WO1999034121B1 - Method and apparatus for transferring drilling energy to a cutting member - Google Patents

Method and apparatus for transferring drilling energy to a cutting member

Info

Publication number
WO1999034121B1
WO1999034121B1 PCT/US1998/027847 US9827847W WO9934121B1 WO 1999034121 B1 WO1999034121 B1 WO 1999034121B1 US 9827847 W US9827847 W US 9827847W WO 9934121 B1 WO9934121 B1 WO 9934121B1
Authority
WO
WIPO (PCT)
Prior art keywords
load cell
detm
strands
wrap
torque
Prior art date
Application number
PCT/US1998/027847
Other languages
French (fr)
Other versions
WO1999034121A1 (en
Inventor
Jack W Romano
Original Assignee
Jack W Romano
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jack W Romano filed Critical Jack W Romano
Priority to BR9814553-3A priority Critical patent/BR9814553A/en
Priority to EP98965032A priority patent/EP1042618A1/en
Priority to JP2000526748A priority patent/JP2002500322A/en
Priority to CA002315749A priority patent/CA2315749A1/en
Priority to AU20230/99A priority patent/AU2023099A/en
Priority to KR1020007007336A priority patent/KR20010033792A/en
Publication of WO1999034121A1 publication Critical patent/WO1999034121A1/en
Publication of WO1999034121B1 publication Critical patent/WO1999034121B1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C1/00Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/02Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
    • F16C1/06Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements with guiding sheathing, tube or box
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • A61B17/16Bone cutting, breaking or removal means other than saws, e.g. Osteoclasts; Drills or chisels for bones; Trepans
    • A61B17/1642Bone cutting, breaking or removal means other than saws, e.g. Osteoclasts; Drills or chisels for bones; Trepans for producing a curved bore
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C1/00Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/02Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C1/00Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/02Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
    • F16C1/04Articulated shafts
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • A61B17/16Bone cutting, breaking or removal means other than saws, e.g. Osteoclasts; Drills or chisels for bones; Trepans
    • A61B17/1613Component parts
    • A61B17/1615Drill bits, i.e. rotating tools extending from a handpiece to contact the worked material
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • A61B17/16Bone cutting, breaking or removal means other than saws, e.g. Osteoclasts; Drills or chisels for bones; Trepans
    • A61B17/17Guides or aligning means for drills, mills, pins or wires
    • A61B17/1796Guides or aligning means for drills, mills, pins or wires for holes for sutures or flexible wires
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2316/00Apparatus in health or amusement
    • F16C2316/10Apparatus in health or amusement in medical appliances, e.g. in diagnosis, dentistry, instruments, prostheses, medical imaging appliances
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/4984Retaining clearance for motion between assembled parts
    • Y10T29/49842Between tube-forming helical coils
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49863Assembling or joining with prestressing of part

Abstract

A continuous congruent length of stranded flexible Drilling Energy Transfer Member (DETM) to transfer and balance action/reaction forces between an energy source and a working tip (9) such that torque, tensile, compression and self supporting forces are constrained while the DETM operates in multiple positions of tight curvature and straight run. The DETM having a core load cell with a plurality of strands (13, 14, 16) sized and layered at a helical angle and an outer wrap load cell with a second plurality of strands (17, 18) sized and layered at a helical angle.

