said struts by spraying cooling water on an outwardly directed surface thereof.
- 20. A method as claimed in claim 17 further comprising drawing a vacuum through apertures in said cooling mandrel that are adapted to be proximate to an inwardly directed surface of said inner tubular member an amount sufficient to cause an inwardly directed surface of said inner tubular member to maintain close proximity to said mandrel.
- 21. A method as claimed in claim 20 further comprising intermittently releasing said vacuum whereby permitting said inwardly directed surface to move away from said cooling mandrel for a period of time that is sufficient to prevent said inwardly directed surface from adhering to said mandrel during said cooling operation.
- 22. A method as claimed in claim 16 further comprising pulling and twisting said solidified extrudate an amount sufficient to form said moldable extrudate into a substantially helical orientation before it is fully solidified, and solidifying said twisted molten extrudate in said helical configuration.
- 23. A method as claimed in claim 22 wherein said inner cylindrical member is tubular and further comprising drawing and twisting said solidified extrudate such that said cooling extrudate follows a helical path about a cooling mandrel, and rotating said mandrel at a sufficient speed and direction to adjust the rotational speed of said inner tubular member relative to the rotational speed of said outer tubular member such as to cause said struts to not substantially deform prior to and during cooling.
- 24. A method as claimed in claim 16 further comprising twisting and drawing said solidified extrudate by closely contacting a plurality of driven belts about an outwardly directed surface of said outer tubular member; wherein different of said belts encounter said outwardly directed surface from different positions such that bending of said composite article is minimized; and driving said belts at a speed sufficient to cause said extrudate to be twisted circumferentially and drawn longitudinally.
- 25. A method as claimed in claim 24 further comprising contacting all of said belts with said tubular article at different positions.
- 26. A method as claimed in claim 24 further comprising contacting at least some of said belts with said tubular article at complementary positions.
- 27. A method as claimed in claim 24 further comprising adjusting the length of said belts to compensate for a change in the diameter of said tubular article.
- 28. A method as claimed in claim 16 further comprising feeding said moldable material to said extruder die from a plurality of feed locations disposed about the periphery of said extruder die.
- 29. A method as claimed in claim 28 further comprising feeding said moldable material to said extruder die from a plurality of feed locations substantially equally spaced about the periphery of said extruder die.
- 30. A method as claimed in claim 28 further comprising:
A. subdividing a feed of said moldable material into a plurality of first feed streams; B. subdividing at least some of said plurality of first feed streams into a plurality of second feed streams C. repeating step B a sufficient number of times to produce a plurality of feed streams each of which has a substantially smaller volume than said feed; and D. feeding the product of step C substantially evenly distributed about the periphery of an extrusion die.
- 31. A method of transversely cutting a composite tubular body as claimed in claim 16 further comprising:
circumferentially applying a “v” shaped cutter about said composite tube, whereby cutting a “v” groove partially through said composite tube and leaving a web of uncut tubular material; and thereafter, in a separate step, cutting all the way through the web of tubular material.
- 32. A method as claimed in claim 31 further comprising:
axially rotating said tubular body while longitudinally progressing said body; causing said “v” cutter to move longitudinally at substantially the same speed as said cylindrical body is longitudinally progressing: and rotating said “v” cutter while pressing it into said rotating cylindrical body while rotating said “v” about said cylindrical body; and pressing said “v” cutter into said rotating cylindrical body whereby said rotation of said “v” cutter causes said “v” cutter to cut a “v” groove in said cylindrical body.
- 33. A method as claimed in claim 21 further comprising, during release of said vacuum, and applying an overpressure of gas through at least some of said apertures in an amount and at a velocity sufficient to cause said inwardly directed surface to move away from said mandrel.