Claims

55AMENDED CLAIMS[received by the International Bureau on 22 June 1999 (22.06.99); original claims 1-6, 8-14 and 18 amended; new claims 23-60 added; remaining claims unchanged (19 pages)]
1. A flexible DETM comprising; an inner core load cell comprising a first plurality of strands sized and laid at a helical angle sufficient for transmitting predetermined tensile and compression loads under rotary drilling pressure, and an outer wrap load cell comprising a second plurality of strands sized and laid at a helical angle sufficient for transmitting predetermined torque loads under rotary drilling pressure, the force fields and mass distribution of said load cells being balanced in function such that said first load cell structurally supports said second load cell against destruction by axially directed forces and said second load cell structurally supports said first load cell against destruction by rotationally directed torque forces and maintains longitudinal support therefor .
2. A multi strand flexible DETM for tight radius rotary drilling comprising; a core construction composed of a first plurality of strands comprising a first load cell for transmitting tensile and compression loads while under rotary drilling pressure, said first plurality of strands being generally axially directed and laid at a flat helical angle, an outer wrap construction surrounding said core and composed of a second plurality of strands comprising a second load cell for transmitting rotational torque loads while under rotary drilling pressure, said second plurality of strands being generally circumferentially directed and laid at a steep helical 56
angle, the force fields and mass distribution of said first and second load cells being balanced in function such that said first load cell structurally supports said second load cell against destruction by axially directed forces and said second load cell structurally supports said first load cell against destruction by rotationally directed torque forces and maintains longitudinal support therefor.
3. The DETM of claim 2 wherein; said first plurality of strands are sized and laid at a helical angle sufficient for transmitting predetermined tensile and compression loads under rotary drilling pressure, and said second plurality of strands are sized and laid at a helical angle sufficient for transmitting predetermined torque loads under rotary drilling pressure .
4. The DETM of claim 3 wherein; said first plurality of strands comprise a single strand mandrel and first and second oppositely directed inner helical strand wraps laid thereon at a flat helical angle forming an interlocking configuration for transmitting axial loads.
5. The DETM of claim 4 wherein; said second plurality of strands comprises first and second oppositely directed outer helical strand wraps laid at a steep helical angle forming an interlocking configuration for transmitting torque loads .
6. The DETM of claim 3 wherein; said DETM has a given total mass and said first and second load cells comprise primary load cells, the mass of said first load cell constitutes approximatley 41.6% of the total mass, and the mass of said second load cell comprises the balance of the total mass.
7. The DETM of claim 6 wherein; said second load cell comprises separate radially successive first and second reversely wound helical torque wraps, each wrap including a plurality of strands, said first torque wrap comprising a middle torque wrap constituting approximately 25.1% of the total mass, and said second torque wrap comprising an outer torque wrap constituting approximately 32.2% of the total mass.
8. The DETM of claim 7 wherein; said first load cell comprises a central mandrel strand and inner and outer reversely wound helical core wraps, each wrap including a plurality of strands, said inner core wrap constitutes 12.6% of the total mass, said outer core wrap constitutes 27% of the total mass, and said mandrel strand constitutes 1.8% of the total mass.
9. The DETM of claim 8 wherein; said middle torque wrap comprises five right hand 58
laid strands, said outer torque wrap comprises seven left hand laid strands, said inner core wrap comprises six right hand laid strands, and said outer core wrap comprises twelve right hand laid strands.
10. The DETM of claim 5 wherein; said first and second inner helical strand wraps are laid at a 10°-15° helical angle, and said first and second outer helical strand wraps are laid at 60°-68° and 68°-72° helical angles respectively.
11. The DETM of claim 8 wherein; said inner core and outer core wraps are laid at a 10°-15° helical angle, and said middle and outer torque wraps are laid at 60°- 68° and 68°-72° helical angles respectively.
12. A method for constructing a DETM comprising; laying a first wrap of a plurality of wire strands about a single wire mandrel at helical angle of 10°-15° in a first direction, laying a second wrap of a plurality of wire strands on a said first wrap at a helical angle of 10°-
15° in the opposite direction, laying a third wrap of a plurality of wire strands on said second wrap at a helical angle of 60°-68° in said first direction, and laying a fourth wrap of a plurality of wire 59
strands on said third wrap at a helical angle of 68°-72° in said opposite direction.
13. A flexible DETM comprising; a core load cell for transmitting axial tensile and compression loads during drilling pressure, and an outer wrap torque transmitting load cell, said core load cell including a single strand mandrel, a first six strand right hand laid wrap and a second twelve strand left hand laid wrap, said outer wrap load cell including a first five strand outer wrap laid on said twelve strand wrap in a right hand direction and a second seven strand outer wrap laid on said five strand wrap in a left hand direction.
14. The DETM of claim 13 wherein; the overall diameter of said DETM is .045 inches, said six strand and said twelve strand wraps are laid to a helical angle of 10°-15°, said five strand wrap is laid at a helical angle of 60°-68°, and said seven strand wrap is laid at a helical angle of 68°-72°.
15. The DETM of claim 14 wherein; said mandrel, said six strand wrap and said twelve strand wrap comprise .0045 inch diameter wires, said five strand wrap comprises .0065 inch diameter wires, and said seven strand wrap comprises .006 inch diameter wires. 60
16. A rigid construction for connecting a cutter head to the terminal end of a flexible rotary shaft having a given diameter comprising; a hollow cylindrical stem on said cutter head, said hollow stem having an internal diameter sized to snugly receive a portion of the terminal end of said shaft; and at least one fused weld extending through the body of said stem into the center area of said shaft.
17. The construction of claim 16 wherein said fused weld comprises a plurality of radially directed fused areas spaced circumferentially about the wall of said stem. said fused areas extending from the outer surface of the stem to the center of said shaft.
18. A rigid construction for connecting a cutter head to the end of a flexible rotary shaft having a given diameter comprising; a hollow cylindrical stem on said cutter head, said stem having an internal diameter sized to snugly receive a portion of the terminal end of said shaft, a shoulder on said cutter head located immediately adjacent the bottom of said hollow stem, and at least one fused weld extending obliquely through said shoulder into the center area of said shaft .
19. A rigid construction for connecting a cutter head to the terminal end of a flexible rotary shaft having a given diameter comprising; 6 1
a stem on said cutter head having a diameter equal to the diameter of said shaft and adapted to abuttingly engage the terminal end thereof, a hollow cylindrical sleeve having an internal diameter sized to receive said shaft and said stem thereon with a snug fit, and at least one fused weld extending through the body of said sleeve into the center area of the abating end faces of said stem and said shaft.
20. The construction of claim 19 wherein said fused weld comprises a plurality of radially directed fused areas spaced circumferentially about the wall of said sleeve.
21. The construction of claim 19 wherein said fused weld is located adjacent one end of said sleeve adjacent said cutter head.
22. The construction of claim 20 including; a rigid collar attached to the outside of said sleeve for contacting the drill grid of a drilling apparatus .
23. A flexible DETM comprising in combination; an inner load cell, an outer load cell concentric with said inner load cell, said inner load cell comprising substantially longitudinally laid load bearing units, and said outer load cell comprising helically laid load bearing units. 62
24. The DETM of claim 23 wherein; said inner load cell comprises a core with the load bearing units thereof being wrapped substantially linearally for carrying longitudinally directed loads and resisting longitudinal deformation, said outer load cell comprises helically wrapped torque load cell units for transferring rotary shear torque drilling energy.
25. A multi-strand flexible DETM having two primary functionally balanced load cells comprising; an inner load cell having an inner cross sectional area and an outer load cell having an outer cross sectional area, said inner cross sectional area being approximately 25% with respect to the total and approximately 66.7% less than the outer cross sectional area, the volume of said inner load cell being approximately 25% with respect to the total and approximately 66.7% less than the volume of the outer load cell, the mass of said inner load cell being approximately 41.6% with respect to the total and approximately 20.7% less than the mass of the outer load cell, the strands of said inner and outer load cells being laid with predetermined helical slopes wherein the net slope vectors of the inner load cell is 204 % with respect to the net slope vectors of the outer load cell, whereby the total combined net sloping force is balanced to function; said inner and outer load cells each having a work priority wherein the inner load cell primarily 63