- 34. A method of producing a composite tubular article which comprises:
A. feeding a moldable material through an extrusion die to form a molten unitary extrudate having a more inward tubular member, at least one radially spaced apart more outward tubular member, and a plurality of struts, disposed at angles other than perpendicular and in supporting contact relationship between said more inward tubular member and a next adjacent more outwardly spaced apart tubular member; B passing said molten unitary extrudate through a cooling zone under conditions sufficient to substantially cool said extrudate and form a solidified unitary extrudate; C. drawing said solidified unitary extrudate in a downstream direction while simultaneously twisting the solidified unitary extrudate; whereby causing said molten extrudate to be twisted circumferentially and be drawn downstream from said extrusion die into cooling relation with said cooling zone; whereby causing said molten, twisted, drawn extrudate to traverse said cooling zone along a path that has both longitudinal and circumferential components and substantially corresponds to the degree of twisting and downstream drawing imparted to said extrudate; and D. while said tube is progressing downstream along a path having longitudinal and circumferential vectors, cutting said tube into discrete lengths.
- 35. A method as claimed in claim 34 further comprising forming the opposite ends of at least some of said discrete lengths of tubing into male and mating female profiles, respectively.
- 36. Cancelled
- 37. A method as claimed in claim 16 wherein said struts are joined to said outer tubular member and said inner cylindrical member, respectively, as they are being extruded.
- 38. An extruded composite structure as claimed in claim 1 wherein at least some of said alternatingly angularly disposed struts are extruded in simultaneous contact with and adhered to said inner cylindrical member and said outer tubular member, respectively, at location(s) that are adjacent to the location where a next adjacent strut is contacted with and adhered to said inward cylindrical member and said outwardly directed tubular member, respectively, whereby said next adjacent, angularly disposed struts together with the portion of respectively intercepted inwardly directed or outwardly directed walls of said tubular member and said cylindrical member, respectively, define cells having a substantially triangular cross section.
- 39. CANCELLED
- 40. Apparatus for forming a substantially rigid, unitary, cylindrical structure, wherein said structure comprises an inner cylindrical member, an outer tubular member surrounding said inner cylindrical member and radially spaced there from and a plurality of struts, disposed in an annular space between said inner and outer members, respectively, in spacing and supporting relationship to said members; which apparatus comprises:
an extruder adapted to simultaneously extrude through a die a unitary molten extrudate comprising:
an inner cylindrical member, an outer tubular member radially spaced from said inner cylindrical member, and a plurality of said spacing and supporting struts; cooling means disposed downstream of said extruder die means, comprising:
means to cool an inner surface of said extrudate and to solidify said inner cylindrical member and a portion of said struts adjacent thereto; means to cool an outer surface of said extrudate and to solidify said outer tubular member and a portion of said struts adjacent thereto; and a path inscribed on said means to cool said inner cylindrical member adapted to be followed by said molten extrudate during said cooling, wherein said cooling means is adapted to freeze said molten extrudate into solid extrudate; and drawing and twisting means downstream of said cooling means, and comprising means to twist said solid extrudate in a circumferential direction and means to draw said solid extrudate in a downstream, axial direction; wherein operation of said drawing and twisting means is adapted to be operative to draw and twist said solidified extrudate and to thereby cause said molten unitary extrudate to be twisted and drawn into a configuration having a circumferential component and a longitudinal component; and wherein said path is consistent with the twisted and drawn configuration of said solidified extrudate.
- 41. The apparatus as claimed in claim 40 wherein said path is substantially a helix.
- 42. The apparatus as claimed in claim 40 wherein said drawing and twisting means are a plurality of belt means adapted to be in frictional, helical contact with a sufficient portion of the circumference of said solidified extrudate such that said pulling and twisting are accomplished substantially simultaneously.
- 43. The apparatus as claimed in claim 40 wherein said inner member is tubular and wherein said cooling means further comprises:
a cooling mandrel adapted to fit within said inner tubular member; a cooling sleeve adapted to substantially surround said outer tubular member; means to apply cooling from said mandrel in an amount sufficient to solidify said inner tubular member and at least a portion of said struts that are proximate to said inner tubular member; and means to apply cooling from said sleeve in an amount sufficient to solidify at least said outer tubular member and at least a portion of said struts that are proximate to said outer tubular member.
- 44. The apparatus as claimed in claim 43 wherein said mandrel is tapered in a downstream direction and said taper is at an angle that corresponds to an amount of shrinkage that said inner tubular member will realize in passing through said cooling zone.