functions in balance with the outer load cell to withstand and resist linear deformation and the outer load cell primarily functions to transfer and constrain drilling energy in helical torque and shear.
26. The DETM of claim 25 wherein said inner load cell has a net center of mass leverage value of 3x and said outer load cell has a net center of mass leverage value of 7x.
27. The DETM of claim 25 wherein said two primary load cells are functionally balanced for load bearing primarily tensile to torque and torque to tensile, linear to rotary and rotary to linear.
28. The DETM of claim 26 wherein said two primary load cells are functionally balanced for load bearing primarily tensile to torque and torque to tensile, linear to rotary and rotary to linear.
29. A multi-strand flexible DETM comprising; inner and outer helically laid concentric load cells, said load cells being functionally balanced with respect to net vector slope, net mass, net volume, net cross sectional area and net load cell center of mass leverage valves, such that the inner load cell resists linear elongation and deformation and the outer load cell provides the balance of transfer of torque forces.
30. The DETM of claim 29 wherein said inner and outer load cells are functionally balanced for load 64
bearing primarily tensile to torque and torque to tensile, linear to rotary and rotary to linear.
31. The DETM of claim 23 wherein; said inner load cell is laid longitudinally to the axis of the DETM, said outer load cell comprising a pair of cross linked opposing units for the transmission of helical shear load.
32. The DETM of claim 23 including; an energy source, a working tip, said DETM being connected between said energy source and said working tip to transfer drilling energy therebetween, said inner load cell laid and wrapped to withstand extension and compression forces, said outer load cell comprising a pair of cross linked interlocking cell units for transferring and constraining helical shear torque rotary forces between said energy source and said working tip.
33. A DETM for transferring drilling energy between an energy source and a working tip comprising; an inner tensile load cell an outer cross linked pair of stranded load cells, the outer cross linked load cells being stranded and laid for transmission of rotary torque shear forces between the energy source and the working tip, the net slope vector forces of the cross 65
linked load cells being balanced in function and equilibrium to provide counter opposing interlocking constraint .
34. The DETM of claim 25 wherein; said outer load cell comprises counter opposing right and left lay load cell units, said outer load cell comprising the balance of the cross sectional area, volume and mass of the DETM, said inner load cell comprising a net vector slope approximately 148% to the total, directed 88% toward tensile load, and said outer load units having a net vector slope directed 430% toward torque load.
35. The DETM of claim 34 including; an energy source, a working tip, said DETM being connected between said energy source and said working tip to transfer drilling energy therebetween .
36. The DETM of claim 32 wherein; the diameter of said DETM is one half the diameter of said working tip and configured to operate in the curved bore formed thereby.
37. The DETM of claim 36 wherein said DETM is configured to transfer drilling energy along a curved bore radius of approximately .25 inches and to rotate and reciprocate therein.
38. The DETM of claim 37 wherein; 66
the cubic load cell units space volume changes upon rotation throughout the curve bore path, the helical pitch excursion and the shifting thereof being made in proportion to the radius of operation of the DETM to the outside diameter thereof, the force field distribution being so high as to close gaps between the load cell units in the curved path causing side-by-side contact of the load cell units upon excursion in reaction to rotation and translation within the curved path.
39. Curved bore drilling apparatus comprising in combination; a rotary drive means; a cutter tip; a drill shaft adapted for connection to said rotary drive means, said drill shaft means having a distal flexible DETM with said cutter tip attached thereto, mounting means supporting said drill shaft for movement in a rectilinear path, and guide means to guide said flexible DETM and said cutter tip form said rectilinear path along a curved path to form said curved bore, said flexible DETM comprising an inner load cell and a concentric outer load cell, said inner load cell comprising substantially longitudinally laid load bearing units for transmitting tensile forces, and said outer load cell comprising helically laid load bearing units for transferring rotary torque drilling energy, the force fields and mass distribution of 67