- 45. The apparatus as claimed in claim 43 wherein said mandrel comprises apertures in a surface that is adapted to be proximate to said inner tubular member and further comprising vacuum drawing means operatively associated with said apertures in an amount sufficient to maintain said inner tubular member in close proximity to said cooling mandrel during at least a portion of said cooling.
- 46. The apparatus as claimed in claim 45 further comprising means to periodically relieve said vacuum at a frequency such that said inner tubular member will not permanently adhere to said mandrel.
- 47. The apparatus as claimed in claim 46 further comprising means to intermittently release said vacuum and exert outwardly directed pressure through said apertures in an amount and frequency such as to cause said inner tubular member to intermittently move away from said mandrel.
- 48. CANCELLED.
- 49. An apparatus for cooling and solidifying a tubular extrudate comprising:
a mandrel adapted to support a molten tubular extrudate about a surface thereof; apertures in said surface that are adapted to be proximate to said an inside surface of said tubular extrudate; means to apply cooling to said surface and vacuum drawing means, operatively associated with said apertures, adapted to draw sufficient vacuum through said apertures to maintain said tubular extrudate in close proximity to said cooling mandrel during at least a portion of said cooling.
- 50. The apparatus as claimed in claim 49 further comprising means to periodically relieve said vacuum at a frequency that is adapted to prevent said molten extrudate from permanently adhering to said mandrel.
- 51. The apparatus as claimed in claim 50 further comprising means to intermittently release said vacuum and exert outwardly directed pressure through said apertures in an amount and frequency that is adapted to cause said molten extrudate to periodically move away from said mandrel.
- 52. The apparatus as claimed in claim 50 wherein said vacuum relief is accomplished at a frequency of about 100 to 400 times per minute.
- 53. An apparatus for pulsing a pressure change to a housing comprising:
an upper plate having an aperture there through; a lower plate having an aperture there through; wherein said apertures are adapted to have overlapping cross sections; and a disk that is adapted to be disposed between said upper plate and said lower plate; wherein said disk has a slot there through disposed proximate to, and radially internal of, a peripheral edge of said disk; said slot passing through the entire thickness of said disk; and ends of said slot being separated by a solid portion of said disk of a size that is sufficient to be interposed between said apertures; wherein said overlapping cross sections of said apertures are adapted to be aligned with each other and with said slot; wherein said plates are rotatable in relation to said disk such that said apertures are adapted to communicate with each other through said slot and are adapted to not communicate with each other when they are separated by said solid portion; and wherein the rate of rotation of said plates relative to said disk determines the pulse rate.
- 54. The apparatus as claimed in claim 53 further comprising vacuum drawing means operatively associated with one of said apertures and said housing being operatively associated with the other of said apertures.
- 55. The apparatus as claimed in claim 54 further comprising pressure generating means operatively associated with the aperture with which said vacuum drawing means is associated and switching means adapted to alternately apply vacuum and pressure to said housing through said apertures.
- 56. The apparatus as claimed in claim 55 wherein said solid portion of said disk further comprises a recessed portion, facing a first of said plates, so configured that when said solid portion of said disk is interposed between said plates, there is a passageway from one end of the aperture in said first plate through said aperture and thence through space between said first plate and said recessed portion; and
wherein there is substantially no passageway between said solid portion and the aperture in said second plate.
- 57. A method of producing a cylindrical shaped object comprising a tubular member, said method comprising:
extruding a tubular profile, moldable extrudate from an extruder, while in a moldable condition, causing said tubular extrudate to be twisted circumferentially and drawn down stream from said extruder; cooling said molten extrudate by passing it through a cooling zone along a twisting path that has longitudinal and circumferential directional components that substantially correspond to a rate of circumferential twisting and a rate of down stream drawing, and cooling said structure an amount sufficient to solidify it; and downstream of said cooling step, drawing said solidified composite structure downstream and twisting it so as to cause said molten extrudate, at a location between said extruding and said cooling, to be pulled downstream and twisted, as aforesaid, whereby causing said structure to become oriented in both longitudinal and circumferential directions prior to solidifying it.
- 58. The method as claimed in claim 57 wherein said downstream drawing and twisting are carried out substantially simultaneously.