said load cells being balanced in function such that the inner load cell structurally supports said outer load cell against destruction by axially directed forces and said outer load cell structurally supports said inner load cell against destruction by rotationally directed torque forces and maintains longitudinal support therefor.
40. The drilling apparatus of claim 39 wherein; said inner and outer load cells comprise helically wrapped cross linked load cell units,
41. The drilling apparatus of claim 40 wherein; said inner load cell includes a single strand mandrel and said load cell units comprise a plurality of helically laid strands, the diameter of said DETM being approximately
.045 inches and said curved bore has a radius of approximately .25 inches.
42. The DETM of claim 24 wherein; said inner load cell includes; a single strand mandrel unit for linear support, a right hand wound six strand load sharing cell unit, and a left hand wound twelve strand load sharing cell unit, the load cell units of said inner load cell resisting substantially linear deforming loads.
43. The DETM of claim 42 wherein said outer load cell includes; 68
and a right hand wound five strand load sharing cell unit, and a left hand wound seven strand load sharing cell unit, the load cell units of said outer load cell resisting shear torque loads,
said inner and outer load cells being balanced in function such that the inner load cell structurally supports said outer load cell against destruction by axially directed forces and said outer load cell structurally supports said inner load cell against destruction by rotationally directed torque forces and maintains longitudinal support therefor.
44. The DETM of claim 43 wherein; the strands of said load cell units comprise wires drawn and cold worked to a desired material temper and wrapped in layers having a cold work effect and maintaining a spring load, the DETM being heat tempered as stranded and close to operating excursion pitch angle to stress relieve said strands.
45. The DETM of claim 44 wherein; the spring temper is killed at operating excursion so that land flats are formed on said strands to provide pivotal fulcrums as the strands move and shift in reaction to change in run mode patterns as the DETM moves through a curved path.
46. A method for transferring rotary torque and axial tensile and compression forces from a source of 69
rotary power to a working tip with a flexible DETM for forming curved bore comprising the steps of; wrapping a plurality of inner strands to form an inner load cell, said inner strands being wrapped at a helical angle, represented as a given first load cell force vector, chosen to transmit a predetermined primarily axial tensile/compression force, wrapping a plurality of outer strands to form an outer load cell, said outer strands being wrapped at a helical angle, represented as a given second load cell force vector, chosen to transmit a predetermined primarily rotary torque force, connecting said inner and outer load cells to said power source and said working tip, balancing said first and second load cell force vectors to function, whereby said inner load cell structurally supports said outer load cell against destruction by axially directed forces and said outer load cell structurally supports said inner load cell against destruction by rotationally directed torque forces and maintains longitudinal support therefor.
47. The method of claim 46 wherein; the overall diameter of said DETM is approximately .045 inches, and the radius of said curved bore is approximately .25 inches.
48. The method of claim 46 wherein said inner strands are wrapped about a single strand mandrel, and 70
including the steps of; laying said inner load cell in double cross link layers providing inner load cell units, laying said outer load cell in double cross link layers providing outer load cell units.
49. The method of claim 48 wherein; said inner load cell units comprise a first inner layer six strand right hand laid wrap and a second twelve strand left hand laid wrap, and said outer load cell units comprises a first five stand right hand laid wrap and a second seven strand left hand wrap.
50. The method of claim 49 including the steps of; laying the strands of said inner load cells at a 10°-15° helical angle, and laying the first and second outer load cell units a 60°-68° and 68°-72° helical angles respectively.
51. The method of claim 50 wherein; the overall diameter of said DETM is approximately .045 inches, said mandrel, said six stand wrap and said twelve strand wrap comprise .0045 inch diameter wires, said five strand wrap comprises .0065 inch diameter wires, and said seven strand wrap comprises .006 inch diameter wires.
52. The method of claim 48 including the steps 7 1
of ; directing said flexible DETM along a rectilinear approach path toward the surface of the material to be bored, maintaining a portion of said DETM within said rectilinear approach path, and simultaneously guiding the distal end of said flexible DETM and working tip through a curved path, said working tip forming a curved bore into said material, and advancing and retracting said DETM from said curved bore to effect material cutting and chip removal .
53. The method of claim 52 including the steps of; supporting said DETM with a curved drill guide along said curved path, said DETM being unsupported through said rectilinear path.
54. The method of claim 53 including the steps of; moving said DETM progressively and regressively through 3 o'clock, 6 o'clock, 9 o'clock and 12 o'clock positions causing cubic space volume changes in said DETM and operational pitch excursion shifts between the stands of said cross linked wraps of a magnitude related generally to the proportional relationship between the radius of operation of the DETM and the diameter thereof, the vector force balance between said inner and outer load cells providing the strength and flexibility for support of said DETM in the unsupported 72
rectilinear path and during supported rotation and reciprocation into and out of said curved path.
55. The method of claim 48 including the steps of; forming the strand of said cross linked layers from cold work tempered wire stands and laying said strands at predetermined helical pitch angles so as to form land flats on the cross linked strands which act as fulcrum points for angle excursion between cross stands during curved path drilling, and heat treating said DETM at operating torque pitch conditions to release the spring stress in said strands .
56. The method of claim 55 wherein; the overall diameter of said DETM is approximately .045 inches, and the radius of said curved bore is approximately .25 inches.
57. The method of claim 49 including the steps of; forming the strands of said cross linked layers from cold work tempered wire strands and laying said strands at predetermined helical pitch angles so as to form land flats on the cross linked strands which act as fulcrum points for angle excursion between cross stands during curved path drilling, and heat treating said DETM at operating torque pitch conditions to release the spring stress in said strands . 73
58. A method of manufacturing a flexible force transmission shaft for transmitting axial and torque forces along a curved path comprising the steps of; cold working wire strands to obtain a desired diameter and predetermined temper and tensile strength, tightly wrapping a plurality of said strands in cross linked layers with sufficient tension to form land flats on the strands which act as fulcrum points for angle excursion between crossed strands during movement of the shaft through a curved path, and heat treating said shaft at operating torque conditions to release the spring stress in said strands .
59. The method of claim 57 wherein; the overall diameter of said DETM is approximately .045 inches, and the radius of said curved bore is approximately .25 inches.
60. The method of claim 58 including the steps of; laying said strands to form a shaft having a diameter of approximately .045 inches and wrapping said strands in a configuration having sufficient flexibility for transmitting tensile and torque loads during reciprocation of said shaft into and out of a curved path having a radius of approximately .25 inches.
PCT/US1998/027847 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member WO1999034121A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
BR9814553-3A BR9814553A (en) 1997-12-31 1998-12-30 Drilling energy transfer element (detm) flexibly, construction process, and rigid construction for connecting a cutter head to the end of a rotating shaft flexibly having a specific diameter.
EP98965032A EP1042618A1 (en) 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member
JP2000526748A JP2002500322A (en) 1997-12-31 1998-12-30 Method and apparatus for transmitting drilling energy to a cutting member
CA002315749A CA2315749A1 (en) 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member
AU20230/99A AU2023099A (en) 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member
KR1020007007336A KR20010033792A (en) 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US7008197P 1997-12-31 1997-12-31
US60/070,081 1997-12-31

Publications (2)

Publication Number Publication Date
WO1999034121A1 WO1999034121A1 (en) 1999-07-08
WO1999034121B1 true WO1999034121B1 (en) 1999-08-12

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PCT/US1998/027847 WO1999034121A1 (en) 1997-12-31 1998-12-30 Method and apparatus for transferring drilling energy to a cutting member

Country Status (9)

Country Link
US (3) US6267679B1 (en)
EP (1) EP1042618A1 (en)
JP (1) JP2002500322A (en)
KR (1) KR20010033792A (en)
CN (1) CN1285900A (en)
AU (1) AU2023099A (en)
BR (1) BR9814553A (en)
CA (1) CA2315749A1 (en)
WO (1) WO1999034121A1 (en)

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CA2315749A1 (en) 1999-07-08
US6375573B2 (en) 2002-04-23
AU2023099A (en) 1999-07-19
KR20010033792A (en) 2001-04-25
EP1042618A1 (en) 2000-10-11
CN1285900A (en) 2001-02-28
US6526645B2 (en) 2003-03-04
US6267679B1 (en) 2001-07-31
US20010041620A1 (en) 2001-11-15
US20020090999A1 (en) 2002-07-11
BR9814553A (en) 2000-10-10

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