- 59. The method as claimed in claim 57 further comprising drawing and twisting said moldable extrudate an amount sufficient to convert it into a helically shaped tube.
- 60. The method as claimed in claim 57 further comprising cooling and solidifying said twisted extrudate from both the inside and the outside of said twisted molten tubular extrudate.
- 61. The method as claimed in claim 57 further comprising extruding said molten extrudate comprising an inner tubular member and an outer tubular member.
- 62. The method as claimed in claim 57 further comprising drawing a vacuum through apertures in said cooling mandrel sufficient to maintain said tubular extrudate proximate to and in cooling relationship with, said cooling mandrel.
- 63. The method as claimed in claim 62 further comprising periodically stopping the vacuum being drawn through said mandrel apertures, and thereby permitting said tubular extrudate to move away from said cooling mandrel.
- 64. The method as claimed in claim 63 further comprising, during the time that the vacuum is not being drawn through said cooling mandrel apertures, applying positive pressure through said cooling mandrel apertures, and thereby forcing said tubular extrudate away from said cooling mandrel.
- 65. A method of producing a shaped object comprising a cylindrical member, said method comprising:
extruding a cylindrical profile, moldable extrudate from an extruder, while in a moldable condition, causing said cylindrical extrudate to be twisted circumferentially and drawn down stream from said extruder; passing said extrudate through a cooling zone, along a twisting path that has longitudinal and circumferential directional components that substantially correspond to a rate of circumferential twisting and a rate of down stream drawing, and cooling said structure an amount sufficient to solidify it; and downstream of said cooling step, drawing said solidified composite structure downstream and twisting it so as to cause said molten cylindrical extrudate, at a location between said extruding and said cooling, to be drawn downstream and twisted, as aforesaid, whereby causing said structure to become oriented in both longitudinal and circumferential directions prior to solidifying it; wherein said drawing and twisting operations are carried out substantially simultaneously and said substantially simultaneous drawing and twisting cause the resultant cylindrical profile article to have a greater uniformity of cross section and a greater straightness than would a cylindrical profile that had not been made using said substantially simultaneous drawing and twisting
- 66 A method as claimed in claim 65 further comprising drawing and twisting said extrudate by wrapping a plurality of moveable belts longitudinally spaced from each other and disposed helically about, and in frictional contact with, said solidified cylindrical profile; and moving said belts in a helical direction relative to the axis of said cylindrical profile under frictional conditions sufficient to cause said cylindrical profile to be moved in a helical direction relative to its axis.
- 67 An extrusion apparatus comprising:
an extruder barrel having:
at least one aperture adapted to have extrudable material fed therethrough, means to heat said feed material to a molten condition; and means to move molten feed through said barrel; an extruder die; an exit conduit from said extruder barrel adapted to convey molten feed material downstream of said extruder barrel and through said extruder die; means between said barrel and said die adapted to subdivide molten feed into a plurality of molten streams; means to subdivide said subdivided molten streams into an additional plurality of molten streams; and a plurality of conduits adapted to convey said plurality of molten streams to a die assembly; wherein said extruder die assembly comprises a die aperture operatively communicating with a plurality of said conduits that are adapted to contain said plurality of molten streams, wherein said die aperture comprises: an inner arcuate die aperture portion, an outer arcuate die aperture portion radially spaced from said inner die aperture portion, and a plurality of radially disposed die aperture portions in communicating relationship with said both said inner and outer arcuate die aperture portions.
- 68. An extrusion apparatus as claimed in claim 67 further comprising a plurality of extruder die conduit means through said extruder die assembly communicating between ambient atmosphere outside said extrusion apparatus and areas of said extruder die disposed between next adjacent radially disposed die apertures, and between said inner arcuate due aperture and said outer arcuate die aperture;
wherein said extruder die conduit means are adapted to pass gas into regions between extrudate streams emerging from said channel die apertures and to thereby assist in maintaining open, longitudinal cells between by next adjacent extrudate streams exiting from said inner arcuate die aperture portion, said outer arcuate die aperture portion and proximate radially disposed die aperture portions.
- 69. An apparatus adapted to substantially simultaneously draw a work piece down stream and twist the work piece about a longitudinal axis of said work piece, said apparatus comprising:
a plurality of substantially endless belts adapted to be frictionally disposed helically about said work piece in non overlapping relationship; and means to independently move each of said plurality of belts in the same direction and at substantially the same rate of speed, whereby enabling said belts to frictionally engage said work piece and to thereby twist said work piece circumferentially and substantially simultaneously draw said work piece downstream.
- 70. An apparatus as claimed in claim 69 comprising two said belts.
- 71. An apparatus as claimed in claim 69 wherein said belts are adapted to be longitudinally non-overlapping where they contact said work piece.
- 72. An apparatus as claimed in claim 69 wherein said work piece is cylindrical in profile about a longitudinal axis; and wherein each of said belts is adapted to engage the surface of said work piece along an area that extends from a line segment where the belt first intercepts the surface of the work piece to a line segment where the belt last intercepts the surface of the work piece, and wherein said line segments are parts of the same line in a direction axial to said work piece.
- 73. An apparatus as claimed in claim 69 wherein said means to move said belts comprises a driven drawing roller spaced from said work piece, wherein said belt is adapted to be wrapped at least partially around said drawing roller and is in sufficient frictional contact with said drawing roller not to slip to any substantial extent when in an operative relationship to said work piece.
- 74. An apparatus as claimed in claim 73 further comprising a small diameter, first idler roller adapted to be in operative relationship with said belt and adapted to be disposed downstream of said drawing roller such that the axis of said first idler roller is disposed at an angle of about 90° with respect to the axis of said drawing roller,
wherein, when in operation, said belt is adapted to first contact said drawing roller and then contact said first idler roller and wherein said drawing and first idler rollers cooperate to cause said belt to turn substantially 90° between leaving said drawing roller and entering said first idler roller.
- 75. An apparatus as claimed in claim 74 wherein the axis of said drawing roller is disposed at an angle with respect to the axis of said work piece such as to maintain a helical angle between said belt and said work piece.
- 76. An apparatus as claimed in claim 75 further comprising a second idler roller disposed downstream of said first idler roller, wherein said belt is adapted to be in operative contact with both of said idler rollers, and wherein the axes of said first and second idler rollers are substantially coplanar.
- 77. An apparatus as claimed in claim 75 further comprising at least one tensioning means disposed in operative relationship to said belt.
- 78. An apparatus as claimed in claim 76 further comprising a lead in roller disposed between said second idler roller and said work piece, wherein said belt is adapted to be in operative contact with said second idler roller, said lead in roller and thence said work piece.
- 79. An apparatus as claimed in claim 78 wherein the axis of said lead in roller is in substantially the same plane as the axis of said drawing roller, whereby being adapted to lead said belt onto said work piece at substantially the same angle, with respect to the axis of the work piece, as said belt leaves said work piece toward said drawing roller.
- 80. An apparatus as claimed in claim 79 wherein the plane of the axes of said first and second idler rollers is transverse to the plane of the axes of said lead in and drawing rollers.
- 81. An apparatus as acclaimed in claim 80 wherein said belt is endless.
- 82. An apparatus as claimed in claim 81 comprising two belts adapted to be disposed in an axial nesting arrangement on the surface of said work piece; and wherein each of said belts is adapted to be operatively associated with a separate drawing means, drawing roller, idler rollers and lead in roller.
- 83. A composite tube as claimed in claim 1 that is seamless.
- 84. A composite tube made by the method of claim 16.
- 85. A composite tube made by the method of claim 53.
Parent Case Info
[0001] This application is a continuation in part of application Ser. No. 09/626,886 filed Jul. 27, 2000, now U.S. Pat. No. 6,405,974 which was a continuation in part of PCT Application Number PCT/US99/17172, filed Jul. 29, 1999 which was a continuation in part of Provisional Application Serial No. 60/096,237, filed Aug. 12, 1998 and Provisional Application Serial No. 60/101,935, filed Sep. 25, 1998. This application is a continuation in part of Provisional Application Serial No. 60/309,494, filed Aug. 3, 2001.
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/US02/24437 |
8/1/2002 |
WO |
|
Provisional Applications (1)
|
Number |
Date |
Country |
|
60309494 |
Aug 2001 |
US |